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Sample records for checs commanding hardware

  1. CHeCS Commanding Hardware

    NASA Technical Reports Server (NTRS)

    Moore, Jamie

    2010-01-01

    This slide presentation reviews the Crew Health Care System (CHeCS) commanding hardware. It includes information on the hardware status, commanding plan, and command training status with specific information the EV-CPDS 2 and 3, TEPC, MEC, and T2

  2. CHeCS: International Space Station Medical Hardware Catalog

    NASA Technical Reports Server (NTRS)

    2008-01-01

    The purpose of this catalog is to provide a detailed description of each piece of hardware in the Crew Health Care System (CHeCS), including subpacks associated with the hardware, and to briefly describe the interfaces between the hardware and the ISS. The primary user of this document is the Space Medicine/Medical Operations ISS Biomedical Flight Controllers (ISS BMEs).

  3. CHeCS (Crew Health Care Systems): International Space Station (ISS) Medical Hardware Catalog. Version 10.0

    NASA Technical Reports Server (NTRS)

    2011-01-01

    The purpose of this catalog is to provide a detailed description of each piece of hardware in the Crew Health Care System (CHeCS), including subpacks associated with the hardware, and to briefly describe the interfaces between the hardware and the ISS. The primary user of this document is the Space Medicine/Medical Operations ISS Biomedical Flight Controllers (ISS BMEs).

  4. CHECS rack move

    NASA Image and Video Library

    2009-08-13

    ISS020-E-030661 (13 Aug. 2009) --- Canadian Space Agency astronaut Robert Thirsk (right) and European Space Agency astronaut Frank De Winne, both Expedition 20 flight engineers, prepare to relocate the Crew Health Care System (CHeCS) rack in the Destiny laboratory to the Kibo laboratory of the International Space Station.

  5. Hardware-in-the-Loop Rendezvous Tests of a Novel Actuators Command Concept

    NASA Astrophysics Data System (ADS)

    Gomes dos Santos, Willer; Marconi Rocco, Evandro; Boge, Toralf; Benninghoff, Heike; Rems, Florian

    2016-12-01

    Integration, test and validation results, in a real-time environment, of a novel concept for spacecraft control are presented in this paper. The proposed method commands simultaneously a group of actuators optimizing a given set of objective functions based on a multiobjective optimization technique. Since close proximity maneuvers play an important role in orbital servicing missions, the entire GNC system has been integrated and tested at a hardware-in-the-loop (HIL) rendezvous and docking simulator known as European Proximity Operations Simulator (EPOS). During the test campaign at EPOS facility, a visual camera has been used to provide the necessary measurements for calculating the relative position with respect to the target satellite during closed-loop simulations. In addition, two different configurations of spacecraft control have been considered in this paper: a thruster reaction control system and a mixed actuators mode which includes thrusters, reaction wheels, and magnetic torqrods. At EPOS, results of HIL closed-loop tests have demonstrated that a safe and stable rendezvous approach can be achieved with the proposed GNC loop.

  6. Hardware

    NASA Technical Reports Server (NTRS)

    1999-01-01

    The full complement of EDOMP investigations called for a broad spectrum of flight hardware ranging from commercial items, modified for spaceflight, to custom designed hardware made to meet the unique requirements of testing in the space environment. In addition, baseline data collection before and after spaceflight required numerous items of ground-based hardware. Two basic categories of ground-based hardware were used in EDOMP testing before and after flight: (1) hardware used for medical baseline testing and analysis, and (2) flight-like hardware used both for astronaut training and medical testing. To ensure post-landing data collection, hardware was required at both the Kennedy Space Center (KSC) and the Dryden Flight Research Center (DFRC) landing sites. Items that were very large or sensitive to the rigors of shipping were housed permanently at the landing site test facilities. Therefore, multiple sets of hardware were required to adequately support the prime and backup landing sites plus the Johnson Space Center (JSC) laboratories. Development of flight hardware was a major element of the EDOMP. The challenges included obtaining or developing equipment that met the following criteria: (1) compact (small size and light weight), (2) battery-operated or requiring minimal spacecraft power, (3) sturdy enough to survive the rigors of spaceflight, (4) quiet enough to pass acoustics limitations, (5) shielded and filtered adequately to assure electromagnetic compatibility with spacecraft systems, (6) user-friendly in a microgravity environment, and (7) accurate and efficient operation to meet medical investigative requirements.

  7. McArthur rotates the CHeCS Rack during Expedition 12

    NASA Image and Video Library

    2005-12-09

    ISS012-E-10806 (9 December 2005) --- Astronaut William S. (Bill) McArthur Jr., Expedition 12 commander and NASA space station science officer, rotates the Crew Health Care System (CHeCS) rack in order to access the Avionics Air Assembly (AAA) air ducts during in-flight maintenance (IFM) in the Destiny laboratory of the International Space Station.

  8. McArthur removes AAA clamps and ducts inside the CHeCS Rack during Expedition 12

    NASA Image and Video Library

    2005-12-09

    ISS012-E-10817 (9 December 2005) --- Astronaut William S. (Bill) McArthur Jr., Expedition 12 commander and NASA space station science officer, opens the back panel of the Crew Health Care System (CHeCS) rack and removes the Avionics Air Assembly (AAA) air ducts during in-flight maintenance (IFM) in the Destiny laboratory of the International Space Station.

  9. McArthur rotates the CHeCS rack back into position after cleaning the AAA fan

    NASA Image and Video Library

    2005-12-01

    ISS012-E-09931 (1 December 2005) --- Astronaut William S. (Bill) McArthur Jr., Expedition 12 commander and NASA space station science officer, rotates the Crew Health Care System (CHeCS) rack back into position after cleaning the Avionics Air Assembly fan in the Destiny laboratory of the International Space Station.

  10. McArthur installs an ITCS coolant sampling tool onto the CHeCS Rack during Expedition 12

    NASA Image and Video Library

    2005-12-09

    ISS012-E-10792 (9 December 2005) --- Astronaut William S. (Bill) McArthur Jr., Expedition 12 commander and NASA space station science officer, prepares to remove the Avionics Air Assembly (AAA) from the Crew Health Care System (CHeCS) rack during in-flight maintenance (IFM) in the Destiny laboratory of the International Space Station.

  11. Burbank participates in a CHeCS Medical Contingency Drill in the U.S. Laboratory

    NASA Image and Video Library

    2011-12-16

    ISS030-E-012609 (16 Dec. 2011) --- NASA astronaut Dan Burbank (foreground), Expedition 30 commander, and Russian cosmonaut Anton Shkaplerov, flight engineer, participate in a Crew Health Care System (CHeCS) medical contingency drill in the Destiny laboratory of the International Space Station. This drill gives crew members the opportunity to work as a team in resolving a simulated medical emergency onboard the space station.

  12. Burbank participates in a CHeCS Medical Contingency Drill in the U.S. Laboratory

    NASA Image and Video Library

    2011-12-16

    ISS030-E-012613 (16 Dec. 2011) --- NASA astronaut Dan Burbank (foreground), Expedition 30 commander, and Russian cosmonaut Anton Shkaplerov, flight engineer, participate in a Crew Health Care System (CHeCS) medical contingency drill in the Destiny laboratory of the International Space Station. This drill gives crew members the opportunity to work as a team in resolving a simulated medical emergency onboard the space station.

  13. Ford and Novitskiy participate in a CHeCS Medical Contingency Drill in the U.S. Laboratory

    NASA Image and Video Library

    2012-11-26

    ISS034-E-005268 (26 Nov. 2012) --- NASA astronaut Kevin Ford (background), Expedition 34 commander; and Russian cosmonaut Oleg Novitskiy, flight engineer, participate in a Crew Health Care System (CHeCS) medical contingency drill in the Destiny laboratory of the International Space Station. This drill gives crew members the opportunity to work as a team in resolving a simulated medical emergency onboard the space station.

  14. Thirsk during CHeCS medical emergency training

    NASA Image and Video Library

    2009-07-02

    ISS020-E-016866 (2 July 2009) --- Canadian Space Agency astronaut Robert Thirsk, Expedition 20 flight engineer, participates in Crew Health Care Systems (CHeCS) medical emergency training in the Destiny laboratory of the International Space Station.

  15. Crew Health Care System (CHeCS) Design Research, Documentations, and Evaluations

    NASA Technical Reports Server (NTRS)

    CLement, Bethany M.

    2011-01-01

    The Crew Health Care System (CHeCS) is a group within the Space Life Science Directorate (SLSD) that focuses on the overall health of astronauts by reinforcing the three divisions - the Environmental Maintenance System (EMS), the Countermeasures System (CMS), and the Health Maintenance System (HMS). This internship provided opportunity to gain knowledge, experience, and skills in CHeCS engineering and operations tasks. Various and differing tasks allowed for occasions to work independently, network to get things done, and show leadership abilities. Specific exercises included reviewing hardware certification, operations, and documentation within the ongoing Med Kit Redesign (MKR) project, and learning, writing, and working various common pieces of paperwork used in the engineering and design process. Another project focused on the distribution of various pieces of hardware to off-site research facilities with an interest in space flight health care. The main focus of this internship, though, was on a broad and encompassing understanding of the engineering process as time was spent looking at each individual step in a variety of settings and tasks.

  16. Williams deactivates the CHeCS in the U.S. Laboratory during Expedition 13

    NASA Image and Video Library

    2006-06-13

    ISS013-E-36887 (13 June 2006) --- Astronaut Jeffrey N. Williams, Expedition 13 NASA space station science officer and flight engineer, deactivates the Crew Health Care System (CHeCS) rack in the Destiny laboratory of the International Space Station.

  17. Space Station Freedom CHeCS overview. [Crew Health Care System

    NASA Technical Reports Server (NTRS)

    Boyce, Joey B.

    1990-01-01

    The current status, progress, and future plans for development of the Crew Health Care System (CHeCS) for the International Space Station Freedom are presented. Essential operational biomedical support requirements for the astronauts, including medical care, environmental habitat monitoring, and countermeasures for the potentially maladaptive physiological effects of space flight will be provided by the CHeCS. Three integral parts will make up the system: a health maintenance facility, an environmental health system, and the exercise countermeasures facility. Details of each of the major systems and their subsystems are presented.

  18. Space Station Freedom CHeCS overview. [Crew Health Care System

    NASA Technical Reports Server (NTRS)

    Boyce, Joey B.

    1990-01-01

    The current status, progress, and future plans for development of the Crew Health Care System (CHeCS) for the International Space Station Freedom are presented. Essential operational biomedical support requirements for the astronauts, including medical care, environmental habitat monitoring, and countermeasures for the potentially maladaptive physiological effects of space flight will be provided by the CHeCS. Three integral parts will make up the system: a health maintenance facility, an environmental health system, and the exercise countermeasures facility. Details of each of the major systems and their subsystems are presented.

  19. Space vehicle onboard command encoder

    NASA Technical Reports Server (NTRS)

    1975-01-01

    A flexible onboard encoder system was designed for the space shuttle. The following areas were covered: (1) implementation of the encoder design into hardware to demonstrate the various encoding algorithms/code formats, (2) modulation techniques in a single hardware package to maintain comparable reliability and link integrity of the existing link systems and to integrate the various techniques into a single design using current technology. The primary function of the command encoder is to accept input commands, generated either locally onboard the space shuttle or remotely from the ground, format and encode the commands in accordance with the payload input requirements and appropriately modulate a subcarrier for transmission by the baseband RF modulator. The following information was provided: command encoder system design, brassboard hardware design, test set hardware and system packaging, and software.

  20. Ivanishin participates in a CHeCS Medical Contingency Drill in the U.S. Laboratory

    NASA Image and Video Library

    2011-12-16

    ISS030-E-012604 (16 Dec. 2011) --- Russian cosmonauts Anatoly Ivanishin (foreground) and Anton Shkaplerov, both Expedition 30 flight engineers, participate in a Crew Health Care System (CHeCS) medical contingency drill in the Destiny laboratory of the International Space Station. This drill gives crew members the opportunity to work as a team in resolving a simulated medical emergency onboard the space station.

  1. Novitskiy participates in a CHeCS medical contingency drill in the U.S. Laboratory

    NASA Image and Video Library

    2012-11-26

    ISS034-E-005266 (26 Nov. 2012) --- Russian cosmonaut Oleg Novitskiy, Expedition 34 flight engineer, participates in a Crew Health Care System (CHeCS) medical contingency drill in the Destiny laboratory of the International Space Station. This drill gives crew members the opportunity to work as a team in resolving a simulated medical emergency onboard the space station.

  2. Novitskiy participates in a CHeCS medical contingency drill in the U.S. Laboratory

    NASA Image and Video Library

    2012-11-26

    ISS034-E-005260 (26 Nov. 2012) --- Russian cosmonaut Oleg Novitskiy, Expedition 34 flight engineer, participates in a Crew Health Care System (CHeCS) medical contingency drill in the Destiny laboratory of the International Space Station. This drill gives crew members the opportunity to work as a team in resolving a simulated medical emergency onboard the space station.

  3. Shkaplerov participates in a CHeCS Medical Contingency Drill in the U.S. Laboratory

    NASA Image and Video Library

    2011-12-16

    ISS030-E-012600 (16 Dec. 2011) --- Russian cosmonaut Anton Shkaplerov, Expedition 30 flight engineer, participates in a Crew Health Care System (CHeCS) medical contingency drill in the Destiny laboratory of the International Space Station. This drill gives crew members the opportunity to work as a team in resolving a simulated medical emergency onboard the space station.

  4. Community Health Education Consortia (CHEC) Feasibility Study of Northeast Central Nebraska. Final Report.

    ERIC Educational Resources Information Center

    Hutkin, Ronald M.; Holmberg, Mary Lou

    This study sought to determine the extent of existing in-service education programs in health care available in northeast central Nebraska and to determine if there was a need for a Community Health Education Consortium (CHEC). Two questionnaires were developed for the study and were mailed to hospitals and nursing homes in a 22 county area; 86%…

  5. Only in Canada: A Study of National Market Potential for Christian Higher Education Canada (CHEC) Institutions

    ERIC Educational Resources Information Center

    Hiebert, Al

    2011-01-01

    In July 2007 Ipsos Reid delivered to Christian Higher Education Canada (CHEC) a report entitled "Christian Post-Secondary Education in Canada, Phase 3: Defining the Market". This article is a selective summary of the full 353-page report. It tabulates and analyzes findings from 1,000 phone interviews and 6,689 online surveys from six…

  6. Fan filter cleaning on the CHeCS AAA in the US Lab

    NASA Image and Video Library

    2009-05-05

    ISS019-E-013710 (5 May 2009) --- Japan Aerospace Exploration Agency (JAXA) astronaut Koichi Wakata, Expedition 19/20 flight engineer, cleans a fan filter on the Crew Health Care System Avionics Air Assembly (CHeCS AAA) in the Destiny laboratory of the International Space Station.

  7. Only in Canada: A Study of National Market Potential for Christian Higher Education Canada (CHEC) Institutions

    ERIC Educational Resources Information Center

    Hiebert, Al

    2011-01-01

    In July 2007 Ipsos Reid delivered to Christian Higher Education Canada (CHEC) a report entitled "Christian Post-Secondary Education in Canada, Phase 3: Defining the Market". This article is a selective summary of the full 353-page report. It tabulates and analyzes findings from 1,000 phone interviews and 6,689 online surveys from six…

  8. Plazmennyi-Kristall-3 plus hardware installation

    NASA Image and Video Library

    2010-06-30

    ISS024-E-007108 (30 June 2010) --- Russian cosmonaut Alexander Skvortsov, Expedition 24 commander, installs hardware for the new Plasma Crystal-3 Plus experiment in the Poisk Mini-Research Module 2 (MRM2) of the International Space Station.

  9. Command system

    NASA Technical Reports Server (NTRS)

    Burow, N. A.; Tam, M. K.

    1982-01-01

    The Multimission Command (MMC) System is described. The major components within the MMC System are discussed, with the emphasis on the telecommunication-related implementations. Two versions of the spacecraft command detection system (the Viking heritage command detector and the NASA standard command detector) are discussed in detail. The former prevails in the existing flight projects and the latter will likely be adopted by the missions of the near future. The preparation of design control tables for the control of command link performance between deep space stations and the spacecraft is also discussed.

  10. Hardware-Efficient Monitoring of I/O Signals

    NASA Technical Reports Server (NTRS)

    Driscoll, Kevin R.; Hall, Brendan; Paulitsch, Michael

    2009-01-01

    In this invention, command and monitor functionality is moved between the two independent pieces of hardware, in which one had been dedicated to command and the other had been dedicated to monitor, such that some command and some monitor functionality appears in each. The only constraint is that the monitor for signal cannot be in the same hardware as the command I/O it is monitoring. The splitting of the command outputs between independent pieces of hardware may require some communication between them, i.e. an intra-switch trunk line. This innovation reduces the amount of wasted hardware and allows the two independent pieces of hardware to be designed identically in order to save development costs.

  11. Hardly Hardware

    ERIC Educational Resources Information Center

    Lott, Debra

    2007-01-01

    In a never-ending search for new and inspirational still-life objects, the author discovered that home improvement retailers make great resources for art teachers. Hardware and building materials are inexpensive and have interesting and variable shapes. She especially liked the dryer-vent coils and the electrical conduit. These items can be…

  12. Hardly Hardware

    ERIC Educational Resources Information Center

    Lott, Debra

    2007-01-01

    In a never-ending search for new and inspirational still-life objects, the author discovered that home improvement retailers make great resources for art teachers. Hardware and building materials are inexpensive and have interesting and variable shapes. She especially liked the dryer-vent coils and the electrical conduit. These items can be…

  13. Novitskiy and Tarelkin both participate in a CHeCS medical contingency drill in the U.S. Laboratory

    NASA Image and Video Library

    2012-11-26

    ISS034-E-005261 (26 Nov. 2012) --- Russian cosmonauts Oleg Novitskiy (left) and Evgeny Tarelkin, both Expedition 34 flight engineers, participate in a Crew Health Care System (CHeCS) medical contingency drill in the Destiny laboratory of the International Space Station. This drill gives crew members the opportunity to work as a team in resolving a simulated medical emergency onboard the space station.

  14. Fincke unbolts the front panel of the CHeCS Rack for inspection and cleaning during Expedition 9

    NASA Image and Video Library

    2004-09-16

    ISS009-E-23061 (16 September 2004) --- Astronaut Edward M. (Mike) Fincke, Expedition 9 NASA ISS science officer and flight engineer, uses a drill to unfasten a panel on the CHeCS Rack in the Destiny laboratory of the International Space Station (ISS). Fincke was about to perform an inspection of the Avionics Air Assembly.

  15. Lessons Learned from the Crew Health Care System (CHeCS) Rack 1 Environmental Control and Life Support (ECLS) Design

    NASA Technical Reports Server (NTRS)

    Williams, David E.

    2006-01-01

    This paper will provide an overview of the International Space Station (ISS) Environmental Control and Life Support (ECLS) design of the Crew Health Care System (CHeCS) Rack 1 and it will document some of the lessons that have been learned to date for the ECLS equipment in this rack.

  16. Lessons Learned from the Crew Health Care System (CHeCS) Rack 1 Environmental Control and Life Support (ECLS) Design

    NASA Technical Reports Server (NTRS)

    Williams, David E.

    2006-01-01

    This paper will provide an overview of the International Space Station (ISS) Environmental Control and Life Support (ECLS) design of the Crew Health Care System (CHeCS) Rack 1 and it will document some of the lessons that have been learned to date for the ECLS equipment in this rack.

  17. Network command processing system overview

    NASA Technical Reports Server (NTRS)

    Nam, Yon-Woo; Murphy, Lisa D.

    1993-01-01

    The Network Command Processing System (NCPS) developed for the National Aeronautics and Space Administration (NASA) Ground Network (GN) stations is a spacecraft command system utilizing a MULTIBUS I/68030 microprocessor. This system was developed and implemented at ground stations worldwide to provide a Project Operations Control Center (POCC) with command capability for support of spacecraft operations such as the LANDSAT, Shuttle, Tracking and Data Relay Satellite, and Nimbus-7. The NCPS consolidates multiple modulation schemes for supporting various manned/unmanned orbital platforms. The NCPS interacts with the POCC and a local operator to process configuration requests, generate modulated uplink sequences, and inform users of the ground command link status. This paper presents the system functional description, hardware description, and the software design.

  18. Facteurs prédictifs de l’échec de traitement antituberculeux en Guinée Conakry

    PubMed Central

    Nimagan, Souleymane; Bopaka, Regis Gothard; Diallo, Mamadou Mouctar; Diallo, Boubacar Djelo; Diallo, Mamadou Bailo; Sow, Oumou Younoussa

    2015-01-01

    La tuberculose est un véritable problème de santé publique. C'est une maladie guérissable et cette guérison passe par une bonne prise en charge thérapeutique. Il arrive parfois on assiste à l’échec thérapeutique, d'où l'intérêt de notre étude portant sur les facteurs prédictifs de ses échecs. Dans l'espace d'une année sur 1300 cas de tuberculose toute forme confondue, 700 cas de tuberculose pulmonaire à microscopie positive ont été répertorié dont 100 cas transférés. La tranche d’âge de 15-25 ans a été la plus touchée avec un sexe-ratio de 2 en faveur des hommes et 41,66% de nos malades ont été les ouvriers suivis de 20,83% des commerçants. La majorité de nos patients provenait de Conakry soit 99, 5%. Sur 600 patients suivis les nouveaux cas représentaient 83,33% et l’échec thérapeutique représentait 12 cas soit 2%. L'interruption du traitement représente le principal facteur de l’échec. Les facteurs qui ont influencé la régularité des malades au traitement ont été multiples. Des facteurs liés à l'organisation du système de santé, la rupture des médicaments antituberculeux, l’éducation sanitaire insuffisante, les contraintes de la supervision du traitement, l'implication insuffisante et la vente des médicaments par le personnel de santé. Des facteurs liés aux patients eux-mêmes, la crainte de perte d'emploi, les contraintes financières. Les renforcements de l'organisation du système sanitaire et l’éducation thérapeutiques pourront réduire le taux d’échec du traitement antituberculeux. L'amélioration de la qualité de la prise en charge des malades en situation d’échec devrait passer par une culture systématique des expectorations avec antibiogramme. PMID:26889327

  19. Hardware efficient monitoring of input/output signals

    NASA Technical Reports Server (NTRS)

    Driscoll, Kevin R. (Inventor); Hall, Brendan (Inventor); Paulitsch, Michael (Inventor)

    2012-01-01

    A communication device comprises first and second circuits to implement a plurality of ports via which the communicative device is operable to communicate over a plurality of communication channels. For each of the plurality of ports, the communication device comprises: command hardware that includes a first transmitter to transmit data over a respective one of the plurality of channels and a first receiver to receive data from the respective one of the plurality of channels; and monitor hardware that includes a second receiver coupled to the first transmitter and a third receiver coupled to the respective one of the plurality of channels. The first circuit comprises the command hardware for a first subset of the plurality of ports. The second circuit comprises the monitor hardware for the first subset of the plurality of ports and the command hardware for a second subset of the plurality of ports.

  20. Hardware multiplier processor

    DOEpatents

    Pierce, P.E.

    A hardware processor is disclosed which in the described embodiment is a memory mapped multiplier processor that can operate in parallel with a 16 bit microcomputer. The multiplier processor decodes the address bus to receive specific instructions so that in one access it can write and automatically perform single or double precision multiplication involving a number written to it with or without addition or subtraction with a previously stored number. It can also, on a single read command automatically round and scale a previously stored number. The multiplier processor includes two concatenated 16 bit multiplier registers, two 16 bit concatenated 16 bit multipliers, and four 16 bit product registers connected to an internal 16 bit data bus. A high level address decoder determines when the multiplier processor is being addressed and first and second low level address decoders generate control signals. In addition, certain low order address lines are used to carry uncoded control signals. First and second control circuits coupled to the decoders generate further control signals and generate a plurality of clocking pulse trains in response to the decoded and address control signals.

  1. Hardware multiplier processor

    DOEpatents

    Pierce, Paul E.

    1986-01-01

    A hardware processor is disclosed which in the described embodiment is a memory mapped multiplier processor that can operate in parallel with a 16 bit microcomputer. The multiplier processor decodes the address bus to receive specific instructions so that in one access it can write and automatically perform single or double precision multiplication involving a number written to it with or without addition or subtraction with a previously stored number. It can also, on a single read command automatically round and scale a previously stored number. The multiplier processor includes two concatenated 16 bit multiplier registers, two 16 bit concatenated 16 bit multipliers, and four 16 bit product registers connected to an internal 16 bit data bus. A high level address decoder determines when the multiplier processor is being addressed and first and second low level address decoders generate control signals. In addition, certain low order address lines are used to carry uncoded control signals. First and second control circuits coupled to the decoders generate further control signals and generate a plurality of clocking pulse trains in response to the decoded and address control signals.

  2. The Internet--Flames, Firewalls and the Future. Proceedings for the 1995 Conference of the Council for Higher Education Computing Services (CHECS) (Roswell, New Mexico, November 8-10, 1995).

    ERIC Educational Resources Information Center

    Suiter, Martha, Ed.

    This set of proceedings assembles papers presented at the 1995 Council for Higher Education Computing Services (CHECS) conference, held at the New Mexico Military Institute in Roswell, New Mexico. CHECS members are higher education computing services organizations within the state of New Mexico. The main focus of the conference was the Internet…

  3. Hardware Review: What Hardware Should We Buy?

    ERIC Educational Resources Information Center

    Tinker, Robert

    1984-01-01

    Discusses trends and changes in hardware production. For example Sinclair/Timex has stopped mass marketing its computers while others (such as the IBM junior) has finally made its appearance. Strongly advises schools to re-evaluate their hardware purchasing programs in light of these and other changes. (JN)

  4. Movable Ground Based Recovery System for Reuseable Space Flight Hardware

    NASA Technical Reports Server (NTRS)

    Sarver, George L. (Inventor)

    2013-01-01

    A reusable space flight launch system is configured to eliminate complex descent and landing systems from the space flight hardware and move them to maneuverable ground based systems. Precision landing of the reusable space flight hardware is enabled using a simple, light weight aerodynamic device on board the flight hardware such as a parachute, and one or more translating ground based vehicles such as a hovercraft that include active speed, orientation and directional control. The ground based vehicle maneuvers itself into position beneath the descending flight hardware, matching its speed and direction and captures the flight hardware. The ground based vehicle will contain propulsion, command and GN&C functionality as well as space flight hardware landing cushioning and retaining hardware. The ground based vehicle propulsion system enables longitudinal and transverse maneuverability independent of its physical heading.

  5. Health Maintenance System (HMS) Hardware Research, Design, and Collaboration

    NASA Technical Reports Server (NTRS)

    Gonzalez, Stefanie M.

    2010-01-01

    The Space Life Sciences division (SLSD) concentrates on optimizing a crew member's health. Developments are translated into innovative engineering solutions, research growth, and community awareness. This internship incorporates all those areas by targeting various projects. The main project focuses on integrating clinical and biomedical engineering principles to design, develop, and test new medical kits scheduled for launch in the Spring of 2011. Additionally, items will be tagged with Radio Frequency Interference Devices (RFID) to keep track of the inventory. The tags will then be tested to optimize Radio Frequency feed and feed placement. Research growth will occur with ground based experiments designed to measure calcium encrusted deposits in the International Space Station (ISS). The tests will assess the urine calcium levels with Portable Clinical Blood Analyzer (PCBA) technology. If effective then a model for urine calcium will be developed and expanded to microgravity environments. To support collaboration amongst the subdivisions of SLSD the architecture of the Crew Healthcare Systems (CHeCS) SharePoint site has been redesigned for maximum efficiency. Community collaboration has also been established with the University of Southern California, Dept. of Aeronautical Engineering and the Food and Drug Administration (FDA). Hardware disbursements will transpire within these communities to support planetary surface exploration and to serve as an educational tool demonstrating how ground based medicine influenced the technological development of space hardware.

  6. RAF and Mission Command

    DTIC Science & Technology

    2015-02-01

    of the art of command, i.e., the mission command philosophy , by examining six guiding principles. The third section analyzes RAF through the...describes mission command as a “ philosophy and a warfighting function;” it is also the framework for the Army’s execution of military operations in...support of Unified Land Operations (ULO).35 The mission command philosophy is described as “the exercise of authority and direction by the commander

  7. The automated command transmission

    NASA Astrophysics Data System (ADS)

    Inoue, Y.; Satoh, S.

    A technique for automated command transmission (ACT) to GEO-stationed satellites is presented. The system is intended for easing the command center workload. The ACT system determines the relation of the commands to on-board units, connects the telemetry with on-board units, defines the control path on the spacecraft, identifies the correspondence of back-up units to primary units, and ascertains sunlight or eclipse conditions. The system also has the address of satellite and command decoders, the ID and content for the mission command sequence, group and inhibit codes, a listing of all available commands, and restricts the data to a command sequence. Telemetry supplies data for automated problem correction. All other missions operations are terminated during system recovery data processing after a crash. The ACT system is intended for use with the GMS spacecraft.

  8. Coleman moves MSL Hardware

    NASA Image and Video Library

    2011-01-07

    ISS026-E-016614 (7 Jan. 2011) --- NASA astronaut Catherine (Cady) Coleman, Expedition 26 flight engineer, moves Material Science Laboratory (MSL) hardware from the Harmony node to the Destiny laboratory of the International Space Station.

  9. Hardware description languages

    NASA Technical Reports Server (NTRS)

    Tucker, Jerry H.

    1994-01-01

    Hardware description languages are special purpose programming languages. They are primarily used to specify the behavior of digital systems and are rapidly replacing traditional digital system design techniques. This is because they allow the designer to concentrate on how the system should operate rather than on implementation details. Hardware description languages allow a digital system to be described with a wide range of abstraction, and they support top down design techniques. A key feature of any hardware description language environment is its ability to simulate the modeled system. The two most important hardware description languages are Verilog and VHDL. Verilog has been the dominant language for the design of application specific integrated circuits (ASIC's). However, VHDL is rapidly gaining in popularity.

  10. Hardware removal - extremity

    MedlinePlus

    ... enable JavaScript. Surgeons use hardware such as pins, plates, or screws to help fix a broken bone ... SW, Hotchkiss RN, Pederson WC, Kozin SH, Cohen MS, eds. Green's Operative Hand Surgery . 7th ed. Philadelphia, ...

  11. Initial Hardware Development Schedule

    NASA Technical Reports Server (NTRS)

    Culpepper, William X.

    1991-01-01

    The hardware development schedule for the Common Lunar Lander's (CLLs) tracking system is presented. Among the topics covered are the following: historical perspective, solution options, industry contacts, and the rationale for selection.

  12. Detonation command and control

    DOEpatents

    Mace, Jonathan L.; Seitz, Gerald J.; Echave, John A.; Le Bas, Pierre-Yves

    2016-05-31

    The detonation of one or more explosive charges and propellant charges by a detonator in response to a fire control signal from a command and control system comprised of a command center and instrumentation center with a communications link there between. The fire control signal is selectively provided to the detonator from the instrumentation center if plural detonation control switches at the command center are in a fire authorization status, and instruments, and one or more interlocks, if included, are in a ready for firing status. The instrumentation and command centers are desirably mobile, such as being respective vehicles.

  13. Detonation command and control

    DOEpatents

    Mace, Jonathan L.; Seitz, Gerald J.; Echave, John A.; Le Bas, Pierre-Yves

    2015-11-10

    The detonation of one or more explosive charges and propellant charges by a detonator in response to a fire control signal from a command and control system comprised of a command center and instrumentation center with a communications link therebetween. The fire control signal is selectively provided to the detonator from the instrumentation center if plural detonation control switches at the command center are in a fire authorization status, and instruments, and one or more interlocks, if included, are in a ready for firing status. The instrumentation and command centers are desirably mobile, such as being respective vehicles.

  14. Hardware Correlator Development at SHAO

    NASA Astrophysics Data System (ADS)

    Xu, Zhijun; Gan, Jiangying; Guo, Shaoguang

    2016-12-01

    Hardware correlators have been used in the Chinese Chang'E missions. Recently, a hardware correlator based on uniboard has been developed. This article presents the development of the hardware correlator at SHAO and some results.

  15. Managing the Risk of Command File Errors

    NASA Technical Reports Server (NTRS)

    Meshkat, Leila; Bryant, Larry W.

    2013-01-01

    Command File Error (CFE), as defined by the Jet Propulsion Laboratory's (JPL) Mission Operations Assurance (MOA) is, regardless of the consequence on the spacecraft, either: an error in a command file sent to the spacecraft, an error in the process for developing and delivering a command file to the spacecraft, or the omission of a command file that should have been sent to the spacecraft. The risk consequence of a CFE can be mission ending and thus a concern to space exploration projects during their mission operations. A CFE during space mission operations is often the symptom of some kind of imbalance or inadequacy within the system that comprises the hardware & software used for command generation and the human experts involved in this endeavour. As we move into an era of enhanced collaboration with other NASA centers and commercial partners, these systems become more and more complex and hence it is all the more important to formally model and analyze CFEs in order to manage the risk of CFEs. Here we will provide a summary of the ongoing efforts at JPL in this area and also explain some more recent developments in the area of developing quantitative models for the purpose of managing CFE's.

  16. Managing the Risk of Command File Errors

    NASA Technical Reports Server (NTRS)

    Meshkat, Leila; Bryant, Larry W.

    2013-01-01

    Command File Error (CFE), as defined by the Jet Propulsion Laboratory's (JPL) Mission Operations Assurance (MOA) is, regardless of the consequence on the spacecraft, either: an error in a command file sent to the spacecraft, an error in the process for developing and delivering a command file to the spacecraft, or the omission of a command file that should have been sent to the spacecraft. The risk consequence of a CFE can be mission ending and thus a concern to space exploration projects during their mission operations. A CFE during space mission operations is often the symptom of some kind of imbalance or inadequacy within the system that comprises the hardware & software used for command generation and the human experts involved in this endeavour. As we move into an era of enhanced collaboration with other NASA centers and commercial partners, these systems become more and more complex and hence it is all the more important to formally model and analyze CFEs in order to manage the risk of CFEs. Here we will provide a summary of the ongoing efforts at JPL in this area and also explain some more recent developments in the area of developing quantitative models for the purpose of managing CFE's.

  17. A natural command language for C/3/I applications

    NASA Astrophysics Data System (ADS)

    Mergler, J. P.

    1980-03-01

    The article discusses the development of a natural command language and a control and analysis console designed to simplify the task of the operator in field of Command, Control, Communications, and Intelligence. The console is based on a DEC LSI-11 microcomputer, supported by 16-K words of memory and a serial interface component. Discussion covers the language, which utilizes English and a natural syntax, and how it is integrated with the hardware. It is concluded that results have demonstrated the effectiveness of this natural command language.

  18. Expedition 21 Commander De Winne poses for a photo with a MSL FLSS

    NASA Image and Video Library

    2009-10-14

    ISS021-E-018952 (14 Oct. 2009) --- European Space Agency astronaut Frank De Winne, Expedition 21 commander, is pictured with Materials Science Laboratory (MSL) hardware in the Kibo laboratory of the International Space Station.

  19. McArthur stows SLAMMD hardware in the U.S. Lab during Expedition 12

    NASA Image and Video Library

    2005-12-16

    ISS012-E-12641 (16 Dec. 2005) --- Astronaut William S. (Bill) McArthur Jr., Expedition 12 commander and NASA space station science officer, stows the Space Linear Acceleration Mass Measurement Device (SLAMMD) hardware after conducting test operations. SLAMMD hardware was stowed in a stowage drawer on the Human Research Facility (HRF) rack in the Destiny laboratory of the International Space Station.

  20. NASA HUNCH Hardware

    NASA Technical Reports Server (NTRS)

    Hall, Nancy R.; Wagner, James; Phelps, Amanda

    2014-01-01

    What is NASA HUNCH? High School Students United with NASA to Create Hardware-HUNCH is an instructional partnership between NASA and educational institutions. This partnership benefits both NASA and students. NASA receives cost-effective hardware and soft goods, while students receive real-world hands-on experiences. The 2014-2015 was the 12th year of the HUNCH Program. NASA Glenn Research Center joined the program that already included the NASA Johnson Space Flight Center, Marshall Space Flight Center, Langley Research Center and Goddard Space Flight Center. The program included 76 schools in 24 states and NASA Glenn worked with the following five schools in the HUNCH Build to Print Hardware Program: Medina Career Center, Medina, OH; Cattaraugus Allegheny-BOCES, Olean, NY; Orleans Niagara-BOCES, Medina, NY; Apollo Career Center, Lima, OH; Romeo Engineering and Tech Center, Washington, MI. The schools built various parts of an International Space Station (ISS) middeck stowage locker and learned about manufacturing process and how best to build these components to NASA specifications. For the 2015-2016 school year the schools will be part of a larger group of schools building flight hardware consisting of 20 ISS middeck stowage lockers for the ISS Program. The HUNCH Program consists of: Build to Print Hardware; Build to Print Soft Goods; Design and Prototyping; Culinary Challenge; Implementation: Web Page and Video Production.

  1. TRAVEL WITH COMMANDER QUALICIA

    EPA Science Inventory

    Commander Qualicia is a cartoon character created for an on-line training course that describes the quality system for the National Exposure Research Laboratory. In the training, which was developed by the QA staff and graphics/IT support contractors, Commander Qualicia and the ...

  2. TRAVEL WITH COMMANDER QUALICIA

    EPA Science Inventory

    Commander Qualicia is a cartoon character created for an on-line training course that describes the quality system for the National Exposure Research Laboratory. In the training, which was developed by the QA staff and graphics/IT support contractors, Commander Qualicia and the ...

  3. Command and Control.

    ERIC Educational Resources Information Center

    Thwaites, Donald

    1992-01-01

    Provides background information as an introduction to three articles on command and control simulations that involve police and fire departments. Elements of command and control situations are discussed, including leadership, management of people and resources, communication, and coordination; the effectiveness of simulations is considered; and…

  4. Skylab biomedical hardware development

    NASA Technical Reports Server (NTRS)

    Huffstetler, W. J., Jr.; Lem, J. D.

    1974-01-01

    The development of hardware to support biomedical experimentation and operations in the Skylab vehicle presented unique technical problems. Designs were required to enable the accurate measurement of many varied physiological parameters and to compensate for zero g such that uninhibited equipment operation would be possible. Because of problems that occurred during the orbital workshop launch, special tests were run and new equipment was designed and built for use by the first Skylab crew. Design concepts used in the development of hardware to support cardiovascular, pulmonary, vestibular, body, and specimen mass measuring experiments are discussed. Additionally, major problem areas and the corresponding design solutions, as well as knowledge gained that will be pertinent for future life sciences hardware development, are presented.

  5. Computer hardware fault administration

    DOEpatents

    Archer, Charles J.; Megerian, Mark G.; Ratterman, Joseph D.; Smith, Brian E.

    2010-09-14

    Computer hardware fault administration carried out in a parallel computer, where the parallel computer includes a plurality of compute nodes. The compute nodes are coupled for data communications by at least two independent data communications networks, where each data communications network includes data communications links connected to the compute nodes. Typical embodiments carry out hardware fault administration by identifying a location of a defective link in the first data communications network of the parallel computer and routing communications data around the defective link through the second data communications network of the parallel computer.

  6. Borisenko Hands Over Command to Fossum

    NASA Image and Video Library

    Expedition 28 Commander Andrey Borisenko handed over station command duties to Flight Engineer Mike Fossum. Fossum will command Expedition 29. The traditional Change of Command Ceremony took place ...

  7. Station Commander Praises AMS

    NASA Image and Video Library

    When asked what's the most important International Space Station experiment, Commander Chris Hadfield names the Alpha Magnetic Spectrometer-2, a state-of-the-art particle physics detector that coul...

  8. Tactical Mission Command (TMC)

    DTIC Science & Technology

    2016-03-01

    is now engaged in transitioning to the web -based Command Post Computing Environment (CPCE). TMC FAMILY OF SYSTEMS Legacy Products...all MCS 6.4 and BCS3 CPD requirements to the web based environment in support of Army objectives. TacApps also aims to minimize administrative...older Ventrilo technology resident within CPOF. - Command Web Collaborative Data Infrastructure gives the non-provisioned user a web -based

  9. Command Overview 2012

    DTIC Science & Technology

    2012-08-01

    XXXX = Xxx 1 Captain William W. DeBow Commander Port Hueneme Division Naval Surface Warfare Center COMMAND OVERVIEW 2012 Report Documentation... Xxx XXXX = Xxx 3 Bumper Washington D.C. *  Headquarters Virginia Beach *  Radars White Sands *  Missile Systems *  Overland Testing *  HE...Homeport for Navy’s Test Ship •  Deep Water Port •  49 Years of Fleet Support XXXX = Xxx XXXX = Xxx 4 Bumper Unique Facilities Deep Water

  10. Joint Mission Command Implementation

    DTIC Science & Technology

    2016-01-22

    continues to be challenging. The paper will evaluate scientific articles describing trust as, in the opinion of the author, the principle shortfall... scientific literature regarding trust and examines the biology of trust. Dempsey describes trust in his white paper as a behavior that commanders can...ground and air. The USMC formalized the structure in 1963 14 and placed it under a single commander.66 This makes the Marine Air Ground Task Force

  11. DCSP hardware maintenance system

    SciTech Connect

    Pazmino, M.

    1995-11-01

    This paper discusses the necessary changes to be implemented on the hardware side of the DCSP database. DCSP is currently tracking hardware maintenance costs in six separate databases. The goal is to develop a system that combines all data and works off a single database. Some of the tasks that will be discussed in this paper include adding the capability for report generation, creating a help package and preparing a users guide, testing the executable file, and populating the new database with data taken from the old database. A brief description of the basic process used in developing the system will also be discussed. Conclusions about the future of the database and the delivery of the final product are then addressed, based on research and the desired use of the system.

  12. Sterilization of space hardware.

    NASA Technical Reports Server (NTRS)

    Pflug, I. J.

    1971-01-01

    Discussion of various techniques of sterilization of space flight hardware using either destructive heating or the action of chemicals. Factors considered in the dry-heat destruction of microorganisms include the effects of microbial water content, temperature, the physicochemical properties of the microorganism and adjacent support, and nature of the surrounding gas atmosphere. Dry-heat destruction rates of microorganisms on the surface, between mated surface areas, or buried in the solid material of space vehicle hardware are reviewed, along with alternative dry-heat sterilization cycles, thermodynamic considerations, and considerations of final sterilization-process design. Discussed sterilization chemicals include ethylene oxide, formaldehyde, methyl bromide, dimethyl sulfoxide, peracetic acid, and beta-propiolactone.

  13. Sterilization of space hardware.

    NASA Technical Reports Server (NTRS)

    Pflug, I. J.

    1971-01-01

    Discussion of various techniques of sterilization of space flight hardware using either destructive heating or the action of chemicals. Factors considered in the dry-heat destruction of microorganisms include the effects of microbial water content, temperature, the physicochemical properties of the microorganism and adjacent support, and nature of the surrounding gas atmosphere. Dry-heat destruction rates of microorganisms on the surface, between mated surface areas, or buried in the solid material of space vehicle hardware are reviewed, along with alternative dry-heat sterilization cycles, thermodynamic considerations, and considerations of final sterilization-process design. Discussed sterilization chemicals include ethylene oxide, formaldehyde, methyl bromide, dimethyl sulfoxide, peracetic acid, and beta-propiolactone.

  14. Hardware Accelerated Simulated Radiography

    SciTech Connect

    Laney, D; Callahan, S; Max, N; Silva, C; Langer, S; Frank, R

    2005-04-12

    We present the application of hardware accelerated volume rendering algorithms to the simulation of radiographs as an aid to scientists designing experiments, validating simulation codes, and understanding experimental data. The techniques presented take advantage of 32 bit floating point texture capabilities to obtain validated solutions to the radiative transport equation for X-rays. An unsorted hexahedron projection algorithm is presented for curvilinear hexahedra that produces simulated radiographs in the absorption-only regime. A sorted tetrahedral projection algorithm is presented that simulates radiographs of emissive materials. We apply the tetrahedral projection algorithm to the simulation of experimental diagnostics for inertial confinement fusion experiments on a laser at the University of Rochester. We show that the hardware accelerated solution is faster than the current technique used by scientists.

  15. Command/response protocols and concurrent software

    NASA Astrophysics Data System (ADS)

    Bynum, W. L.

    1987-06-01

    A version of the program to control the parallel jaw gripper is documented. The parallel jaw end-effector hardware and the Intel 8031 processor that is used to control the end-effector are briefly described. A general overview of the controller program is given and a complete description of the program's structure and design are contained. There are three appendices: a memory map of the on-chip RAM, a cross-reference listing of the self-scheduling routines, and a summary of the top-level and monitor commands.

  16. Command/response protocols and concurrent software

    NASA Technical Reports Server (NTRS)

    Bynum, W. L.

    1987-01-01

    A version of the program to control the parallel jaw gripper is documented. The parallel jaw end-effector hardware and the Intel 8031 processor that is used to control the end-effector are briefly described. A general overview of the controller program is given and a complete description of the program's structure and design are contained. There are three appendices: a memory map of the on-chip RAM, a cross-reference listing of the self-scheduling routines, and a summary of the top-level and monitor commands.

  17. Defense Headquarters: Geographic Combatant Commands Rely on Subordinate Commands for Mission Management and Execution

    DTIC Science & Technology

    2016-06-30

    European Command, U.S. Northern Command, U.S. Pacific Command, and U.S. Southern Command. In March 2015, the Chairman of the Senate Armed Services...combatant commands (U.S. Africa Command, U.S. European Command, U.S. Northern Command, U.S. Pacific Command, and U.S. Southern Command) and their... Pacific Command includes four service component commands, three subordinate unified commands, and a joint task force. The joint task forces in the

  18. RRFC hardware operation manual

    SciTech Connect

    Abhold, M.E.; Hsue, S.T.; Menlove, H.O.; Walton, G.

    1996-05-01

    The Research Reactor Fuel Counter (RRFC) system was developed to assay the {sup 235}U content in spent Material Test Reactor (MTR) type fuel elements underwater in a spent fuel pool. RRFC assays the {sup 235}U content using active neutron coincidence counting and also incorporates an ion chamber for gross gamma-ray measurements. This manual describes RRFC hardware, including detectors, electronics, and performance characteristics.

  19. BASS Hardware Setup

    NASA Image and Video Library

    2016-01-27

    ISS046e025945 (01/27/2016) --- NASA astronaut Tim Kopra sets up hardware for the Burning and Suppression of Solids – Milliken, or BASS-M, experiment. The BASS-M investigation tests flame-retardant cotton fabrics to determine how well they resist burning in microgravity. Results benefit research on flame-retardant textiles that can be used on Earth and in space

  20. Cassini Radar hardware technologies

    SciTech Connect

    Wheeler, K.; Renick, P.

    1996-03-01

    The hardware development portion of the Cassini Radar task is complete. The flight model Digital Assembly and Energy Storage Assembly have been integrated and tested, as has the engineering/qualification model Radio Frequency Electronics Assembly. Integration of the flight model Radio Frequency Electronics Assembly is ready to begin. The intent of this paper is to describe some of the more interesting technologies implemented in the electronics to achieve the requirements of the Cassini Radar experiment. {copyright} {ital 1996 American Institute of Physics.}

  1. Imaging near orthopedic hardware.

    PubMed

    Koff, Matthew F; Burge, Alissa J; Koch, Kevin M; Potter, Hollis G

    2017-07-01

    Over one million total joint replacement surgeries were performed in the US in 2013 alone, and this number is expected to more than double by 2030. Traditional imaging techniques for postoperative evaluation of implanted devices, such as radiography, computerized tomography, or ultrasound, utilize ionizing radiation, suffer from beam hardening artifact, or lack the inherent high contrast necessary to adequately evaluate soft tissues around the implants, respectively. Magnetic resonance imaging (MRI), due to its ability to generate multiplanar, high-contrast images without the use of ionizing radiation is ideal for evaluating periprosthetic soft tissues but has traditionally suffered from in-plane and through-plane data misregistration due to the magnetic susceptibility of implanted materials. A recent renaissance in the interest of imaging near arthroplasty and implanted orthopedic hardware has led to the development of new techniques that help to mitigate the effects of magnetic susceptibility. This article describes the challenges of performing imaging near implanted orthopedic hardware, how to generate clinically interpretable images when imaging near implanted devices, and how the images may be interpreted for clinical use. We will also describe current developments of utilizing MRI to evaluate implanted orthopedic hardware. 3 Technical Efficacy: Stage 2 J. MAGN. RESON. IMAGING 2017;46:24-39. © 2017 International Society for Magnetic Resonance in Medicine.

  2. Échecs thérapeutiques chez les enfants infectés par le VIH en suivi de routine dans un contexte à ressources limitées au Cameroun

    PubMed Central

    Penda, Calixte Ida; Bebey, Francine Same; Mangamba, Danielle Kedy; Moukoko, Else Carole Eboumbou; Ngwa, Victoria; Makouet, Nicaise; Bissek, Anne-Cécile; Minkemdefo, Blaise Dupont; Tetanye, Ekoe; Ndombo, Paul Koki

    2013-01-01

    Introduction L'objectif de cette étude était de déterminer les facteurs associés aux échecs thérapeutiques chez les enfants infectés par le VIH à l'Hôpital Laquintinie de Douala. Méthodes Une étude transversale rétrospective a été menée sur une période de 5 mois en 2010, recrutant 222 enfants âgés de 1 à 18 ans et sous TARV depuis au moins 24 semaines. Les données sociodémographiques, cliniques, biologiques et de l'observance thérapeutique des patients ont été collectés à partir des dossiers des patients, et analysées avec le logiciel SPSS (version 16). Résultats 39 (17,6%) des enfants étaient en échec thérapeutique (délai moyen de survenue 26,8 mois) et 73,4% d'entre eux sont passés en seconde ligne. Les garçons avaient en moyenne un risque 5 fois plus élevé de faire un échec thérapeutique que les filles (OR=3,9; p=0,035). 94,4% des enfants suivis avaient un faible taux de CD4 à l'initiation (‘ 25%) associé au risque élevé d’échec thérapeutique (OR=5,2; p=0,007). Les enfants issus de famille monoparentale représentaient près de la moitié des cas d’échecs thérapeutiques. Sur 39 cas en échec thérapeutique, 41% des enfants étaient des orphelins. Parmi les enfants sous TARV, 46% prenaient leur trithérapie sous forme de médicaments séparés parmi lesquels 52,1% étaient en échec thérapeutique. Conclusion Les échecs thérapeutiques et le passage en seconde ligne dépendaient du contexte familial des enfants, de leur statut immunologique à l'initiation du traitement, de leur sexe et de la forme galénique du TARV. PMID:24171063

  3. Automatic Command Sequence Generation

    NASA Technical Reports Server (NTRS)

    Fisher, Forest; Gladded, Roy; Khanampompan, Teerapat

    2007-01-01

    Automatic Sequence Generator (Autogen) Version 3.0 software automatically generates command sequences for the Mars Reconnaissance Orbiter (MRO) and several other JPL spacecraft operated by the multi-mission support team. Autogen uses standard JPL sequencing tools like APGEN, ASP, SEQGEN, and the DOM database to automate the generation of uplink command products, Spacecraft Command Message Format (SCMF) files, and the corresponding ground command products, DSN Keywords Files (DKF). Autogen supports all the major multi-mission mission phases including the cruise, aerobraking, mapping/science, and relay mission phases. Autogen is a Perl script, which functions within the mission operations UNIX environment. It consists of two parts: a set of model files and the autogen Perl script. Autogen encodes the behaviors of the system into a model and encodes algorithms for context sensitive customizations of the modeled behaviors. The model includes knowledge of different mission phases and how the resultant command products must differ for these phases. The executable software portion of Autogen, automates the setup and use of APGEN for constructing a spacecraft activity sequence file (SASF). The setup includes file retrieval through the DOM (Distributed Object Manager), an object database used to store project files. This step retrieves all the needed input files for generating the command products. Depending on the mission phase, Autogen also uses the ASP (Automated Sequence Processor) and SEQGEN to generate the command product sent to the spacecraft. Autogen also provides the means for customizing sequences through the use of configuration files. By automating the majority of the sequencing generation process, Autogen eliminates many sequence generation errors commonly introduced by manually constructing spacecraft command sequences. Through the layering of commands into the sequence by a series of scheduling algorithms, users are able to rapidly and reliably construct the

  4. Use of CCSDS Packets Over SpaceWire to Control Hardware

    NASA Technical Reports Server (NTRS)

    Haddad, Omar; Blau, Michael; Haghani, Noosha; Yuknis, William; Albaijes, Dennis

    2012-01-01

    For the Lunar Reconnaissance Orbiter, the Command and Data Handling subsystem consisted of several electronic hardware assemblies that were connected with SpaceWire serial links. Electronic hardware would be commanded/controlled and telemetry data was obtained using the SpaceWire links. Prior art focused on parallel data buses and other types of serial buses, which were not compatible with the SpaceWire and the core flight executive (CFE) software bus. This innovation applies to anything that utilizes both SpaceWire networks and the CFE software. The CCSDS (Consultative Committee for Space Data Systems) packet contains predetermined values in its payload fields that electronic hardware attached at the terminus of the SpaceWire node would decode, interpret, and execute. The hardware s interpretation of the packet data would enable the hardware to change its state/configuration (command) or generate status (telemetry). The primary purpose is to provide an interface that is compatible with the hardware and the CFE software bus. By specifying the format of the CCSDS packet, it is possible to specify how the resulting hardware is to be built (in terms of digital logic) that results in a hardware design that can be controlled by the CFE software bus in the final application

  5. Flight Avionics Hardware Roadmap

    NASA Technical Reports Server (NTRS)

    Hodson, Robert; McCabe, Mary; Paulick, Paul; Ruffner, Tim; Some, Rafi; Chen, Yuan; Vitalpur, Sharada; Hughes, Mark; Ling, Kuok; Redifer, Matt; Wallace, Shawn

    2013-01-01

    As part of NASA's Avionics Steering Committee's stated goal to advance the avionics discipline ahead of program and project needs, the committee initiated a multi-Center technology roadmapping activity to create a comprehensive avionics roadmap. The roadmap is intended to strategically guide avionics technology development to effectively meet future NASA missions needs. The scope of the roadmap aligns with the twelve avionics elements defined in the ASC charter, but is subdivided into the following five areas: Foundational Technology (including devices and components), Command and Data Handling, Spaceflight Instrumentation, Communication and Tracking, and Human Interfaces.

  6. Parameterized hardware description as object oriented hardware model implementation

    NASA Astrophysics Data System (ADS)

    Drabik, Pawel K.

    2010-09-01

    The paper introduces novel model for design, visualization and management of complex, highly adaptive hardware systems. The model settles component oriented environment for both hardware modules and software application. It is developed on parameterized hardware description research. Establishment of stable link between hardware and software, as a purpose of designed and realized work, is presented. Novel programming framework model for the environment, named Graphic-Functional-Components is presented. The purpose of the paper is to present object oriented hardware modeling with mentioned features. Possible model implementation in FPGA chips and its management by object oriented software in Java is described.

  7. Testing the newly installed PCE (Proximity Communications Equipment) hardware

    NASA Image and Video Library

    2005-06-29

    ISS011-E-09816 (28 June 2005) --- Cosmonaut Sergei K. Krikalev, Expedition 11 commander representing Russia's Federal Space Agency, tests the newly installed Proximity Communications Equipment (PCE) hardware of the ASN-M satellite navigation system for the European Automated Transfer Vehicle (ATV) “Jules Verne” in the Zvezda Service Module of the International Space Station. The ATV is scheduled to arrive at the Station next year.

  8. Testing the newly installed PCE (Proximity Communications Equipment) hardware

    NASA Image and Video Library

    2005-06-28

    ISS011-E-09812 (28 June 2005) --- Cosmonaut Sergei K. Krikalev, Expedition 11 commander representing Russia's Federal Space Agency, tests the newly installed Proximity Communications Equipment (PCE) hardware of the ASN-M satellite navigation system for the European Automated Transfer Vehicle (ATV) “Jules Verne” in the Zvezda Service Module of the international space station. The ATV is scheduled to arrive at the station next year.

  9. Installing the new PCE (Proximity Communications Equipment) hardware

    NASA Image and Video Library

    2005-06-29

    ISS011-E-09799 (27 June 2005) --- Cosmonaut Sergei K. Krikalev, Expedition 11 commander representing Russia's Federal Space Agency, works with the new Proximity Communications Equipment (PCE) hardware of the ASN-M satellite navigation system for the European Automated Transfer Vehicle (ATV) “Jules Verne” in the Zvezda Service Module of the International Space Station. The ATV is scheduled to arrive at the Station next year.

  10. Hardware, software, brainware, noware

    NASA Astrophysics Data System (ADS)

    Scheeline, Alexander

    1995-04-01

    Developments in politics, communications, economics, and population have all had profound effects on the market for analytical chemical instrumentation. This essay examines the assumptions behind the current training of instrumentation scientists and marketing of instruments, and suggests changes in both. The market must be taken to be all of society, not just technically literate society. Cost tradeoffs between hardware and software are context- dependent. Chemometrics allows extraction of information from data that leaves the typical reductionist scientist queasy. And clever chemistry can sometimes obliterate entire markets. The implications of this evolution are explored.

  11. GRASS Hardware Configurations Guide

    DTIC Science & Technology

    1989-03-01

    portability rather than limit users to a single brand of hardware. Within GRASS, there are many processor inten- sive functions. Therefore, processor...Expansion Unit 2,000 558 RR13 2 60 MB. 1 4V tape drive 1.233 SYSI,2 2-User Licene N, C Total $ 26,710 $ 23,290 IhLs erem is not supplij, bv ,un Nficrosyterms...DOS world there are a ’arge number of vendors that can supply you with the basic 386 personal computer that wili work in place of the brand of computer

  12. Mir hardware heritage

    NASA Technical Reports Server (NTRS)

    Portree, David S. F.

    1995-01-01

    The heritage of the major Mir complex hardware elements is described. These elements include Soyuz-TM and Progress-M; the Kvant, Kvant 2, and Kristall modules; and the Mir base block. Configuration changes and major mission events of the Salyut 6, Salyut 7, and Mir multiport space stations are described in detail for the period 1977-1994. A comparative chronology of U.S. and Soviet/Russian manned spaceflight is also given for that period. The 68 illustrations include comparative scale drawings of U.S. and Russian spacecraft as well as sequential drawings depicting missions and mission events.

  13. Cost efficient command management

    NASA Technical Reports Server (NTRS)

    Brandt, Theresa; Murphy, C. W.; Kuntz, Jon; Barlett, Tom

    1996-01-01

    The design and implementation of a command management system (CMS) for a NASA control center, is described. The technology innovations implemented in the CMS provide the infrastructure required for operations cost reduction and future development cost reduction through increased operational efficiency and reuse in future missions. The command management design facilitates error-free operations which enables the automation of the routine control center functions and allows for the distribution of scheduling responsibility to the instrument teams. The reusable system was developed using object oriented methodologies.

  14. Nidia Diaz, Guerrilla Commander

    DTIC Science & Technology

    1997-03-01

    and was part of logistics.”18 She returned to Guatemala after the offensive to have her son Jose Alejandro, who was born on 2 June 1981, 5 weeks...FMLN delegation that participated in the peace talks with President Duarte at La Palma. Upon her return, she was sent to command the San Vicente ...exercised her military skills while in the field where she commanded the guerrillas in the province of San Vicente . Her work there can be compared to that of

  15. What is Combatant Command?

    DTIC Science & Technology

    1993-06-04

    the leadership of a civilian Secretary and established the co-equal Departments of the Army, Navy, and Air Force. In 1949 Congress ammended the National...a single Service force commander ( 1st CAV DIV functioning as the theater reserve), a Joint Task Force used to conduct a noncombatant evacuation of

  16. Economy of Command

    ERIC Educational Resources Information Center

    Medeiros, David Peter

    2012-01-01

    This dissertation proposes a principle of "economy of command", arguing that it provides a simple and natural explanation for some well-known properties of human language syntax. The focus is on the abstract combinatorial system that constructs the hierarchical structure of linguistic expressions, with long-distance dependencies…

  17. Examining Cyber Command Structures

    DTIC Science & Technology

    2015-03-01

    COMMAND STRUCTURES by Leah Tanner March 2015 Thesis Advisor: Dorothy Denning Second Reader: Daniel Verheul THIS PAGE INTENTIONALLY LEFT...from the NAVAL POSTGRADUATE SCHOOL March 2015 Author: Leah Tanner Approved by: Dorothy Denning Thesis Advisor Daniel...advisors, Dr. Dorothy Denning, and CAPT Daniel Verheul, thank you for your guidance and mentorship, and for the patience to review countless versions. To

  18. The REL Command Language.

    ERIC Educational Resources Information Center

    Gomberg, Sara

    Three basic notions--version, session and command language--are discussed which are essential for a user of the Rapidly Extensible Language (REL) system. The first is defined as a language--data base package consisting of a language, data and definitions. A session is stipulated to be the period during which the user operates at a terminal, and…

  19. Squadron Commander Involvement Program

    DTIC Science & Technology

    1989-05-01

    Colonel Bodie R. Bodenheim , Ratnntion of 2_SSk to Elven Ye-ar Fightttr Pilot: The Environment. Research Report No. AU-AWC-86-021. (Maxwell Air Force Base...Creer Couneelinq: Time f r Dynamc Action. Maxwell Air Force Bane, Alabama: Air Command and Staff College, May 1972. Bodenheim , Colonel Bodie R

  20. Command History for 1990

    DTIC Science & Technology

    1991-05-01

    Marine Corps Tiaining Systems (CBESS) memorization training Inteligence Center, Dam Neck Threat memorization training Commander Tactical Wings, Atlantic...Other finalists in the competition included Timothy T. Liang and Ben B. Buclatin for their paper "Improving the Utilization of Training Resources

  1. Command, Control and Emerging Technologies: Implications for the Operational COmmander

    DTIC Science & Technology

    1994-05-16

    of these cost effective solutions and alternatives will be required to insure the military’s unique needs are satisfied. Command and control, C2 Technology, Operational command and control, Emerging technology .

  2. Apollo Guidance, Navigation, and Control (GNC) Hardware Overview

    NASA Technical Reports Server (NTRS)

    Interbartolo, Michael

    2009-01-01

    This viewgraph presentation reviews basic guidance, navigation and control (GNC) concepts, examines the Command and Service Module (CSM) and Lunar Module (LM) GNC organization and discusses the primary GNC and the CSM Stabilization and Control System (SCS), as well as other CSM-specific hardware. The LM Abort Guidance System (AGS), Control Electronics System (CES) and other LM-specific hardware are also addressed. Three subsystems exist on each vehicle: the computer subsystem (CSS), the inertial subsystem (ISS) and the optical subsystem (OSS). The CSS and ISS are almost identical between CSM and LM and each is designed to operate independently. CSM SCS hardware are highlighted, including translation control, rotation controls, gyro assemblies, a gyro display coupler and flight director attitude indicators. The LM AGS hardware are also highlighted and include the abort electronics assembly and the abort sensor assembly; while the LM CES hardware includes the attitude controller assembly, thrust/translation controller assemblies and the ascent engine arming assemble. Other common hardware including the Orbital Rate Display - Earth and Lunar (ORDEAL) and the Crewman Optical Alignment Sight (COAS), a docking aid, are also highlighted.

  3. Mapping of topological quantum circuits to physical hardware.

    PubMed

    Paler, Alexandru; Devitt, Simon J; Nemoto, Kae; Polian, Ilia

    2014-04-11

    Topological quantum computation is a promising technique to achieve large-scale, error-corrected computation. Quantum hardware is used to create a large, 3-dimensional lattice of entangled qubits while performing computation requires strategic measurement in accordance with a topological circuit specification. The specification is a geometric structure that defines encoded information and fault-tolerant operations. The compilation of a topological circuit is one important aspect of programming a quantum computer, another is the mapping of the topological circuit into the operations performed by the hardware. Each qubit has to be controlled, and measurement results are needed to propagate encoded quantum information from input to output. In this work, we introduce an algorithm for mapping an topological circuit to the operations needed by the physical hardware. We determine the control commands for each qubit in the computer and the relevant measurements that are needed to track information as it moves through the circuit.

  4. Robustness in Digital Hardware

    NASA Astrophysics Data System (ADS)

    Woods, Roger; Lightbody, Gaye

    The growth in electronics has probably been the equivalent of the Industrial Revolution in the past century in terms of how much it has transformed our daily lives. There is a great dependency on technology whether it is in the devices that control travel (e.g., in aircraft or cars), our entertainment and communication systems, or our interaction with money, which has been empowered by the onset of Internet shopping and banking. Despite this reliance, there is still a danger that at some stage devices will fail within the equipment's lifetime. The purpose of this chapter is to look at the factors causing failure and address possible measures to improve robustness in digital hardware technology and specifically chip technology, giving a long-term forecast that will not reassure the reader!

  5. Hardware platform for multiple mobile robots

    NASA Astrophysics Data System (ADS)

    Parzhuber, Otto; Dolinsky, D.

    2004-12-01

    This work is concerned with software and communications architectures that might facilitate the operation of several mobile robots. The vehicles should be remotely piloted or tele-operated via a wireless link between the operator and the vehicles. The wireless link will carry control commands from the operator to the vehicle, telemetry data from the vehicle back to the operator and frequently also a real-time video stream from an on board camera. For autonomous driving the link will carry commands and data between the vehicles. For this purpose we have developed a hardware platform which consists of a powerful microprocessor, different sensors, stereo- camera and Wireless Local Area Network (WLAN) for communication. The adoption of IEEE802.11 standard for the physical and access layer protocols allow a straightforward integration with the internet protocols TCP/IP. For the inspection of the environment the robots are equipped with a wide variety of sensors like ultrasonic, infrared proximity sensors and a small inertial measurement unit. Stereo cameras give the feasibility of the detection of obstacles, measurement of distance and creation of a map of the room.

  6. 32 CFR 536.14 - Commanders of major Army commands.

    Code of Federal Regulations, 2010 CFR

    2010-07-01

    ... 32 National Defense 3 2010-07-01 2010-07-01 true Commanders of major Army commands. 536.14 Section 536.14 National Defense Department of Defense (Continued) DEPARTMENT OF THE ARMY CLAIMS AND ACCOUNTS CLAIMS AGAINST THE UNITED STATES The Army Claims System § 536.14 Commanders of major Army...

  7. 32 CFR 724.406 - Commander, Naval Medical Command.

    Code of Federal Regulations, 2014 CFR

    2014-07-01

    ... 32 National Defense 5 2014-07-01 2014-07-01 false Commander, Naval Medical Command. 724.406 Section 724.406 National Defense Department of Defense (Continued) DEPARTMENT OF THE NAVY PERSONNEL NAVAL..., Naval Medical Command. Custodian of Navy and Marine Corps health records. (See subpart C). ...

  8. 32 CFR 724.406 - Commander, Naval Medical Command.

    Code of Federal Regulations, 2012 CFR

    2012-07-01

    ... 32 National Defense 5 2012-07-01 2012-07-01 false Commander, Naval Medical Command. 724.406 Section 724.406 National Defense Department of Defense (Continued) DEPARTMENT OF THE NAVY PERSONNEL NAVAL..., Naval Medical Command. Custodian of Navy and Marine Corps health records. (See subpart C). ...

  9. 32 CFR 724.406 - Commander, Naval Medical Command.

    Code of Federal Regulations, 2010 CFR

    2010-07-01

    ... 32 National Defense 5 2010-07-01 2010-07-01 false Commander, Naval Medical Command. 724.406 Section 724.406 National Defense Department of Defense (Continued) DEPARTMENT OF THE NAVY PERSONNEL NAVAL..., Naval Medical Command. Custodian of Navy and Marine Corps health records. (See subpart C). ...

  10. 32 CFR 724.406 - Commander, Naval Medical Command.

    Code of Federal Regulations, 2011 CFR

    2011-07-01

    ... 32 National Defense 5 2011-07-01 2011-07-01 false Commander, Naval Medical Command. 724.406 Section 724.406 National Defense Department of Defense (Continued) DEPARTMENT OF THE NAVY PERSONNEL NAVAL..., Naval Medical Command. Custodian of Navy and Marine Corps health records. (See subpart C). ...

  11. Station Change of Command Ceremony

    NASA Image and Video Library

    The reins of the International Space Station were passed from Expedition 29 Commander Mike Fossum of NASA to his NASA colleague, newly arrived Expedition 30 Commander Dan Burbank in a ceremony on t...

  12. Aircraft roll steering command system

    NASA Technical Reports Server (NTRS)

    Lambregts, Antonius A. (Inventor)

    1985-01-01

    Aircraft roll command signals are generated as a function of the Microwave Landing System based azimuth, groundtrack, groundspeed and azimuth rate or range distance input parameters. On initial approach, roll command signals are inhibited until a minimum roll command requirement is met. As the aircraft approaches the centerline of the runway, the system reverts to a linear track control.

  13. Studies in Battle Command

    DTIC Science & Technology

    1995-01-01

    battlefield innovator, a commander with a will of iron, and a gambler of no mean stature. To supply the necessary bridging material, Gustav-us ordered his... beat the vaunted British Regulars In battle. After the fight at Chippewa, Brown was abIe to advance the American army across the Chippewa River to...considered timeless. Too messy to fit into neat categories, too random to quantify successfully, these human factors nevertheless affect military operations

  14. Understanding Command and Control

    DTIC Science & Technology

    2006-01-01

    discussion of models, with a focus on what a conceptual reference model—the instantiation of a model— is and the differences between a value view and a...environments in which militaries operate. Given that this book is focused on C2 for transformation, the history of C2 is not discussed in any detail.17 In...identified above are discussed . Note that the functions of command establish the guidance for and the focus of the functions of control. Hence, every

  15. Former Battalion Commander Survey

    DTIC Science & Technology

    1991-04-08

    sovuument Aesmy. FORMER BATTALION COMMANDER SURVEY BY SB D4 LIEUTENANT COLONEL HAROLD W. LORD, JR. LIEUTENANT COLONEL MICHAEL J. PETRUCCI LIEUTENANT...J. Petrucci & LTC Henry C. Rutf 13a. TYPE OF REPORT 13b. TIME COVERED 14. DATE OF REPORT (Year, Month, Day) 15. PAGE COUNT Group Study FROM TO 91 Apr...GROUP STUDY PROJECT by Lieutenant Colonel Harold W. Lord, Jr., OD Lieutenant Colonel Michael J. Petrucci , AD Lieutenant Colonel Henry C. Ruth, AV

  16. Hardware Removal in Craniomaxillofacial Trauma

    PubMed Central

    Cahill, Thomas J.; Gandhi, Rikesh; Allori, Alexander C.; Marcus, Jeffrey R.; Powers, David; Erdmann, Detlev; Hollenbeck, Scott T.; Levinson, Howard

    2015-01-01

    Background Craniomaxillofacial (CMF) fractures are typically treated with open reduction and internal fixation. Open reduction and internal fixation can be complicated by hardware exposure or infection. The literature often does not differentiate between these 2 entities; so for this study, we have considered all hardware exposures as hardware infections. Approximately 5% of adults with CMF trauma are thought to develop hardware infections. Management consists of either removing the hardware versus leaving it in situ. The optimal approach has not been investigated. Thus, a systematic review of the literature was undertaken and a resultant evidence-based approach to the treatment and management of CMF hardware infections was devised. Materials and Methods A comprehensive search of journal articles was performed in parallel using MEDLINE, Web of Science, and ScienceDirect electronic databases. Keywords and phrases used were maxillofacial injuries; facial bones; wounds and injuries; fracture fixation, internal; wound infection; and infection. Our search yielded 529 articles. To focus on CMF fractures with hardware infections, the full text of English-language articles was reviewed to identify articles focusing on the evaluation and management of infected hardware in CMF trauma. Each article’s reference list was manually reviewed and citation analysis performed to identify articles missed by the search strategy. There were 259 articles that met the full inclusion criteria and form the basis of this systematic review. The articles were rated based on the level of evidence. There were 81 grade II articles included in the meta-analysis. Result Our meta-analysis revealed that 7503 patients were treated with hardware for CMF fractures in the 81 grade II articles. Hardware infection occurred in 510 (6.8%) of these patients. Of those infections, hardware removal occurred in 264 (51.8%) patients; hardware was left in place in 166 (32.6%) patients; and in 80 (15.6%) cases

  17. Command decoder unit. [performance tests of data processing terminals and data converters for space shuttle orbiters

    NASA Technical Reports Server (NTRS)

    1976-01-01

    The design and testing of laboratory hardware (a command decoder unit) used in evaluating space shuttle instrumentation, data processing, and ground check-out operations is described. The hardware was a modification of another similar instrumentation system. A data bus coupler was designed and tested to interface the equipment to a central bus controller (computer). A serial digital data transfer mechanism was also designed. Redundant power supplies and overhead modules were provided to minimize the probability of a single component failure causing a catastrophic failure. The command decoder unit is packaged in a modular configuration to allow maximum user flexibility in configuring a system. Test procedures and special test equipment for use in testing the hardware are described. Results indicate that the unit will allow NASA to evaluate future software systems for use in space shuttles. The units were delivered to NASA and appear to be adequately performing their intended function. Engineering sketches and photographs of the command decoder unit are included.

  18. Flight Avionics Hardware Roadmap

    NASA Technical Reports Server (NTRS)

    Some, Raphael; Goforth, Monte; Chen, Yuan; Powell, Wes; Paulick, Paul; Vitalpur, Sharada; Buscher, Deborah; Wade, Ray; West, John; Redifer, Matt; hide

    2014-01-01

    The Avionics Technology Roadmap takes an 80% approach to technology investment in spacecraft avionics. It delineates a suite of technologies covering foundational, component, and subsystem-levels, which directly support 80% of future NASA space mission needs. The roadmap eschews high cost, limited utility technologies in favor of lower cost, and broadly applicable technologies with high return on investment. The roadmap is also phased to support future NASA mission needs and desires, with a view towards creating an optimized investment portfolio that matures specific, high impact technologies on a schedule that matches optimum insertion points of these technologies into NASA missions. The roadmap looks out over 15+ years and covers some 114 technologies, 58 of which are targeted for TRL6 within 5 years, with 23 additional technologies to be at TRL6 by 2020. Of that number, only a few are recommended for near term investment: 1. Rad Hard High Performance Computing 2. Extreme temperature capable electronics and packaging 3. RFID/SAW-based spacecraft sensors and instruments 4. Lightweight, low power 2D displays suitable for crewed missions 5. Radiation tolerant Graphics Processing Unit to drive crew displays 6. Distributed/reconfigurable, extreme temperature and radiation tolerant, spacecraft sensor controller and sensor modules 7. Spacecraft to spacecraft, long link data communication protocols 8. High performance and extreme temperature capable C&DH subsystem In addition, the roadmap team recommends several other activities that it believes are necessary to advance avionics technology across NASA: center dot Engage the OCT roadmap teams to coordinate avionics technology advances and infusion into these roadmaps and their mission set center dot Charter a team to develop a set of use cases for future avionics capabilities in order to decouple this roadmap from specific missions center dot Partner with the Software Steering Committee to coordinate computing hardware

  19. Command shaping for residual vibration free crane maneuvers

    SciTech Connect

    Parker, G.G.; Petterson, B.; Dohrmann, C.; Robinett, R.D.

    1995-07-01

    Cranes used in the construction and transportation industries are generally devices with multiple degrees of freedom including variable load-line length, variable jib length (usually via a trolley), and variable boom angles. Point-to-point payload maneuvers using cranes are performed so as not to excite the spherical pendulum modes of their cable and payload assemblies. Typically, these pendulum modes, although time-varying, exhibit low frequencies. Current crane maneuvers are therefore performed slowly contributing to high construction and transportation costs. This investigation details a general method for applying command shaping to various multiple degree of freedom cranes such that the payload moves to a specified point without residual oscillation. A dynamic programming method is used for general command shaping for optimal maneuvers. Computationally, the dynamic programming approach requires order M calculations to arrive at a solution, where M is the number of discretizations of the input commands. This feature is exploited for the crane command shaping problem allowing for rapid calculation of command histories. Fast generation of commands is a necessity for practical use of command shaping for the applications described in this work. These results are compared to near-optimal solutions where the commands are linear combinations of acceleration pulse basis functions. The pulse shape is required due to hardware requirements. The weights on the basis functions are chosen as the solution to a parameter optimization problem solved using a Recursive Quadratic Programming technique. Simulation results and experimental verification for a variable load-line length rotary crane are presented using both design procedures.

  20. The absolute path command

    SciTech Connect

    Moody, A.

    2012-05-11

    The ap command traveres all symlinks in a given file, directory, or executable name to identify the final absolute path. It can print just the final path, each intermediate link along with the symlink chan, and the permissions and ownership of each directory component in the final path. It has functionality similar to "which", except that it shows the final path instead of the first path. It is also similar to "pwd", but it can provide the absolute path to a relative directory from the current working directory.

  1. Automation Hardware & Software for the STELLA Robotic Telescope

    NASA Astrophysics Data System (ADS)

    Weber, M.; Granzer, Th.; Strassmeier, K. G.

    The STELLA telescope (a joint project of the AIP, Hamburger Sternwarte and the IAC) is to operate in fully robotic mode, with no human interaction necessary for regular operation. Thus, the hardware must be kept as simple as possible to avoid unnecessary failures, and the environmental conditions must be monitored accurately to protect the telescope in case of bad weather. All computers are standard PCs running Linux, and communication with specialized hardware is done via a RS232/RS485 bus system. The high level (java based) control software consists of independent modules to ease bug-tracking and to allow the system to be extended without changing existing modules. Any command cycle consists of three messages, the actual command sent from the central node to the operating device, an immediate acknowledge, and a final done message, both sent back from the receiving device to the central node. This reply-splitting allows a direct distinction between communication problems (no acknowledge message) and hardware problems (no or a delayed done message). To avoid bug-prone packing of all the sensor-analyzing software into a single package, each sensor-reading and interaction with other sensors is done within a self-contained thread. Weather-decision making is therefore totally decoupled from the core control software to avoid dead-locks in the core module.

  2. Empowered Commanders: The Cornerstone to Agile, Flexible Command and Control

    DTIC Science & Technology

    2015-02-01

    1 VIEWS Empowered Commanders The Cornerstone to Agile , Flexible Command and Control Maj Eric Theriault, USAF We cannot solve our problems with...FEB 2015 2. REPORT TYPE 3. DATES COVERED 00-00-2015 to 00-00-2015 4. TITLE AND SUBTITLE Empowered Commanders: The Cornerstone to Agile ...implements combat plans in support of the C2 function and the agility to modify those plans as necessary to meet evolving operational requirementsY This

  3. A spacecraft computer repairable via command.

    NASA Technical Reports Server (NTRS)

    Fimmel, R. O.; Baker, T. E.

    1971-01-01

    The MULTIPAC is a central data system developed for deep-space probes with the distinctive feature that it may be repaired during flight via command and telemetry links by reprogramming around the failed unit. The computer organization uses pools of identical modules which the program organizes into one or more computers called processors. The interaction of these modules is dynamically controlled by the program rather than hardware. In the event of a failure, new programs are entered which reorganize the central data system with a somewhat reduced total processing capability aboard the spacecraft. Emphasis is placed on the evolution of the system architecture and the final overall system design rather than the specific logic design.

  4. Optical Properties of Nanosatellite Hardware

    NASA Technical Reports Server (NTRS)

    Finckenor, M. M.; Coker, R. F.

    2014-01-01

    Over the last decade, a number of very small satellites have been launched into space. These have been called nanosatellites (generally of a weight between 1 and 10 kg) or picosatellites (weight <1 kg). This also includes CubeSats, which are based on 10-cm cube units. With the addition of the Japanese Experiment Module (JEM) Small Satellite Orbital Deployer (J-SSOD) to the International Space Station (ISS), CubeSats are easily cycled through the JEM airlock and deployed into space (fig. 1). The number of CubeSats launched since 2003 was approaching 100 at the time of publication, and the authors expect this trend in research to continue, particularly for high school and college flight experiments. Because these spacecraft are so small, there is usually no allowance for shielding or active heating or cooling of the avionics and other hardware. Parts that are usually ignored in the thermal analysis of larger spacecraft may contribute significantly to the heat load of a tiny satellite. In addition, many small satellites have commercial-off-the-shelf (COTS) components. To reduce costs, many providers of COTS components do not include the optical and physical parameters necessary for accurate thermal analysis. Marshall Space Flight Center participated in the development and analysis of the Space Missile Defense Command-Operational Nanosatellite Effect (SMDC-ONE) and the Edison Demonstration of Smallsat Networks (EDSN) nanosatellites. These optical property measurements are documented here in hopes that they may benefit future nanosatellite and picosatellite programs and aid thermal analysis to ensure project goals are met, with the understanding that material properties may vary by vendor, batch, manufacturing process, and preflight handling. Where possible, complementary data are provided from ground simulations of the space environment and flight experiments, such as the Materials on International Space Station Experiment (MISSE) series. NASA gives no recommendation

  5. PromISS 4 hardware set up in the MSG during Expedition 12

    NASA Image and Video Library

    2006-01-18

    ISS012-E-16184 (18 Jan. 2006) --- Astronaut William S. (Bill) McArthur, Jr., Expedition 12 commander and NASA space station science officer, sets up the Protein Crystal Growth Monitoring by Digital Holographic Microscope (PromISS) experiment hardware inside the Microgravity Science Glovebox (MSG) facility in the Destiny laboratory on the International Space Station.

  6. Theater Special Operations Commands Realignment

    DTIC Science & Technology

    2014-06-01

    D. Teske Mr. William C. Fleser United States Special Operations Command 7701 Tampa Point Boulevard MacDill Air Force Base, Florida 33621 Point...of Contact Ken D. Teske United States Special Operations Command 7701 Tampa Point Boulevard MacDill Air Force Base, Florida 33621 (757) 510...Theater Special Operations Commands Realignment Mr. Michael D. Tisdel Mr. Ken D. Teske Mr. William C. Fleser 19th ICCRTS 17 June 2014 Paper ID

  7. The National Military Command Structure,

    DTIC Science & Technology

    1978-07-01

    Defense Command ( ADCOM )--a Specified Command--is the single manager of US forces for the surveillance, warning, and defense of the United States against...Force has conducted a study of alternatives for changing the management of assets currently assigned to ADCOM without changing its basic missions. This...issues, the President should consider the formation of a group of National Military Advisers. 78 SLOSSARY ADCOM Aerospace Defense Command ASD/ISA

  8. Interactive Raytracing: The nirt Command

    DTIC Science & Technology

    2009-04-01

    Interactive Raytracing : The nirt Command by Clifford Yapp ARL-CR-624 April 2009 prepared by Quantum Research...Laboratory Aberdeen Proving Ground, MD 21005-5068 ARL-CR-624 April 2009 Interactive Raytracing : The nirt Command Clifford Yapp Quantum...DATES COVERED (From - To) June 2008–October 2008 4. TITLE AND SUBTITLE Interactive Raytracing : The nirt Command 5a. CONTRACT NUMBER W911QX-06-F

  9. Making the right hardware choices.

    PubMed

    DeGaspari, John

    2011-12-01

    A rapid expansion of computing hardware options is paving the way to better patient engagement and increased productivity. For that to happen, CIOs must balance their choices against workflow issues, infrastructure requirements, and budgetary constraints.

  10. NDAS Hardware Translation Layer Development

    NASA Technical Reports Server (NTRS)

    Nazaretian, Ryan N.; Holladay, Wendy T.

    2011-01-01

    The NASA Data Acquisition System (NDAS) project is aimed to replace all DAS software for NASA s Rocket Testing Facilities. There must be a software-hardware translation layer so the software can properly talk to the hardware. Since the hardware from each test stand varies, drivers for each stand have to be made. These drivers will act more like plugins for the software. If the software is being used in E3, then the software should point to the E3 driver package. If the software is being used at B2, then the software should point to the B2 driver package. The driver packages should also be filled with hardware drivers that are universal to the DAS system. For example, since A1, A2, and B2 all use the Preston 8300AU signal conditioners, then the driver for those three stands should be the same and updated collectively.

  11. Hardware Index to Permutation Converter

    DTIC Science & Technology

    2012-05-01

    Hardware Index to Permutation Converter J. T. Butler T. Sasao Department of Electrical and Computer Engineering Department of Computer Science...generates a permutation in response to an index. Since there are n! n-element permutations , the index ranges from 0 to n! − 1. Such a circuit is needed...in the hardware implementation of unique- permutation hash functions to specify how parallel machines interact through a shared memory. Such a circuit

  12. Command and Control of Joint Air Operations through Mission Command

    DTIC Science & Technology

    2016-06-01

    trust.”14 Such trust is mandatory for leading and executing in today’s complex global and geographically dispersed environments. To the joint force...those tactical-level commanders in the control and reporting center (CRC), Airborne Warning and Control System (AWACS), Marine air command and control

  13. Commander Wilcutt works at the commander's workstation during STS-106

    NASA Image and Video Library

    2000-09-11

    STS106-352-009 (8-20 September 2000) --- Astronaut Terrence W. Wilcutt, STS-106 mission commander, performs a firing of the reaction control system on the flight deck of the Space Shuttle Atlantis. Earth’s horizon is visible through the commander’s window.

  14. Commander Crippen at Forward Flight Deck Commanders Station

    NASA Technical Reports Server (NTRS)

    1983-01-01

    Commander Crippen, wearing launch and entry helmet (LEH), operates controls at Forward Flight Deck Commanders Station during entry procedures. Plasma ionization glow is visible through forward windows and data is displayed on control panel F7 CRT. Flight mirror assembly (ASSY), head-up display (HUD), and checklists appear in view.

  15. Maximizing TDRS Command Load Lifetime

    NASA Technical Reports Server (NTRS)

    Brown, Aaron J.

    2002-01-01

    The GNC software onboard ISS utilizes TORS command loads, and a simplistic model of TORS orbital motion to generate onboard TORS state vectors. Each TORS command load contains five "invariant" orbital elements which serve as inputs to the onboard propagation algorithm. These elements include semi-major axis, inclination, time of last ascending node crossing, right ascension of ascending node, and mean motion. Running parallel to the onboard software is the TORS Command Builder Tool application, located in the JSC Mission Control Center. The TORS Command Builder Tool is responsible for building the TORS command loads using a ground TORS state vector, mirroring the onboard propagation algorithm, and assessing the fidelity of current TORS command loads onboard ISS. The tool works by extracting a ground state vector at a given time from a current TORS ephemeris, and then calculating the corresponding "onboard" TORS state vector at the same time using the current onboard TORS command load. The tool then performs a comparison between these two vectors and displays the relative differences in the command builder tool GUI. If the RSS position difference between these two vectors exceeds the tolerable lim its, a new command load is built using the ground state vector and uplinked to ISS. A command load's lifetime is therefore defined as the time from when a command load is built to the time the RSS position difference exceeds the tolerable limit. From the outset of TORS command load operations (STS-98), command load lifetime was limited to approximately one week due to the simplicity of both the onboard propagation algorithm, and the algorithm used by the command builder tool to generate the invariant orbital elements. It was soon desired to extend command load lifetime in order to minimize potential risk due to frequent ISS commanding. Initial studies indicated that command load lifetime was most sensitive to changes in mean motion. Finding a suitable value for mean motion

  16. The eutrophication commandments.

    PubMed

    Fulweiler, R W; Rabalais, N N; Heiskanen, A S

    2012-10-01

    Typically, rising atmospheric carbon dioxide concentrations are used to illustrate how humans have impacted the earth. However, we have also dramatically altered the amount of nitrogen (N) and phosphorus (P) cycling through the biosphere. Eventually these nutrients are carried to coastal receiving waters where they cause severe, often negative consequences including increased phytoplankton and macroalgae blooms, loss of submerged aquatic vegetation, low oxygen events, and decreased biodiversity. In many systems mitigation efforts are now underway to return these ecosystems to a less impacted state. While many uncertainties about the best way to manage eutrophic systems remain it is clear that we must take action to lessen our human nutrient footprint. Based on our current understanding of eutrophic systems we present ten eutrophication commandments or guidelines as a tool for scientists, policy makers, managers, and the public.

  17. 32 CFR 724.405 - Commandant of the Marine Corps or the Commander, Naval Military Personnel Command.

    Code of Federal Regulations, 2014 CFR

    2014-07-01

    ... 32 National Defense 5 2014-07-01 2014-07-01 false Commandant of the Marine Corps or the Commander... Department Discharge Review System § 724.405 Commandant of the Marine Corps or the Commander, Naval Military Personnel Command. Personnel managers of the Marine Corps and the Navy; responsible for providing...

  18. 32 CFR 724.405 - Commandant of the Marine Corps or the Commander, Naval Military Personnel Command.

    Code of Federal Regulations, 2011 CFR

    2011-07-01

    ... Department Discharge Review System § 724.405 Commandant of the Marine Corps or the Commander, Naval Military... 32 National Defense 5 2011-07-01 2011-07-01 false Commandant of the Marine Corps or the Commander, Naval Military Personnel Command. 724.405 Section 724.405 National Defense Department of Defense...

  19. Hardware structures of hydronic systems for speed control

    NASA Astrophysics Data System (ADS)

    Avram, M.; Spânu, A.; Bucşan, C.; Besnea, D.

    2016-08-01

    Most hydraulic actuating systems use constant flow pumps, for economic reasons. The resistive method is then used to control the speed of the actuated load. In the case of high performance systems the flow area is modified using analogical or numeric electric commands applied to proportional flow control devices. In the first part of the paper some hardware structures of hydronic actuating systems used for speed control are presented, and in the second part two experimental models of such systems are presented. Some aspects regarding the output improvement of such a system are also considered.

  20. Burbank uses the Neurospat hardware in the Columbus Module

    NASA Image and Video Library

    2012-03-15

    ISS030-E-177227 (15 March 2012) --- NASA astronaut Dan Burbank, Expedition 30 commander, uses Neurospat hardware to perform a science session with the European Space Agency PASSAGES experiment in the Columbus laboratory of the International Space Station. PASSAGES is designed to test how astronauts interpret visual information in weightlessness. It aims at studying the effects of microgravity on the use of the 'Eye-Height' strategy for estimating allowed actions in an environment, and whether this could possibly decrease after a long exposure to weightlessness.

  1. Burbank uses the Neurospat hardware in the Columbus Module

    NASA Image and Video Library

    2012-03-15

    ISS030-E-177225 (15 March 2012) --- NASA astronaut Dan Burbank, Expedition 30 commander, uses Neurospat hardware to perform a science session with the European Space Agency PASSAGES experiment in the Columbus laboratory of the International Space Station. PASSAGES is designed to test how astronauts interpret visual information in weightlessness. It aims at studying the effects of microgravity on the use of the 'Eye-Height' strategy for estimating allowed actions in an environment, and whether this could possibly decrease after a long exposure to weightlessness.

  2. Web tools to monitor and debug DAQ hardware

    SciTech Connect

    Eugene Desavouret; Jerzy M. Nogiec

    2003-06-04

    A web-based toolkit to monitor and diagnose data acquisition hardware has been developed. It allows for remote testing, monitoring, and control of VxWorks data acquisition computers and associated instrumentation using the HTTP protocol and a web browser. This solution provides concurrent and platform independent access, supplementary to the standard single-user rlogin mechanism. The toolkit is based on a specialized web server, and allows remote access and execution of select system commands and tasks, execution of test procedures, and provides remote monitoring of computer system resources and connected hardware. Various DAQ components such as multiplexers, digital I/O boards, analog to digital converters, or current sources can be accessed and diagnosed remotely in a uniform and well-organized manner. Additionally, the toolkit application supports user authentication and is able to enforce specified access restrictions.

  3. Commanding an Air Force Squadron

    DTIC Science & Technology

    1993-12-01

    6 The Base Environment ................... 7 Getting Started and Setting the Course-The First Three Months ..... 10 Your Position...34 ........................ 17 The Wing’s Mission ................. 19 Setting the Direction ...................... 19 N otes...last minute trying to set up a new flightsuit. New commanders usually have an opportunity to address the audi- ence at the change-of-command ceremony

  4. Predicting compliance with command hallucinations.

    PubMed

    Junginger, J

    1990-02-01

    Of 44 patients who experienced command hallucinations, those with hallucination-related delusions and hallucinatory voices they could identify were more likely to comply with the commands. The danger of the behaviors specified by the hallucinations did not appear to be a factor in compliance.

  5. Company Command: The Bottom Line

    DTIC Science & Technology

    1990-11-20

    Develop a joint inventory schedule. " Resolve any problems. " Be cordial , open, and clear. * Don’t be intimidated. If the outgoing commander is...Company Command/Meyer Anytime you have a unit function where alcohol is pres- Tip ent, also have non-alcoholic beverages readily available. Give your

  6. Safety aspects of spacecraft commanding

    NASA Technical Reports Server (NTRS)

    Peccia, N.

    1994-01-01

    The commanding of spacecraft is a potentially hazardous activity for the safety of the spacecraft. Present day control systems contain safety features in their commanding subsystem and in addition, strict procedures are also followed by operations staff. However, problems have occurred on a number of missions as a result of erroneous commanding leading in some cases to spacecraft contingencies and even to near loss of the spacecraft. The problems of checking commands in advance are increased by the tendency in modern spacecraft to use blocked/time-tagged commands and the increased usage of on-board computers, for which commands changing on-board software tables can radically change spacecraft or subsystem behavior. This paper reports on an on-going study. The study aims to improve the approach to safety of spacecraft commanding. It will show how ensuring 'safe' commanding can be carried out more efficiently, and with greater reliability, with the help of knowledge based systems and/or fast simulators. The whole concept will be developed based on the Object-Oriented approach.

  7. Hardware cleanliness methodology and certification

    NASA Technical Reports Server (NTRS)

    Harvey, Gale A.; Lash, Thomas J.; Rawls, J. Richard

    1995-01-01

    Inadequacy of mass loss cleanliness criteria for selection of materials for contamination sensitive uses, and processing of flight hardware for contamination sensitive instruments is discussed. Materials selection for flight hardware is usually based on mass loss (ASTM E-595). However, flight hardware cleanliness (MIL 1246A) is a surface cleanliness assessment. It is possible for materials (e.g. Sil-Pad 2000) to pass ASTM E-595 and fail MIL 1246A class A by orders of magnitude. Conversely, it is possible for small amounts of nonconforming material (Huma-Seal conformal coating) to not present significant cleanliness problems to an optical flight instrument. Effective cleaning (precleaning, precision cleaning, and ultra cleaning) and cleanliness verification are essential for contamination sensitive flight instruments. Polish cleaning of hardware, e.g. vacuum baking for vacuum applications, and storage of clean hardware, e.g. laser optics, is discussed. Silicone materials present special concerns for use in space because of the rapid conversion of the outgassed residues to glass by solar ultraviolet radiation and/or atomic oxygen. Non ozone depleting solvent cleaning and institutional support for cleaning and certification are also discussed.

  8. 14 CFR 91.1031 - Pilot in command or second in command: Designation required.

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... 14 Aeronautics and Space 2 2011-01-01 2011-01-01 false Pilot in command or second in command... RULES Fractional Ownership Operations Program Management § 91.1031 Pilot in command or second in command...; and (2) Second in command for each program flight requiring two pilots. (b) The pilot in command,...

  9. 14 CFR 91.1031 - Pilot in command or second in command: Designation required.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... 14 Aeronautics and Space 2 2010-01-01 2010-01-01 false Pilot in command or second in command... RULES Fractional Ownership Operations Program Management § 91.1031 Pilot in command or second in command...; and (2) Second in command for each program flight requiring two pilots. (b) The pilot in command,...

  10. 14 CFR 91.1031 - Pilot in command or second in command: Designation required.

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... 14 Aeronautics and Space 2 2013-01-01 2013-01-01 false Pilot in command or second in command... RULES Fractional Ownership Operations Program Management § 91.1031 Pilot in command or second in command...; and (2) Second in command for each program flight requiring two pilots. (b) The pilot in command,...

  11. 14 CFR 91.1031 - Pilot in command or second in command: Designation required.

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... 14 Aeronautics and Space 2 2012-01-01 2012-01-01 false Pilot in command or second in command... RULES Fractional Ownership Operations Program Management § 91.1031 Pilot in command or second in command...; and (2) Second in command for each program flight requiring two pilots. (b) The pilot in command,...

  12. 14 CFR 91.1031 - Pilot in command or second in command: Designation required.

    Code of Federal Regulations, 2014 CFR

    2014-01-01

    ... 14 Aeronautics and Space 2 2014-01-01 2014-01-01 false Pilot in command or second in command... RULES Fractional Ownership Operations Program Management § 91.1031 Pilot in command or second in command...; and (2) Second in command for each program flight requiring two pilots. (b) The pilot in command,...

  13. 32 CFR 536.12 - Commanding General, U.S. Army Medical Command.

    Code of Federal Regulations, 2014 CFR

    2014-07-01

    ... 32 National Defense 3 2014-07-01 2014-07-01 false Commanding General, U.S. Army Medical Command.... Army Medical Command. (a) After consulting with the Commander USARCS on the selection of medical claims attorneys, the Commander of the U.S. Army MEDCOM, the European Medical Command, or other regional...

  14. 32 CFR 536.12 - Commanding General, U.S. Army Medical Command.

    Code of Federal Regulations, 2012 CFR

    2012-07-01

    ... 32 National Defense 3 2012-07-01 2009-07-01 true Commanding General, U.S. Army Medical Command.... Army Medical Command. (a) After consulting with the Commander USARCS on the selection of medical claims attorneys, the Commander of the U.S. Army MEDCOM, the European Medical Command, or other regional...

  15. An Analysis of Division Commander Lessons Learned

    DTIC Science & Technology

    1989-02-24

    Department of the Army. Division Command Lessons Learned Program : Experiences in Division Command. Carlisle Barracks: U.S. Army Military History Institute...1985. 2. U.S. Department of the Army. Division Command Lessons Learned Program : Experiences in Division Command. Carlisle Barracks: U.S. Army...Military History Institute, 1986. 3. U.S. Department of the Army. Division Command Lessons Learned Program : Experiences in Division Command. Carlisle 4

  16. Command in a field hospital.

    PubMed

    Bricknell, M C M

    2003-03-01

    This paper examines the challenges involved in commanding a field hospital. There are frequent, dynamic tensions between the military culture that is based on a task-focussed, hierarchical structure and the clinical culture that is based on flat, process-focussed, multidisciplinary teams. The paper outlines the cultural environment of the field hospital and then examines the deployment sequence whereby a functioning clinical facility may be created from a group of disparate individuals. There are a number of tools that may assist with this including the personality of the Commanding Officer, individual skills, the creation of an organizational identity and the choice of command structure.

  17. Commander Collins seated in the flight deck commander's station

    NASA Image and Video Library

    1999-07-24

    S93-E-5031 (23 July 1999) --- Astronaut Eileen M. Collins, mission commander, looks over a procedures checklist at the commander's station on the forward flight deck of the Space Shuttle Columbia on Flight Day 1. The most important event of this day was the deployment of the Chandra X-Ray Observatory, the world's most powerful X-Ray telescope. The photo was recorded with an electronic still camera (ESC).

  18. Commander Collins seated in the flight deck commander's station

    NASA Image and Video Library

    1999-07-24

    S93-E-5033 (23 July 1999) --- Astronaut Eileen M. Collins, mission commander, looks over a procedures checklist at the commander's station on the forward flight deck of the Space Shuttle Columbia on Flight Day 1. The most important event of this day was the deployment of the Chandra X-Ray Observatory, the world's most powerful X-Ray telescope. The photo was recorded with an electronic still camera (ESC).

  19. Microcomputer Hardware. Energy Technology Series.

    ERIC Educational Resources Information Center

    Technical Education Research Centre-Southwest, Waco, TX.

    This course in microcomputer hardware is one of 16 courses in the Energy Technology Series developed for an Energy Conservation-and-Use Technology curriculum. Intended for use in two-year postsecondary technical institutions to prepare technicians for employment, the courses are also useful in industry for updating employees in company-sponsored…

  20. Police Communications: Humans and Hardware.

    ERIC Educational Resources Information Center

    Zannes, Estelle

    This volume presents an overview of police communications and analyzes the relationships between the people and hardware in the police system. Chapters discuss the development and use of such communication devices as the telegraph, telephone, and computers; the role of mass media, feedback, and communicative settings in human communication;…

  1. Hardware Selection: A Nontechnical Approach.

    ERIC Educational Resources Information Center

    Kiteka, Sebastian F.

    Presented in nontechnical language, this guide suggests criteria for the selection of three computer hardware essentials--a microcomputer, a monitor, and a printer. Factors to be considered in selecting the microcomputer are identified and discussed, including what the computer is to be used for, dealer support, software availability, modem…

  2. Satellite Communication Hardware Emulation System (SCHES)

    NASA Technical Reports Server (NTRS)

    Kaplan, Ted

    1993-01-01

    Satellite Communication Hardware Emulator System (SCHES) is a powerful simulator that emulates the hardware used in TDRSS links. SCHES is a true bit-by-bit simulator that models communications hardware accurately enough to be used as a verification mechanism for actual hardware tests on user spacecraft. As a credit to its modular design, SCHES is easily configurable to model any user satellite communication link, though some development may be required to tailor existing software to user specific hardware.

  3. Station Commander Sends Holiday Greetings

    NASA Image and Video Library

    Aboard the International Space Station, Expedition 30 Commander Dan Burbank of NASA sends season's greetings to the world and shares his thoughts about being in orbit aboard the space-based laborat...

  4. Advanced Command Destruct System (ACDS) Enhanced Flight Termination System (EFTS)

    NASA Technical Reports Server (NTRS)

    Tow, David

    2009-01-01

    NASA Dryden started working towards a single vehicle enhanced flight termination system (EFTS) in January 2008. NASA and AFFTC combined their efforts to work towards final operating capability for multiple vehicle and multiple missions simultaneously, to be completed by the end of 2011. Initially, the system was developed to support one vehicle and one frequency per mission for unmanned aerial vehicles (UAVs) at NASA Dryden. By May 2008 95% of design and hardware builds were completed, however, NASA Dryden's change of software safety scope and requirements caused delays after May 2008. This presentation reviews the initial and final operating capabilities for the Advanced Command Destruct System (ACDS), including command controller and configuration software development. A requirements summary is also provided.

  5. The SAS-3 delayed command system

    NASA Technical Reports Server (NTRS)

    Hoffman, E. J.

    1975-01-01

    To meet the requirements arising from the increased complexity of the power, attitude control and telemetry systems, a full redundant high-performance control section with delayed command capability was designed for the Small Astronomy Satellite-3 (SAS-3). The relay command system of SAS-3 is characterized by 56 bystate relay commands, with capability for handling up to 64 commands in future versions. The 'short' data command service of SAS-1 and SAS-2 consisting of shifting 24-bit words to two users was expanded to five users and augmented with a 'long load' data command service (up to 4080 bits) used to program the telemetry system and the delayed command subsystem. The inclusion of a delayed command service ensures a program of up to 30 relay or short data commands to be loaded for execution at designated times. The design and system operation of the SAS-3 command section are analyzed, with special attention given to the delayed command subsystem.

  6. 66 Stories of Battle Command

    DTIC Science & Technology

    2000-01-01

    collection of information if it does not display a currently valid OMB control number. 1 . REPORT DATE 2000 2 . REPORT TYPE 3. DATES COVERED 00-00...Frame, James W. Lussier, Editors xi, 255 p. maps; 23 cm. Includes index. ISBN 1 . Military Command, Modern - - 21st century. 2 . Military Decision...xi Introduction 1 by GENERAL FRED FRANKS, JR., US ARMY (RETIRED) Battle Command Stories 1 . Company Team Knows Its Sector 7 2

  7. Command Process Modeling & Risk Analysis

    NASA Technical Reports Server (NTRS)

    Meshkat, Leila

    2011-01-01

    Commanding Errors may be caused by a variety of root causes. It's important to understand the relative significance of each of these causes for making institutional investment decisions. One of these causes is the lack of standardized processes and procedures for command and control. We mitigate this problem by building periodic tables and models corresponding to key functions within it. These models include simulation analysis and probabilistic risk assessment models.

  8. Command Process Modeling & Risk Analysis

    NASA Technical Reports Server (NTRS)

    Meshkat, Leila

    2011-01-01

    Commanding Errors may be caused by a variety of root causes. It's important to understand the relative significance of each of these causes for making institutional investment decisions. One of these causes is the lack of standardized processes and procedures for command and control. We mitigate this problem by building periodic tables and models corresponding to key functions within it. These models include simulation analysis and probabilistic risk assessment models.

  9. Modular hardware synthesis using an HDL. [Hardware Description Language

    NASA Technical Reports Server (NTRS)

    Covington, J. A.; Shiva, S. G.

    1981-01-01

    Although hardware description languages (HDL) are becoming more and more necessary to automated design systems, their application is complicated due to the difficulty in translating the HDL description into an implementable format, nonfamiliarity of hardware designers with high-level language programming, nonuniform design methodologies and the time and costs involved in transfering HDL design software. Digital design language (DDL) suffers from all of the above problems and in addition can only by synthesized on a complete system and not on its subparts, making it unsuitable for synthesis using standard modules or prefabricated chips such as those required in LSI or VLSI circuits. The present paper presents a method by which the DDL translator can be made to generate modular equations that will allow the system to be synthesized as an interconnection of lower-level modules. The method involves the introduction of a new language construct called a Module which provides for the separate translation of all equations bounded by it.

  10. Modular hardware synthesis using an HDL. [Hardware Description Language

    NASA Technical Reports Server (NTRS)

    Covington, J. A.; Shiva, S. G.

    1981-01-01

    Although hardware description languages (HDL) are becoming more and more necessary to automated design systems, their application is complicated due to the difficulty in translating the HDL description into an implementable format, nonfamiliarity of hardware designers with high-level language programming, nonuniform design methodologies and the time and costs involved in transfering HDL design software. Digital design language (DDL) suffers from all of the above problems and in addition can only by synthesized on a complete system and not on its subparts, making it unsuitable for synthesis using standard modules or prefabricated chips such as those required in LSI or VLSI circuits. The present paper presents a method by which the DDL translator can be made to generate modular equations that will allow the system to be synthesized as an interconnection of lower-level modules. The method involves the introduction of a new language construct called a Module which provides for the separate translation of all equations bounded by it.

  11. Strategic Global Climate Command?

    NASA Astrophysics Data System (ADS)

    Long, J. C. S.

    2016-12-01

    Researchers have been exploring geoengineering because Anthropogenic GHG emissions could drive the globe towards unihabitability for people, wildlife and vegetation. Potential global deployment of these technologies is inherently strategic. For example, solar radiation management to reflect more sunlight might be strategically useful during a period of time where the population completes an effort to cease emissions and carbon removal technologies might then be strategically deployed to move the atmospheric concentrations back to a safer level. Consequently, deployment of these global technologies requires the ability to think and act strategically on the part of the planet's governments. Such capacity most definitely does not exist today but it behooves scientists and engineers to be involved in thinking through how global command might develop because the way they do the research could support the development of a capacity to deploy intervention rationally -- or irrationally. Internationalizing research would get countries used to working together. Organizing the research in a step-wise manner where at each step scientists become skilled at explaining what they have learned, the quality of the information they have, what they don't know and what more they can do to reduce or handle uncertainty, etc. Such a process can increase societal confidence in being able to make wise decisions about deployment. Global capacity will also be enhanced if the sceintific establishment reinvents misssion driven research so that the programs will identify the systemic issues invovled in any proposed technology and systematically address them with research while still encouraging individual creativity. Geoengineering will diverge from climate science in that geoengineering research needs to design interventions for some publically desirable goal and investigates whether a proposed intervention will acheive desired outcomes. The effort must be a systems-engineering design problem

  12. REDSTONE ARSENAL GARRISON COMMANDER, COL. THOMAS (DOC) HOLLIDAY

    NASA Image and Video Library

    2017-03-03

    REDSTONE ARSENAL GARRISON COMMANDER COL. THOMAS "DOC" HOLLIDAY, LEFT, DISCUSSES THE PROCESSES AND HARDWARE USED IN NASA IN-SPACE MANUFACTURING TECHNIQUES WITH KEN COOPER, A STRUCTURAL MATERIALS ENGINEER AT NASA'S MARSHALL SPACE FLIGHT CENTER. COOPER, PART OF THE MARSHALL ENGINEERING DIRECTORATE'S ADVANCED MANUFACTURING AND DIGITAL SOLUTIONS TEAM, WAS AMONG NUMEROUS SUBJECT-MATTER EXPERTS WHO SHARED KEY MARSHALL CAPABILITIES DURING HOLLIDAY'S MARCH 3 MARSHALL TOUR. HOLLIDAY, A DECORATED OFFICER WHOSE MILITARY CAREER BEGAN IN 1992, GAINED FIRSTHAND INSIGHT INTO MARSHALL'S ADVANCED MANUFACTURING AND 3-D PRINTING TECHNIQUES; ROUND-THE-CLOCK INTERNATIONAL SPACE STATION SCIENCE AND COMMUNICATIONS SUPPORT BY THE PAYLOAD OPERATIONS INTEGRATION CENTER TEAM; AND THE LATEST UPGRADES TO MARSHALL TEST STANDS IN SUPPORT OF NEXT-GENERATION LAUNCH VEHICLE AND FLIGHT HARDWARE DEVELOPMENT. MARSHALL, A REDSTONE ARSENAL TENANT, ROUTINELY SHARES CUTTING-EDGE RESEARCH AND MANUFACTURING ADVANCES WITH ITS MILITARY AND FEDERAL AGENCY COUNTERPARTS, WORKING IN PARTNERSHIP TO ADVANCE NASA'S MISSION AND MAINTAIN THE NATION'S TECHNOLOGICAL LEADERSHIP.

  13. DSN command system Mark IV-85

    NASA Technical Reports Server (NTRS)

    Thorman, H. C.

    1986-01-01

    A functional description of the Deep Space Network Command System and its subsystem is presented. The DSP command system was implemented in 1986. Store and forward command functions are reviewed. Throughput command functions for Earth orbiter missions and subsystems configurations for Mark IV-85 system are summarized.

  14. Microbiologic assay of space hardware.

    NASA Technical Reports Server (NTRS)

    Favero, M. S.

    1971-01-01

    Review of the procedures used in the microbiological examination of space hardware. The general procedure for enumerating aerobic and anaerobic microorganisms and spores is outlined. Culture media and temperature-time cycles used for incubation are reviewed, along with assay systems designed for the enumeration of aerobic and anaerobic spores. The special problems which are discussed are involved in the precise and accurate enumeration of microorganisms on surfaces and in the neutralization of viable organisms buried inside solid materials that could be released to a planet's surface if the solid should be fractured. Special attention is given to sampling procedures including also the indirect techniques of surface assays of space hardware such as those using detachable or fallout strips. Some data on comparative levels of microbial contamination on lunar and planetary spacecraft are presented.

  15. Hardware-Accelerated Simulated Radiography

    SciTech Connect

    Laney, D; Callahan, S; Max, N; Silva, C; Langer, S; Frank, R

    2005-08-04

    We present the application of hardware accelerated volume rendering algorithms to the simulation of radiographs as an aid to scientists designing experiments, validating simulation codes, and understanding experimental data. The techniques presented take advantage of 32-bit floating point texture capabilities to obtain solutions to the radiative transport equation for X-rays. The hardware accelerated solutions are accurate enough to enable scientists to explore the experimental design space with greater efficiency than the methods currently in use. An unsorted hexahedron projection algorithm is presented for curvilinear hexahedral meshes that produces simulated radiographs in the absorption-only regime. A sorted tetrahedral projection algorithm is presented that simulates radiographs of emissive materials. We apply the tetrahedral projection algorithm to the simulation of experimental diagnostics for inertial confinement fusion experiments on a laser at the University of Rochester.

  16. Microbiologic assay of space hardware.

    NASA Technical Reports Server (NTRS)

    Favero, M. S.

    1971-01-01

    Review of the procedures used in the microbiological examination of space hardware. The general procedure for enumerating aerobic and anaerobic microorganisms and spores is outlined. Culture media and temperature-time cycles used for incubation are reviewed, along with assay systems designed for the enumeration of aerobic and anaerobic spores. The special problems which are discussed are involved in the precise and accurate enumeration of microorganisms on surfaces and in the neutralization of viable organisms buried inside solid materials that could be released to a planet's surface if the solid should be fractured. Special attention is given to sampling procedures including also the indirect techniques of surface assays of space hardware such as those using detachable or fallout strips. Some data on comparative levels of microbial contamination on lunar and planetary spacecraft are presented.

  17. Hardware Support for Software Debugging

    DTIC Science & Technology

    2011-05-01

    Architecture • Concurrency Debugging - ReEnact • Conclusions Cost of Software Defects • Financial Costs • In a study by NIST in 2002 it was found that... ReEnact • Leverages modified Thread-Level Speculation (TLS) hardware • Create partial orderings of threads in a multithreaded program using...logical vector clocks • Using these orderings, ReEnact is able to detect and often repair data race conditions in a multithreaded program • Experiments

  18. LWH & ACH Helmet Hardware Study

    DTIC Science & Technology

    2015-11-30

    in the microstructures. 2.3 Hardness Tests on Polished Cross Sections Rockwell hardness ( ASTM E18 Standard Test Methods for Rockwell Hardness of...microhardness measurements ( ASTM E384 Standard Test Method for Microindentation Hardness of Materials) were made on the exterior surfaces of screws...using conventional techniques (e.g. ASTM E3 Preparation of Metallographic Specimens). The hardware pieces were cross- sectioned using a low-speed diamond

  19. Hunting for hardware changes in data centres

    NASA Astrophysics Data System (ADS)

    Coelho dos Santos, M.; Steers, I.; Szebenyi, I.; Xafi, A.; Barring, O.; Bonfillou, E.

    2012-12-01

    With many servers and server parts the environment of warehouse sized data centres is increasingly complex. Server life-cycle management and hardware failures are responsible for frequent changes that need to be managed. To manage these changes better a project codenamed “hardware hound” focusing on hardware failure trending and hardware inventory has been started at CERN. By creating and using a hardware oriented data set - the inventory - with detailed information on servers and their parts as well as tracking changes to this inventory, the project aims at, for example, being able to discover trends in hardware failure rates.

  20. Mission Analysis: Giving Commanders What They Need

    DTIC Science & Technology

    2002-01-01

    Commanders The mission analysis does not reflect the dynamic nature of command personalities and the various manners in which commanders give , receive ...and think about information. Getting to know how the commander gives information, receives information, and thinks about information is a key factor...Approved for Public Release; Distribution is Unlimited Mission Analysis: Giving Commanders What They Need A Monograph by MAJ James M. Loffert U.S

  1. 14 CFR 135.109 - Pilot in command or second in command: Designation required.

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... ON BOARD SUCH AIRCRAFT Flight Operations § 135.109 Pilot in command or second in command: Designation required. (a) Each certificate holder shall designate a— (1) Pilot in command for each flight; and (2) Second in command for each flight requiring two pilots. (b) The pilot in command, as designated by...

  2. 14 CFR 135.109 - Pilot in command or second in command: Designation required.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... ON BOARD SUCH AIRCRAFT Flight Operations § 135.109 Pilot in command or second in command: Designation required. (a) Each certificate holder shall designate a— (1) Pilot in command for each flight; and (2) Second in command for each flight requiring two pilots. (b) The pilot in command, as designated by...

  3. 14 CFR 135.109 - Pilot in command or second in command: Designation required.

    Code of Federal Regulations, 2014 CFR

    2014-01-01

    ... ON BOARD SUCH AIRCRAFT Flight Operations § 135.109 Pilot in command or second in command: Designation required. (a) Each certificate holder shall designate a— (1) Pilot in command for each flight; and (2) Second in command for each flight requiring two pilots. (b) The pilot in command, as designated by...

  4. 14 CFR 135.109 - Pilot in command or second in command: Designation required.

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... ON BOARD SUCH AIRCRAFT Flight Operations § 135.109 Pilot in command or second in command: Designation required. (a) Each certificate holder shall designate a— (1) Pilot in command for each flight; and (2) Second in command for each flight requiring two pilots. (b) The pilot in command, as designated by...

  5. 14 CFR 135.109 - Pilot in command or second in command: Designation required.

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... ON BOARD SUCH AIRCRAFT Flight Operations § 135.109 Pilot in command or second in command: Designation required. (a) Each certificate holder shall designate a— (1) Pilot in command for each flight; and (2) Second in command for each flight requiring two pilots. (b) The pilot in command, as designated by...

  6. McArthur sets up the SLAMMD hardware in the U.S. Lab during Expedition 12

    NASA Image and Video Library

    2005-12-16

    ISS012-E-12577 (16 Dec. 2005) --- Astronaut William S. (Bill) McArthur Jr., Expedition 12 commander and NASA space station science officer, sets up the Space Linear Acceleration Mass Measurement Device (SLAMMD) hardware attached to the Human Research Facility (HRF) rack in the Destiny laboratory of the International Space Station.

  7. A novel visual hardware behavioral language

    NASA Technical Reports Server (NTRS)

    Li, Xueqin; Cheng, H. D.

    1992-01-01

    Most hardware behavioral languages just use texts to describe the behavior of the desired hardware design. This is inconvenient for VLSI designers who enjoy using the schematic approach. The proposed visual hardware behavioral language has the ability to graphically express design information using visual parallel models (blocks), visual sequential models (processes) and visual data flow graphs (which consist of primitive operational icons, control icons, and Data and Synchro links). Thus, the proposed visual hardware behavioral language can not only specify hardware concurrent and sequential functionality, but can also visually expose parallelism, sequentiality, and disjointness (mutually exclusive operations) for the hardware designers. That would make the hardware designers capture the design ideas easily and explicitly using this visual hardware behavioral language.

  8. Hardware and software reliability estimation using simulations

    NASA Technical Reports Server (NTRS)

    Swern, Frederic L.

    1994-01-01

    The simulation technique is used to explore the validation of both hardware and software. It was concluded that simulation is a viable means for validating both hardware and software and associating a reliability number with each. This is useful in determining the overall probability of system failure of an embedded processor unit, and improving both the code and the hardware where necessary to meet reliability requirements. The methodologies were proved using some simple programs, and simple hardware models.

  9. United States Transportation Command Annual Command Report 2006

    DTIC Science & Technology

    2006-01-01

    environment through the appropriate review and prioritization of command require­ ments and through the continued development and evolution of new...loads trucks with humanitarian supplies for ground transportation at Chaklala C-5A Galaxy aircraft at Moron Air Base, Spain, while deployed in support

  10. Solid-Liquid Interface Characterization Hardware

    NASA Technical Reports Server (NTRS)

    Peters, Palmer N.

    2000-01-01

    The objective is to develop enabling technology to characterize the solid-liquid interface during directional solidification to unprecedented levels with real-time measurement hardware. Existing x-ray imaging hardware is combined with compact Seebeck furnaces and thermal profiling hardware, under development, to accomplish the measurements. Furnace thermal profiles are continuously measured in addition to the sample characteristics.

  11. Instrumentation Hardware Abstraction Language (IHAL) Handbook

    DTIC Science & Technology

    2017-01-01

    Telemetry Group DOCUMENT 128-17 INSTRUMENTATION HARDWARE ABSTRACTION LANGUAGE (IHAL) HANDBOOK DISTRIBUTION A...intentionally left blank DOCUMENT 128-17 INSTRUMENTATION HARDWARE ABSTRACTION LANGUAGE (IHAL) HANDBOOK January 2017...5100 This page intentionally left blank. Instrumentation Hardware Abstract Language (IHAL) Handbook, RCC Document 128-17, January 2017 iii

  12. Door Hardware and Installations; Carpentry: 901894.

    ERIC Educational Resources Information Center

    Dade County Public Schools, Miami, FL.

    The curriculum guide outlines a course designed to provide instruction in the selection, preparation, and installation of hardware for door assemblies. The course is divided into five blocks of instruction (introduction to doors and hardware, door hardware, exterior doors and jambs, interior doors and jambs, and a quinmester post-test) totaling…

  13. Ford works with the InSpace-3 Hardware in the U.S. Laboratory

    NASA Image and Video Library

    2013-01-24

    ISS034-E-033733 (24 Jan. 2013) --- NASA astronaut Kevin Ford, Expedition 34 commander, works with the InSPACE-3 hardware inside the Microgravity Science Glovebox (MSG) in the Destiny laboratory of the International Space Station. InSPACE-3 applies different magnetic fields to vials of colloids, or liquids with microscopic particles, and observes how fluids can behave like a solid. Results may improve the strength and design of materials for stronger buildings and bridges.

  14. GENI: Grid Hardware and Software

    SciTech Connect

    2012-01-09

    GENI Project: The 15 projects in ARPA-E’s GENI program, short for “Green Electricity Network Integration,” aim to modernize the way electricity is transmitted in the U.S. through advances in hardware and software for the electric grid. These advances will improve the efficiency and reliability of electricity transmission, increase the amount of renewable energy the grid can utilize, and provide energy suppliers and consumers with greater control over their power flows in order to better manage peak power demand and cost.

  15. X-15 Hardware Design Challenges

    NASA Technical Reports Server (NTRS)

    Storms, Harrison A., Jr.

    1991-01-01

    Historical events in the development of the X-15 hardware design are presented. Some of the topics covered include: (1) drivers that led to the development of the X-15; (2) X-15 space research objectives; (3) original performance targets; (4) the X-15 typical mission; (5) X-15 dimensions and weight; (5) the propulsion system; (6) X-15 development milestones; (7) engineering and manufacturing challenges; (8) the X-15 structure; (9) ballistic flight control; (10) landing gear; (11) nose gear; and (12) an X-15 program recap.

  16. Exascale Hardware Architectures Working Group

    SciTech Connect

    Hemmert, S; Ang, J; Chiang, P; Carnes, B; Doerfler, D; Leininger, M; Dosanjh, S; Fields, P; Koch, K; Laros, J; Noe, J; Quinn, T; Torrellas, J; Vetter, J; Wampler, C; White, A

    2011-03-15

    The ASC Exascale Hardware Architecture working group is challenged to provide input on the following areas impacting the future use and usability of potential exascale computer systems: processor, memory, and interconnect architectures, as well as the power and resilience of these systems. Going forward, there are many challenging issues that will need to be addressed. First, power constraints in processor technologies will lead to steady increases in parallelism within a socket. Additionally, all cores may not be fully independent nor fully general purpose. Second, there is a clear trend toward less balanced machines, in terms of compute capability compared to memory and interconnect performance. In order to mitigate the memory issues, memory technologies will introduce 3D stacking, eventually moving on-socket and likely on-die, providing greatly increased bandwidth but unfortunately also likely providing smaller memory capacity per core. Off-socket memory, possibly in the form of non-volatile memory, will create a complex memory hierarchy. Third, communication energy will dominate the energy required to compute, such that interconnect power and bandwidth will have a significant impact. All of the above changes are driven by the need for greatly increased energy efficiency, as current technology will prove unsuitable for exascale, due to unsustainable power requirements of such a system. These changes will have the most significant impact on programming models and algorithms, but they will be felt across all layers of the machine. There is clear need to engage all ASC working groups in planning for how to deal with technological changes of this magnitude. The primary function of the Hardware Architecture Working Group is to facilitate codesign with hardware vendors to ensure future exascale platforms are capable of efficiently supporting the ASC applications, which in turn need to meet the mission needs of the NNSA Stockpile Stewardship Program. This issue is

  17. Command hallucinations, compliance, and risk assessment.

    PubMed

    Hersh, K; Borum, R

    1998-01-01

    Command hallucinations are auditory hallucinations that instruct a patient to act in specific ways; these commands can range in seriousness from innocuous to life-threatening. This article summarizes two areas of research regarding command hallucinations: rates of compliance with command hallucinations; and factors associated with compliance. Researchers have reported rates of compliance ranging from 39.2 percent to 88.5 percent. Compliance has not been consistently related to dangerousness of commands. Instead, research suggests that Individuals are more likely to comply with commands if they recognize the hallucinated voice and if their hallucinations are related to a delusion. Implications for risk assessment are discussed in light of the research.

  18. Electronic processing and control system with programmable hardware

    NASA Technical Reports Server (NTRS)

    Alkalaj, Leon (Inventor); Fang, Wai-Chi (Inventor); Newell, Michael A. (Inventor)

    1998-01-01

    A computer system with reprogrammable hardware allowing dynamically allocating hardware resources for different functions and adaptability for different processors and different operating platforms. All hardware resources are physically partitioned into system-user hardware and application-user hardware depending on the specific operation requirements. A reprogrammable interface preferably interconnects the system-user hardware and application-user hardware.

  19. Command History 1970. Volume 4

    DTIC Science & Technology

    1970-01-01

    Threat Part III - Politica I/Polic y Influences Part IV - Command Structure/Relationships Part V - Air Operations Part VI - Support Activities 20-2/TSNF...muffler system, a six-bladed wooden propellor, and .... no oxtra frdis on the.. exterior which might make noise in the... wind." UNCLASSIFIED H-32 (U) The

  20. 10 commandments of smile esthetics

    PubMed Central

    Machado, Andre Wilson

    2014-01-01

    The search for esthetic treatment has persisted in the routine of dental professionals. Following this trend, dental patients have sought treatment with the primary aim of improving smile esthetics. The aim of this article is to present a protocol to assess patient's smile: The 10 Commandments of smile esthetics. PMID:25279532

  1. The Extended Battalion Command Tour.

    DTIC Science & Technology

    1983-05-13

    number ATZI -NCR-83-2). 3. Your cooperation and frank responses will be a major contribution to a study of considerable importance to the Army. The...answers you provide will be completely confidential. Signature or identification is not required. Major General, USA Commandant ATZI -NCR-MA-83-2

  2. Ten Commandments of System Conversions.

    ERIC Educational Resources Information Center

    Chabotar, Kent John

    1998-01-01

    Administrators at Bowdoin College (Maine) have translated lessons learned from the process of administrative software conversion into ten commandments for other small colleges undertaking such changes. Three approaches to management information systems are outlined, with advantages and limitations highlighted, as well as the ten recommendations,…

  3. 10 commandments of smile esthetics.

    PubMed

    Machado, Andre Wilson

    2014-01-01

    The search for esthetic treatment has persisted in the routine of dental professionals. Following this trend, dental patients have sought treatment with the primary aim of improving smile esthetics. The aim of this article is to present a protocol to assess patient's smile: The 10 Commandments of smile esthetics.

  4. HOTOL Command and Control Systems

    NASA Astrophysics Data System (ADS)

    Rowley, J. D.

    1988-04-01

    HOTOL is intended to provide a low cost means of delivering payloads to low earth orbit. The vehicle is thus designed for unmanned and largely autonomous operations with very limited contact with a ground station. This paper outlines the Command and Control Systems studies undertaken to date and proposed for future phases.

  5. STS-71 hardware assembly view

    NASA Image and Video Library

    1994-12-02

    S94-47810 (2 Dec. 1994) --- Lockheed Space Operations Company workers in the Extended Duration Orbiter (EDO) Facility, located inside the Vehicle Assembly Building (VAB), carefully hoist the Orbiter Docking System (ODS) from its shipping container into a test stand. The ODS was shipped in a horizontal position to the Kennedy Space Center (KSC) from contractor Rockwell Aerospace's Downey plant. Once the ODS is upright, work can continue to prepare the hardware for the first docking of the United States Space Shuttle and Russian Space Station MIR in 1995. The ODS contains both United States-made and Russian-made hardware. The black band is Russian-made thermal insulation protecting part of the docking mechanism, also Russian-made, called the Androgynous Peripheral Docking System (APDS). A red protective cap covers the APDS itself. Other elements of the ODS, most of it protected by white United States-made thermal insulation, were developed by Rockwell, which also integrated and checked out the assembled Russian-United States system.

  6. 32 CFR 724.405 - Commandant of the Marine Corps or the Commander, Naval Military Personnel Command.

    Code of Federal Regulations, 2012 CFR

    2012-07-01

    ... Department Discharge Review System § 724.405 Commandant of the Marine Corps or the Commander, Naval Military... support to the Naval Discharge Review Board and for implementation of departmental discharge review decisions. (See subpart C). ...

  7. 32 CFR 724.405 - Commandant of the Marine Corps or the Commander, Naval Military Personnel Command.

    Code of Federal Regulations, 2010 CFR

    2010-07-01

    ... (Continued) DEPARTMENT OF THE NAVY PERSONNEL NAVAL DISCHARGE REVIEW BOARD Principal Elements of the Navy Department Discharge Review System § 724.405 Commandant of the Marine Corps or the Commander, Naval Military...

  8. Advanced interactive displays for deployable command and control centers

    NASA Astrophysics Data System (ADS)

    Jedrysik, Peter A.; Parada, Francisco E.; Stedman, Terrance A.; Zhang, Jingyuan

    2003-09-01

    Command and control in today's battlefield environment requires efficient and effective control of massive amounts of constantly changing information from a variety of databases and real-time sensors. Using advanced information technology for presentation and interactive control enables more extensive data fusion and correlation to present an accurate picture of the battlespace to commanders and their staffs. The Interactive DataWall being developed by the Advanced Displays and Intelligent Interfaces (ADII) technology team of the Air Force Research Laboratory's Information Directorate (AFRL/IF) is a strong contender for solving the information management problems facing the 21st century military commander. It provides an ultra high-resolution large screen display with multi-modal, wireless interaction. Commercial off-the-shelf (COTS) technology has been combined with specialized hardware and software developed in-house to provide a unique capability for multimedia data display and control. The technology once isolated to a laboratory environment has been packaged into deployable systems that have been successfully transitioned to support the warfighter in the field.

  9. A Friendly Command, Control, and Information System for Astronomy

    NASA Astrophysics Data System (ADS)

    McGraw, John T.; Duric, Nebojsa; Sjulin, Michael; Slezak, Scott; Westpfahl, David

    Virtually real user interfaces and device independent communications systems provide a robust, secure and efficient means for remote control of telescopes, data transfer, and interaction among personnel at distant sites. A variety of techniques has been implemented for remote operation of telescopes. This paper describes a new system incorporating secured, compacted, simultaneous information transfer of multiple data types, robust command structure and a user interface which pre-tests commands for security. Testing is accomplished by manipulating and displaying planned allowable motions using a virtual telescope and instrument before real hardware executes the desired motions. Embedded in this system is the ability to create efficient interfaces for all classes of users, data and system security, error correction and multiple forms of data compression. The system results from a merger of a military command and control system and a control system for robots operating in hazardous environments. Both systems were developed by Sandia National Laboratories. The merged system is proposed to enable elementary school children to access remotely operable telescopes and other assets of the LodeStar Project, which provides science education and research capability throughout New Mexico. The definition and constraints on the system are appropriate for its use by the professional astronomical community, as well, perhaps as a standard control and communications system supported, in part, within the national laboratories. In this paper we discuss implementation of the prototype system, its features, and its constraints, particularly with respect to bandwidth limitations.

  10. 32 CFR 700.1053 - Commander of a task force.

    Code of Federal Regulations, 2012 CFR

    2012-07-01

    ... 32 National Defense 5 2012-07-01 2012-07-01 false Commander of a task force. 700.1053 Section 700... Command Detail to Duty § 700.1053 Commander of a task force. (a) A geographic fleet commander, and any other naval commander, may detail in command of a task force, or other task command, any eligible...

  11. 32 CFR 700.1053 - Commander of a task force.

    Code of Federal Regulations, 2013 CFR

    2013-07-01

    ... 32 National Defense 5 2013-07-01 2013-07-01 false Commander of a task force. 700.1053 Section 700... Command Detail to Duty § 700.1053 Commander of a task force. (a) A geographic fleet commander, and any other naval commander, may detail in command of a task force, or other task command, any eligible...

  12. 32 CFR 700.1053 - Commander of a task force.

    Code of Federal Regulations, 2011 CFR

    2011-07-01

    ... 32 National Defense 5 2011-07-01 2011-07-01 false Commander of a task force. 700.1053 Section 700... Command Detail to Duty § 700.1053 Commander of a task force. (a) A geographic fleet commander, and any other naval commander, may detail in command of a task force, or other task command, any eligible...

  13. 32 CFR 700.1053 - Commander of a task force.

    Code of Federal Regulations, 2014 CFR

    2014-07-01

    ... 32 National Defense 5 2014-07-01 2014-07-01 false Commander of a task force. 700.1053 Section 700... Command Detail to Duty § 700.1053 Commander of a task force. (a) A geographic fleet commander, and any other naval commander, may detail in command of a task force, or other task command, any eligible...

  14. 32 CFR 700.1053 - Commander of a task force.

    Code of Federal Regulations, 2010 CFR

    2010-07-01

    ... 32 National Defense 5 2010-07-01 2010-07-01 false Commander of a task force. 700.1053 Section 700... Command Detail to Duty § 700.1053 Commander of a task force. (a) A geographic fleet commander, and any other naval commander, may detail in command of a task force, or other task command, any eligible...

  15. Imaging of current spinal hardware: lumbar spine.

    PubMed

    Ha, Alice S; Petscavage-Thomas, Jonelle M

    2014-09-01

    The purposes of this article are to review the indications for and the materials and designs of hardware more commonly used in the lumbar spine; to discuss alternatives for each of the types of hardware; to review normal postoperative imaging findings; to describe the appropriateness of different imaging modalities for postoperative evaluation; and to show examples of hardware complications. Stabilization and fusion of the lumbar spine with intervertebral disk replacement, artificial ligaments, spinous process distraction devices, plate-and-rod systems, dynamic posterior fusion devices, and newer types of material incorporation are increasingly more common in contemporary surgical practice. These spinal hardware devices will be seen more often in radiology practice. Successful postoperative radiologic evaluation of this spinal hardware necessitates an understanding of fundamental hardware design, physiologic objectives, normal postoperative imaging appearances, and unique complications. Radiologists may have little training and experience with the new and modified types of hardware used in the lumbar spine.

  16. Cancer risks in a population-based study of 70,570 agricultural workers: results from the Canadian census health and Environment cohort (CanCHEC).

    PubMed

    Kachuri, Linda; Harris, M Anne; MacLeod, Jill S; Tjepkema, Michael; Peters, Paul A; Demers, Paul A

    2017-05-19

    Agricultural workers may be exposed to potential carcinogens including pesticides, sensitizing agents and solar radiation. Previous studies indicate increased risks of hematopoietic cancers and decreased risks at other sites, possibly due to differences in lifestyle or risk behaviours. We present findings from CanCHEC (Canadian Census Health and Environment Cohort), the largest national population-based cohort of agricultural workers. Statistics Canada created the cohort using deterministic and probabilistic linkage of the 1991 Canadian Long Form Census to National Cancer Registry records for 1992-2010. Self-reported occupations were coded using the Standard Occupational Classification (1991) system. Analyses were restricted to employed persons aged 25-74 years at baseline (N = 2,051,315), with follow-up until December 31, 2010. Hazard ratios (HR) and 95% confidence intervals (CI) were modeled using Cox proportional hazards for all workers in agricultural occupations (n = 70,570; 70.8% male), stratified by sex, and adjusted for age at cohort entry, province of residence, and highest level of education. A total of 9515 incident cancer cases (7295 in males) occurred in agricultural workers. Among men, increased risks were observed for non-Hodgkin lymphoma (HR = 1.10, 95% CI = 1.00-1.21), prostate (HR = 1.11, 95% CI = 1.06-1.16), melanoma (HR = 1.15, 95% CI = 1.02-1.31), and lip cancer (HR = 2.14, 95% CI = 1.70-2.70). Decreased risks in males were observed for lung, larynx, and liver cancers. Among female agricultural workers there was an increased risk of pancreatic cancer (HR = 1.36, 95% CI = 1.07-1.72). Increased risks of melanoma (HR = 1.79, 95% CI = 1.17-2.73), leukemia (HR = 2.01, 95% CI = 1.24-3.25) and multiple myeloma (HR = 2.25, 95% CI = 1.16-4.37) were observed in a subset of female crop farmers. Exposure to pesticides may have contributed to increased risks of hematopoietic cancers, while increased risks of lip cancer

  17. HHDTC - Cmdr Halsell photographs hardware

    NASA Image and Video Library

    2016-08-12

    STS083-313-012 (4-8 April 1997) --- Astronaut James D. Halsell, Jr., mission commander, uses a Hi-8mm camcorder to videotape the Hand Held Diffusion Test Cells (HHDTC), in the Spacelab Module aboard the Earth-orbiting Space Shuttle Columbia. Each test cell has three chambers containing a protein solution, a buffer solution and a precipitant solution chamber. Using the liquid-liquid diffusion method, the different fluids are brought into contact but not mixed. Over a period of time, the fluids will diffuse into each other through the random motion of molecules. The gradual increase in concentration of the precipitant within the protein solution causes the proteins to crystallize.

  18. Neural command of electromotor output in mormyrids

    PubMed

    Grant; von der Emde G; Sena; Mohr

    1999-05-01

    The electric discharge of mormyrid fish has an irregular pattern controlled by the electromotor command nucleus in the medulla. Anatomical studies suggest that much of the descending information integrated by the command nucleus comes from the diencephalic precommand nucleus. But field potentials related to the motor command occur later in the precommand nucleus than in the command nucleus, suggesting that they are a corollary rather than a cause of electromotor command initiation. Recorded extracellularly, certain precommand nucleus units fire spontaneously between electromotor commands but pause briefly following each command; others units fire a burst of spikes only during the post-command pause. The firing frequency of the former is correlated with the duration of the interval between successive electromotor commands when the fish is discharging at more than approximately 5 Hz. The post-command pause in spontaneous firing is due to corollary-discharge-mediated feedback inhibition, probably generated by the activity of the bursting units that fire only during this period. Precommand nucleus neurons are activated by electrosensory input, and stimulation of the precommand nucleus modulates the endogenous pattern of electromotor command. We propose that the irregular rhythm of the motor command depends largely on the integration of descending information of various origins, conveyed via the precommand nucleus to the command nucleus, and that this process is regulated by corollary discharge feedback inhibition to the precommand nucleus.

  19. Product Assurance for Spaceflight Hardware

    NASA Technical Reports Server (NTRS)

    Monroe, Mike

    1995-01-01

    This report contains information about the tasks I have completed and the valuable experience I have gained at NASA. The report is divided into two different sections followed by a program summary sheet. The first section describes the two reports I have completed for the Office of Mission Assurance (OMA). I describe the approach and the resources and facilities used to complete each report. The second section describes my experience working in the Receipt Inspection/Quality Assurance Lab (RI/QA). The first report described is a Product Assurance Plan for the Gas Permeable Polymer Materials (GPPM) mission. The purpose of the Product Assurance Plan is to define the various requirements which are to be met through completion of the GPPM mission. The GPPM experiment is a space payload which will be flown in the shuttle's SPACEHAB module. The experiment will use microgravity to enable production of complex polymeric gas permeable materials. The second report described in the first section is a Fracture Analysis for the Mir Environmental Effects Payload (MEEP). The Fracture Analysis report is a summary of the fracture control classifications for all structural elements of the MEEP. The MEEP hardware consists of four experiment carriers, each of which contains an experiment container holding a passive experiment. The MEEP hardware will be attached to the cargo bay of the space shuttle. It will be transferred by Extravehicular Activity and mounted on the Mir space station. The second section of this report describes my experiences in the RVQA lab. I listed the different equipment I used at the lab and their functions. I described the extensive inspection process that must be completed for spaceflight hardware. Included, at the end of this section, are pictures of most of the equipment used in the lab. There is a summary sheet located at the end of this report. It briefly describes the valuable experience I have gained at NASA this summer and what I will be able to take

  20. Beyond Mission Command: Maneuver Warfare for Cyber Command and Control

    DTIC Science & Technology

    2015-05-18

    operation in an A2AD environment. 15. SUBJECT TERMS command and control; maneuver warfare; cyberspace; cyberspace operations; cyber warfare , mission...Some Principles of Cyber Warfare (NWC 2160) (U.S. Naval War College, Joint Military Operations Department, Newport, RI: U.S. Naval War College...research/ innovationleadership.pdf. Crowell, Richard M. Some Principles of Cyber Warfare (NWC 2160). U.S. Naval War College, Joint Military Operations

  1. Applying the Combatant Command Construct to the DHS Command Structure

    DTIC Science & Technology

    2012-06-17

    human trafficking, insurgency, narcotics smuggling, and even narco -terrorism. As described in a Strategic Studies Institute publication “…Unrestrained...of El Chapo ,” The Virginian-Pilot, October 29, 2011. 39 Naler, “Are We Ready for and Interagency Combatant Command?”, p. 26. 63 concerns...Publication 1. Washington, DC: Joint Chiefs of Staff, May 2, 2007. William Booth and Nick Miroff, “The Ballad of El Chapo ,” The Virginian Pilot

  2. Ready...Set... Command! Rethinking Training for Squadron Commanders

    DTIC Science & Technology

    2016-02-16

    their abilities to lead people , solve problems, and develop action plans to overcome future challenges, they are not adequately trained to maximize...Chief of Staff, General John P. Jumper stated, “[t]he very nature of command is unique to the military; there is no civilian equivalent for this level...Force officers are leaders by design and are expected to lead people from the time they are commissioned as new lieutenants. As officers progress

  3. Tactical satellites for air command and control

    NASA Astrophysics Data System (ADS)

    Crochet, M.; Cymbalista, J.; Leveque, L.

    1993-02-01

    This paper is divided in three parts corresponding to the following items: (1) air command and control functions and deficiencies; (2) contribution of TACSATS to air command and control; and (3) operational improvements due to TACSATS.

  4. 76 FR 19893 - Unified Command Plan 2011

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-04-08

    ...#0;#0; ] Memorandum of April 6, 2011 Unified Command Plan 2011 Memorandum for the Secretary of... the revised Unified Command Plan. Consistent with title 10, United States Code, section 161(b)(2) and...

  5. Expedition 33/34 Change of Command

    NASA Image and Video Library

    Expedition 33 Commander Suni Williams ceremonially handed over command of the International Space Station on Saturday to fellow NASA astronaut Kevin Ford on the eve of her departure from the comple...

  6. British Airways' pre-command training program

    NASA Technical Reports Server (NTRS)

    Holdstock, L. F. J.

    1980-01-01

    Classroom, flight simulator, and in-flight sessions of an airline pilot training program are briefly described. Factors discussed include initial command potential assessment, precommand airline management studies course, precommand course, and command course.

  7. Hardware design for Hash functions

    NASA Astrophysics Data System (ADS)

    Lee, Yong Ki; Knežević, Miroslav; Verbauwhede, Ingrid M. R.

    Due to its cryptographic and operational key features such as the one-way function property, high speed and a fixed output size independent of input size the hash algorithm is one of the most important cryptographic primitives. A critical drawback of most cryptographic algorithms is the large computational overhead. This is getting more critical since the data amount to process or communicate is increasing a lot. In many cases, a proper use of the hash algorithm reduces the computational overhead. Digital signature generation and the message authentication are the most common applications of the hash algorithms. The increasing data size also motivates hardware designers to have a throughput optimal architecture for a given hash algorithm. In this chapter, some popular hash algorithms and their cryptanalysis are briefly introduced, and a design methodology for throughput optimal architectures of MD4-based hash algorithms is described in detail.

  8. Command History 1970. Volume 3. Sanitized

    DTIC Science & Technology

    1970-01-01

    H-j-~3t\\) SH0• H H HEADQUARTERS UNITED STATES MILITARY ASSISTANCE COMMAND, APO SAN FRANCISCO 96222 .4fair ’I ’COMMAND HISTORY 1970L VOLUME , C,- 41...G-42). UNCLASSIFIED UNCLASS I FIED SECURITY CLASSIFICATION OF THIS PACWfl.n 04.0 tI*# * .. ,.~ -~ UNCLASSIFIED - HEADQUA RTERS - UNITED STATES ...Reports from UnifieC Commands in the# Pacific Command. 2. This document contains information affecting the security of the United States within the

  9. APOLLO XII - ART CONCEPT - COMMAND MODULE

    NASA Image and Video Library

    1969-11-10

    S69-58005 (10 Nov. 1969) --- An artist's concept of the Apollo 12 Command Module's (CM) interior, with the command module pilot at the controls. The Apollo 12 Lunar Module (LM) and a portion of the lunar surface are seen out of the window. Astronaut Richard F. Gordon Jr. will maneuver the Apollo 12 Command and Service Modules (CSM) in lunar orbit while astronauts Charles Conrad Jr., commander, and Alan L. Bean, lunar module pilot, explore the moon.

  10. The UAV and the Operational Commander

    DTIC Science & Technology

    2007-11-02

    Commander, Command and Control, Operational Functions, Battle Space Awareness 15.Abstract: This paper will address the UAV’s evolution into a...distribution unlimited Supplementary Notes Abstract This paper will address the UAVs evolution into a valuable asset for the operational commander. The...address the UAV’s evolution into a valuable asset for the operational commander. The writer argues that the integration of UAV sensor data into a

  11. Garrison Command: The First 90 Days

    DTIC Science & Technology

    2009-01-01

    energy. The deputy commanding general of IMCOM has taken a more direct approach by e - mailing his DCG Bi- Weekly Update to region directors, commanders...nagging issues and concerns that capture their attention and energy. The deputy commanding general of IMCOM has taken a more direct approach by e ... mailing his DCG Bi- Weekly Update to region directors, commanders, and staff for special areas of emphasis. A more traditional source is represented by

  12. Command hallucinations and criminality: a clinical quandary.

    PubMed

    Rogers, R; Nussbaum, D; Gillis, R

    1988-01-01

    Clinical literature on the role of command hallucinations in producing antisocial behavior is sparse and fragmented. This article reviews exploratory models of auditory hallucinations and the prevalence of command hallucinations in clinical and forensic settings. In addition, clinical guidelines are offered for assessing the authenticity of command hallucinations and their relevance to criminal behavior within the context of forensic evaluations.

  13. Command History. 1969. Volume 1. Sanitized

    DTIC Science & Technology

    1969-01-01

    FORCE 41 thru 50 14 & 15 COMMANDANT, USMC 51 thro 55 10 & II COMMANDANT, USCG - & 57 CINCEUR CINCSO CINCAL 1) CINCSTRIKE CINCSAC CG, CONARC COMUS JAPAN...portion of chastened optimism, we will find a path, CHARLES B. MACDONALD The CINCPAC Instruction 5000. 5B of 15 October 1969 requires the Commander...Senisor Prbg rants.............. ............ ................. V11- I Herbicidt Oppratiomn. ...................................... .VI- 15 Vii

  14. Command and Control: A Contemporary Perspective

    DTIC Science & Technology

    1974-07-20

    A______RAT This study focuses on the current paradoxical state of command and control taith special emphasis on the Navy. While the technological ...emphasis on the Navy. While the technological advances associated with command and control and its subsystem communications have been significant, the goal...TRENDS IN NAVAL COMMAND, CONTROL AND COMMUNICATIONS. . ........ ........... 38 Climate for Change ..... ............ 38 Technology

  15. NASA standard communications and data handling subsystem. [for command and telemetry between spacecraft and earth stations

    NASA Technical Reports Server (NTRS)

    Robinson, D. L.

    1977-01-01

    The paper gives a functional description and discusses hardware implementation for the Communication and Data Handling (C&DH) subsystem of the Multimission Modular Spacecraft. The C&DH subsystem: (1) provides the command and telemetry link between the spacecraft and the terrestrial system, (2) distributes commands to and collects telemetry from all spacecraft systems via a duplex serial multiplex data bus and remote interface units, and (3) contains onboard computation capability. The C&DH is a single 4 x 4 x 1-1/2 foot module; the stuffed module weighs 270 lbs including 60 lbs of mission unique weight. The hardware is versatile and cost effective, and its modular structure permits repair, refurbishment, and even modification/updating in space

  16. Joint Command Decision Support System

    DTIC Science & Technology

    2011-06-01

    Greenley et al. 2006) resulted in the identification of a set of overarching principles for the implementation of Joint Command Decision Support (Hales...and adjustment of resources, and longer term feasibility planning. As highlighted in the Joint Staff Front End Analysis report ( Greenley et al. 2006...Townsend (2006). The Federal Response to Hurricane Katrina Lessons Learned, Washington, D.C. February 2006. Greenley , A., Baker, K. & Cochran, L. (2006

  17. Identification of Brigade Command Competencies

    DTIC Science & Technology

    2011-06-01

    environment (COE), quantifying the extent to which officers ’ pre-command courses and military education foster the development of these competencies, and...bureaucratic to be useful, especially for jobs involving strategic leadership (Reed, Bullis , Collins, & Paparone, 2004). Additionally, it is difficult to...additional information (Briscoe & Hall, 1999). The Army Training and Leader Development Panel Officer Study (ATLDP; U.S. Department of the Army, 2001

  18. Compulsions developing into command hallucinations.

    PubMed

    Klemperer, F

    1996-01-01

    Intrusive, uncontrollable and bizarre thoughts occur in both obsessive-compulsive disorder (OCD) and psychosis. The origin of these mental phenomena and the relationship between them is unclear. A case is described in which long-standing compulsions and the associated resistance temporarily developed the characteristics of command hallucinations, in the absence of any other psychotic symptoms. The implications for psychopathological theories of hallucinations are discussed.

  19. Unity of Command and Interdiction

    DTIC Science & Technology

    1994-07-01

    Those issues suggest three possible methods of study. The first is a simple analysis of interdiction procedures. Combining that approach with a...coordination line; rather, that will be a key part of analysis . The Army’s vested interest in air interdiction is also central to the discussion. Is...With Battlefield Preparation (Carlisle Barracs Pem: U.S. Army War College, 15 April 1993), 29. ’U.S. Army Concepts and Analysis Command, Deuert

  20. Command in the Objective Force

    DTIC Science & Technology

    2006-05-31

    G-7. 31 See U.S. Army, FM 6-0, Command and Control (DRAG Edition), Appendix A; William S . Lind, Maneuver Warfare Handbook (Boulder, Colorado: Westview...0’ s cognitive hierarchy lists data, information, knowledge, and understanding as the levels for processing information. The word information is used...foundation of the Roman commander’s ability to communicate rapidly lay with the implementation of military standards, or battle flags and guidons . Although

  1. Developing an Effective Command Philosophy

    DTIC Science & Technology

    2012-10-01

    States, Germany, and Bosnia. PHOTO : U.S. Army CPT Evan Davies, right, Apache troop commander, 5th Squadron, 7th Cavalry Regiment, Iraq, talks with a...philosophy.” A well thought out leadership philosophy is a critical foundational tool to use to develop influential leaders and create positive...art, music, raising kids, investing money, politics, and countless other personal and professional concerns. These philosophies create a collage

  2. Understanding Commanders’ Information Needs

    DTIC Science & Technology

    1989-06-01

    being one whit more capable of dealing with the information needed for the command process than were their predecessors a century or even a millennium ...that, given the news of the persistent chemical attack, he no longer views the enemy as intending to force a breakthrough in the 1st Brigade sector. He...Gifted Learners ," in M. C. Wittrock (ed.), Handbook of Research on Teaching (3rd ed.), Macmillan, New York, 1986. ,

  3. On Preparing for Squadron Command

    DTIC Science & Technology

    1988-04-01

    Requirements 5. NCO Professional Military Education (PNE) Program 6. SOS Selection Procedures and Criteria 7. Officer PFE 3. Decorations Progrars 9... Audit Program 42, Commander’s Management System (CXS) 43. Economic Analysis (EA) Charter 44. Internal Control Review Program 45. Management Assistance...Comptroller I, Overview of Financial Structure 2. Your Role as a Financial Manager 3. Audit Focal Point 4. Military Pay 5. Per Diem and Travel

  4. Company Command: The Bottom Line

    DTIC Science & Technology

    1992-07-01

    OERs Personnel Actions .................................... 85 Awards-Reenlistment-Hometown News Release ( HTNR ] -Lcave-Meal Cards-Flagging Actions...your 1SG to resolve problems. "* Recognition for good work. HOMETOWN NEWS RELEASE ( HTNR ): Unfortu- nately, commanders rarely see *he hometown news...release pay off; cc isequently, many don’t support the program. The HTNR program tells the public of your soldier’s accomplish- ment, and, at the same time

  5. Company Command: The Bottom Line

    DTIC Science & Technology

    1990-01-01

    retention NCO. "* Easy access to you and your ISG to resolve problems. "* Recognition for good work. HOMETOWN NEWS RELEASE ( HTNR ): Unlortu- nately...commanders rarely see the hometown news release pay off: consequently, many don’t support the program. The HTNR program tells the public of your...soldier’s accomplish- ment. and, at the same time, advertises the Army. Remem- ber, it’s mondutort’ to have an HTNR program. but your soldiers

  6. A modular suite of hardware enabling spaceflight cell culture research

    NASA Technical Reports Server (NTRS)

    Hoehn, Alexander; Klaus, David M.; Stodieck, Louis S.

    2004-01-01

    BioServe Space Technologies, a NASA Research Partnership Center (RPC), has developed and operated various middeck payloads launched on 23 shuttle missions since 1991 in support of commercial space biotechnology projects. Modular cell culture systems are contained within the Commercial Generic Bioprocessing Apparatus (CGBA) suite of flight-qualified hardware, compatible with Space Shuttle, SPACEHAB, Spacelab and International Space Station (ISS) EXPRESS Rack interfaces. As part of the CGBA family, the Isothermal Containment Module (ICM) incubator provides thermal control, data acquisition and experiment manipulation capabilities, including accelerometer launch detection for automated activation and thermal profiling for culture incubation and sample preservation. The ICM can accommodate up to 8 individually controlled temperature zones. Command and telemetry capabilities allow real-time downlink of data and video permitting remote payload operation and ground control synchronization. Individual cell culture experiments can be accommodated in a variety of devices ranging from 'microgravity test tubes' or standard 100 mm Petri dishes, to complex, fed-batch bioreactors with automated culture feeding, waste removal and multiple sample draws. Up to 3 levels of containment can be achieved for chemical fixative addition, and passive gas exchange can be provided through hydrophobic membranes. Many additional options exist for designing customized hardware depending on specific science requirements.

  7. A modular suite of hardware enabling spaceflight cell culture research.

    PubMed

    Hoehn, Alexander; Klaus, David M; Stodieck, Louis S

    2004-03-01

    BioServe Space Technologies, a NASA Research Partnership Center (RPC), has developed and operated various middeck payloads launched on 23 shuttle missions since 1991 in support of commercial space biotechnology projects. Modular cell culture systems are contained within the Commercial Generic Bioprocessing Apparatus (CGBA) suite of flight-qualified hardware, compatible with Space Shuttle, SPACEHAB, Spacelab and International Space Station (ISS) EXPRESS Rack interfaces. As part of the CGBA family, the Isothermal Containment Module (ICM) incubator provides thermal control, data acquisition and experiment manipulation capabilities, including accelerometer launch detection for automated activation and thermal profiling for culture incubation and sample preservation. The ICM can accommodate up to 8 individually controlled temperature zones. Command and telemetry capabilities allow real-time downlink of data and video permitting remote payload operation and ground control synchronization. Individual cell culture experiments can be accommodated in a variety of devices ranging from 'microgravity test tubes' or standard 100 mm Petri dishes, to complex, fed-batch bioreactors with automated culture feeding, waste removal and multiple sample draws. Up to 3 levels of containment can be achieved for chemical fixative addition, and passive gas exchange can be provided through hydrophobic membranes. Many additional options exist for designing customized hardware depending on specific science requirements.

  8. A modular suite of hardware enabling spaceflight cell culture research

    NASA Technical Reports Server (NTRS)

    Hoehn, Alexander; Klaus, David M.; Stodieck, Louis S.

    2004-01-01

    BioServe Space Technologies, a NASA Research Partnership Center (RPC), has developed and operated various middeck payloads launched on 23 shuttle missions since 1991 in support of commercial space biotechnology projects. Modular cell culture systems are contained within the Commercial Generic Bioprocessing Apparatus (CGBA) suite of flight-qualified hardware, compatible with Space Shuttle, SPACEHAB, Spacelab and International Space Station (ISS) EXPRESS Rack interfaces. As part of the CGBA family, the Isothermal Containment Module (ICM) incubator provides thermal control, data acquisition and experiment manipulation capabilities, including accelerometer launch detection for automated activation and thermal profiling for culture incubation and sample preservation. The ICM can accommodate up to 8 individually controlled temperature zones. Command and telemetry capabilities allow real-time downlink of data and video permitting remote payload operation and ground control synchronization. Individual cell culture experiments can be accommodated in a variety of devices ranging from 'microgravity test tubes' or standard 100 mm Petri dishes, to complex, fed-batch bioreactors with automated culture feeding, waste removal and multiple sample draws. Up to 3 levels of containment can be achieved for chemical fixative addition, and passive gas exchange can be provided through hydrophobic membranes. Many additional options exist for designing customized hardware depending on specific science requirements.

  9. Voice command weapons launching system

    NASA Astrophysics Data System (ADS)

    Brown, H. E.

    1984-09-01

    This abstract discloses a voice-controlled weapons launching system for use by a pilot of an aircraft against a plurality of simultaneously appearing (i.e., existing) targets, such as two or more aggressor aircraft (or tanks, or the like) attacking more aggressor aircraft. The system includes, in combination, a voice controlled input device linked to and controlling a computer; apparatus (such as a television camera, receiver, and display), linked to and actuated by the computer by a voice command from the pilot, for acquiring and displaying an image of the multi-target area; a laser, linked to and actuated by the computer by a voice command from the pilot to point to (and to lock on to) any one of the plurality of targets, with the laser emitting a beam toward the designated (i.e., selected) target; and a plurality of laser beam-rider missiles, with a different missile being launched toward and attacking each different designated target by riding the laser beam to that target. Unlike the prior art, the system allows the pilot to use his hands full-time to fly and to control the aircraft, while also permitting him to launch each different missile in rapid sequence by giving a two-word spoken command after he has visually selected each target of the plurality of targets, thereby making it possible for the pilot of a single defender aircraft to prevail against the plurality of simultaneously attacking aircraft, or tanks, or the like.

  10. Terrain commander UGS operational trials

    NASA Astrophysics Data System (ADS)

    Steadman, Robert L.

    2004-09-01

    Operational trials of Textron Systems" Terrain Commander unattended ground sensor (UGS) system are described. Terrain Commander is a powerful new concept in surveillance and remote situational awareness. It leverages a diverse suite of sophisticated unattended ground sensors, day/night electro-optics, satellite data communications, and an advanced Windows based graphic user interface. Terrain Commander OASIS (Optical Acoustic SATCOM Integrated Sensor) provides next generation target detection, classification, and tracking through smart sensor fusion of beam-forming acoustic, seismic, passive infrared, and magnetic sensors. With its fully integrated SATCOM system using internet protocols, virtually any site in the world can be monitored from almost any other location. Multiple remote sites such as airfields, landing zones, base perimeters, road junctions, flanks, and border crossings are monitored with ease from a central location. Intruding personnel or vehicles are automatically detected, classified, and imaged. Results from early operational trials in the outback of Australia and in various locations in the US are described. Probability of detection and recognition against a wide variety of targets including personnel, military and civilian vehicles, in-shore watercraft, and low altitude aircraft are discussed. Environments include snow cover, tropical savannah, rainforest, and woodlands. Experience with alternative SATCOM systems during the trials is also touched upon.

  11. Hardware Implementation of Singular Value Decomposition

    NASA Astrophysics Data System (ADS)

    Majumder, Swanirbhar; Shaw, Anil Kumar; Sarkar, Subir Kumar

    2016-06-01

    Singular value decomposition (SVD) is a useful decomposition technique which has important role in various engineering fields such as image compression, watermarking, signal processing, and numerous others. SVD does not involve convolution operation, which make it more suitable for hardware implementation, unlike the most popular transforms. This paper reviews the various methods of hardware implementation for SVD computation. This paper also studies the time complexity and hardware complexity in various methods of SVD computation.

  12. Hardware Assisted ROP Detection Mode (HARD Mode)

    DTIC Science & Technology

    2013-08-01

    Distribution A. Cleared for public release; unlimited distribution. USAFA-CN-2013-457 Hardware Assisted ROP Detection Mode (HARD Mode) NATHANIEL HART...457 This report, "Hardware Assisted ROP Detection Mode (HARD Mode)" is presented as a competent treatment of the subj ect, worthy of publication. The...Technical 20120810-20121215 Hardware Assisted ROP Detection Mode (HARD Mode) NATHANIEL HART MICHAEL WINSTEAD MARTIN CARLISLE RODNEY LYKINS MICHAEL

  13. Electronic hardware implementations of neutral networks

    NASA Technical Reports Server (NTRS)

    Thakoor, A. P.; Moopenn, A.; Lambe, John; Khanna, S. K.

    1987-01-01

    This paper examines some of the present work on the development of electronic neural network hardware. In particular, the investigations currently under way at JPL on neural network hardware implementations based on custom VLSI technology, novel thin film materials, and an analog-digital hybrid architecture are reviewed. The availability of such hardware will greatly benefit and enhance the present intense research effort on the potential computational capabilities of highly parallel systems based on neural network models.

  14. The clinical significance of command hallucinations.

    PubMed

    Hellerstein, D; Frosch, W; Koenigsberg, H W

    1987-02-01

    Patients with command hallucinations (voices ordering particular acts, often violent or destructive ones) are commonly assumed to be at high risk for dangerous behavior. The authors reviewed 789 consecutive inpatient admissions. Of 151 patients with auditory hallucinations, 58 (38.4%) heard commands. The presence of auditory hallucinations was significantly associated with diagnosis, demographic variables, and use of maximal observation and seclusion. However, patients with command hallucinations were not significantly different from patients without commands on demographic and behavioral variables, including suicidal ideation or behavior and assaultiveness. These findings suggest that command hallucinations alone may not imply greater risk for acute, life-threatening behavior.

  15. Thermal Hardware for the Thermal Analyst

    NASA Technical Reports Server (NTRS)

    Steinfeld, David

    2015-01-01

    The presentation will be given at the 26th Annual Thermal Fluids Analysis Workshop (TFAWS 2015) hosted by the Goddard Space Flight Center (GSFC) Thermal Engineering Branch (Code 545). NCTS 21070-1. Most Thermal analysts do not have a good background into the hardware which thermally controls the spacecraft they design. SINDA and Thermal Desktop models are nice, but knowing how this applies to the actual thermal hardware (heaters, thermostats, thermistors, MLI blanketing, optical coatings, etc...) is just as important. The course will delve into the thermal hardware and their application techniques on actual spacecraft. Knowledge of how thermal hardware is used and applied will make a thermal analyst a better engineer.

  16. Constructing Hardware in a Scale Embedded Language

    SciTech Connect

    Bachan, John

    2014-08-21

    Chisel is a new open-source hardware construction language developed at UC Berkeley that supports advanced hardware design using highly parameterized generators and layered domain-specific hardware languages. Chisel is embedded in the Scala programming language, which raises the level of hardware design abstraction by providing concepts including object orientation, functional programming, parameterized types, and type inference. From the same source, Chisel can generate a high-speed C++-based cycle-accurate software simulator, or low-level Verilog designed to pass on to standard ASIC or FPGA tools for synthesis and place and route.

  17. Constructing Hardware in a Scale Embedded Language

    SciTech Connect

    Bachan, John

    2014-08-21

    Chisel is a new open-source hardware construction language developed at UC Berkeley that supports advanced hardware design using highly parameterized generators and layered domain-specific hardware languages. Chisel is embedded in the Scala programming language, which raises the level of hardware design abstraction by providing concepts including object orientation, functional programming, parameterized types, and type inference. From the same source, Chisel can generate a high-speed C++-based cycle-accurate software simulator, or low-level Verilog designed to pass on to standard ASIC or FPGA tools for synthesis and place and route.

  18. Open-source hardware for medical devices.

    PubMed

    Niezen, Gerrit; Eslambolchilar, Parisa; Thimbleby, Harold

    2016-04-01

    Open-source hardware is hardware whose design is made publicly available so anyone can study, modify, distribute, make and sell the design or the hardware based on that design. Some open-source hardware projects can potentially be used as active medical devices. The open-source approach offers a unique combination of advantages, including reducing costs and faster innovation. This article compares 10 of open-source healthcare projects in terms of how easy it is to obtain the required components and build the device.

  19. Open-source hardware for medical devices

    PubMed Central

    2016-01-01

    Open-source hardware is hardware whose design is made publicly available so anyone can study, modify, distribute, make and sell the design or the hardware based on that design. Some open-source hardware projects can potentially be used as active medical devices. The open-source approach offers a unique combination of advantages, including reducing costs and faster innovation. This article compares 10 of open-source healthcare projects in terms of how easy it is to obtain the required components and build the device. PMID:27158528

  20. 14 CFR 417.303 - Command control system requirements.

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... flight termination system used for each launch. (f) Electromagnetic interference. Each command control system component must function within the electromagnetic environment to which it is exposed. A command... must prevent electromagnetic interference. (g) Command transmitter failover. A command control...

  1. 14 CFR 417.303 - Command control system requirements.

    Code of Federal Regulations, 2014 CFR

    2014-01-01

    ... flight termination system used for each launch. (f) Electromagnetic interference. Each command control system component must function within the electromagnetic environment to which it is exposed. A command... must prevent electromagnetic interference. (g) Command transmitter failover. A command control...

  2. 14 CFR 417.303 - Command control system requirements.

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... flight termination system used for each launch. (f) Electromagnetic interference. Each command control system component must function within the electromagnetic environment to which it is exposed. A command... must prevent electromagnetic interference. (g) Command transmitter failover. A command control...

  3. 14 CFR 417.303 - Command control system requirements.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... flight termination system used for each launch. (f) Electromagnetic interference. Each command control system component must function within the electromagnetic environment to which it is exposed. A command... must prevent electromagnetic interference. (g) Command transmitter failover. A command control...

  4. 14 CFR 417.303 - Command control system requirements.

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... flight termination system used for each launch. (f) Electromagnetic interference. Each command control system component must function within the electromagnetic environment to which it is exposed. A command... must prevent electromagnetic interference. (g) Command transmitter failover. A command control...

  5. 13. SAC command center, weather center, underground structure, building 501, ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    13. SAC command center, weather center, underground structure, building 501, undated - Offutt Air Force Base, Strategic Air Command Headquarters & Command Center, Command Center, 901 SAC Boulevard, Bellevue, Sarpy County, NE

  6. Acting on command hallucinations: a cognitive approach.

    PubMed

    Beck-Sander, A; Birchwood, M; Chadwick, P

    1997-02-01

    This study explores factors influencing compliance with command hallucinations. The most widely acknowledged factor is the content of the command. Three categories of command content were found to be discrete in terms of compliance: "innocuous' commands, "severe' commands and commands to self-harm. This study takes a cognitive approach and highlights the importance of the beliefs individuals hold about their voices. Beliefs appear to be important in determining whether or not individuals comply with commands and the affect generated. A belief that the voice is benevolent was associated with compliance with both innocuous and severe commands. In addition, participants who believed they retained subjective control over their voices were less likely to comply with all types of command. Furthermore, qualitative evidence suggested that several other beliefs may influence compliance with command hallucinations such as beliefs about the effects of transgression, beliefs about the power and authority of the commander, beliefs about the social acceptability of the action (which may be closely correlated or synonymous with severity) and its effectiveness in achieving a valued goal. Further research is necessary to investigate the importance of these beliefs and their interrelationships more fully.

  7. Facteurs prédictifs de l’échec du Traitement Préventif Intermittent du paludisme à la sulfadoxine – pyriméthamine (TPIp-SP) dans une population de femmes enceintes à Yaoundé

    PubMed Central

    Essiben, Félix; Foumane, Pascal; de Nguefack, Marcelle Aurelie Tsafack; Eko, Filbert Eko; Njotang, Philip Nana; Enow, Robinson Mbu; Mboudou, Emile Telesphore

    2016-01-01

    Introduction Le traitement préventif intermittent à la sulfadoxine-pyriméthamine (TPIp-SP) est recommandé pour prévenir le paludisme pendant la grossesse. Nous avons recherché les facteurs associés à l’échec de cette stratégie. Méthodes Nous avons mené une étude cas - témoins dans deux formations sanitaires de Yaoundé, du 1er Mai 2014 au 30 Avril 2015. Les femmes enceintes sous TPIp-SP hospitalisées pour paludisme ayant un Test de Diagnostic Rapide (TDR) positif (cas) étaient comparées aux femmes enceintes sous TPIp-SP ayant un TDR négatif (témoins). Les logiciels Epi info 7 et SPSS 18.0 ont été utilisés avec P < 0,05 comme seuil de significativité. Résultats Nous avons recruté 234 sujets, 109 cas (46,6%) et 125 témoins (53,4%). Les facteurs associés retrouvés étaient: la primiparité (P=0,03; OR=1,15; IC= 0,32 - 4,10), la non utilisation de la MILDA (P=0,006; OR= 2,31; IC= 1,26 - 4,25), un antécédent d'hospitalisation pour paludisme (P=0,007; OR= 2,19; IC= 1,23 - 3,89), le début de la TPIp-SP après la 28ème semaine de grossesse (P=0,001, OR= 3,55; IC= 1,7 - 7,61). Après régression logistique, la primiparité (P=0,024; OR=2,01; IC=1,1-3,7) et un antécédent d'hospitalisation pour paludisme (P=0,001; OR=2,83; IC=1,50-5,4) restaient associés à l’échec du TPIp-SP. Conclusion Un antécédent d'hospitalisation pour accès palustre et la primiparité sont des facteurs prédictifs indépendants de l’échec de la TPIp-SP. PMID:27303570

  8. Stability boundaries for command augmentation systems

    NASA Technical Reports Server (NTRS)

    Shrivastava, P. C.

    1987-01-01

    The Stability Augmentation System (SAS) is a special case of the Command Augmentation System (CAS). Control saturation imposes bounds on achievable commands. The state equilibrium depends only on the open loop dynamics and control deflection. The control magnitude to achieve a desired command equilibrium is independent of the feedback gain. A feedback controller provides the desired response, maintains the system equilibrium under disturbances, but it does not affect the equilibrium values of states and control. The saturation boundaries change with commands, but the location of the equilibrium points in the saturated region remains unchanged. Nonzero command vectors yield saturation boundaries that are asymmetric with respect to the state equilibrium. Except for the saddle point case with MCE control law, the stability boundaries change with commands. For the cases of saddle point and unstable nodes, the region of stability decreases with increasing command magnitudes.

  9. Nonlinear interfaces for acceleration-commanded control of spacecraft and manipulators

    NASA Technical Reports Server (NTRS)

    Dwyer, T. A. W., III; Lee, G. K. F.; Chen, N.

    1986-01-01

    Nominal command generation in real time for the control of manipulators or of maneuvering spacecraft is hampered by the nonlinearity of the equations of motion. Likewise the real time tracking of a computed nominal trajectory in the presence of disturbances requires the computation of time-varying Jacobians of the motion. An alternative approach is the formulation of acceleration-commanded control laws in appropriately chosen generalized advantageous to design dedicated circuit interfaces to perform the required transformation. It is also possible to guarantee that actuator and sensor saturation limits are not exceeded, by means of feedback-biased circuits that implement automatic overload limitation of acceleration commands. Recent developments following this 'hardware computation' point of view will be discussed.

  10. Lunar and Martian hardware commonality

    NASA Technical Reports Server (NTRS)

    Davis, Hubert P.; Johnson, Robert E.; Phillips, Paul G.; Spear, Donald S.; Stump, William R.; Williams, Franklin U.

    1986-01-01

    A number of different hardware elements were examined for possible Moon/Mars program commonality. These include manned landers; cargo landers, a trans-Mars injection (TMI) stage, traverse vehicles, unmanned surface rovers, habitation modules, and power supplies. Preliminary analysis indicates that it is possible to build a common two-stage manned lander. A single-stage, reusable lander may be practical for the lunar cast, but much less so for the Martian case, and commonality may therefore exist only at the subsystem level. A modified orbit transfer vehicle was examined as a potential cargo lander. Potential cargoes to various destinations were calculated for a Shuttle external tank sized TMI stage. A nuclear powered, long range traverse vehicle was conceptually designed and commonality is considered feasible. Short range, unmanned rovers can be made common without great effort. A surface habitation module may be difficult to make common due to difficulties in landing certain shapes on the Martian surface with aerobraking landers. Common nuclear power sources appear feasible. High temperature radiators appear easy to make common. Low temperature radiators may be difficult to make common. In most of these cases, Martian requirements determine the design.

  11. Manipulation hardware for microgravity research

    SciTech Connect

    Herndon, J.N.; Glassell, R.L.; Butler, P.L.; Williams, D.M. ); Rohn, D.A. . Lewis Research Center); Miller, J.H. )

    1990-01-01

    The establishment of permanent low earth orbit occupation on the Space Station Freedom will present new opportunities for the introduction of productive flexible automation systems into the microgravity environment of space. The need for robust and reliable robotic systems to support experimental activities normally intended by astronauts will assume great importance. Many experimental modules on the space station are expected to require robotic systems for ongoing experimental operations. When implementing these systems, care must be taken not to introduce deleterious effects on the experiments or on the space station itself. It is important to minimize the acceleration effects on the experimental items being handled while also minimizing manipulator base reaction effects on adjacent experiments and on the space station structure. NASA Lewis Research Center has been performing research on these manipulator applications, focusing on improving the basic manipulator hardware, as well as developing improved manipulator control algorithms. By utilizing the modular manipulator concepts developed during the Laboratory Telerobotic Manipulator program, Oak Ridge National Laboratory has developed an experimental testbed system called the Microgravity Manipulator, incorporating two pitch-yaw modular positioners to provide a 4 dof experimental manipulator arm. A key feature in the design for microgravity manipulation research was the use of traction drives for torque transmission in the modular pitch-yaw differentials.

  12. Life Sciences Division Spaceflight Hardware

    NASA Technical Reports Server (NTRS)

    Yost, B.

    1999-01-01

    The Ames Research Center (ARC) is responsible for the development, integration, and operation of non-human life sciences payloads in support of NASA's Gravitational Biology and Ecology (GB&E) program. To help stimulate discussion and interest in the development and application of novel technologies for incorporation within non-human life sciences experiment systems, three hardware system models will be displayed with associated graphics/text explanations. First, an Animal Enclosure Model (AEM) will be shown to communicate the nature and types of constraints physiological researchers must deal with during manned space flight experiments using rodent specimens. Second, a model of the Modular Cultivation System (MCS) under development by ESA will be presented to highlight technologies that may benefit cell-based research, including advanced imaging technologies. Finally, subsystems of the Cell Culture Unit (CCU) in development by ARC will also be shown. A discussion will be provided on candidate technology requirements in the areas of specimen environmental control, biotelemetry, telescience and telerobotics, and in situ analytical techniques and imaging. In addition, an overview of the Center for Gravitational Biology Research facilities will be provided.

  13. Ideas to hardware at SNLA

    SciTech Connect

    Plomp, P.W.

    1984-01-01

    Sandia's Processes Engineering and Fabrication (P/F) Directorate 7400 is a direct support organization providing shop services for the weapon and nonweapon programs. The directorate is divided into two departments, which are in turn subdivided into divisions. These divisions are comprised of functional groups which are generally supervised by a craft trained employee, whose title is a section supervisor. The functional groups are called sections and are responsible for unique craft services. The interaction with the customer (technical aides, engineers, and scientists) occurs at the section level. Cost and delivery estimates are provided at that level, and after receipt of a Work Order, the section makes all the arrangements to complete the requested services. A centralized production control function using sophisticated software is not used, rather, control is maintained by each functional group. This paper provides a sampling of the prototype hardware that has recently been manufactured by the P/F Directorate, gives a snapshot of the organization, describes the methods for controlling the flow-of-work, and shows a small sample of the specialized equipment found within the P/F Directorate.

  14. Life Sciences Division Spaceflight Hardware

    NASA Technical Reports Server (NTRS)

    Yost, B.

    1999-01-01

    The Ames Research Center (ARC) is responsible for the development, integration, and operation of non-human life sciences payloads in support of NASA's Gravitational Biology and Ecology (GB&E) program. To help stimulate discussion and interest in the development and application of novel technologies for incorporation within non-human life sciences experiment systems, three hardware system models will be displayed with associated graphics/text explanations. First, an Animal Enclosure Model (AEM) will be shown to communicate the nature and types of constraints physiological researchers must deal with during manned space flight experiments using rodent specimens. Second, a model of the Modular Cultivation System (MCS) under development by ESA will be presented to highlight technologies that may benefit cell-based research, including advanced imaging technologies. Finally, subsystems of the Cell Culture Unit (CCU) in development by ARC will also be shown. A discussion will be provided on candidate technology requirements in the areas of specimen environmental control, biotelemetry, telescience and telerobotics, and in situ analytical techniques and imaging. In addition, an overview of the Center for Gravitational Biology Research facilities will be provided.

  15. Tinker's Toys: Lessons from Bank Street: Hardware.

    ERIC Educational Resources Information Center

    Tinker, Robert

    1985-01-01

    Bank Street Laboratory (a set of hardware/software tools for measuring temperature, light, and sound) consists of a board that plugs into Apple microcomputers, cabling, software, and six probes. Discusses the laboratory's hardware, including the analog-to-digital converter, multiplier chip, and modular connectors. Circuit diagrams of components…

  16. Computer hardware description languages - A tutorial

    NASA Technical Reports Server (NTRS)

    Shiva, S. G.

    1979-01-01

    The paper introduces hardware description languages (HDL) as useful tools for hardware design and documentation. The capabilities and limitations of HDLs are discussed along with the guidelines needed in selecting an appropriate HDL. The directions for future work are provided and attention is given to the implementation of HDLs in microcomputers.

  17. Returned Solar Max hardware degradation study results

    NASA Technical Reports Server (NTRS)

    Triolo, Jack J.; Ousley, Gilbert W.

    1989-01-01

    The Solar Maximum Repair Mission returned with the replaced hardware that had been in low Earth orbit for over four years. The materials of this returned hardware gave the aerospace community an opportunity to study the realtime effects of atomic oxygen, solar radiation, impact particles, charged particle radiation, and molecular contamination. The results of these studies are summarized.

  18. 16 CFR 1508.6 - Hardware.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... 16 Commercial Practices 2 2010-01-01 2010-01-01 false Hardware. 1508.6 Section 1508.6 Commercial Practices CONSUMER PRODUCT SAFETY COMMISSION FEDERAL HAZARDOUS SUBSTANCES ACT REGULATIONS REQUIREMENTS FOR FULL-SIZE BABY CRIBS § 1508.6 Hardware. (a) A crib shall be designed and constructed in a manner...

  19. 16 CFR 1509.7 - Hardware.

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... NON-FULL-SIZE BABY CRIBS § 1509.7 Hardware. (a) The hardware in a non-full-size baby crib shall be... abuse. (b) Non-full-size baby cribs shall incorporate locking or latching devices for dropsides or... non-full-size baby crib....

  20. 16 CFR 1509.7 - Hardware.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... NON-FULL-SIZE BABY CRIBS § 1509.7 Hardware. (a) The hardware in a non-full-size baby crib shall be... abuse. (b) Non-full-size baby cribs shall incorporate locking or latching devices for dropsides or... non-full-size baby crib....

  1. 16 CFR 1508.6 - Hardware.

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... 16 Commercial Practices 2 2011-01-01 2011-01-01 false Hardware. 1508.6 Section 1508.6 Commercial Practices CONSUMER PRODUCT SAFETY COMMISSION FEDERAL HAZARDOUS SUBSTANCES ACT REGULATIONS REQUIREMENTS FOR FULL-SIZE BABY CRIBS § 1508.6 Hardware. (a) A crib shall be designed and constructed in a manner...

  2. Hardware survey for the avionics test bed

    NASA Technical Reports Server (NTRS)

    Cobb, J. M.

    1981-01-01

    A survey of maor hardware items that could possibly be used in the development of an avionics test bed for space shuttle attached or autonomous large space structures was conducted in NASA Johnson Space Center building 16. The results of the survey are organized to show the hardware by laboratory usage. Computer systems in each laboratory are described in some detail.

  3. Expanding the Lessons Learned Program to Include Corps Support Command Commanders and Theater Army Area Command Commanders

    DTIC Science & Technology

    1989-03-10

    il !wi# c’t~ red by the apptwpriate MilitIfty 80rncc or EXPANDING T"I’l LESSONS LEARNED PROGRAM TO INCLUDECORI 3 St3PPOFT COMMAND COMHADERS A𔃻 THEATER...COVERED EXPANDING THE LESSONS LEARNED PROGRAM . . . Study Project 6. PERFORMING ORG. REPORT NCMBER 7. AUTHOR(&) S. CONTRACT OR GRANT NUMBER(a) LTC Kenneth M...publication until It has been cleared by the sppropriate mlitary Gervice or goverrment agency. EXPANDING THE LESSONS LEARNED PROGRAM TO INCLUDE CORPS

  4. The Command of the Air,

    DTIC Science & Technology

    1983-01-01

    should round out my thoughts on the subject of air power. Part II of Book One should therefore be considered complementary to Part I. The ideas...of the two can be hit and put out of action by the defender. But if both sides are armed with rifles which can fire thirty rounds a minute, to have...the same mathematical certainty the trench must be stormed by thirty-one men. All the rounds 12 The Command of The Air these men might have fired

  5. PEP-II Hardware Reliability

    SciTech Connect

    Allen, C. W.

    2005-04-28

    Hardware reliability takes on special importance in large accelerator facilities intended to work as factories; i.e., when they are expected to deliver design performance for extended periods of time. The PEP-II B-Factory at SLAC is such a facility. In this paper, we summarize PEP-II reliability statistics from the first four years of production running. The four running periods extended from January 12 through October 31, 2000, from February 4, 2001 through June 30, 2002, from November 15, 2002 through June 30, 2003, and from September 9, 2003 through July 31, 2004. These four periods are designated Runs 1, 2, 3, and 4 in the discussion and tables presented in the paper. The first four runs encompassed 30,359 hours. During this time, PEP-II was delivering luminosity to the BaBar detector 57.9 percent of the time. In addition, 5.3 percent of the time was used for scheduled dedicated machine development work, and 4.5 percent was scheduled off for maintenance, installations, or safety checks. Injection and tuning accounted for 19.9 percent. The remaining 12.4 percent was lost due to malfunctions. During this time period, a total of 9701 malfunctions were reported, but most did not interrupt the running program. The unscheduled down time, a total of 3883 hours, was attributed to 1724 of these malfunctions. Mean Time to Fail (MTTF) and Mean Time to Repair (MTTR) are presented for each of the major subsystems, and long-term availability trends are discussed.

  6. An evaluation of Skylab habitability hardware

    NASA Technical Reports Server (NTRS)

    Stokes, J.

    1974-01-01

    For effective mission performance, participants in space missions lasting 30-60 days or longer must be provided with hardware to accommodate their personal needs. Such habitability hardware was provided on Skylab. Equipment defined as habitability hardware was that equipment composing the food system, water system, sleep system, waste management system, personal hygiene system, trash management system, and entertainment equipment. Equipment not specifically defined as habitability hardware but which served that function were the Wardroom window, the exercise equipment, and the intercom system, which was occasionally used for private communications. All Skylab habitability hardware generally functioned as intended for the three missions, and most items could be considered as adequate concepts for future flights of similar duration. Specific components were criticized for their shortcomings.

  7. Comparative Modal Analysis of Sieve Hardware Designs

    NASA Technical Reports Server (NTRS)

    Thompson, Nathaniel

    2012-01-01

    The CMTB Thwacker hardware operates as a testbed analogue for the Flight Thwacker and Sieve components of CHIMRA, a device on the Curiosity Rover. The sieve separates particles with a diameter smaller than 150 microns for delivery to onboard science instruments. The sieving behavior of the testbed hardware should be similar to the Flight hardware for the results to be meaningful. The elastodynamic behavior of both sieves was studied analytically using the Rayleigh Ritz method in conjunction with classical plate theory. Finite element models were used to determine the mode shapes of both designs, and comparisons between the natural frequencies and mode shapes were made. The analysis predicts that the performance of the CMTB Thwacker will closely resemble the performance of the Flight Thwacker within the expected steady state operating regime. Excitations of the testbed hardware that will mimic the flight hardware were recommended, as were those that will improve the efficiency of the sieving process.

  8. Current trends in hardware and software for brain-computer interfaces (BCIs).

    PubMed

    Brunner, P; Bianchi, L; Guger, C; Cincotti, F; Schalk, G

    2011-04-01

    A brain-computer interface (BCI) provides a non-muscular communication channel to people with and without disabilities. BCI devices consist of hardware and software. BCI hardware records signals from the brain, either invasively or non-invasively, using a series of device components. BCI software then translates these signals into device output commands and provides feedback. One may categorize different types of BCI applications into the following four categories: basic research, clinical/translational research, consumer products, and emerging applications. These four categories use BCI hardware and software, but have different sets of requirements. For example, while basic research needs to explore a wide range of system configurations, and thus requires a wide range of hardware and software capabilities, applications in the other three categories may be designed for relatively narrow purposes and thus may only need a very limited subset of capabilities. This paper summarizes technical aspects for each of these four categories of BCI applications. The results indicate that BCI technology is in transition from isolated demonstrations to systematic research and commercial development. This process requires several multidisciplinary efforts, including the development of better integrated and more robust BCI hardware and software, the definition of standardized interfaces, and the development of certification, dissemination and reimbursement procedures.

  9. Current trends in hardware and software for brain-computer interfaces (BCIs)

    NASA Astrophysics Data System (ADS)

    Brunner, P.; Bianchi, L.; Guger, C.; Cincotti, F.; Schalk, G.

    2011-04-01

    A brain-computer interface (BCI) provides a non-muscular communication channel to people with and without disabilities. BCI devices consist of hardware and software. BCI hardware records signals from the brain, either invasively or non-invasively, using a series of device components. BCI software then translates these signals into device output commands and provides feedback. One may categorize different types of BCI applications into the following four categories: basic research, clinical/translational research, consumer products, and emerging applications. These four categories use BCI hardware and software, but have different sets of requirements. For example, while basic research needs to explore a wide range of system configurations, and thus requires a wide range of hardware and software capabilities, applications in the other three categories may be designed for relatively narrow purposes and thus may only need a very limited subset of capabilities. This paper summarizes technical aspects for each of these four categories of BCI applications. The results indicate that BCI technology is in transition from isolated demonstrations to systematic research and commercial development. This process requires several multidisciplinary efforts, including the development of better integrated and more robust BCI hardware and software, the definition of standardized interfaces, and the development of certification, dissemination and reimbursement procedures.

  10. System design of the Pioneer Venus spacecraft. Volume 8: Command/data handling subsystems studies

    NASA Technical Reports Server (NTRS)

    Vesely, D. D.

    1973-01-01

    Study tasks for the command and data handling subsystems have been directed to: (1) determining ground data systems, (GDS) interfaces and deep space network (DSN) changes, if required, (2) defining subsystem requirements, (3) surveying existing hardware that could be used or modified to meet subsystem requirements, and (4) establishing a baseline design. Study of the existing GDS led to the conclusion that the Viking configuration GDS can be used with only minor changes required for the Pioneer Venus baseline. Those changes required are associated with providing a predetection recording capability used during probe entry and descent. Subsystem requirements were first formulated with sufficient latitude so that surveys of existing hardware could lead to low cost hardware which, in turn, could modify more narrowly defined subsystem requirements.

  11. Transforming the Army with Mission Command

    DTIC Science & Technology

    2015-06-12

    mission command through the lens of a well-respected scholarly model of organizational change . The reason for scrutinizing the mission command...implementation plans against a well-respected scholarly model of change was to determine if there were processes that could improve the Army’s current...using Kotter’s Eight-Stage Process of Creating Major Change ? The secondary research questions were: Why mission command? What is the Army’s plan to

  12. Developing Flexible Command and Control of Airpower

    DTIC Science & Technology

    2011-01-01

    organizational level. The most famous practitioner of this concept, Gen Elwood “Pete” Quesada , commanded all tactical air forces on the continent, some more...XIX Tactical Air Command of Gen Otto “Opie” Weyland, who famously supported Gen George Patton’s charge across central France. Quesada trained all...understood his com- mand intent. He also worked closely with Lt Gen Courtney Hodges, commander of Army forces in France. Quesada saw to it that

  13. Hardware Removal after Osseous Free Flap Reconstruction

    PubMed Central

    Day, Kristine E.; Desmond, Renee; Magnuson, J. Scott; Carroll, William R.; Rosenthal, Eben L.

    2015-01-01

    Objective Identifying risk factors for hardware removal in patients undergoing mandibular reconstruction with vascularized osseous free flaps remains a challenge. The purpose of this study is to identify potential risk factors, including osteocutaneous radial forearm versus fibular flap, for need for removal and to describe the fate of implanted hardware. Study Design Case series with chart review. Setting Academic tertiary care medical center. Subjects and Methods Two hundred thirteen patients undergoing 227 vascularized osseous mandibular reconstructions between the years 2004 and 2012. Data were compiled through a manual chart review, and patients incurring hardware removals were identified. Results Thirty-four of 213 evaluable vascularized osseous free flaps (16%) underwent surgical removal of hardware. The average length of time to removal was 16.2 months (median 10 months), with the majority of removals occurring within the first year. Osteocutaneous radial forearm free flaps (OCRFFF) incurred a slightly higher percentage of hardware removals (9.9%) compared to fibula flaps (6.1%). Partial removal was performed in 8 of 34 cases, and approximately 38% of these required additional surgery for removal. Conclusion Hardware removal was associated with continued tobacco use after mandibular reconstruction (P = .03). Removal of the supporting hardware most commonly occurs from infection or exposure in the first year. In the majority of cases the bone is well healed and the problem resolves with removal. PMID:24201061

  14. Hardware removal after osseous free flap reconstruction.

    PubMed

    Day, Kristine E; Desmond, Renee; Magnuson, J Scott; Carroll, William R; Rosenthal, Eben L

    2014-01-01

    Identifying risk factors for hardware removal in patients undergoing mandibular reconstruction with vascularized osseous free flaps remains a challenge. The purpose of this study is to identify potential risk factors, including osteocutaneous radial forearm versus fibular flap, for need for removal and to describe the fate of implanted hardware. Case series with chart review Setting Academic tertiary care medical center. Two hundred thirteen patients undergoing 227 vascularized osseous mandibular reconstructions between the years 2004 and 2012. Data were compiled through a manual chart review, and patients incurring hardware removals were identified. Thirty-four of 213 evaluable vascularized osseous free flaps (16%) underwent surgical removal of hardware. The average length of time to removal was 16.2 months (median 10 months), with the majority of removals occurring within the first year. Osteocutaneous radial forearm free flaps (OCRFFF) incurred a slightly higher percentage of hardware removals (9.9%) compared to fibula flaps (6.1%). Partial removal was performed in 8 of 34 cases, and approximately 38% of these required additional surgery for removal. Hardware removal was associated with continued tobacco use after mandibular reconstruction (P = .03). Removal of the supporting hardware most commonly occurs from infection or exposure in the first year. In the majority of cases the bone is well healed and the problem resolves with removal.

  15. Debarment: A Guide for Installation Commanders

    DTIC Science & Technology

    2001-04-01

    U.S. v. May, et. al., 622 F.2d 1000 (1980), for the proposition that commanders —bar“ individuals from base, but see, Flower v. United States, 407 U.S...installations by order of the installation commander. In Flower v. United States,30 the Supreme Court began to clarify it‘s holding in McElroy, and...articulate the parameters within which an installation commander can operate in protecting assets and people under his command. In Flower , the Supreme

  16. Station Commander Congratulates New Flight Directors

    NASA Image and Video Library

    Aboard the International Space Station, Expedition 29 Commander Mike Fossum congratulates Judd Frieling, Tomas Gonzalez-Torres and Greg Whitney on being selected as NASA's newest flight directors. ...

  17. Applying a Genetic Algorithm to Reconfigurable Hardware

    NASA Technical Reports Server (NTRS)

    Wells, B. Earl; Weir, John; Trevino, Luis; Patrick, Clint; Steincamp, Jim

    2004-01-01

    This paper investigates the feasibility of applying genetic algorithms to solve optimization problems that are implemented entirely in reconfgurable hardware. The paper highlights the pe$ormance/design space trade-offs that must be understood to effectively implement a standard genetic algorithm within a modem Field Programmable Gate Array, FPGA, reconfgurable hardware environment and presents a case-study where this stochastic search technique is applied to standard test-case problems taken from the technical literature. In this research, the targeted FPGA-based platform and high-level design environment was the Starbridge Hypercomputing platform, which incorporates multiple Xilinx Virtex II FPGAs, and the Viva TM graphical hardware description language.

  18. Space shuttle main engine hardware simulation

    NASA Technical Reports Server (NTRS)

    Vick, H. G.; Hampton, P. W.

    1985-01-01

    The Huntsville Simulation Laboratory (HSL) provides a simulation facility to test and verify the space shuttle main engine (SSME) avionics and software system using a maximum complement of flight type hardware. The HSL permits evaluations and analyses of the SSME avionics hardware, software, control system, and mathematical models. The laboratory has performed a wide spectrum of tests and verified operational procedures to ensure system component compatibility under all operating conditions. It is a test bed for integration of hardware/software/hydraulics. The HSL is and has been an invaluable tool in the design and development of the SSME.

  19. Modeling to Improve the Risk Reduction Process for Command File Errors

    NASA Technical Reports Server (NTRS)

    Meshkat, Leila; Bryant, Larry; Waggoner, Bruce

    2013-01-01

    The Jet Propulsion Laboratory has learned that even innocuous errors in the spacecraft command process can have significantly detrimental effects on a space mission. Consequently, such Command File Errors (CFE), regardless of their effect on the spacecraft, are treated as significant events for which a root cause is identified and corrected. A CFE during space mission operations is often the symptom of imbalance or inadequacy within the system that encompasses the hardware and software used for command generation as well as the human experts and processes involved in this endeavor. As we move into an era of increased collaboration with other NASA centers and commercial partners, these systems become more and more complex. Consequently, the ability to thoroughly model and analyze CFEs formally in order to reduce the risk they pose is increasingly important. In this paper, we summarize the results of applying modeling techniques previously developed to the DAWN flight project. The original models were built with the input of subject matter experts from several flight projects. We have now customized these models to address specific questions for the DAWN flight project and formulating use cases to address their unique mission needs. The goal of this effort is to enhance the project's ability to meet commanding reliability requirements for operations and to assist them in managing their Command File Errors.

  20. Modeling to Improve the Risk Reduction Process for Command File Errors

    NASA Technical Reports Server (NTRS)

    Meshkat, Leila; Bryant, Larry; Waggoner, Bruce

    2013-01-01

    The Jet Propulsion Laboratory has learned that even innocuous errors in the spacecraft command process can have significantly detrimental effects on a space mission. Consequently, such Command File Errors (CFE), regardless of their effect on the spacecraft, are treated as significant events for which a root cause is identified and corrected. A CFE during space mission operations is often the symptom of imbalance or inadequacy within the system that encompasses the hardware and software used for command generation as well as the human experts and processes involved in this endeavor. As we move into an era of increased collaboration with other NASA centers and commercial partners, these systems become more and more complex. Consequently, the ability to thoroughly model and analyze CFEs formally in order to reduce the risk they pose is increasingly important. In this paper, we summarize the results of applying modeling techniques previously developed to the DAWN flight project. The original models were built with the input of subject matter experts from several flight projects. We have now customized these models to address specific questions for the DAWN flight project and formulating use cases to address their unique mission needs. The goal of this effort is to enhance the project's ability to meet commanding reliability requirements for operations and to assist them in managing their Command File Errors.

  1. Framework for Enhanced Military Cooperation Among North American Aerospace Defense Command, United States Northern Command and Canada Command

    DTIC Science & Technology

    2009-09-01

    Ongoing right of passage authority • Command may be supporting/supported to a national command • Liaison with other government departments (OGO...architectures • Compatible national ROE • Coordinated procedures • Requested right of passage • Supporting/supported relationship not applicable

  2. Responding to command hallucinations to harm: the unpleasant voices scale and harm command safety protocol.

    PubMed

    Gerlock, April A; Buccheri, Robin; Buffum, Martha D; Trygstad, Louise; Dowling, Glenna A

    2010-05-01

    Command hallucinations are relatively common in voice hearers and are taken seriously because of the potential threat to self and others. Many variables mediate the relationship between hearing commands and acting on them. This article describes the implementation of the Harm Command Safety Protocol and the Unpleasant Voices Scale to respond to command hallucinations to harm in the context of the dissemination of a multisite, evidence-based behavioral management course for patients with auditory hallucinations.

  3. Command and Control: Toward Arctic Unity of Command and Unity of Effort

    DTIC Science & Technology

    2011-05-19

    is the most effective command and control structure to provide the requisite unity of command and unity of effort in the Arctic? (Maximum 200 Words...frame discusses recent climate change effects on transportation, shipping, resources, and international relationships. Four potential problems are...chief, what is the most effective command and control structure to provide the requisite unity of command and unity of effort in the Arctic? Looking

  4. Command and Service Module Communications

    NASA Technical Reports Server (NTRS)

    Interbartolo, Michael

    2009-01-01

    This viewgraph presentation examines Command and Service Module (CSM) Communications. The communication system's capabilities are defined, including CSM-Earth, CSM-Lunar Module and CSM-Extravehicular crewman communications. An overview is provided for S-band communications, including data transmission and receiving rates, operating frequencies and major system components (pre-modulation processors, unified S-band electronics, S-band power amplifier and S-band antennas). Additionally, data transmission rates, operating frequencies and the capabilities of VHF communications are described. Major VHF components, including transmitters and receivers, and the VHF multiplexer and antennas are also highlighted. Finally, communications during pre-launch, ascent, in-flight and entry are discussed. Overall, the CSM communication system was rated highly by flight controllers and crew. The system was mostly autonomous for both crew and flight controllers and no major issues were encountered during flight.

  5. KENNEDY SPACE CENTER, FLA. - Greeted by cheers from wellwishers at KSC and eager for their ventur into space on the Microgrvity Science Laboratory-1 (MSL-1) mission, the STS-83 astronauts depart the Operations and Checkout Building on their way to Launch Pad 39A. Leading the seven-member crew is Mission Commander James D. Halsell Jr. Behind Halsell and to his right is Pilot Susan L. Still. Behind Still is Payload Commander Janice Voss, with Mission Specialist Donald A. Thomas to her left. Behind Thomas, in order, are Mission Specialist Michael L. Gernhardt and Payload Specialists Roger K. Crouch and Gregory T. Linteris. During the scheduled 16-day STS-83 mission, the MSL-1 will be used to test some of the hardware, facilities and procedures that are planned for use on the International Space Station while the flight crew conducts combustion, protein crystal growth and materials processing experiments. Also onboard is the Hitchhiker Cryogenic Flexible Diode (CRYOFD) experiment payload, which is attched to the right side of Columbia's payload bay.

    NASA Image and Video Library

    1997-04-04

    KENNEDY SPACE CENTER, FLA. - Greeted by cheers from wellwishers at KSC and eager for their ventur into space on the Microgrvity Science Laboratory-1 (MSL-1) mission, the STS-83 astronauts depart the Operations and Checkout Building on their way to Launch Pad 39A. Leading the seven-member crew is Mission Commander James D. Halsell Jr. Behind Halsell and to his right is Pilot Susan L. Still. Behind Still is Payload Commander Janice Voss, with Mission Specialist Donald A. Thomas to her left. Behind Thomas, in order, are Mission Specialist Michael L. Gernhardt and Payload Specialists Roger K. Crouch and Gregory T. Linteris. During the scheduled 16-day STS-83 mission, the MSL-1 will be used to test some of the hardware, facilities and procedures that are planned for use on the International Space Station while the flight crew conducts combustion, protein crystal growth and materials processing experiments. Also onboard is the Hitchhiker Cryogenic Flexible Diode (CRYOFD) experiment payload, which is attched to the right side of Columbia's payload bay.

  6. Converting a commercial electric direct-drive robot to operate from joint torque commands

    SciTech Connect

    Muir, P.F.

    1991-07-01

    Many robot control algorithms for high performance in-contact operations including hybrid force/position, stiffness control and impedance control approaches require the command the joint torques. However, most commercially available robots do not provide joint torque command capabilities. The joint command at the user level is typically position or velocity and at the control developer level is voltage, current, or pulse-width, and the torque generated is a nonlinear function of the command and joint position. To enable the application of high performance in-contact control algorithms to commercially available robots, and thereby facilitate technology transfer from the robot control research community to commercial applications, an methodology has been developed to linearize the torque characteristics of electric motor-amplifier combinations. A four degree of freedom Adept 2 robot, having pulse-width modulation amplifiers and both variable reluctance and brushless DC motors, is converted to operate from joint torque commands to demonstrate the methodology. The commercial robot controller is replaced by a VME-based system incorporating special purpose hardware and firmware programmed from experimental data. The performance improvement is experimentally measured and graphically displayed using three-dimensional plots of torque vs command vs position. The average percentage torque deviation over the command and position ranges is reduced from as much as 76% to below 5% for the direct-drive joints 1, 2 and 4 and is cut by one half in the remaining ball-screw driven joint 3. Further, the torque deviation of the direct-drive joints drops below 2.5% if only the upper 90% of the torque range is considered. 23 refs., 20 figs., 2 tabs.

  7. 32 CFR 536.12 - Commanding General, U.S. Army Medical Command.

    Code of Federal Regulations, 2010 CFR

    2010-07-01

    ... 32 National Defense 3 2010-07-01 2010-07-01 true Commanding General, U.S. Army Medical Command. 536.12 Section 536.12 National Defense Department of Defense (Continued) DEPARTMENT OF THE ARMY CLAIMS AND ACCOUNTS CLAIMS AGAINST THE UNITED STATES The Army Claims System § 536.12 Commanding General,...

  8. Nespoli works with ERB2 Hardware

    NASA Image and Video Library

    2011-01-08

    ISS026-E-017685 (8 Jan. 2011) --- European Space Agency astronaut Paolo Nespoli, Expedition 26 flight engineer, works with European Recording Binocular (ERB2) hardware in the Harmony node of the International Space Station.

  9. Nespoli works with ERB2 Hardware

    NASA Image and Video Library

    2011-01-08

    ISS026-E-017683 (8 Jan. 2011) --- European Space Agency astronaut Paolo Nespoli, Expedition 26 flight engineer, works with European Recording Binocular (ERB2) hardware in the Harmony node of the International Space Station.

  10. Orbiter CIU/IUS communications hardware evaluation

    NASA Technical Reports Server (NTRS)

    Huth, G. K.

    1979-01-01

    Inertial Upper Stage (IUS) and DoD Communication Interface Unit (CIU) communication system design, hardware specifications, and interfaces were evaluated to determine their compatibility with the Orbiter payload communication and data handling equipment and the Orbiter network communication equipment.

  11. Hardware device binding and mutual authentication

    DOEpatents

    Hamlet, Jason R; Pierson, Lyndon G

    2014-03-04

    Detection and deterrence of device tampering and subversion by substitution may be achieved by including a cryptographic unit within a computing device for binding multiple hardware devices and mutually authenticating the devices. The cryptographic unit includes a physically unclonable function ("PUF") circuit disposed in or on the hardware device, which generates a binding PUF value. The cryptographic unit uses the binding PUF value during an enrollment phase and subsequent authentication phases. During a subsequent authentication phase, the cryptographic unit uses the binding PUF values of the multiple hardware devices to generate a challenge to send to the other device, and to verify a challenge received from the other device to mutually authenticate the hardware devices.

  12. BTKh-26 STRUKTURA (Luch-2) Hardware

    NASA Image and Video Library

    2012-06-30

    ISS032-E-005012 (30 June 2012) --- Russian cosmonaut Sergei Revin, Expedition 32 flight engineer, is pictured near Russian biotechnology experiment BTKh-26 STRUKTURA (Luch-2) hardware floating freely in the Zvezda Service Module of the International Space Station.

  13. Rapid Production of Composite Prototype Hardware

    NASA Technical Reports Server (NTRS)

    DeLay, T. K.

    2000-01-01

    The objective of this research was to provide a mechanism to cost-effectively produce composite hardware prototypes. The task was to take a hands-on approach to developing new technologies that could benefit multiple future programs.

  14. Thirsk with FPEF MS hardware in Kibo

    NASA Image and Video Library

    2009-10-07

    ISS020-E-048792 (7 Oct. 2009) --- Canadian Space Agency astronaut Robert Thirsk, Expedition 20/21 flight engineer, holds Fluid Physics Experiment Facility/Marangoni Surface (FPEF MS) Core hardware in the Kibo laboratory of the International Space Station.

  15. IDD Archival Hardware Architecture and Workflow

    SciTech Connect

    Mendonsa, D; Nekoogar, F; Martz, H

    2008-10-09

    This document describes the functionality of every component in the DHS/IDD archival and storage hardware system shown in Fig. 1. The document describes steps by step process of image data being received at LLNL then being processed and made available to authorized personnel and collaborators. Throughout this document references will be made to one of two figures, Fig. 1 describing the elements of the architecture and the Fig. 2 describing the workflow and how the project utilizes the available hardware.

  16. Development of robotics facility docking test hardware

    NASA Technical Reports Server (NTRS)

    Loughead, T. E.; Winkler, R. V.

    1984-01-01

    Design and fabricate test hardware for NASA's George C. Marshall Space Flight Center (MSFC) are reported. A docking device conceptually developed was fabricated, and two docking targets which provide high and low mass docking loads were required and were represented by an aft 61.0 cm section of a Hubble space telescope (ST) mockup and an upgrading of an existing multimission modular spacecraft (MSS) mockup respectively. A test plan is developed for testing the hardware.

  17. Towards composition of verified hardware devices

    NASA Technical Reports Server (NTRS)

    Schubert, E. Thomas; Levitt, K.; Cohen, G. C.

    1991-01-01

    Computers are being used where no affordable level of testing is adequate. Safety and life critical systems must find a replacement for exhaustive testing to guarantee their correctness. Through a mathematical proof, hardware verification research has focused on device verification and has largely ignored system composition verification. To address these deficiencies, we examine how the current hardware verification methodology can be extended to verify complete systems.

  18. Software for Managing Inventory of Flight Hardware

    NASA Technical Reports Server (NTRS)

    Salisbury, John; Savage, Scott; Thomas, Shirman

    2003-01-01

    The Flight Hardware Support Request System (FHSRS) is a computer program that relieves engineers at Marshall Space Flight Center (MSFC) of most of the non-engineering administrative burden of managing an inventory of flight hardware. The FHSRS can also be adapted to perform similar functions for other organizations. The FHSRS affords a combination of capabilities, including those formerly provided by three separate programs in purchasing, inventorying, and inspecting hardware. The FHSRS provides a Web-based interface with a server computer that supports a relational database of inventory; electronic routing of requests and approvals; and electronic documentation from initial request through implementation of quality criteria, acquisition, receipt, inspection, storage, and final issue of flight materials and components. The database lists both hardware acquired for current projects and residual hardware from previous projects. The increased visibility of residual flight components provided by the FHSRS has dramatically improved the re-utilization of materials in lieu of new procurements, resulting in a cost savings of over $1.7 million. The FHSRS includes subprograms for manipulating the data in the database, informing of the status of a request or an item of hardware, and searching the database on any physical or other technical characteristic of a component or material. The software structure forces normalization of the data to facilitate inquiries and searches for which users have entered mixed or inconsistent values.

  19. 46 CFR 5.801 - Commandant's review.

    Code of Federal Regulations, 2011 CFR

    2011-10-01

    ... 46 Shipping 1 2011-10-01 2011-10-01 false Commandant's review. 5.801 Section 5.801 Shipping COAST... REGULATIONS-PERSONNEL ACTION Review of Administrative Law Judge's Decisions in Cases Where Charges Have Been Found Proved § 5.801 Commandant's review. Any decision of an Administrative Law Judge, in which...

  20. 32 CFR 637.3 - Installation Commander.

    Code of Federal Regulations, 2010 CFR

    2010-07-01

    ... 32 National Defense 4 2010-07-01 2010-07-01 true Installation Commander. 637.3 Section 637.3 National Defense Department of Defense (Continued) DEPARTMENT OF THE ARMY (CONTINUED) LAW ENFORCEMENT AND CRIMINAL INVESTIGATIONS MILITARY POLICE INVESTIGATION Investigations § 637.3 Installation Commander. The...

  1. 32 CFR 637.3 - Installation Commander.

    Code of Federal Regulations, 2011 CFR

    2011-07-01

    ... 32 National Defense 4 2011-07-01 2011-07-01 false Installation Commander. 637.3 Section 637.3 National Defense Department of Defense (Continued) DEPARTMENT OF THE ARMY (CONTINUED) LAW ENFORCEMENT AND CRIMINAL INVESTIGATIONS MILITARY POLICE INVESTIGATION Investigations § 637.3 Installation Commander. The...

  2. 32 CFR 637.3 - Installation Commander.

    Code of Federal Regulations, 2012 CFR

    2012-07-01

    ... 32 National Defense 4 2012-07-01 2011-07-01 true Installation Commander. 637.3 Section 637.3 National Defense Department of Defense (Continued) DEPARTMENT OF THE ARMY (CONTINUED) LAW ENFORCEMENT AND CRIMINAL INVESTIGATIONS MILITARY POLICE INVESTIGATION Investigations § 637.3 Installation Commander. The...

  3. 32 CFR 637.3 - Installation Commander.

    Code of Federal Regulations, 2013 CFR

    2013-07-01

    ... 32 National Defense 4 2013-07-01 2013-07-01 false Installation Commander. 637.3 Section 637.3 National Defense Department of Defense (Continued) DEPARTMENT OF THE ARMY (CONTINUED) LAW ENFORCEMENT AND CRIMINAL INVESTIGATIONS MILITARY POLICE INVESTIGATION Investigations § 637.3 Installation Commander. The...

  4. 32 CFR 637.3 - Installation Commander.

    Code of Federal Regulations, 2014 CFR

    2014-07-01

    ... 32 National Defense 4 2014-07-01 2013-07-01 true Installation Commander. 637.3 Section 637.3 National Defense Department of Defense (Continued) DEPARTMENT OF THE ARMY (CONTINUED) LAW ENFORCEMENT AND CRIMINAL INVESTIGATIONS MILITARY POLICE INVESTIGATION Investigations § 637.3 Installation Commander. The...

  5. The Marihuana Dilemma: Challenge to Commanders.

    DTIC Science & Technology

    The marihuana dilemma poses a major challenge to commanders in the US Army today. The problem was analyzed as to the characteristics of the drug...available to commanders to meet the challenge. The essay concludes that marihuana should not be legalized; drug users or former drug users should not be

  6. Air Force Materiel Command Reorganization Analysis

    DTIC Science & Technology

    2012-01-01

    Gen Judith Fedder, Deputy Chief of Staff for Logistics, Installations, and Mission Support (AF/A4/7); Patricia Young, Assistant Deputy Chief of...Bruce Carlson as AFMC Commander on November 21, 2008. Lt Gen Terry L. Gabreski and Steven Butler continued on as Vice Commander and Executive

  7. BCS-18A command decoder-selector

    NASA Astrophysics Data System (ADS)

    Laping, H.

    1980-08-01

    This report describes an 18-channel command decoder-selector which operates in conjunction with an HF command receiver to allow secure and reliable radio control of high altitude balloon payloads. A detailed technical description and test results are also included.

  8. Astronaut Young at the commander's station

    NASA Image and Video Library

    1983-11-28

    STS009-128-858 (28 Nov-8 Dec 1983) --- Astronaut John W. Young takes notes in the commander?s station on the flight deck of the Columbia. The cathode ray tube (CRT) among the forward panels displays the orbiter?s position in relation to the Earth on its monitor. Astronaut Brewster H. Shaw Jr., pilot, took this photograph.

  9. XTCE. XML Telemetry and Command Exchange Tutorial

    NASA Technical Reports Server (NTRS)

    Rice, Kevin; Kizzort, Brad; Simon, Jerry

    2010-01-01

    An XML Telemetry Command Exchange (XTCE) tutoral oriented towards packets or minor frames is shown. The contents include: 1) The Basics; 2) Describing Telemetry; 3) Describing the Telemetry Format; 4) Commanding; 5) Forgotten Elements; 6) Implementing XTCE; and 7) GovSat.

  10. 32 CFR 215.7 - Command relationships.

    Code of Federal Regulations, 2014 CFR

    2014-07-01

    ... 32 National Defense 2 2014-07-01 2014-07-01 false Command relationships. 215.7 Section 215.7 National Defense Department of Defense (Continued) OFFICE OF THE SECRETARY OF DEFENSE (CONTINUED) MISCELLANEOUS EMPLOYMENT OF MILITARY RESOURCES IN THE EVENT OF CIVIL DISTURBANCES § 215.7 Command relationships...

  11. 32 CFR 215.7 - Command relationships.

    Code of Federal Regulations, 2013 CFR

    2013-07-01

    ... 32 National Defense 2 2013-07-01 2013-07-01 false Command relationships. 215.7 Section 215.7 National Defense Department of Defense (Continued) OFFICE OF THE SECRETARY OF DEFENSE (CONTINUED) MISCELLANEOUS EMPLOYMENT OF MILITARY RESOURCES IN THE EVENT OF CIVIL DISTURBANCES § 215.7 Command relationships...

  12. 32 CFR 215.7 - Command relationships.

    Code of Federal Regulations, 2012 CFR

    2012-07-01

    ... 32 National Defense 2 2012-07-01 2012-07-01 false Command relationships. 215.7 Section 215.7 National Defense Department of Defense (Continued) OFFICE OF THE SECRETARY OF DEFENSE (CONTINUED) MISCELLANEOUS EMPLOYMENT OF MILITARY RESOURCES IN THE EVENT OF CIVIL DISTURBANCES § 215.7 Command relationships...

  13. 32 CFR 215.7 - Command relationships.

    Code of Federal Regulations, 2010 CFR

    2010-07-01

    ... 32 National Defense 2 2010-07-01 2010-07-01 false Command relationships. 215.7 Section 215.7 National Defense Department of Defense (Continued) OFFICE OF THE SECRETARY OF DEFENSE (CONTINUED) MISCELLANEOUS EMPLOYMENT OF MILITARY RESOURCES IN THE EVENT OF CIVIL DISTURBANCES § 215.7 Command relationships...

  14. 32 CFR 215.7 - Command relationships.

    Code of Federal Regulations, 2011 CFR

    2011-07-01

    ... 32 National Defense 2 2011-07-01 2011-07-01 false Command relationships. 215.7 Section 215.7 National Defense Department of Defense (Continued) OFFICE OF THE SECRETARY OF DEFENSE (CONTINUED) MISCELLANEOUS EMPLOYMENT OF MILITARY RESOURCES IN THE EVENT OF CIVIL DISTURBANCES § 215.7 Command relationships...

  15. DSN command system Mark III-80

    NASA Technical Reports Server (NTRS)

    Thorman, H. C.

    1980-01-01

    The Deep Space Network command system configuration and functional operation are described. Voyager and Helios command operations are supported with Deep Space Station store and forward data handling; Viking and Pioneer are supported with the older, near real time data handling method.

  16. Capturing a Commander's decision making style

    NASA Astrophysics Data System (ADS)

    Santos, Eugene; Nguyen, Hien; Russell, Jacob; Kim, Keumjoo; Veenhuis, Luke; Boparai, Ramnjit; Stautland, Thomas Kristoffer

    2017-05-01

    A Commander's decision making style represents how he weighs his choices and evaluates possible solutions with regards to his goals. Specifically, in the naval warfare domain, it relates the way he processes a large amount of information in dynamic, uncertain environments, allocates resources, and chooses appropriate actions to pursue. In this paper, we describe an approach to capture a Commander's decision style by creating a cognitive model that captures his decisionmaking process and evaluate this model using a set of scenarios using an online naval warfare simulation game. In this model, we use the Commander's past behaviors and generalize Commander's actions across multiple problems and multiple decision making sequences in order to recommend actions to a Commander in a manner that he may have taken. Our approach builds upon the Double Transition Model to represent the Commander's focus and beliefs to estimate his cognitive state. Each cognitive state reflects a stage in a Commander's decision making process, each action reflects the tasks that he has taken to move himself closer to a final decision, and the reward reflects how close he is to achieving his goal. We then use inverse reinforcement learning to compute a reward for each of the Commander's actions. These rewards and cognitive states are used to compare between different styles of decision making. We construct a set of scenarios in the game where rational, intuitive and spontaneous decision making styles will be evaluated.

  17. Controlling robots with spoken commands

    SciTech Connect

    Beugelsdijk, T.; Phelan, P.

    1987-10-01

    A robotic system for handling radioactive materials has been developed at Los Alamos National Laboratory. Because of safety considerations, the robot must be under the control of a human operator continuously. In this paper we describe the implementation of a voice-recognition system that makes such control possible, yet permits the robot to perform preprogrammed manipulations without the operator's intervention. We also describe the training given both the operator and the voice recognition-system, as well as practical problems encountered during routine operation. A speech synthesis unit connected to the robot's control computer provides audible feedback to the operator. Thus, when a task is completed or if an emergency develops, the computer provides an appropriate spoken message. Implementation and operation of this commercially available hardware are discussed.

  18. American-built hardware for ASPT undergoes pre-delivery preparations

    NASA Image and Video Library

    1974-09-11

    S74-28295 (September 1974) --- American-built hardware for the joint U.S.-USSR Apollo-Soyuz Test Project mission undergoes pre-delivery preparations in the giant clean room at Rockwell International Corporation?s Space Division at Downey, California. The U.S. portion of the ASTP docking system is in the right foreground. In the right background is the cylindrical-shaped docking module, which is designed to link the Apollo and Soyuz spacecraft when they dock in Earth orbit next summer. In the left background is the Apollo Command Module which they will carry the three American astronauts into Earth orbit. Photo credit: NASA

  19. American-built hardware for ASPT undergoes pre-delivery preparations

    NASA Technical Reports Server (NTRS)

    1974-01-01

    American-built hardware for the joint U.S.-USSR Apollo Soyuz Test Project (ASTP) mission undergoes pre-delivery preparations in the giant clean room at Rockwell International Corporation's Space Division at Downey, California. The U.S. portion of the ASTP docking system is in the right foreground. In the right background is the cylindrical-shaped Docking Module, which is designed to link the Apollo and Soyuz spacecraft when they dock in Earth orbit. In the left background is the Apollo Command Module which will carry the three American astronauts into Earth orbit.

  20. 32 CFR 700.1056 - Command of a ship.

    Code of Federal Regulations, 2013 CFR

    2013-07-01

    ... 32 National Defense 5 2013-07-01 2013-07-01 false Command of a ship. 700.1056 Section 700.1056... Command Detail to Duty § 700.1056 Command of a ship. (a) The officer detailed to command a commissioned ship shall be an officer of the line in the Navy eligible for command at sea. (b) The officer detailed...

  1. 32 CFR 700.1056 - Command of a ship.

    Code of Federal Regulations, 2010 CFR

    2010-07-01

    ... 32 National Defense 5 2010-07-01 2010-07-01 false Command of a ship. 700.1056 Section 700.1056... Command Detail to Duty § 700.1056 Command of a ship. (a) The officer detailed to command a commissioned ship shall be an officer of the line in the Navy eligible for command at sea. (b) The officer detailed...

  2. 32 CFR 700.1056 - Command of a ship.

    Code of Federal Regulations, 2011 CFR

    2011-07-01

    ... 32 National Defense 5 2011-07-01 2011-07-01 false Command of a ship. 700.1056 Section 700.1056... Command Detail to Duty § 700.1056 Command of a ship. (a) The officer detailed to command a commissioned ship shall be an officer of the line in the Navy eligible for command at sea. (b) The officer detailed...

  3. 32 CFR 700.1056 - Command of a ship.

    Code of Federal Regulations, 2012 CFR

    2012-07-01

    ... 32 National Defense 5 2012-07-01 2012-07-01 false Command of a ship. 700.1056 Section 700.1056... Command Detail to Duty § 700.1056 Command of a ship. (a) The officer detailed to command a commissioned ship shall be an officer of the line in the Navy eligible for command at sea. (b) The officer detailed...

  4. 32 CFR 700.1056 - Command of a ship.

    Code of Federal Regulations, 2014 CFR

    2014-07-01

    ... 32 National Defense 5 2014-07-01 2014-07-01 false Command of a ship. 700.1056 Section 700.1056... Command Detail to Duty § 700.1056 Command of a ship. (a) The officer detailed to command a commissioned ship shall be an officer of the line in the Navy eligible for command at sea. (b) The officer detailed...

  5. Relating Downlink Data Products to Uplink Commands

    NASA Technical Reports Server (NTRS)

    Backes, Paul; Norris, Jeffrey; Powell, Mark

    2003-01-01

    An improved data-labeling system provides for automatic association of data products of an exploratory robot (downlink information) with previously transmitted commands (uplink information) that caused the robot to gather the data. Such association is essential to correct and timely analysis of the data products -- including, for example, association of the data with the correct targets. The system was developed for use on Mars Rover missions during the next few years. The system could also be adapted to terrestrial exploratory telerobots for which delays between commands and data returns are long enough to give rise to questions as to which commands resulted in which data returns. The main advantage of this system over prior data-labeling systems is that given a downlink data product, the uplink command and sequence hierarchy that produced it are automatically provided, and given an uplink sequence and command, the downlink data products that it produced are automatically provided.

  6. Autonomous Command Operation of the WIRE Spacecraft

    NASA Technical Reports Server (NTRS)

    Prior, Mike; Walyus, Keith; Saylor, Rick

    1999-01-01

    This paper presents the end-to-end design architecture for an autonomous commanding capability to be used on the Wide Field Infrared Explorer (WIRE) mission for the uplink of command loads during unattended station contacts. The WIRE mission is the fifth and final mission of NASA's Goddard Space Flight Center Small Explorer (SMEX) series to be launched in March of 1999. Its primary mission is the targeting of deep space fields using an ultra-cooled infrared telescope. Due to its mission design WIRE command loads are large (approximately 40 Kbytes per 24 hours) and must be performed daily. To reduce the cost of mission operations support that would be required in order to uplink command loads, the WIRE Flight Operations Team has implemented an autonomous command loading capability. This capability allows completely unattended operations over a typical two-day weekend period.

  7. Power Efficient Hardware Architecture of SHA-1 Algorithm for Trusted Mobile Computing

    NASA Astrophysics Data System (ADS)

    Kim, Mooseop; Ryou, Jaecheol

    The Trusted Mobile Platform (TMP) is developed and promoted by the Trusted Computing Group (TCG), which is an industry standard body to enhance the security of the mobile computing environment. The built-in SHA-1 engine in TMP is one of the most important circuit blocks and contributes the performance of the whole platform because it is used as key primitives supporting platform integrity and command authentication. Mobile platforms have very stringent limitations with respect to available power, physical circuit area, and cost. Therefore special architecture and design methods for low power SHA-1 circuit are required. In this paper, we present a novel and efficient hardware architecture of low power SHA-1 design for TMP. Our low power SHA-1 hardware can compute 512-bit data block using less than 7,000 gates and has a power consumption about 1.1 mA on a 0.25μm CMOS process.

  8. Veggie and the VEG-01 Hardware Validation Test

    NASA Technical Reports Server (NTRS)

    Massa, Gioia; wheeler, Ray; Smith, Trent

    2015-01-01

    This presentation presents a brief overview of KSC plant science hardware for space and then details the Veggie hardware and the VEG-01 hardware validation test. The test results and future plans are discussed.

  9. Hardware Testing and System Evaluation: Procedures to Evaluate Commodity Hardware for Production Clusters

    SciTech Connect

    Goebel, J

    2004-02-27

    Without stable hardware any program will fail. The frustration and expense of supporting bad hardware can drain an organization, delay progress, and frustrate everyone involved. At Stanford Linear Accelerator Center (SLAC), we have created a testing method that helps our group, SLAC Computer Services (SCS), weed out potentially bad hardware and purchase the best hardware at the best possible cost. Commodity hardware changes often, so new evaluations happen periodically each time we purchase systems and minor re-evaluations happen for revised systems for our clusters, about twice a year. This general framework helps SCS perform correct, efficient evaluations. This article outlines SCS's computer testing methods and our system acceptance criteria. We expanded the basic ideas to other evaluations such as storage, and we think the methods outlined in this article has helped us choose hardware that is much more stable and supportable than our previous purchases. We have found that commodity hardware ranges in quality, so systematic method and tools for hardware evaluation were necessary. This article is based on one instance of a hardware purchase, but the guidelines apply to the general problem of purchasing commodity computer systems for production computational work.

  10. Speech Understanding in Noise in the Bison Command, Control, Communications and Intelligence (C3I) Mobile Command Post (MCP)

    DTIC Science & Technology

    2010-12-01

    Speech Understanding in Noise in the Bison Command, Control, Communications and Intelligence ( Bison C3I) Mobile Command Post...2010-169 December 2010 Speech Understanding in Noise in the Bison Command, Control, Communications and Intelligence ( Bison ...loudspeakers or a headset used in the Bison Command, Control, Communications and Intelligence ( Bison C3I) mobile command post (MCP). The messages were

  11. NAVSPASUR sensor system digital signal processing receiver. Volume 1: Hardware and software overview

    NASA Astrophysics Data System (ADS)

    Morris, Carl J.; Bryant, Carolyn F.; Earl, Marilyn P.; Myers, Tamara A.

    1993-09-01

    This is a system description of the Naval Space Surveillance (NAVSPASUR) Sensor System Digital Signal Processing Receiver (DSPR). The NAVSPASUR system began as an advanced research project in June 1958, was commissioned as an operational Naval command in February 1961, and is operated by the Naval Space Surveillance Center (NSSC) in Dahlgren, Virginia. The DSPR is a real-time radar data acquisition and analysis system. Its function is to detect, with no prior information, all space objects whose orbits cross the continental United States and to compute their subsequent orbits. It provides vital satellite information in support of national defense mission objectives of space intelligence, satellite attack warning, satellite intercept support, and space mission support. This system description was prepared as part of a modernization program that has replaced DSPR hardware for which parts are no longer available. Volume 1 (NRL/FR/8154--93-9577) describes the DSPR system in terms of current operation and hardware and software environment. Functions of the major subsystems and the relationship between them are discussed. Volume 2 (NRL/FR/8154--93-9578) discusses the function and capabilities of software and hardware components of the subsystems that provide the digital functions of the DSPR. For each subsystem, individual software modules and hardware components used primarily by that subsystem are described.

  12. Development of display design and command usage guidelines for Spacelab experiment computer applications

    NASA Technical Reports Server (NTRS)

    Dodson, D. W.; Shields, N. L., Jr.

    1979-01-01

    Individual Spacelab experiments are responsible for developing their CRT display formats and interactive command scenarios for payload crew monitoring and control of experiment operations via the Spacelab Data Display System (DDS). In order to enhance crew training and flight operations, it was important to establish some standardization of the crew/experiment interface among different experiments by providing standard methods and techniques for data presentation and experiment commanding via the DDS. In order to establish optimum usage guidelines for the Spacelab DDS, the capabilities and limitations of the hardware and Experiment Computer Operating System design had to be considered. Since the operating system software and hardware design had already been established, the Display and Command Usage Guidelines were constrained to the capabilities of the existing system design. Empirical evaluations were conducted on a DDS simulator to determine optimum operator/system interface utilization of the system capabilities. Display parameters such as information location, display density, data organization, status presentation and dynamic update effects were evaluated in terms of response times and error rates.

  13. Symptomatic Hardware Removal After First Tarsometatarsal Arthrodesis.

    PubMed

    Peterson, Kyle S; McAlister, Jeffrey E; Hyer, Christopher F; Thompson, John

    2016-01-01

    Severe hallux valgus deformity with proximal instability creates pain and deformity in the forefoot. First tarsometatarsal joint arthrodesis is performed to reduce the intermetatarsal angle and stabilize the joint. Dorsomedial locking plate fixation with adjunctive lag screw fixation is used because of its superior construct strength and healing rate. Despite this, questions remain regarding whether this hardware is more prominent and more likely to need removal. The purpose of the present study was to determine the incidence of symptomatic hardware at the first tarsometatarsal joint and to determine the incidence of hardware removal resulting from prominence and/or discomfort. A review of 165 medical records of consecutive patients who had undergone first tarsometatarsal joint arthrodesis with plate fixation was conducted. The outcome of interest was the incidence of symptomatic hardware removal in patients with clinical union. The mean age was 55 (range 18.4 to 78.8) years. The mean follow-up duration was 65.9 ± 34.0 (range 7.0 to 369.0) weeks. In our cohort, 25 patients (15.2%) had undergone hardware removed because of pain and irritation. Of these patients, 18 (72.0%) had a locking plate and lag screw removed, and 7 (28.0%) had crossing lag screws removed. The fixation of a first tarsometatarsal joint fusion poses a difficult situation owing to minimal soft tissue coverage and the inherent need for robust fixation to promote fusion. Hardware can become prominent postoperatively and can become painful and/or induce cutaneous compromise. The results of the present observational investigation imply that surgeons can reasonably inform patients that the incidence of symptomatic hardware removal after first tarsometatarsal arthrodesis is approximately 15% within a median duration of 9.0 months after surgery. Copyright © 2016 American College of Foot and Ankle Surgeons. Published by Elsevier Inc. All rights reserved.

  14. VEG-01: Veggie Hardware Verification Testing

    NASA Technical Reports Server (NTRS)

    Massa, Gioia; Newsham, Gary; Hummerick, Mary; Morrow, Robert; Wheeler, Raymond

    2013-01-01

    The Veggie plant/vegetable production system is scheduled to fly on ISS at the end of2013. Since much of the technology associated with Veggie has not been previously tested in microgravity, a hardware validation flight was initiated. This test will allow data to be collected about Veggie hardware functionality on ISS, allow crew interactions to be vetted for future improvements, validate the ability of the hardware to grow and sustain plants, and collect data that will be helpful to future Veggie investigators as they develop their payloads. Additionally, food safety data on the lettuce plants grown will be collected to help support the development of a pathway for the crew to safely consume produce grown on orbit. Significant background research has been performed on the Veggie plant growth system, with early tests focusing on the development of the rooting pillow concept, and the selection of fertilizer, rooting medium and plant species. More recent testing has been conducted to integrate the pillow concept into the Veggie hardware and to ensure that adequate water is provided throughout the growth cycle. Seed sanitation protocols have been established for flight, and hardware sanitation between experiments has been studied. Methods for shipping and storage of rooting pillows and the development of crew procedures and crew training videos for plant activities on-orbit have been established. Science verification testing was conducted and lettuce plants were successfully grown in prototype Veggie hardware, microbial samples were taken, plant were harvested, frozen, stored and later analyzed for microbial growth, nutrients, and A TP levels. An additional verification test, prior to the final payload verification testing, is desired to demonstrate similar growth in the flight hardware and also to test a second set of pillows containing zinnia seeds. Issues with root mat water supply are being resolved, with final testing and flight scheduled for later in 2013.

  15. Command and Data Handling Branch Internship

    NASA Technical Reports Server (NTRS)

    Billings, Rachel Mae

    2016-01-01

    Modular Integrated Stackable Layers (MISL) is a computer system designed for simple, fast, and cost effective flexible reconfiguration in space environments such as the ISS and Orion projects for various uses. Existing applications include wireless and wired communications, data acquisition and instrumentation, and camera systems, and potential applications include bus protocol converters and subsystem control. MISL is based on Texas Instruments (TI)' MSP430 16-bit ultra-low-power microcontroller device. The purpose of my project was to integrate the MISL system with a liquid crystal display (LCD) touchscreen. The LCD, manufactured by Crystalfontz and part number CFAF320240F-035T-TS, is a 320 by 240 RGB resistive color screen including an optional carrier board. The vast majority of the project was done with Altium Designer, a tool for printed circuit board (PCB) schematic capture, 3D design, and FPGA (Field Programmable Gate Array) development. The new PCB was to allow the LCD to directly stack to the rest of MISL. Research was done with datasheets for the TI microcontroller and touchscreen display in order to meet desired hardware specifications. Documentation on prior MISL projects was also utilized. The initial step was to create a schematic for the LCD, power bus, and data bus connections between components. A layout was then designed with the required physical dimensions, routed traces and vias, power and ground planes, layer stacks, and other specified design rules such as plane clearance and hole size. Multiple consultation sessions were held with Hester Yim, the technical discipline lead for the Command and Data Handling Branch, and Christy Herring, the lead PCB layout designer in the Electronic Design and Manufacturing Branch in order to ensure proper configuration. At the moment, the PCB is awaiting revision by the latter-mentioned branch. Afterwards, the board will begin to undergo the manufacturing and testing process. Throughout the internship at

  16. Cortical commands in active touch.

    PubMed

    Brecht, Michael

    2006-01-01

    The neocortex is an enormous network of extensively interconnected neurons. It has become clear that the computations performed by individual cortical neurons will critically depend on the quantitative composition of cortical activity. Here we discuss quantitative aspects of cortical activity and modes of cortical processing in the context of rodent active touch. Through in vivo whole-cell recordings one observes widespread subthreshold and very sparse evoked action potential (AP) activity in the somatosensory cortex both for passive whisker deflection in anaesthetized animals and during active whisker movements in awake animals. Neurons of the somatosensory cortex become either suppressed during whisking or activated by an efference copy of whisker movement signal that depolarize cells at certain phases of the whisking cycle. To probe the read out of cortical motor commands we applied intracellular stimulation in rat whisker motor cortex. We find that APs in individual cortical neurons can evoke long sequences of small whisker movements. The capacity of an individual neuron to evoke movements is most astonishing given the large number of neurons in whisker motor cortex. Thus, few cortical APs may suffice to control motor behaviour and such APs can be translated into action with the utmost precision. We conclude that there is very widespread subthreshold cortical activity and very sparse, highly specific cortical AP activity.

  17. Detail of west wall of south wing of commandant's house ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    Detail of west wall of south wing of commandant's house with scale Fort Simcoe commandant's house & blockhouse - Fort Simcoe, Commandant's House & Blockhouse, Fort Simcoe Road, White Swan, Yakima County, WA

  18. 14 CFR 1214.703 - Chain of command.

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... Shuttle Commander § 1214.703 Chain of command. (a) The Commander is a career NASA astronaut who has been.... (b) The pilot is a career NASA astronaut who has been designated to serve as the pilot on a...

  19. 14 CFR 1214.703 - Chain of command.

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... Shuttle Commander § 1214.703 Chain of command. (a) The Commander is a career NASA astronaut who has been.... (b) The pilot is a career NASA astronaut who has been designated to serve as the pilot on a...

  20. Expedition 33/34 Change of Command Ceremony

    NASA Image and Video Library

    Expedition 33 Commander Suni Williams hands over station command to Expedition 34 Commander Kevin Ford in a ceremony that took place Saturday Nov. 17, 2012. Williams returned to Earth with two crew...

  1. Astronaut John Young in Command Module Simulator during Apollo Simulation

    NASA Technical Reports Server (NTRS)

    1968-01-01

    Astronaut John W. Young, command module pilot, inside the Command Module Simulator in bldg 5 during an Apollo Simulation. Astronauts Thomas P. Stafford, commander and Eugene A. Cernan, lunar module pilot are out of the view.

  2. Three astronauts inside Command Module Simulator during Apollo Simulation

    NASA Technical Reports Server (NTRS)

    1968-01-01

    Three astronauts inside the Command Module Simulator in bldg 5 during an Apollo Simulation. Left to right are Astronauts Thomas P. Stafford, commander; John W. Young, command module pilot; and Eugene A. Cernan, lunar module pilot.

  3. Astronauts Prepare for Mission With Virtual Reality Hardware

    NASA Technical Reports Server (NTRS)

    2001-01-01

    Astronauts John M. Grunsfeld (left), STS-109 payload commander, and Nancy J. Currie, mission specialist, use the virtual reality lab at Johnson Space Center to train for upcoming duties aboard the Space Shuttle Columbia. This type of computer interface paired with virtual reality training hardware and software helps to prepare the entire team to perform its duties for the fourth Hubble Space Telescope Servicing mission. The most familiar form of virtual reality technology is some form of headpiece, which fits over your eyes and displays a three dimensional computerized image of another place. Turn your head left and right, and you see what would be to your sides; turn around, and you see what might be sneaking up on you. An important part of the technology is some type of data glove that you use to propel yourself through the virtual world. Currently, the medical community is using the new technologies in four major ways: To see parts of the body more accurately, for study, to make better diagnosis of disease and to plan surgery in more detail; to obtain a more accurate picture of a procedure during surgery; to perform more types of surgery with the most noninvasive, accurate methods possible; and to model interactions among molecules at a molecular level.

  4. Astronaut Prepares for Mission With Virtual Reality Hardware

    NASA Technical Reports Server (NTRS)

    2001-01-01

    Astronaut John M. Grunsfeld, STS-109 payload commander, uses virtual reality hardware at Johnson Space Center to rehearse some of his duties prior to the STS-109 mission. The most familiar form of virtual reality technology is some form of headpiece, which fits over your eyes and displays a three dimensional computerized image of another place. Turn your head left and right, and you see what would be to your sides; turn around, and you see what might be sneaking up on you. An important part of the technology is some type of data glove that you use to propel yourself through the virtual world. This technology allows NASA astronauts to practice International Space Station work missions in advance. Currently, the medical community is using the new technologies in four major ways: To see parts of the body more accurately, for study, to make better diagnosis of disease and to plan surgery in more detail; to obtain a more accurate picture of a procedure during surgery; to perform more types of surgery with the most noninvasive, accurate methods possible; and to model interactions among molecules at a molecular level.

  5. Essential SpaceWire Hardware Capabilities for a Robust Network

    NASA Technical Reports Server (NTRS)

    Birmingham, Michael; Krimchansky, Alexander; Anderson, William; Lombardi, Matthew

    2016-01-01

    The Geostationary Operational Environmental Satellite R-Series Program (GOES-R) mission is a joint program between National Oceanic & Atmospheric Administration (NOAA) and National Aeronautics & Space Administration (NASA) Goddard Space Flight Center (GSFC). GOES-R project selected SpaceWire as the best solution to satisfy the desire for simple and flexible instrument to spacecraft command and telemetry communications. GOES-R development and integration is complete and the observatory is scheduled for launch October 2016. The spacecraft design was required to support redundant SpaceWire links for each instrument side, as well as to route the fewest number of connections through a Slip Ring Assembly necessary to support Solar pointing instruments. The final design utilized two different router designs. The SpaceWire standard alone does not ensure the most practical or reliable network. On GOES-R a few key hardware capabilities were identified that merit serious consideration for future designs. Primarily these capabilities address persistent port stalls and the prevention of receive buffer overflows. Workarounds were necessary to overcome shortcomings that could be avoided in future designs if they utilize the capabilities, discussed in this paper, above and beyond the requirements of the SpaceWire standard.

  6. Astronauts Prepare for Mission With Virtual Reality Hardware

    NASA Technical Reports Server (NTRS)

    2001-01-01

    Astronauts John M. Grunsfeld (left), STS-109 payload commander, and Nancy J. Currie, mission specialist, use the virtual reality lab at Johnson Space Center to train for upcoming duties aboard the Space Shuttle Columbia. This type of computer interface paired with virtual reality training hardware and software helps to prepare the entire team to perform its duties for the fourth Hubble Space Telescope Servicing mission. The most familiar form of virtual reality technology is some form of headpiece, which fits over your eyes and displays a three dimensional computerized image of another place. Turn your head left and right, and you see what would be to your sides; turn around, and you see what might be sneaking up on you. An important part of the technology is some type of data glove that you use to propel yourself through the virtual world. Currently, the medical community is using the new technologies in four major ways: To see parts of the body more accurately, for study, to make better diagnosis of disease and to plan surgery in more detail; to obtain a more accurate picture of a procedure during surgery; to perform more types of surgery with the most noninvasive, accurate methods possible; and to model interactions among molecules at a molecular level.

  7. Astronaut Prepares for Mission With Virtual Reality Hardware

    NASA Technical Reports Server (NTRS)

    2001-01-01

    Astronaut John M. Grunsfeld, STS-109 payload commander, uses virtual reality hardware at Johnson Space Center to rehearse some of his duties prior to the STS-109 mission. The most familiar form of virtual reality technology is some form of headpiece, which fits over your eyes and displays a three dimensional computerized image of another place. Turn your head left and right, and you see what would be to your sides; turn around, and you see what might be sneaking up on you. An important part of the technology is some type of data glove that you use to propel yourself through the virtual world. This technology allows NASA astronauts to practice International Space Station work missions in advance. Currently, the medical community is using the new technologies in four major ways: To see parts of the body more accurately, for study, to make better diagnosis of disease and to plan surgery in more detail; to obtain a more accurate picture of a procedure during surgery; to perform more types of surgery with the most noninvasive, accurate methods possible; and to model interactions among molecules at a molecular level.

  8. Relation between command hallucinations and dangerous behavior.

    PubMed

    Rudnick, A

    1999-01-01

    This article presents an updated review of studies on the relation between command hallucinations and dangerous behavior. The author reviewed all studies published between 1966 and 1997 according to MEDLINE and between 1974 and 1997 according to PSYCLIT. Forty-one studies were found, of which 82.9 percent dealt with the relation between command hallucinations and dangerous behavior. Of these studies, 32.3 percent were controlled, and they were grouped into three partially overlapping classes: those concerned with violent behavior, those concerned with suicidal behavior, and those concerned with mediating variables. Most of these studies agreed on the non-existence of an immediate relation between command hallucinations and dangerous (violent or suicidal) behavior. Even though the studies were divided about the existence of a relation between severity/dangerousness of command content and compliance with the commands, there was agreement about the existence of a direct relation between compliance with commands and both benevolence and familiarity of commanding voice. It seems that the research and knowledge available to date on this subject is both scant and methodologically weak. Future study should probably concentrate on mediating factors, such as appraisal and coping attitudes and behaviors.

  9. Wheel slide protection control using a command map and Smith predictor for the pneumatic brake system of a railway vehicle

    NASA Astrophysics Data System (ADS)

    Lee, Nam-Jin; Kang, Chul-Goo

    2016-10-01

    In railway vehicles, excessive sliding or wheel locking can occur while braking because of a temporarily degraded adhesion between the wheel and the rail caused by the contaminated or wet surface of the rail. It can damage the wheel tread and affect the performance of the brake system and the safety of the railway vehicle. To safeguard the wheelset from these phenomena, almost all railway vehicles are equipped with wheel slide protection (WSP) systems. In this study, a new WSP algorithm is proposed. The features of the proposed algorithm are the use of the target sliding speed, the determination of a command for WSP valves using command maps, and compensation for the time delay in pneumatic brake systems using the Smith predictor. The proposed WSP algorithm was verified using experiments with a hardware-in-the-loop simulation system including the hardware of the pneumatic brake system.

  10. A command and data subsystem for deep space exploration based on the RCA 1802 microprocessor in a distributed configuration

    NASA Technical Reports Server (NTRS)

    Thomas, J. S.

    1980-01-01

    The Command and Data Subsystem (CDS) is an RCA 1802microprocessor based subsystem that acts as the central nervous system for the Galileo Orbiter Spacecraft. All communication between the ground and spacecraft flows through the CDS. The CDS also distributes commands in real time, algorithmetrically expanded from a data base loaded from the ground and in response to spacecraft alarms. The distributed microprocessor system is configured as a redundant set of hardware with three microprocessors on each half. The microprocessors are surrounded by a group of special purpose hardware components which greatly enhance the ability of the software to perform its task. It is shown how the software architecture makes a distributed system of six microprocessors appear to each user as a single virtual machine, and collectively as a set of cooperating virtual machines that prevent the simultaneous presence of the several users from interfering destructively with each other.

  11. Literature review on medical incident command.

    PubMed

    Rimstad, Rune; Braut, Geir Sverre

    2015-04-01

    It is not known what constitutes the optimal emergency management system, nor is there a consensus on how effectiveness and efficiency in emergency response should be measured or evaluated. Literature on the role and tasks of commanders in the prehospital emergency services in the setting of mass-casualty incidents has not been summarized and published. This comprehensive literature review addresses some of the needs for future research in emergency management through three research questions: (1) What are the basic assumptions underlying incident command systems (ICSs)? (2) What are the tasks of ambulance and medical commanders in the field? And (3) How can field commanders' performances be measured and assessed? A systematic literature search in MEDLINE, PubMed, PsycINFO, Embase, Cochrane Central Register of Controlled Trials, Cochrane Library, ISI Web of Science, Scopus, International Security & Counter Terrorism Reference Center, Current Controlled Trials, and PROSPERO covering January 1, 1990 through March 1, 2014 was conducted. Reference lists of included literature were hand searched. Included papers were analyzed using Framework synthesis. The literature search identified 6,049 unique records, of which, 76 articles and books where included in qualitative synthesis. Most ICSs are described commonly as hierarchical, bureaucratic, and based on military principles. These assumptions are contested strongly, as is the applicability of such systems. Linking of the chains of command in cooperating agencies is a basic difficulty. Incident command systems are flexible in the sense that the organization may be expanded as needed. Commanders may command by direction, by planning, or by influence. Commanders' tasks may be summarized as: conducting scene assessment, developing an action plan, distributing resources, monitoring operations, and making decisions. There is considerable variation between authors in nomenclature and what tasks are included or highlighted

  12. Command History. 1969. Volume 3. Sanitized

    DTIC Science & Technology

    1969-01-01

    support of USG activities also found great importance in connection with the real estate requirements of our n’ilitary units. (U) The fol*owing is...RCS CINCPAC 5000-4) SEE DISTRIBUTION 1. The USMACV 1969 Command History (Volume III) is promulgated in response to CINCPAC Instruction 5000. 5B, 15 ...30 12 & 13 DEPT OF THE NAVY 31 thru 40 6 & 7 DEPT OF THE AIR FORCE 41 thru 50 14 & 15 COMMANDANT, USMC 51 thru 55 10 & 11 COMMANDANT, USCG 56 & 57

  13. Krikalev with TVIS hardware in Zvezda

    NASA Image and Video Library

    2005-09-07

    ISS011-E-12494 (7 September 2005) --- Cosmonaut Sergei K. Krikalev, Expedition 11 commander representing Russia's Federal Space Agency, works with the Treadmill Vibration Isolation System (TVIS) during In-Flight Maintenance (IFM) in the Zvezda Service Module of the International Space Station.

  14. View northwest of commander's office for Philadelphia Naval Base. ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    View northwest of commander's office for Philadelphia Naval Base. - Naval Base Philadelphia-Philadelphia Naval Shipyard, Commander's Office-Naval Base, League Island, Philadelphia, Philadelphia County, PA

  15. Office of Command Security Total Quality Management Plan

    DTIC Science & Technology

    1989-07-01

    outlines the Office of Command Security instruction for TQM implementation. Keywords: TQM ( Total Quality Management ), DLA Office of Command Security, Continuous process improvement, Automatic data processing security.

  16. ISS Update: Station Command and Data Handling System

    NASA Image and Video Library

    NASA Public Affairs Officer Kylie Clem interviews ODIN flight controller Amy Brezinski, who monitors and commands the Command and Data Handling System for the International Space Station. Brezinski...

  17. Economic impact of syndesmosis hardware removal.

    PubMed

    Lalli, Trapper A J; Matthews, Leslie J; Hanselman, Andrew E; Hubbard, David F; Bramer, Michelle A; Santrock, Robert D

    2015-09-01

    Ankle syndesmosis injuries are commonly seen with 5-10% of sprains and 10% of ankle fractures involving injury to the ankle syndesmosis. Anatomic reduction has been shown to be the most important predictor of clinical outcomes. Optimal surgical management has been a subject of debate in the literature. The method of fixation, number of screws, screw size, and number of cortices are all controversial. Postoperative hardware removal has also been widely debated in the literature. Some surgeons advocate for elective hardware removal prior to resuming full weightbearing. Returning to the operating room for elective hardware removal results in increased cost to the patient, potential for infection or complication(s), and missed work days for the patient. Suture button devices and bioabsorbable screw fixation present other options, but cortical screw fixation remains the gold standard. This retrospective review was designed to evaluate the economic impact of a second operative procedure for elective removal of 3.5mm cortical syndesmosis screws. Two hundred and two patients with ICD-9 code for "open treatment of distal tibiofibular joint (syndesmosis) disruption" were identified. The medical records were reviewed for those who underwent elective syndesmosis hardware removal. The primary outcome measurements included total hospital billing charges and total hospital billing collection. Secondary outcome measurements included average individual patient operative costs and average operating room time. Fifty-six patients were included in the study. Our institution billed a total of $188,271 (USD) and collected $106,284 (55%). The average individual patient operating room cost was $3579. The average operating room time was 67.9 min. To the best of our knowledge, no study has previously provided cost associated with syndesmosis hardware removal. Our study shows elective syndesmosis hardware removal places substantial economic burden on both the patient and the healthcare system

  18. Extravehicular Activity training and hardware design considerations

    NASA Technical Reports Server (NTRS)

    Thuot, Pierre J.; Harbaugh, Gregory J.

    1993-01-01

    Designing hardware that can be successfully operated by EVA astronauts for EVA tasks required to assemble and maintain Space Station Freedom requires a thorough understanding of human factors and of the capabilities and limitations of the space-suited astronaut, as well as of the effect of microgravity environment on the crew member's capabilities and on the overhead associated with EVA. This paper describes various training methods and facilities that are being designed for training EVA astronauts for Space Station assembly and maintenance, taking into account the above discussed factors. Particular attention is given to the user-friendly hardware design for EVA and to recent EVA flight experience.

  19. Quantum neuromorphic hardware for quantum artificial intelligence

    NASA Astrophysics Data System (ADS)

    Prati, Enrico

    2017-08-01

    The development of machine learning methods based on deep learning boosted the field of artificial intelligence towards unprecedented achievements and application in several fields. Such prominent results were made in parallel with the first successful demonstrations of fault tolerant hardware for quantum information processing. To which extent deep learning can take advantage of the existence of a hardware based on qubits behaving as a universal quantum computer is an open question under investigation. Here I review the convergence between the two fields towards implementation of advanced quantum algorithms, including quantum deep learning.

  20. Magnetic Field Apparatus (MFA) Hardware Test

    NASA Technical Reports Server (NTRS)

    Anderson, Ken; Boody, April; Reed, Dave; Wang, Chung; Stuckey, Bob; Cox, Dave

    1999-01-01

    The objectives of this study are threefold: (1) Provide insight into water delivery in microgravity and determine optimal germination paper wetting for subsequent seed germination in microgravity; (2) Observe the behavior of water exposed to a strong localized magnetic field in microgravity; and (3) Simulate the flow of fixative (using water) through the hardware. The Magnetic Field Apparatus (MFA) is a new piece of hardware slated to fly on the Space Shuttle in early 2001. MFA is designed to expose plant tissue to magnets in a microgravity environment, deliver water to the plant tissue, record photographic images of plant tissue, and deliver fixative to the plant tissue.

  1. Circulation control lift generation experiment: Hardware development

    NASA Technical Reports Server (NTRS)

    Panontin, T. L.

    1985-01-01

    A circulation control airfoil and its accompanying hardware were developed to allow the investigation of lift generation that is independent of airfoil angle of attack and relative flow velocity. The test equipment, designed for use in a water tunnel, includes the blown airfoil, the support systems for both flow visualization and airfoil load measurement, and the fluid control system, which utilizes hydraulic technology. The primary design tasks, the selected solutions, and the unforseen problems involved in the development of these individual components of hardware are described.

  2. Language of CTO interventions - Focus on hardware.

    PubMed

    Mishra, Sundeep

    2016-01-01

    The knowledge of variety of chronic total occlusion (CTO) hardware and the ability to use them represents the key to success of any CTO interventions. However, the multiplicity of CTO hardware and their physical character and the terminology used by experts create confusion in the mind of an average interventional cardiologist, particularly a beginner in this field. This knowledge is available but is scattered. We aim to classify and compare the currently used devices based on their properties focusing on how physical character of each device can be utilized in a specific situation, thus clarifying and simplifying the technical discourse. Copyright © 2016. Published by Elsevier B.V.

  3. Human Centered Hardware Modeling and Collaboration

    NASA Technical Reports Server (NTRS)

    Stambolian Damon; Lawrence, Brad; Stelges, Katrine; Henderson, Gena

    2013-01-01

    In order to collaborate engineering designs among NASA Centers and customers, to in clude hardware and human activities from multiple remote locations, live human-centered modeling and collaboration across several sites has been successfully facilitated by Kennedy Space Center. The focus of this paper includes innovative a pproaches to engineering design analyses and training, along with research being conducted to apply new technologies for tracking, immersing, and evaluating humans as well as rocket, vehic le, component, or faci lity hardware utilizing high resolution cameras, motion tracking, ergonomic analysis, biomedical monitoring, wor k instruction integration, head-mounted displays, and other innovative human-system integration modeling, simulation, and collaboration applications.

  4. Marshall Tests Experiment Hardware in New Glovebox

    NASA Technical Reports Server (NTRS)

    2002-01-01

    This excellent shot of Marshall Space Flight Center's (MSFC's) Mark Whorton, testing experiment hardware in the Microgravity Science Glovebox Ground Unit delivered to MSFC on August 30, 2002, reveals a close look at the components inside of the Glovebox. The unit is being used at Marshall's Microgravity Development Laboratory to test experiment hardware before it is installed in the flight Glovebox aboard the International Space Station (ISS) U.S. Laboratory Module, Destiny. The glovebox is a sealed container with built in gloves on its sides and fronts that enables astronauts to work safely with experiments that involve fluids, flames, particles, and fumes that need to be safely contained.

  5. Hardware accelerator for genomic sequence alignment.

    PubMed

    Chiang, Jason; Studniberg, Michael; Shaw, Jack; Seto, Shaw; Truong, Kevin

    2006-01-01

    To infer homology and subsequently gene function, the Smith-Waterman algorithm is used to find the optimal local alignment between two sequences. When searching sequence databases that may contain billions of sequences, this algorithm becomes computationally expensive. Consequently, in this paper, we focused on accelerating the Smith-Waterman algorithm by modifying the computationally repeated portion of the algorithm by FPGA hardware custom instructions. These simple modifications accelerated the algorithm runtime by an average of 287% compared to the pure software implementation. Therefore, further design of FPGA accelerated hardware offers a promising direction to seeking runtime improvement of genomic database searching.

  6. Magnetic Field Apparatus (MFA) Hardware Test

    NASA Technical Reports Server (NTRS)

    Anderson, Ken; Boody, April; Reed, Dave; Wang, Chung; Stuckey, Bob; Cox, Dave

    1999-01-01

    The objectives of this study are threefold: (1) Provide insight into water delivery in microgravity and determine optimal germination paper wetting for subsequent seed germination in microgravity; (2) Observe the behavior of water exposed to a strong localized magnetic field in microgravity; and (3) Simulate the flow of fixative (using water) through the hardware. The Magnetic Field Apparatus (MFA) is a new piece of hardware slated to fly on the Space Shuttle in early 2001. MFA is designed to expose plant tissue to magnets in a microgravity environment, deliver water to the plant tissue, record photographic images of plant tissue, and deliver fixative to the plant tissue.

  7. Software Technology for Adaptable, Reliable Systems (STARS) (User Manual). Ada Command Environment (ACE) Version 8.0 Sun OS Implementation

    DTIC Science & Technology

    1990-10-29

    LIMITATION OF ABSTRACT OF REPORT OF THIS PAGE OF ABSTRACT TASK: UR20 CDRL: 00980 29 October 1990 USER MANUAL For The SOFTWARE TECHNOLOGY FOR...Octobei � USER MANUAL For The SOFTWARE TECHNOLOGY FOR ADAPTABLE, RELIABLE SYSTEMS (STARS) Ada Command Environment (ACE) Version 8.0 SunOS...4 4 Software and Hardware Environment 4 4.1 Sun Workstation .. .. .. ... ... ... ... ... ... ... ... ..... 5 5 Pragmas Supported

  8. Command profile for Galileo scan platform control

    NASA Astrophysics Data System (ADS)

    Man, G. K.; Breckenridge, W. G.

    1981-08-01

    A recursive command profile is developed for the control of a two-degree-of-freedom scan platform mounted on a flexible structure. Perfect sensors and actuators are assumed for development and testing, and structural vibrations are minimized by actuator torque commands following a smooth torque-time profile. The integral of the smooth torque profile, the rate profile, is recursively generated by a piecewise constant second derivation, and the torque applied by the closk actuator is divided into three components. Results show that the smooth platform motion in response to the command profiles is what the Galileo control systems needs to avoid stator structural vibrations. Position, rate and acceleration profiles are also presented, and the resulting motion of the scan platform in response to command profiles is illustrated.

  9. Commander Truly cleans ARS filters on middeck

    NASA Image and Video Library

    1983-09-05

    STS008-13-336 (5 Sept 1983) --- On middeck, Richard M. Truly, STS-8 commander, uses vacuum cleaner to remove debris from air revitalization system (ARS) filter assembly. Open panel on middeck floor is the ARS access panel.

  10. Station Commander Captures Unprecedented View of Comet

    NASA Image and Video Library

    International Space Station Commander Dan Burbank captured spectacular imagery of Comet Lovejoy as seen from about 240 miles above the Earth’s horizon on Wednesday, Dec. 21. Burbank described se...

  11. Spacecraft command and control using expert systems

    NASA Astrophysics Data System (ADS)

    Norcross, Scott; Grieser, William H.

    1994-11-01

    This paper describes a product called the Intelligent Mission Toolkit (IMT), which was created to meet the changing demands of the spacecraft command and control market. IMT is a command and control system built upon an expert system. Its primary functions are to send commands to the spacecraft and process telemetry data received from the spacecraft. It also controls the ground equipment used to support the system, such as encryption gear, and telemetry front-end equipment. Add-on modules allow IMT to control antennas and antenna interface equipment. The design philosophy for IMT is to utilize available commercial products wherever possible. IMT utilizes Gensym's G2 Real-time Expert System as the core of the system. G2 is responsible for overall system control, spacecraft commanding control, and spacecraft telemetry analysis and display. Other commercial products incorporated into IMT include the SYBASE relational database management system and Loral Test and Integration Systems' System 500 for telemetry front-end processing.

  12. Commander De Wine poses for a photo

    NASA Image and Video Library

    2009-11-08

    ISS021-E-022397 (8 Nov. 2009) --- European Space Agency astronaut Frank De Winne, Expedition 21 commander, holds a stowage bag containing various beverages in the Unity node of the International Space Station.

  13. Spacecraft command and control using expert systems

    NASA Technical Reports Server (NTRS)

    Norcross, Scott; Grieser, William H.

    1994-01-01

    This paper describes a product called the Intelligent Mission Toolkit (IMT), which was created to meet the changing demands of the spacecraft command and control market. IMT is a command and control system built upon an expert system. Its primary functions are to send commands to the spacecraft and process telemetry data received from the spacecraft. It also controls the ground equipment used to support the system, such as encryption gear, and telemetry front-end equipment. Add-on modules allow IMT to control antennas and antenna interface equipment. The design philosophy for IMT is to utilize available commercial products wherever possible. IMT utilizes Gensym's G2 Real-time Expert System as the core of the system. G2 is responsible for overall system control, spacecraft commanding control, and spacecraft telemetry analysis and display. Other commercial products incorporated into IMT include the SYBASE relational database management system and Loral Test and Integration Systems' System 500 for telemetry front-end processing.

  14. Apollo 9 Mission image - Command Module

    NASA Image and Video Library

    1969-03-03

    The Apollo 9 Command/Service Modules photographed through the window from the Lunar Module,"Spider",on the fifth day of the Apollo 9 earth-orbital mission. Docking mechanism is visible in nose of the Command Module,"Gumdrop". Film magazine was F, film type was SO-368 Ektachrome with 0.460 - 0.710 micrometers film / filter transmittance response and haze filter,80mm lens

  15. Database Migration for Command and Control

    DTIC Science & Technology

    2002-11-01

    collection of information is estibated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources ...Transportat ion Enterprise (DTE) ..................42 2.2.4 Recommendations...f ou r commande r s t o command and cont ro l ae rospace forces . The i r Aerospace Opera t ions Cen te r s wi l l be ab le to

  16. Schema for Spacecraft-Command Dictionary

    NASA Technical Reports Server (NTRS)

    Laubach, Sharon; Garcia, Celina; Maxwell, Scott; Wright, Jesse

    2008-01-01

    An Extensible Markup Language (XML) schema was developed as a means of defining and describing a structure for capturing spacecraft command- definition and tracking information in a single location in a form readable by both engineers and software used to generate software for flight and ground systems. A structure defined within this schema is then used as the basis for creating an XML file that contains command definitions.

  17. Commander Ken Bowersox films activity in Spacelab

    NASA Image and Video Library

    1995-11-02

    STS073-230-014 (20 October - 5 November 1995) --- Astronaut Kenneth D. Bowersox, STS-73 mission commander, uses a camcorder to record United States Microgravity Laboratory 2 (USML-2) activities onboard the Space Shuttle Columbia. Nearby, astronaut Kathryn C. Thornton, payload commander, prepares to open a supply chest to support one of many science experiments conducted by the seven-member crew during the 16-day USML-2 flight.

  18. Embedding Mission Command in Army Culture

    DTIC Science & Technology

    2013-03-01

    is imperative given the current and future operating environment. Further underscoring this premise are lessons learned from a decade of war that...leaders accustomed to operating with autonomy , pose a threat to the Army’s ability to fulfill the promise of mission command. Given these dynamics...lessons learned from a decade of war that highlight mission command as a key factor in the success of counter- insurgency operations in Iraq and

  19. Resilient Organizational Architectures for Command and Control

    DTIC Science & Technology

    2014-07-03

    34 Operations Department, Naval War College, Newport, RI, 2009. [38] C. D. Dalton, "Systemic Operational Design: Epistemological Bumpf or the Way Ahead for...Semantic Web, Social Networks and Multiagent Systems, pp. 528-539, 2009. [49] J. Hanna, "Course of Action Simulation Analysis," Science ...2012. [59] A. H. Levis, "A Colored Petri Net Model of Command and Control Nodes," in Toward a Science of Command Control and Communications, Carl R

  20. Cyber Situational Awareness for Joint Force Commanders

    DTIC Science & Technology

    2012-02-15

    Officer assigned to the Air War College, Air University, Maxwell AFB, AL. Lt Col Payne is a graduate of Ohio University with a Bachelor of Science...manner. The central thesis being addressed is that military commanders need a common framework for cyber situation awareness in order to aid the force...The central thesis being addressed is that military commanders need a common framework for cyber SA in order to aid the force with building a

  1. Special Forces Command and Control in Afghanistan

    DTIC Science & Technology

    2007-11-02

    Johann Price, in a web site article, provides a detailed account of the chain of command from the beginning of Operation Enduring Freedom to 1 June 2002...soldiers who were nothing but successful. The song, The Green Beret by SGT Barry Sadler, was a hit on the top music charts. The first Medal of Honor...DC: National Defense University Press. Price, Johann , ed. 2002. Operation Enduring Freedom Chain of Command. Center of Defense information, 26 June

  2. Command Philosophy: The Secret of Organizational Leadership

    DTIC Science & Technology

    1989-03-01

    contemporary leadership issues. It confronts compx social problems, such as sexual harassment, drug and alcohol abuse, and racial disharmony. Specifically...already. Figure Fourteen provides an abbreviated analysis of the survey (see appendix A for the questionaire ). FIGURE 14 DIMENSIONS: COMMAND PHILOSOPHY...written command philosophies have better units in terms of organizational health . So why the hesitation? Certainly, it is personal: even the AWC 1989

  3. Command and Control Vulnerabilities to Communications Jamming

    DTIC Science & Technology

    2013-01-01

    nuclear communications survivability and essential, highest-level command and control. The approach was heavily focused on getting Air Force cadets...toward the “ Arma - geddon” context and did not significantly influence tactical requirements. During Operation Desert Storm in 1991, laser-guided bombs...communica- tions below the highest levels of requirements of nuclear command and control is starting to wend its way into the thinking of military

  4. Command and Control for War and Peace

    DTIC Science & Technology

    1992-01-01

    Office Washington, DO 20402 ISBN 00-a18.000337.3 PTo QUAIJTTY BFOrn COMMAND AND CONTROL FOR WAR AND PEACE I.. S-.... . . . . . . . . . . COMMAND AND...32-91.00045, NDU Press publications are sold by the U,S. Government Printing Office , For ordering information, call (209) 788.5328, or write to...Superintendent of Documents, U,S, Government Printing Office , Washington, D,C, 20402. Library of Congress Cataloging.In-Publiestion Data Coakley, Thomas P

  5. Commander - Unit Psychologist: A Powerful Tandem

    DTIC Science & Technology

    2006-04-01

    which I spent in the operational environment of MND CJTF- 7. All of You should know how “significant” are two years old knowledge and information for...operational deployment in MND- CM helped me to understand the fundamental differences between the demanded qualities of a commander in peacetime and during...commanders on the platoon level. I helped them to realize the differences in understanding the mission (money, interest, discover new places). So my

  6. STS-29 Commander Coats in commanders seat on OV-103's forward flight deck

    NASA Technical Reports Server (NTRS)

    1989-01-01

    Commander Michael L. Coats, smiling, looks up from his work at the commanders station on Discovery's, Orbiter Vehicle (OV) 103's, forward flight deck. While in the commanders seat, Coats updates the STS-29 crew activity plan (CAP). Appearing around him are seat back with parachute harness, forward control panels with empty beverage container velcroed to panel F6, checklist clipped to panel O1, and portable laptop computer setup on top of panel F7.

  7. Quick response airborne command post communications

    NASA Astrophysics Data System (ADS)

    Blaisdell, Randy L.

    1988-08-01

    National emergencies and strategic crises come in all forms and sizes ranging from natural disasters at one end of the scale up to and including global nuclear warfare at the other. Since the early 1960s the U.S. Government has spent billions of dollars fielding airborne command posts to ensure continuity of government and the command and control function during times of theater conventional, theater nuclear, and global nuclear warfare. Unfortunately, cost has prevented the extension of the airborne command post technology developed for these relatively unlikely events to the lower level, though much more likely to occur, crises such as natural disasters, terrorist acts, political insurgencies, etc. This thesis proposes the implementation of an economical airborne command post concept to address the wide variety of crises ignored by existing military airborne command posts. The system is known as the Quick Response Airborne Command Post (QRAC Post) and is based on the exclusive use of commercially owned and operated aircraft, and commercially available automated data processing and communications resources. The thesis addresses the QRAC Post concept at a systems level and is primarily intended to demonstrate how current technology can be exploited to economically achieve a national objective.

  8. Intelligent systems and advanced user interfaces for design, operation, and maintenance of command management systems

    NASA Technical Reports Server (NTRS)

    Potter, William J.; Mitchell, Christine M.

    1993-01-01

    Historically, command management systems (CMS) have been large and expensive spacecraft-specific software systems that were costly to build, operate, and maintain. Current and emerging hardware, software, and user interface technologies may offer an opportunity to facilitate the initial formulation and design of a spacecraft-specific CMS as well as to develop a more generic CMS system. New technologies, in addition to a core CMS common to a range of spacecraft, may facilitate the training and enhance the efficiency of CMS operations. Current mission operations center (MOC) hardware and software include Unix workstations, the C/C++ programming languages, and an X window interface. This configuration provides the power and flexibility to support sophisticated and intelligent user interfaces that exploit state-of-the-art technologies in human-machine interaction, artificial intelligence, and software engineering. One of the goals of this research is to explore the extent to which technologies developed in the research laboratory can be productively applied in a complex system such as spacecraft command management. Initial examination of some of these issues in CMS design and operation suggests that application of technologies such as intelligent planning, case-based reasoning, human-machine systems design and analysis tools (e.g., operator and designer models), and human-computer interaction tools (e.g., graphics, visualization, and animation) may provide significant savings in the design, operation, and maintenance of the CMS for a specific spacecraft as well as continuity for CMS design and development across spacecraft. The first six months of this research saw a broad investigation by Georgia Tech researchers into the function, design, and operation of current and planned command management systems at Goddard Space Flight Center. As the first step, the researchers attempted to understand the current and anticipated horizons of command management systems at Goddard

  9. Digital Hardware Design Teaching: An Alternative Approach

    ERIC Educational Resources Information Center

    Benkrid, Khaled; Clayton, Thomas

    2012-01-01

    This article presents the design and implementation of a complete review of undergraduate digital hardware design teaching in the School of Engineering at the University of Edinburgh. Four guiding principles have been used in this exercise: learning-outcome driven teaching, deep learning, affordability, and flexibility. This has identified…

  10. Design considerations for space flight hardware

    NASA Technical Reports Server (NTRS)

    Glover, Daniel

    1990-01-01

    The environmental and design constraints are reviewed along with some insight into the established design and quality assurance practices that apply to low earth orbit (LEO) space flight hardware. It is intended as an introduction for people unfamiliar with space flight considerations. Some basic data and a bibliography are included.

  11. Computer hardware for radiologists: Part I.

    PubMed

    Indrajit, Ik; Alam, A

    2010-08-01

    Computers are an integral part of modern radiology practice. They are used in different radiology modalities to acquire, process, and postprocess imaging data. They have had a dramatic influence on contemporary radiology practice. Their impact has extended further with the emergence of Digital Imaging and Communications in Medicine (DICOM), Picture Archiving and Communication System (PACS), Radiology information system (RIS) technology, and Teleradiology. A basic overview of computer hardware relevant to radiology practice is presented here. The key hardware components in a computer are the motherboard, central processor unit (CPU), the chipset, the random access memory (RAM), the memory modules, bus, storage drives, and ports. The personnel computer (PC) has a rectangular case that contains important components called hardware, many of which are integrated circuits (ICs). The fiberglass motherboard is the main printed circuit board and has a variety of important hardware mounted on it, which are connected by electrical pathways called "buses". The CPU is the largest IC on the motherboard and contains millions of transistors. Its principal function is to execute "programs". A Pentium(®) 4 CPU has transistors that execute a billion instructions per second. The chipset is completely different from the CPU in design and function; it controls data and interaction of buses between the motherboard and the CPU. Memory (RAM) is fundamentally semiconductor chips storing data and instructions for access by a CPU. RAM is classified by storage capacity, access speed, data rate, and configuration.

  12. Environmental Control System Software & Hardware Development

    NASA Technical Reports Server (NTRS)

    Vargas, Daniel Eduardo

    2017-01-01

    ECS hardware: (1) Provides controlled purge to SLS Rocket and Orion spacecraft. (2) Provide mission-focused engineering products and services. ECS software: (1) NASA requires Compact Unique Identifiers (CUIs); fixed-length identifier used to identify information items. (2) CUI structure; composed of nine semantic fields that aid the user in recognizing its purpose.

  13. Formal hardware verification of digital circuits

    NASA Technical Reports Server (NTRS)

    Joyce, J.; Seger, C.-J.

    1991-01-01

    The use of formal methods to verify the correctness of digital circuits is less constrained by the growing complexity of digital circuits than conventional methods based on exhaustive simulation. This paper briefly outlines three main approaches to formal hardware verification: symbolic simulation, state machine analysis, and theorem-proving.

  14. Shuttle mission simulator hardware conceptual design report

    NASA Technical Reports Server (NTRS)

    Burke, J. F.

    1973-01-01

    The detailed shuttle mission simulator hardware requirements are discussed. The conceptual design methods, or existing technology, whereby those requirements will be fulfilled are described. Information of a general nature on the total design problem plus specific details on how these requirements are to be satisfied are reported. The configuration of the simulator is described and the capabilities for various types of training are identified.

  15. Digital Hardware Design Teaching: An Alternative Approach

    ERIC Educational Resources Information Center

    Benkrid, Khaled; Clayton, Thomas

    2012-01-01

    This article presents the design and implementation of a complete review of undergraduate digital hardware design teaching in the School of Engineering at the University of Edinburgh. Four guiding principles have been used in this exercise: learning-outcome driven teaching, deep learning, affordability, and flexibility. This has identified…

  16. Computer hardware for radiologists: Part I

    PubMed Central

    Indrajit, IK; Alam, A

    2010-01-01

    Computers are an integral part of modern radiology practice. They are used in different radiology modalities to acquire, process, and postprocess imaging data. They have had a dramatic influence on contemporary radiology practice. Their impact has extended further with the emergence of Digital Imaging and Communications in Medicine (DICOM), Picture Archiving and Communication System (PACS), Radiology information system (RIS) technology, and Teleradiology. A basic overview of computer hardware relevant to radiology practice is presented here. The key hardware components in a computer are the motherboard, central processor unit (CPU), the chipset, the random access memory (RAM), the memory modules, bus, storage drives, and ports. The personnel computer (PC) has a rectangular case that contains important components called hardware, many of which are integrated circuits (ICs). The fiberglass motherboard is the main printed circuit board and has a variety of important hardware mounted on it, which are connected by electrical pathways called “buses”. The CPU is the largest IC on the motherboard and contains millions of transistors. Its principal function is to execute “programs”. A Pentium® 4 CPU has transistors that execute a billion instructions per second. The chipset is completely different from the CPU in design and function; it controls data and interaction of buses between the motherboard and the CPU. Memory (RAM) is fundamentally semiconductor chips storing data and instructions for access by a CPU. RAM is classified by storage capacity, access speed, data rate, and configuration. PMID:21042437

  17. Microprocessor Design Using Hardware Description Language

    ERIC Educational Resources Information Center

    Mita, Rosario; Palumbo, Gaetano

    2008-01-01

    The following paper has been conceived to deal with the contents of some lectures aimed at enhancing courses on digital electronic, microelectronic or VLSI systems. Those lectures show how to use a hardware description language (HDL), such as the VHDL, to specify, design and verify a custom microprocessor. The general goal of this work is to teach…

  18. Microprocessor Design Using Hardware Description Language

    ERIC Educational Resources Information Center

    Mita, Rosario; Palumbo, Gaetano

    2008-01-01

    The following paper has been conceived to deal with the contents of some lectures aimed at enhancing courses on digital electronic, microelectronic or VLSI systems. Those lectures show how to use a hardware description language (HDL), such as the VHDL, to specify, design and verify a custom microprocessor. The general goal of this work is to teach…

  19. Experiences with Prototype InfiniBand Hardware

    SciTech Connect

    SCHUTT, JAMES A.

    2001-11-01

    This report describes testing of prototype InfiniBand{trademark} host channel adapters from Intel Corporation, using the Linux(reg sign) operating system. Three generations of prototype hardware were obtained, and Linux device drivers were written which exercised the data movement capabilities of the cards. Latency and throughput results obtained were similar to other SAN technologies, but not significantly better.

  20. Transistor Level Circuit Experiments using Evolvable Hardware

    NASA Technical Reports Server (NTRS)

    Stoica, A.; Zebulum, R. S.; Keymeulen, D.; Ferguson, M. I.; Daud, Taher; Thakoor, A.

    2005-01-01

    The Jet Propulsion Laboratory (JPL) performs research in fault tolerant, long life, and space survivable electronics for the National Aeronautics and Space Administration (NASA). With that focus, JPL has been involved in Evolvable Hardware (EHW) technology research for the past several years. We have advanced the technology not only by simulation and evolution experiments, but also by designing, fabricating, and evolving a variety of transistor-based analog and digital circuits at the chip level. EHW refers to self-configuration of electronic hardware by evolutionary/genetic search mechanisms, thereby maintaining existing functionality in the presence of degradations due to aging, temperature, and radiation. In addition, EHW has the capability to reconfigure itself for new functionality when required for mission changes or encountered opportunities. Evolution experiments are performed using a genetic algorithm running on a DSP as the reconfiguration mechanism and controlling the evolvable hardware mounted on a self-contained circuit board. Rapid reconfiguration allows convergence to circuit solutions in the order of seconds. The paper illustrates hardware evolution results of electronic circuits and their ability to perform under 230 C temperature as well as radiations of up to 250 kRad.

  1. Postflight hardware evaluation (RSRM-29, STS-54)

    NASA Astrophysics Data System (ADS)

    1993-09-01

    This document is the final report for the Clearfield disassembly evaluation and a continuation of the KSC postflight assessment for the RSRM-29 flight set. All observed hardware conditions were documented on PFOR's and are included in Appendices A, B, and C. Appendices D and E contain the measurements and safety factor data for the nozzle and insulation components. This report, along with the KSC Ten-Day Postflight Hardware Evaluation Report (TWR-64221), represents a summary of the RSRM-29 hardware evaluation. Disassembly evaluation photograph numbers are logged in TWA-1990. The RSRM-29 flight set disassembly evaluations described in this document were performed at the RSRM Refurbishment Facility in Clearfield, Utah. The final factory joint demate occurred on September 9, 1993. Detailed evaluations were performed in accordance with the Clearfield PEEP, TWR-50051, Revision A. All observations were compared against limits that are also defined in the PEEP. These limits outline the criteria for categorizing the observations as acceptable, reportable, or critical. Hardware conditions that were unexpected and/or determined to be reportable or critical were evaluated by the applicable CPT and tracked through the PFAR system.

  2. Support for Diagnosis of Custom Computer Hardware

    NASA Technical Reports Server (NTRS)

    Molock, Dwaine S.

    2008-01-01

    The Coldfire SDN Diagnostics software is a flexible means of exercising, testing, and debugging custom computer hardware. The software is a set of routines that, collectively, serve as a common software interface through which one can gain access to various parts of the hardware under test and/or cause the hardware to perform various functions. The routines can be used to construct tests to exercise, and verify the operation of, various processors and hardware interfaces. More specifically, the software can be used to gain access to memory, to execute timer delays, to configure interrupts, and configure processor cache, floating-point, and direct-memory-access units. The software is designed to be used on diverse NASA projects, and can be customized for use with different processors and interfaces. The routines are supported, regardless of the architecture of a processor that one seeks to diagnose. The present version of the software is configured for Coldfire processors on the Subsystem Data Node processor boards of the Solar Dynamics Observatory. There is also support for the software with respect to Mongoose V, RAD750, and PPC405 processors or their equivalents.

  3. An avionics scenario and command model description for Space Generic Open Avionics Architecture (SGOAA)

    NASA Technical Reports Server (NTRS)

    Stovall, John R.; Wray, Richard B.

    1994-01-01

    This paper presents a description of a model for a space vehicle operational scenario and the commands for avionics. This model will be used in developing a dynamic architecture simulation model using the Statemate CASE tool for validation of the Space Generic Open Avionics Architecture (SGOAA). The SGOAA has been proposed as an avionics architecture standard to NASA through its Strategic Avionics Technology Working Group (SATWG) and has been accepted by the Society of Automotive Engineers (SAE) for conversion into an SAE Avionics Standard. This architecture was developed for the Flight Data Systems Division (FDSD) of the NASA Johnson Space Center (JSC) by the Lockheed Engineering and Sciences Company (LESC), Houston, Texas. This SGOAA includes a generic system architecture for the entities in spacecraft avionics, a generic processing external and internal hardware architecture, and a nine class model of interfaces. The SGOAA is both scalable and recursive and can be applied to any hierarchical level of hardware/software processing systems.

  4. Test Telemetry And Command System (TTACS)

    NASA Technical Reports Server (NTRS)

    Fogel, Alvin J.

    1994-01-01

    The Jet Propulsion Laboratory has developed a multimission Test Telemetry and Command System (TTACS) which provides a multimission telemetry and command data system in a spacecraft test environment. TTACS reuses, in the spacecraft test environment, components of the same data system used for flight operations; no new software is developed for the spacecraft test environment. Additionally, the TTACS is transportable to any spacecraft test site, including the launch site. The TTACS is currently operational in the Galileo spacecraft testbed; it is also being provided to support the Cassini and Mars Surveyor Program projects. Minimal personnel data system training is required in the transition from pre-launch spacecraft test to post-launch flight operations since test personnel are already familiar with the data system's operation. Additionally, data system components, e.g. data display, can be reused to support spacecraft software development; and the same data system components will again be reused during the spacecraft integration and system test phases. TTACS usage also results in early availability of spacecraft data to data system development and, as a result, early data system development feedback to spacecraft system developers. The TTACS consists of a multimission spacecraft support equipment interface and components of the multimission telemetry and command software adapted for a specific project. The TTACS interfaces to the spacecraft, e.g., Command Data System (CDS), support equipment. The TTACS telemetry interface to the CDS support equipment performs serial (RS-422)-to-ethernet conversion at rates between 1 bps and 1 mbps, telemetry data blocking and header generation, guaranteed data transmission to the telemetry data system, and graphical downlink routing summary and control. The TTACS command interface to the CDS support equipment is nominally a command file transferred in non-real-time via ethernet. The CDS support equipment is responsible for

  5. Hardware Algorithm Implementation for Mission Specific Processing

    DTIC Science & Technology

    2008-03-01

    developed and fabricated before it can get into the hands of the customer. The design to market can take up to 1-2 years depending on the technology and the...positioning systems, radar systems, and different communication devices. These devices, being mobile or not, are required for them to operate in the...field and communicate with Command and Control. For this reason it is essential that these libraries be built and perfected. With any circuit design

  6. 32 CFR 700.1058 - Command of a submarine.

    Code of Federal Regulations, 2012 CFR

    2012-07-01

    ... 32 National Defense 5 2012-07-01 2012-07-01 false Command of a submarine. 700.1058 Section 700... Command Detail to Duty § 700.1058 Command of a submarine. The officer detailed to command a submarine... submarines....

  7. 32 CFR 700.1058 - Command of a submarine.

    Code of Federal Regulations, 2013 CFR

    2013-07-01

    ... 32 National Defense 5 2013-07-01 2013-07-01 false Command of a submarine. 700.1058 Section 700... Command Detail to Duty § 700.1058 Command of a submarine. The officer detailed to command a submarine... submarines....

  8. 32 CFR 700.1058 - Command of a submarine.

    Code of Federal Regulations, 2014 CFR

    2014-07-01

    ... 32 National Defense 5 2014-07-01 2014-07-01 false Command of a submarine. 700.1058 Section 700... Command Detail to Duty § 700.1058 Command of a submarine. The officer detailed to command a submarine... submarines....

  9. 32 CFR 700.1058 - Command of a submarine.

    Code of Federal Regulations, 2011 CFR

    2011-07-01

    ... 32 National Defense 5 2011-07-01 2011-07-01 false Command of a submarine. 700.1058 Section 700... Command Detail to Duty § 700.1058 Command of a submarine. The officer detailed to command a submarine... submarines....

  10. 32 CFR 700.1054 - Command of a naval base.

    Code of Federal Regulations, 2010 CFR

    2010-07-01

    ... 32 National Defense 5 2010-07-01 2010-07-01 false Command of a naval base. 700.1054 Section 700.1054 National Defense Department of Defense (Continued) DEPARTMENT OF THE NAVY UNITED STATES NAVY... Command Detail to Duty § 700.1054 Command of a naval base. The officer detailed to command a naval...

  11. 46 CFR 147.5 - Commandant (CG-522); address.

    Code of Federal Regulations, 2010 CFR

    2010-10-01

    ... 46 Shipping 5 2010-10-01 2010-10-01 false Commandant (CG-522); address. 147.5 Section 147.5... General Provisions § 147.5 Commandant (CG-522); address. Commandant (CG-522) is the Office of Operating... Commandant (CG-522), U.S. Coast Guard Headquarters, 2100 2nd St. SW., Stop 7126, Washington, DC...

  12. 46 CFR 147.5 - Commandant (CG-522); address.

    Code of Federal Regulations, 2011 CFR

    2011-10-01

    ... 46 Shipping 5 2011-10-01 2011-10-01 false Commandant (CG-522); address. 147.5 Section 147.5... General Provisions § 147.5 Commandant (CG-522); address. Commandant (CG-522) is the Office of Operating... Commandant (CG-522), U.S. Coast Guard Headquarters, 2100 2nd St. SW., Stop 7126, Washington, DC...

  13. 32 CFR 700.1058 - Command of a submarine.

    Code of Federal Regulations, 2010 CFR

    2010-07-01

    ... 32 National Defense 5 2010-07-01 2010-07-01 false Command of a submarine. 700.1058 Section 700... Command Detail to Duty § 700.1058 Command of a submarine. The officer detailed to command a submarine... submarines....

  14. 32 CFR 700.1054 - Command of a naval base.

    Code of Federal Regulations, 2014 CFR

    2014-07-01

    ... 32 National Defense 5 2014-07-01 2014-07-01 false Command of a naval base. 700.1054 Section 700.1054 National Defense Department of Defense (Continued) DEPARTMENT OF THE NAVY UNITED STATES NAVY... Command Detail to Duty § 700.1054 Command of a naval base. The officer detailed to command a naval...

  15. 32 CFR 700.1054 - Command of a naval base.

    Code of Federal Regulations, 2013 CFR

    2013-07-01

    ... 32 National Defense 5 2013-07-01 2013-07-01 false Command of a naval base. 700.1054 Section 700.1054 National Defense Department of Defense (Continued) DEPARTMENT OF THE NAVY UNITED STATES NAVY... Command Detail to Duty § 700.1054 Command of a naval base. The officer detailed to command a naval...

  16. 32 CFR 700.1054 - Command of a naval base.

    Code of Federal Regulations, 2012 CFR

    2012-07-01

    ... 32 National Defense 5 2012-07-01 2012-07-01 false Command of a naval base. 700.1054 Section 700.1054 National Defense Department of Defense (Continued) DEPARTMENT OF THE NAVY UNITED STATES NAVY... Command Detail to Duty § 700.1054 Command of a naval base. The officer detailed to command a naval...

  17. 32 CFR 700.1054 - Command of a naval base.

    Code of Federal Regulations, 2011 CFR

    2011-07-01

    ... 32 National Defense 5 2011-07-01 2011-07-01 false Command of a naval base. 700.1054 Section 700.1054 National Defense Department of Defense (Continued) DEPARTMENT OF THE NAVY UNITED STATES NAVY... Command Detail to Duty § 700.1054 Command of a naval base. The officer detailed to command a naval...

  18. Maritime Homeland Command Control: Teaching an Old Dog New Tricks

    DTIC Science & Technology

    2002-02-04

    Security, Command and Control, Navy, Coast Guard, Customs Service, Centralized Control, Decentralized Execution, Organization by Objectives 15.Abstract...primarily responsible for the maritime homeland, the Navy, the Coast guard, the Customs Service, should provide resources and command capabilities to a...Coast Guard, the Customs Service, should provide resources and command capabilities to a unified command and control structure. Coast Guard forces and

  19. Hardware Description of Mass Weather Dissemination System Exploratory Engineering Model.

    DTIC Science & Technology

    1982-09-01

    resets the UART DAVI to zero. This pulse also serves to provide the external command strobe ( TRIGO ) to the Lanier control logic. When the mass weather...of the command nibble to header control (C). This pulse also causes TRIGO to go low to provide a command strobe so that the Lanier control logic will...modifies rewind command to listen RTEI Ready tone enable SIN Serial input - RS-232C SOUT Serial output - RS-232C TRIGO Trigger - strobe to transfer

  20. Codem: software/hardware codesign for embedded multicore systems supporting hardware services

    NASA Astrophysics Data System (ADS)

    Wang, Chao; Li, Xi; Zhou, Xuehai; Nedjah, Nadia; Wang, Aili

    2015-01-01

    Efficient software/hardware codesign is posing significant challenges to embedded systems. This paper proposes Codem, a software/hardware codesign flow for embedded systems, which models both processors and Intellectual Property (IP) cores as services. Tasks are regarded as abstract instructions which can be scheduled to IP cores for parallel execution automatically. In order to guide the hardware implementations of the hot spot functions, this paper incorporates a novel hot spot-based profiling technique to observe the hot spot functions while the application is being simulated. Furthermore, based on the hot spot of various applications, an adaptive mapping algorithm is presented to partition the application into multiple software/hardware tasks. We test the profiling-based design flow with classic Sort applications. Experimental results demonstrate that Codem can efficiently help researchers to identify the hot spots, and also outline a new direction to combine profiling techniques with state-of-the-art reconfigurable computing platforms for specific task acceleration.

  1. Life sciences flight hardware development for the International Space Station

    NASA Astrophysics Data System (ADS)

    Kern, V. D.; Bhattacharya, S.; Bowman, R. N.; Donovan, F. M.; Elland, C.; Fahlen, T. F.; Girten, B.; Kirven-Brooks, M.; Lagel, K.; Meeker, G. B.; Santos, O.

    During the construction phase of the International Space Station (ISS), early flight opportunities have been identified (including designated Utilization Flights, UF) on which early science experiments may be performed. The focus of NASA's and other agencies' biological studies on the early flight opportunities is cell and molecular biology; with UF-1 scheduled to fly in fall 2001, followed by flights 8A and UF-3. Specific hardware is being developed to verify design concepts, e.g., the Avian Development Facility for incubation of small eggs and the Biomass Production System for plant cultivation. Other hardware concepts will utilize those early research opportunities onboard the ISS, e.g., an Incubator for sample cultivation, the European Modular Cultivation System for research with small plant systems, an Insect Habitat for support of insect species. Following the first Utilization Flights, additional equipment will be transported to the ISS to expand research opportunities and capabilities, e.g., a Cell Culture Unit, the Advanced Animal Habitat for rodents, an Aquatic Facility to support small fish and aquatic specimens, a Plant Research Unit for plant cultivation, and a specialized Egg Incubator for developmental biology studies. Host systems (Figure 1A, B), e.g., a 2.5 m Centrifuge Rotor (g-levels from 0.01-g to 2-g) for direct comparisons between μg and selectable g levels, the Life Sciences Glove☐ for contained manipulations, and Habitat Holding Racks (Figure 1B) will provide electrical power, communication links, and cooling to the habitats. Habitats will provide food, water, light, air and waste management as well as humidity and temperature control for a variety of research organisms. Operators on Earth and the crew on the ISS will be able to send commands to the laboratory equipment to monitor and control the environmental and experimental parameters inside specific habitats. Common laboratory equipment such as microscopes, cryo freezers, radiation

  2. 46 CFR 42.05-25 - Coast Guard District Commander or District Commander.

    Code of Federal Regulations, 2011 CFR

    2011-10-01

    ... 46 Shipping 2 2011-10-01 2011-10-01 false Coast Guard District Commander or District Commander. 42.05-25 Section 42.05-25 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) LOAD LINES DOMESTIC AND FOREIGN VOYAGES BY SEA Definition of Terms Used in This Subchapter § 42.05-25 Coast Guard...

  3. 46 CFR 42.05-25 - Coast Guard District Commander or District Commander.

    Code of Federal Regulations, 2012 CFR

    2012-10-01

    ... 46 Shipping 2 2012-10-01 2012-10-01 false Coast Guard District Commander or District Commander. 42.05-25 Section 42.05-25 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) LOAD LINES DOMESTIC AND FOREIGN VOYAGES BY SEA Definition of Terms Used in This Subchapter § 42.05-25 Coast Guard...

  4. 46 CFR 42.05-25 - Coast Guard District Commander or District Commander.

    Code of Federal Regulations, 2014 CFR

    2014-10-01

    ... 46 Shipping 2 2014-10-01 2014-10-01 false Coast Guard District Commander or District Commander. 42.05-25 Section 42.05-25 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) LOAD LINES DOMESTIC AND FOREIGN VOYAGES BY SEA Definition of Terms Used in This Subchapter § 42.05-25 Coast Guard...

  5. 46 CFR 42.05-25 - Coast Guard District Commander or District Commander.

    Code of Federal Regulations, 2013 CFR

    2013-10-01

    ... 46 Shipping 2 2013-10-01 2013-10-01 false Coast Guard District Commander or District Commander. 42.05-25 Section 42.05-25 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) LOAD LINES DOMESTIC AND FOREIGN VOYAGES BY SEA Definition of Terms Used in This Subchapter § 42.05-25 Coast Guard...

  6. 46 CFR 50.10-5 - Coast Guard District Commander or District Commander.

    Code of Federal Regulations, 2011 CFR

    2011-10-01

    ... 46 Shipping 2 2011-10-01 2011-10-01 false Coast Guard District Commander or District Commander. 50.10-5 Section 50.10-5 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) MARINE ENGINEERING GENERAL PROVISIONS Definition of Terms Used in This Subchapter § 50.10-5 Coast Guard District...

  7. 46 CFR 50.10-5 - Coast Guard District Commander or District Commander.

    Code of Federal Regulations, 2010 CFR

    2010-10-01

    ... 46 Shipping 2 2010-10-01 2010-10-01 false Coast Guard District Commander or District Commander. 50.10-5 Section 50.10-5 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) MARINE ENGINEERING GENERAL PROVISIONS Definition of Terms Used in This Subchapter § 50.10-5 Coast Guard District...

  8. 46 CFR 50.10-5 - Coast Guard District Commander or District Commander.

    Code of Federal Regulations, 2014 CFR

    2014-10-01

    ... 46 Shipping 2 2014-10-01 2014-10-01 false Coast Guard District Commander or District Commander. 50.10-5 Section 50.10-5 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) MARINE ENGINEERING GENERAL PROVISIONS Definition of Terms Used in This Subchapter § 50.10-5 Coast Guard District...

  9. 46 CFR 50.10-5 - Coast Guard District Commander or District Commander.

    Code of Federal Regulations, 2013 CFR

    2013-10-01

    ... 46 Shipping 2 2013-10-01 2013-10-01 false Coast Guard District Commander or District Commander. 50.10-5 Section 50.10-5 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) MARINE ENGINEERING GENERAL PROVISIONS Definition of Terms Used in This Subchapter § 50.10-5 Coast Guard District...

  10. 46 CFR 42.05-25 - Coast Guard District Commander or District Commander.

    Code of Federal Regulations, 2010 CFR

    2010-10-01

    ... 46 Shipping 2 2010-10-01 2010-10-01 false Coast Guard District Commander or District Commander. 42.05-25 Section 42.05-25 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) LOAD LINES DOMESTIC AND FOREIGN VOYAGES BY SEA Definition of Terms Used in This Subchapter § 42.05-25 Coast Guard...

  11. 46 CFR 50.10-5 - Coast Guard District Commander or District Commander.

    Code of Federal Regulations, 2012 CFR

    2012-10-01

    ... 46 Shipping 2 2012-10-01 2012-10-01 false Coast Guard District Commander or District Commander. 50.10-5 Section 50.10-5 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) MARINE ENGINEERING GENERAL PROVISIONS Definition of Terms Used in This Subchapter § 50.10-5 Coast Guard District...

  12. STS-37 Commander Nagel in commanders seat on OV-104's flight deck

    NASA Technical Reports Server (NTRS)

    1991-01-01

    STS-37 Commander Steven R. Nagel, wearing launch and entry suit (LES), sits at commanders station on the forward flight deck of Atlantis, Orbiter Vehicle (OV) 104. Surrounding Nagel are the seat headrest, control panels, checklists, forward flight deck windows, and three drinking water containers with straws attached to forward panel F2.

  13. Joint Command and Control of Cyber Operations: The Joint Force Cyber Component Command (JFCCC)

    DTIC Science & Technology

    2012-05-04

    relies so heavily on complex command and control systems and interconnectivity in general, cyber warfare has become a serious topic of interest at the...defensive cyber warfare into current and future operations and plans. In particular, Joint Task Force (JTF) Commanders must develop an optimum method to

  14. 33 CFR 150.606 - After learning of a possible violation, what does the Sector Commander, or the MSU Commander...

    Code of Federal Regulations, 2013 CFR

    2013-07-01

    ... 33 Navigation and Navigable Waters 2 2013-07-01 2013-07-01 false After learning of a possible violation, what does the Sector Commander, or the MSU Commander, with COTP and OCMI authority do? 150.606....606 After learning of a possible violation, what does the Sector Commander, or the MSU Commander,...

  15. 33 CFR 150.606 - After learning of a possible violation, what does the Sector Commander, or the MSU Commander...

    Code of Federal Regulations, 2014 CFR

    2014-07-01

    ... 33 Navigation and Navigable Waters 2 2014-07-01 2014-07-01 false After learning of a possible violation, what does the Sector Commander, or the MSU Commander, with COTP and OCMI authority do? 150.606....606 After learning of a possible violation, what does the Sector Commander, or the MSU Commander,...

  16. What It Takes. Air Force Command of Joint Operations

    DTIC Science & Technology

    2009-01-01

    ters staff. For the headquarters to reach full functionality, it needs to be augmented with additional staff from both the host service and the other...Operations Command Central SOCPAC Special Operations Command Pacific SOF special operations forces TAC CP tactical command post TACON tactical control ...defines control as 1. Authority that may be less than full command exercised by a commander over part of the activities of subordinate or other

  17. Design guidelines for robotically serviceable hardware

    NASA Technical Reports Server (NTRS)

    Gordon, Scott A.

    1988-01-01

    Research being conducted at the Goddard Space Flight Center into the development of guidelines for the design of robotically serviceable spaceflight hardware is described. A mock-up was built based on an existing spaceflight system demonstrating how these guidelines can be applied to actual hardware. The report examines the basic servicing philosophy being studied and how this philosophy is reflected in the formulation of design guidelines for robotic servicing. A description of the mock-up is presented with emphasis on the design features that make it robot friendly. Three robotic servicing schemes fulfilling the design guidelines were developed for the mock-up. These servicing schemes are examined as to how their implementation was affected by the constraints of the spacecraft system on which the mock-up is based.

  18. HARDWARE AND SOFTWARE STATUS OF QCDOC.

    SciTech Connect

    BOYLE,P.A.; CHEN,D.; CHRIST,N.H.; PETROV.K.; ET AL.

    2003-07-15

    QCDOC is a massively parallel supercomputer whose processing nodes are based on an application-specific integrated circuit (ASIC). This ASIC was custom-designed so that crucial lattice QCD kernels achieve an overall sustained performance of 50% on machines with several 10,000 nodes. This strong scalability, together with low power consumption and a price/performance ratio of $1 per sustained MFlops, enable QCDOC to attack the most demanding lattice QCD problems. The first ASICs became available in June of 2003, and the testing performed so far has shown all systems functioning according to specification. We review the hardware and software status of QCDOC and present performance figures obtained in real hardware as well as in simulation.

  19. Hardware neural network on an SOPC platform

    NASA Astrophysics Data System (ADS)

    Liu, Yifei; Ding, Mingyue; Hu, Xia; Zhou, Yanhong

    2009-10-01

    SOPC (System on Programmable Chip) is an on-chip programmable system based on large scale Field Programmable Arrays (FPGAs). This paper presented an implementation of an SOPC system with a custom hardware neural network using Altera FPGA chip-EP2C35F672C. The embedded Nios processor was used as the test bench. The test result showed that the SOPC Platform with hardware neural network is faster than the software implementation respectively and the accuracy of the design meets the requirement of system. The verified SOPC system can closely model real-world system, which will have wide applications in different areas such as pattern recognition, data mining and signal processing.

  20. Companion Chip: Building a Segregated Hardware Architecture

    NASA Astrophysics Data System (ADS)

    Pareaud, Thomas; Houelle, Alain; Vaucher, Niolas; Albinet, Mathieu; Honvault, Christophe

    2011-08-01

    Partitioning is a more and more mature concept in Space industry. It aims at assuring that some error propagation modes are not possible. This paper gives an overview of an analysis conducted in the frame of a research and technology study performed in 2010/2011. The "Java Companion Chip" study addresses an interesting approach to partitioning using hardware concepts: a SoC architecture integrates a master processor, a companion chip and additional hardware functions aiming at enforcing the time and space segregation between the master processor and the slave one.This paper discusses the benefits and the main challenges of the proposed approach. In addition, it presents an application of these concepts to a case study: a Leon/Java processor architecture able to concurrently execute native and Java applications.

  1. Hardware-Independent Proofs of Numerical Programs

    NASA Technical Reports Server (NTRS)

    Boldo, Sylvie; Nguyen, Thi Minh Tuyen

    2010-01-01

    On recent architectures, a numerical program may give different answers depending on the execution hardware and the compilation. Our goal is to formally prove properties about numerical programs that are true for multiple architectures and compilers. We propose an approach that states the rounding error of each floating-point computation whatever the environment. This approach is implemented in the Frama-C platform for static analysis of C code. Small case studies using this approach are entirely and automatically proved

  2. Verifying Dissolution Of Wax From Hardware Surfaces

    NASA Technical Reports Server (NTRS)

    Montoya, Benjamina G.

    1995-01-01

    Wax removed by cleaning solvent revealed by cooling solution with liquid nitrogen. Such improved procedure and test needed in case of hardware that must be protected by wax during machining or plating but required to be free of wax during subsequent use. Improved cleaning procedure and test take less than 5 minutes. Does not require special skill or equipment and performs at cleaning site. In addition, enables recovery of all cleaning solvent.

  3. Threats and Challenges in Reconfigurable Hardware Security

    DTIC Science & Technology

    2008-07-01

    1996. [15] P. Kocher, J. Jaffe, and B. Jun. Differential power analysis . In Proceedings of Crypto, August 1999. [16] J. I. Lieberman. White paper...1 Introduction Reconfigurable hardware is increasingly being used in sensitive applications. Examples include our national infrastructures ( power ...consumers of the system. The CC describes ten types of assessment required to deter- mine if a system is trustworthy: 1. Analysis and checking of processes

  4. LWH and ACH Helmet Hardware Study

    DTIC Science & Technology

    2015-11-30

    reference nuts is manganese- chromium alloy steel with fine grain structure, consistent with low-alloy steel such as 4140 in a normalized condition. The...different alloy than the reference nuts, which we have not identified. TABLE IV – PRINCIPAL ALLOYING ELEMENTS Hardware Item Manganese wt.% Chromium ... chromium and detecting any other major alloying elements. The principal composition of the reference screws is nominally 1% manganese with traces of

  5. Verifying Dissolution Of Wax From Hardware Surfaces

    NASA Technical Reports Server (NTRS)

    Montoya, Benjamina G.

    1995-01-01

    Wax removed by cleaning solvent revealed by cooling solution with liquid nitrogen. Such improved procedure and test needed in case of hardware that must be protected by wax during machining or plating but required to be free of wax during subsequent use. Improved cleaning procedure and test take less than 5 minutes. Does not require special skill or equipment and performs at cleaning site. In addition, enables recovery of all cleaning solvent.

  6. LWH and ACH Helmet Hardware Study

    DTIC Science & Technology

    2015-11-30

    in the microstructures. 2.3 Hardness Tests on Polished Cross Sections Rockwell hardness ( ASTM E18 Standard Test Methods for Rockwell Hardness of...microhardness measurements ( ASTM E384 Standard Test Method for Microindentation Hardness of Materials) were made on the exterior surfaces of screws...using conventional techniques (e.g. ASTM E3 Preparation of Metallographic Specimens). The hardware pieces were cross- sectioned using a low-speed diamond

  7. Fast Hardware Implementation Of The DOLP Transform

    NASA Astrophysics Data System (ADS)

    Waltz, Frederick M.

    1988-03-01

    The Difference-of-Low-Pass (DOLP) Transform uses a hierarchy of bandpass filters to perform size discrimination and pattern matching of objects and features in a visual field. Like the Discrete Fourier Transform (DFT), it "sorts" entities according to their size or spatial frequencies; but unlike the DFT, it also retains positional information.This positional information is essential for the very common industrial web inspection problem in which a "flaw map" must be produced - mere flaw detection (as provided by the DFT) is not enough. The DOLP Transform is usually implemented using finite-impulse-response difference-of-Gaussian (DOG) filters of progressively increasing kernel size. Various potential industrial applications have been described and demonstrated, but implementations have been hampered by the heavy computational burden involved in the generation of the Transform. This paper describes a fast implementation of Crowley's resampled DOLP Transform using commercially-available board-level hardware. With a moderate investment in hardware modules, a nine-band DOLP Transform can be computed for a 485 by 512 image in about one second. Additional hardware modules could be added to bring the speed up to 30 complete 9-band Transforms per second, if desired. Additional bands beyond the first nine, while seldom needed, require very little additional time, because the image has been repeatedly resampled down to a small size.

  8. Extravehicular activity training and hardware design consideration

    NASA Technical Reports Server (NTRS)

    Thuot, P. J.; Harbaugh, G. J.

    1995-01-01

    Preparing astronauts to perform the many complex extravehicular activity (EVA) tasks required to assemble and maintain Space Station will be accomplished through training simulations in a variety of facilities. The adequacy of this training is dependent on a thorough understanding of the task to be performed, the environment in which the task will be performed, high-fidelity training hardware and an awareness of the limitations of each particular training facility. Designing hardware that can be successfully operated, or assembled, by EVA astronauts in an efficient manner, requires an acute understanding of human factors and the capabilities and limitations of the space-suited astronaut. Additionally, the significant effect the microgravity environment has on the crew members' capabilities has to be carefully considered not only for each particular task, but also for all the overhead related to the task and the general overhead associated with EVA. This paper will describe various training methods and facilities that will be used to train EVA astronauts for Space Station assembly and maintenance. User-friendly EVA hardware design considerations and recent EVA flight experience will also be presented.

  9. Testing Microshutter Arrays Using Commercial FPGA Hardware

    NASA Technical Reports Server (NTRS)

    Rapchun, David

    2008-01-01

    NASA is developing micro-shutter arrays for the Near Infrared Spectrometer (NIRSpec) instrument on the James Webb Space Telescope (JWST). These micro-shutter arrays allow NIRspec to do Multi Object Spectroscopy, a key part of the mission. Each array consists of 62414 individual 100 x 200 micron shutters. These shutters are magnetically opened and held electrostatically. Individual shutters are then programmatically closed using a simple row/column addressing technique. A common approach to provide these data/clock patterns is to use a Field Programmable Gate Array (FPGA). Such devices require complex VHSIC Hardware Description Language (VHDL) programming and custom electronic hardware. Due to JWST's rapid schedule on the development of the micro-shutters, rapid changes were required to the FPGA code to facilitate new approaches being discovered to optimize the array performance. Such rapid changes simply could not be made using conventional VHDL programming. Subsequently, National Instruments introduced an FPGA product that could be programmed through a Labview interface. Because Labview programming is considerably easier than VHDL programming, this method was adopted and brought success. The software/hardware allowed the rapid change the FPGA code and timely results of new micro-shutter array performance data. As a result, numerous labor hours and money to the project were conserved.

  10. Instrument hardware and software upgrades at IPNS

    NASA Astrophysics Data System (ADS)

    Worlton, Thomas; Hammonds, John; Mikkelson, D.; Mikkelson, Ruth; Porter, Rodney; Tao, Julian; Chatterjee, Alok

    2006-11-01

    IPNS is in the process of upgrading their time-of-flight neutron scattering instruments with improved hardware and software. The hardware upgrades include replacing old VAX Qbus and Multibus-based data acquisition systems with new systems based on VXI and VME. Hardware upgrades also include expanded detector banks and new detector electronics. Old VAX Fortran-based data acquisition and analysis software is being replaced with new software as part of the ISAW project. ISAW is written in Java for ease of development and portability, and is now used routinely for data visualization, reduction, and analysis on all upgraded instruments. ISAW provides the ability to process and visualize the data from thousands of detector pixels, each having thousands of time channels. These operations can be done interactively through a familiar graphical user interface or automatically through simple scripts. Scripts and operators provided by end users are automatically included in the ISAW menu structure, along with those distributed with ISAW, when the application is started.

  11. Testing Microshutter Arrays Using Commercial FPGA Hardware

    NASA Technical Reports Server (NTRS)

    Rapchun, David

    2008-01-01

    NASA is developing micro-shutter arrays for the Near Infrared Spectrometer (NIRSpec) instrument on the James Webb Space Telescope (JWST). These micro-shutter arrays allow NIRspec to do Multi Object Spectroscopy, a key part of the mission. Each array consists of 62414 individual 100 x 200 micron shutters. These shutters are magnetically opened and held electrostatically. Individual shutters are then programmatically closed using a simple row/column addressing technique. A common approach to provide these data/clock patterns is to use a Field Programmable Gate Array (FPGA). Such devices require complex VHSIC Hardware Description Language (VHDL) programming and custom electronic hardware. Due to JWST's rapid schedule on the development of the micro-shutters, rapid changes were required to the FPGA code to facilitate new approaches being discovered to optimize the array performance. Such rapid changes simply could not be made using conventional VHDL programming. Subsequently, National Instruments introduced an FPGA product that could be programmed through a Labview interface. Because Labview programming is considerably easier than VHDL programming, this method was adopted and brought success. The software/hardware allowed the rapid change the FPGA code and timely results of new micro-shutter array performance data. As a result, numerous labor hours and money to the project were conserved.

  12. Reconfigurable Hardware Adapts to Changing Mission Demands

    NASA Technical Reports Server (NTRS)

    2003-01-01

    A new class of computing architectures and processing systems, which use reconfigurable hardware, is creating a revolutionary approach to implementing future spacecraft systems. With the increasing complexity of electronic components, engineers must design next-generation spacecraft systems with new technologies in both hardware and software. Derivation Systems, Inc., of Carlsbad, California, has been working through NASA s Small Business Innovation Research (SBIR) program to develop key technologies in reconfigurable computing and Intellectual Property (IP) soft cores. Founded in 1993, Derivation Systems has received several SBIR contracts from NASA s Langley Research Center and the U.S. Department of Defense Air Force Research Laboratories in support of its mission to develop hardware and software for high-assurance systems. Through these contracts, Derivation Systems began developing leading-edge technology in formal verification, embedded Java, and reconfigurable computing for its PF3100, Derivational Reasoning System (DRS ), FormalCORE IP, FormalCORE PCI/32, FormalCORE DES, and LavaCORE Configurable Java Processor, which are designed for greater flexibility and security on all space missions.

  13. "Greenbook Algorithms and Hardware Needs Analysis"

    SciTech Connect

    De Jong, Wibe A.; Oehmen, Chris S.; Baxter, Douglas J.

    2007-01-09

    "This document describes the algorithms, and hardware balance requirements needed to enable the solution of real scientific problems in the DOE core mission areas of environmental and subsurface chemistry, computational and systems biology, and climate science. The MSCF scientific drivers have been outlined in the Greenbook, which is available online at http://mscf.emsl.pnl.gov/docs/greenbook_for_web.pdf . Historically, the primary science driver has been the chemical and the molecular dynamics of the biological science area, whereas the remaining applications in the biological and environmental systems science areas have been occupying a smaller segment of the available hardware resources. To go from science drivers to hardware balance requirements, the major applications were identified. Major applications on the MSCF resources are low- to high-accuracy electronic structure methods, molecular dynamics, regional climate modeling, subsurface transport, and computational biology. The algorithms of these applications were analyzed to identify the computational kernels in both sequential and parallel execution. This analysis shows that a balanced architecture is needed with respect to processor speed, peak flop rate, peak integer operation rate, and memory hierarchy, interprocessor communication, and disk access and storage. A single architecture can satisfy the needs of all of the science areas, although some areas may take greater advantage of certain aspects of the architecture. "

  14. Extravehicular activity training and hardware design consideration.

    PubMed

    Thuot, P J; Harbaugh, G J

    1995-07-01

    Preparing astronauts to perform the many complex extravehicular activity (EVA) tasks required to assemble and maintain Space Station will be accomplished through training simulations in a variety of facilities. The adequacy of this training is dependent on a thorough understanding of the task to be performed, the environment in which the task will be performed, high-fidelity training hardware and an awareness of the limitations of each particular training facility. Designing hardware that can be successfully operated, or assembled, by EVA astronauts in an efficient manner, requires an acute understanding of human factors and the capabilities and limitations of the space-suited astronaut. Additionally, the significant effect the microgravity environment has on the crew members' capabilities has to be carefully considered not only for each particular task, but also for all the overhead related to the task and the general overhead associated with EVA. This paper will describe various training methods and facilities that will be used to train EVA astronauts for Space Station assembly and maintenance. User-friendly EVA hardware design considerations and recent EVA flight experience will also be presented.

  15. Spacecraft command verification: The AI solution

    NASA Technical Reports Server (NTRS)

    Fesq, Lorraine M.; Stephan, Amy; Smith, Brian K.

    1990-01-01

    Recently, a knowledge-based approach was used to develop a system called the Command Constraint Checker (CCC) for TRW. CCC was created to automate the process of verifying spacecraft command sequences. To check command files by hand for timing and sequencing errors is a time-consuming and error-prone task. Conventional software solutions were rejected when it was estimated that it would require 36 man-months to build an automated tool to check constraints by conventional methods. Using rule-based representation to model the various timing and sequencing constraints of the spacecraft, CCC was developed and tested in only three months. By applying artificial intelligence techniques, CCC designers were able to demonstrate the viability of AI as a tool to transform difficult problems into easily managed tasks. The design considerations used in developing CCC are discussed and the potential impact of this system on future satellite programs is examined.

  16. Robot Task Commander with Extensible Programming Environment

    NASA Technical Reports Server (NTRS)

    Hart, Stephen W (Inventor); Yamokoski, John D. (Inventor); Wightman, Brian J (Inventor); Dinh, Duy Paul (Inventor); Gooding, Dustin R (Inventor)

    2014-01-01

    A system for developing distributed robot application-level software includes a robot having an associated control module which controls motion of the robot in response to a commanded task, and a robot task commander (RTC) in networked communication with the control module over a network transport layer (NTL). The RTC includes a script engine(s) and a GUI, with a processor and a centralized library of library blocks constructed from an interpretive computer programming code and having input and output connections. The GUI provides access to a Visual Programming Language (VPL) environment and a text editor. In executing a method, the VPL is opened, a task for the robot is built from the code library blocks, and data is assigned to input and output connections identifying input and output data for each block. A task sequence(s) is sent to the control module(s) over the NTL to command execution of the task.

  17. Evolutionary Telemetry and Command Processor (TCP) architecture

    NASA Technical Reports Server (NTRS)

    Schneider, John R.

    1992-01-01

    A low cost, modular, high performance, and compact Telemetry and Command Processor (TCP) is being built as the foundation of command and data handling subsystems for the next generation of satellites. The TCP product line will support command and telemetry requirements for small to large spacecraft and from low to high rate data transmission. It is compatible with the latest TDRSS, STDN and SGLS transponders and provides CCSDS protocol communications in addition to standard TDM formats. Its high performance computer provides computing resources for hosted flight software. Layered and modular software provides common services using standardized interfaces to applications thereby enhancing software re-use, transportability, and interoperability. The TCP architecture is based on existing standards, distributed networking, distributed and open system computing, and packet technology. The first TCP application is planned for the 94 SDIO SPAS 3 mission. The architecture enhances rapid tailoring of functions thereby reducing costs and schedules developed for individual spacecraft missions.

  18. IT Security Support for the Spaceport Command Control System Development

    NASA Technical Reports Server (NTRS)

    Varise, Brian

    2014-01-01

    My job title is IT Security support for the Spaceport Command & Control System Development. As a cyber-security analyst it is my job to ensure NASA's information stays safe from cyber threats, such as, viruses, malware and denial-of-service attacks by establishing and enforcing system access controls. Security is very important in the world of technology and it is used everywhere from personal computers to giant networks ran by Government agencies worldwide. Without constant monitoring analysis, businesses, public organizations and government agencies are vulnerable to potential harmful infiltration of their computer information system. It is my responsibility to ensure authorized access by examining improper access, reporting violations, revoke access, monitor information request by new programming and recommend improvements. My department oversees the Launch Control System and networks. An audit will be conducted for the LCS based on compliance with the Federal Information Security Management Act (FISMA) and The National Institute of Standards and Technology (NIST). I recently finished analyzing the SANS top 20 critical controls to give cost effective recommendations on various software and hardware products for compliance. Upon my completion of this internship, I will have successfully completed my duties as well as gain knowledge that will be helpful to my career in the future as a Cyber Security Analyst.

  19. Torque linearizing hardware for the electric joint motors of a direct-drive robot

    SciTech Connect

    Muir, P.F.; Bryan, J.R.

    1991-12-31

    Many emerging high-performance robot control algorithms require the command of the joint torques; yet no known commercial robots provide such a capability. In this paper, we describe the design, development, testing and application of a VMEbus-based torque linearizing joint interface board (JIB). One JIB resides between the robot control processor and each joint motor amplifier. The JIB provides the control processor with the capability to read the motor position and apply accurate motor torques. The torque command capability derives from the application of a 128k {times} 8 EPROM lookup table for each motor phase. Because joint motor torque is dependent upon the torque command and the motor position, the hardware is designed to utilize the torque command and the current motor position as the address to retrieve the proper pulse-width for the PWM motor amplifier. The table look-up cycle operates independently of the robot controller at a 40KHz rate to provide constant joint torque as the motor rotates. We identify the proper table entries by an automated in situ data collection procedure. Static torque generation results show that the torque deviations are reduced from as much as 76% to below 5% for each of the three direct-drive motors (two are variable reluctance motors and one is brushless DC) on an AdeptTwo robot. These torque deviations are reduced below 2.5% if only the upper 90% of the torque range is considered. The torque deviations of the non-direct-drive joint are reduced by 50%. Dynamic robot edge following experiments show that the robot speed of operation can be more than doubled for a given applied force accuracy by utilizing the joint torque linearizing boards. 8 refs.

  20. Torque linearizing hardware for the electric joint motors of a direct-drive robot

    SciTech Connect

    Muir, P.F.; Bryan, J.R.

    1991-01-01

    Many emerging high-performance robot control algorithms require the command of the joint torques; yet no known commercial robots provide such a capability. In this paper, we describe the design, development, testing and application of a VMEbus-based torque linearizing joint interface board (JIB). One JIB resides between the robot control processor and each joint motor amplifier. The JIB provides the control processor with the capability to read the motor position and apply accurate motor torques. The torque command capability derives from the application of a 128k {times} 8 EPROM lookup table for each motor phase. Because joint motor torque is dependent upon the torque command and the motor position, the hardware is designed to utilize the torque command and the current motor position as the address to retrieve the proper pulse-width for the PWM motor amplifier. The table look-up cycle operates independently of the robot controller at a 40KHz rate to provide constant joint torque as the motor rotates. We identify the proper table entries by an automated in situ data collection procedure. Static torque generation results show that the torque deviations are reduced from as much as 76% to below 5% for each of the three direct-drive motors (two are variable reluctance motors and one is brushless DC) on an AdeptTwo robot. These torque deviations are reduced below 2.5% if only the upper 90% of the torque range is considered. The torque deviations of the non-direct-drive joint are reduced by 50%. Dynamic robot edge following experiments show that the robot speed of operation can be more than doubled for a given applied force accuracy by utilizing the joint torque linearizing boards. 8 refs.

  1. Torque linearizing hardware for the electric joint motors of a direct-drive robot

    NASA Astrophysics Data System (ADS)

    Muir, P. F.; Bryan, J. R.

    Many emerging high-performance robot control algorithms require the command of the joint torques, yet no known commercial robots provide such a capability. We describe the design, development, testing, and application of a VMEbus-based torque linearizing joint interface board (JIB). One JIB resides between the robot control processor and each joint motor amplifier. The JIB provides the control processor with the capability to read the motor position and apply accurate motor torques. The torque command capability derives from the application of a 128k x 8 EPROM lookup table for each motor phase. Because joint motor torque is dependent upon the torque command and the motor position, the hardware is designed to utilize the torque command and the current motor position as the address to retrieve the proper pulse-width for the PWM motor amplifier. The table look-up cycle operates independently of the robot controller at a 40KHz rate to provide constant joint torque as the motor rotates. We identify the proper table entries by an automated in situ data collection procedure. Static torque generation results show that the torque deviations are reduced from as much as 76 percent to below 5 percent for each of the three direct-drive motors (two are variable reluctance motors and one is brushless DC) on an AdeptTwo robot. These torque deviations are reduced below 2.5 percent if only the upper 90 percent of the torque range is considered. The torque deviations of the non-direct-drive joint are reduced by 50 percent. Dynamic robot edge following experiments show that the robot speed of operation can be more than doubled for a given applied force accuracy by utilizing the joint torque linearizing boards.

  2. Apollo 9 Mission image - Command Module

    NASA Image and Video Library

    1969-03-03

    The Apollo 9 Command/Service Modules photographed from the Lunar Module,"Spider",on the fifth day of the Apollo 9 earth-orbital mission. Docking mechanism is visible in nose of the Command Module,"Gumdrop". Object jutting out from the Service Module aft bulkhead is the high-gain S-Band antenna. Film magazine was F, film type was SO-368 Ektachrome with 0.460 - 0.710 micrometers film / filter transmittance response and haze filter,80mm lens.

  3. Apollo 9 Mission image - Command Module

    NASA Image and Video Library

    1969-03-03

    High Oblique photograph (taken over New Mexico) of the Apollo 9 Command/Service Modules taken from the Lunar Module,"Spider",on the fifth day of the Apollo 9 earth-orbital mission. Docking mechanism is visible in nose of the Command Module,"Gumdrop". Object jutting out from the Service Module aft bulkhead is the high-gain S-Band antenna. Film magazine was F, film type was SO-368 Ektachrome with 0.460 - 0.710 micrometers film / filter transmittance response and haze filter,80mm lens. Cloud cover over the Earth is 70%.

  4. A Command Editor Tool for NEXTSTEP

    DTIC Science & Technology

    1993-07-01

    appears and presents the hierarchy of CEMenuCells A Command Editor Tool for NEXTSTEP 2 of 27 m arble Final Report for Contract # DAAHO1-93-C-R013 in the...icon, "Default" status, state list, textual description, tool sta- A Command Editor Tool for NEXTSTEP 3 of 27 m arble Final Report for Contract... arble Final Report for Contract # DAAH01-93-C-R013 FIGURE 7 Configuration of a TAV 3.0.. Acietr O ev 3.1 luBman d aetn Cmoe a ConQ summw t. Paletta e

  5. Natural language interface for command and control

    NASA Technical Reports Server (NTRS)

    Shuler, Robert L., Jr.

    1986-01-01

    A working prototype of a flexible 'natural language' interface for command and control situations is presented. This prototype is analyzed from two standpoints. First is the role of natural language for command and control, its realistic requirements, and how well the role can be filled with current practical technology. Second, technical concepts for implementation are discussed and illustrated by their application in the prototype system. It is also shown how adaptive or 'learning' features can greatly ease the task of encoding language knowledge in the language processor.

  6. Decision Support for Attack Submarine Commanders.

    DTIC Science & Technology

    1980-10-01

    AD-AO95 892 DECISION SCIENCE CONSORTIUM INC FALLS CHURCH VA F./e 12/2 DECISION SUPPORT FOR ATTACK SUBMARINE COMMANDERS. (U) OCT 80 M S COHEN, R V...BROWN N00014-80-C-0046 UNCLASSIFIED TR-8S-11 ML DECISIN IEN$CE CUIVSURTiUM, MrC. DECISION SUPPORT FOR A TTA CK SUBMARINE COMMANDERS Marvin S . Cohen and...on reverse) DDI ,o..ŕ 1473 EDITION OF I NOV 65 IS OISOLCTZ Unclassified S /N 0102-014-6601 1 SECURITY CLASIFICATION OF TNIS PAGE (10bon DW& tateo* 01

  7. The 10 commandments of nutrition: 2014.

    PubMed

    Deuster, Patricia A; Lindsey, Andrea T; Butler, Frank K

    2014-01-01

    The US Special Operations Command requires sound recommendations on nutrition to ensure optimal performance of Special Operations personnel. New information continues to emerge, and previous recommendations need to be modified as the evidence base continues to grow. The first 10 Commandments of Nutrition were published in the SEAL professional journal Full Mission Profile in 1992, published for the second time in this journal in 2005, and now revised a second time to reflect the newest science. Whether you are part of the Special Operations Forces (SOF) community or an athlete seeking to improve your performance, these are simple and helpful nutrition guidelines to follow. 2014.

  8. Increased productivity in flight with voice commanding

    NASA Technical Reports Server (NTRS)

    Jordan, W. T.

    1985-01-01

    Automatic Speech Recognition technology has matured to the point where it can provide a viable means of increasing productivity by naturalizing the man-machine interface. With ever increasing workloads being placed on astronauts, speech recognition may provide an alternative means of system controlling that would reduce the task burden. Voice commanding, allowing hands-free operation, can be especially effective during operations requiring simultaneous system control. A flight experiment is under development to demonstrate the operational effectiveness of voice control by commanding the Space Shuttle's Closed Circuit Television (CCIV) system. This experiment will help direct future applications of voice entry to space operations.

  9. Increased productivity in flight with voice commanding

    NASA Technical Reports Server (NTRS)

    Jordan, W. T.

    1985-01-01

    Automatic Speech Recognition technology has matured to the point where it can provide a viable means of increasing productivity by naturalizing the man-machine interface. With ever increasing workloads being placed on astronauts, speech recognition may provide an alternative means of system controlling that would reduce the task burden. Voice commanding, allowing hands-free operation, can be especially effective during operations requiring simultaneous system control. A flight experiment is under development to demonstrate the operational effectiveness of voice control by commanding the Space Shuttle's Closed Circuit Television (CCIV) system. This experiment will help direct future applications of voice entry to space operations.

  10. Remote data communications and command system

    NASA Astrophysics Data System (ADS)

    Phillips, Jesse

    Scientific ballooning missions in the continental United States have traditionally been limited in flight time due to the loss of local telemetry capability as the payload drifts beyond the horizon. A Remote Data Communications & Command System has been developed by the NSBF which allows both the recovery and display of limited real-time data and complete command control of a balloon payload that is within the telemetry horizon of a remote station. The general capabilities of this system are discussed here from the standpoint of two virtual systems which can be used independently or together as a single system.

  11. Natural language interface for command and control

    NASA Technical Reports Server (NTRS)

    Shuler, Robert L., Jr.

    1986-01-01

    A working prototype of a flexible 'natural language' interface for command and control situations is presented. This prototype is analyzed from two standpoints. First is the role of natural language for command and control, its realistic requirements, and how well the role can be filled with current practical technology. Second, technical concepts for implementation are discussed and illustrated by their application in the prototype system. It is also shown how adaptive or 'learning' features can greatly ease the task of encoding language knowledge in the language processor.

  12. VIEW OF POPPELL'S HARDWARE, FURNITURE, FEED AND SEED STORE FROM ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    VIEW OF POPPELL'S HARDWARE, FURNITURE, FEED AND SEED STORE FROM NORTHEAST FACING SOUTHWEST - Poppell's Hardware, Furniture, Feed & Seed Store, U.S. Highway 341 at Carter Avenue, Odum, Wayne County, GA

  13. VIEW OF POPPELL'S HARDWARE, FURNITURE, FEED AND SEED STORE FROM ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    VIEW OF POPPELL'S HARDWARE, FURNITURE, FEED AND SEED STORE FROM SOUTHEAST FACING NORTHWEST - Poppell's Hardware, Furniture, Feed & Seed Store, U.S. Highway 341 at Carter Avenue, Odum, Wayne County, GA

  14. Pre-Hardware Optimization of Spacecraft Image Processing Software Algorithms and Hardware Implementation

    NASA Technical Reports Server (NTRS)

    Kizhner, Semion; Flatley, Thomas P.; Hestnes, Phyllis; Jentoft-Nilsen, Marit; Petrick, David J.; Day, John H. (Technical Monitor)

    2001-01-01

    Spacecraft telemetry rates have steadily increased over the last decade presenting a problem for real-time processing by ground facilities. This paper proposes a solution to a related problem for the Geostationary Operational Environmental Spacecraft (GOES-8) image processing application. Although large super-computer facilities are the obvious heritage solution, they are very costly, making it imperative to seek a feasible alternative engineering solution at a fraction of the cost. The solution is based on a Personal Computer (PC) platform and synergy of optimized software algorithms and re-configurable computing hardware technologies, such as Field Programmable Gate Arrays (FPGA) and Digital Signal Processing (DSP). It has been shown in [1] and [2] that this configuration can provide superior inexpensive performance for a chosen application on the ground station or on-board a spacecraft. However, since this technology is still maturing, intensive pre-hardware steps are necessary to achieve the benefits of hardware implementation. This paper describes these steps for the GOES-8 application, a software project developed using Interactive Data Language (IDL) (Trademark of Research Systems, Inc.) on a Workstation/UNIX platform. The solution involves converting the application to a PC/Windows/RC platform, selected mainly by the availability of low cost, adaptable high-speed RC hardware. In order for the hybrid system to run, the IDL software was modified to account for platform differences. It was interesting to examine the gains and losses in performance on the new platform, as well as unexpected observations before implementing hardware. After substantial pre-hardware optimization steps, the necessity of hardware implementation for bottleneck code in the PC environment became evident and solvable beginning with the methodology described in [1], [2], and implementing a novel methodology for this specific application [6]. The PC-RC interface bandwidth problem for the

  15. Evaluation of methods for determining hardware projected life

    NASA Technical Reports Server (NTRS)

    1971-01-01

    An investigation of existing methods of predicting hardware life is summarized by reviewing programs having long life requirements, current research efforts on long life problems, and technical papers reporting work on life predicting techniques. The results indicate that there are no accurate quantitative means to predict hardware life for system level hardware. The effectiveness of test programs and the cause of hardware failures is considered.

  16. The Impact of Flight Hardware Scavenging on Space Logistics

    NASA Technical Reports Server (NTRS)

    Oeftering, Richard C.

    2011-01-01

    For a given fixed launch vehicle capacity the logistics payload delivered to the moon may be only roughly 20 percent of the payload delivered to the International Space Station (ISS). This is compounded by the much lower flight frequency to the moon and thus low availability of spares for maintenance. This implies that lunar hardware is much more scarce and more costly per kilogram than ISS and thus there is much more incentive to preserve hardware. The Constellation Lunar Surface System (LSS) program is considering ways of utilizing hardware scavenged from vehicles including the Altair lunar lander. In general, the hardware will have only had a matter of hours of operation yet there may be years of operational life remaining. By scavenging this hardware the program, in effect, is treating vehicle hardware as part of the payload. Flight hardware may provide logistics spares for system maintenance and reduce the overall logistics footprint. This hardware has a wide array of potential applications including expanding the power infrastructure, and exploiting in-situ resources. Scavenging can also be seen as a way of recovering the value of, literally, billions of dollars worth of hardware that would normally be discarded. Scavenging flight hardware adds operational complexity and steps must be taken to augment the crew s capability with robotics, capabilities embedded in flight hardware itself, and external processes. New embedded technologies are needed to make hardware more serviceable and scavengable. Process technologies are needed to extract hardware, evaluate hardware, reconfigure or repair hardware, and reintegrate it into new applications. This paper also illustrates how scavenging can be used to drive down the cost of the overall program by exploiting the intrinsic value of otherwise discarded flight hardware.

  17. Summary of materials and hardware performance on LDEF

    NASA Technical Reports Server (NTRS)

    Dursch, Harry; Pippin, Gary; Teichman, Lou

    1993-01-01

    A wide variety of materials and experiment support hardware were flown on the Long Duration Exposure Facility (LDEF). Postflight testing has determined the effects of the almost 6 years of low-earth orbit (LEO) exposure on this hardware. An overview of the results are presented. Hardware discussed includes adhesives, fasteners, lubricants, data storage systems, solar cells, seals, and the LDEF structure. Lessons learned from the testing and analysis of LDEF hardware is also presented.

  18. Hardware Trojans - Prevention, Detection, Countermeasures (A Literature Review)

    DTIC Science & Technology

    2011-07-01

    to a software Trojan Horse program (Thompson 1984), a Hardware Trojan is a back-door that can be inserted into hardware. The added advantages of a...characterization for ic authentication and trojan horse detection, in Hardware-Oriented Security and Trust, 2008. HOST 2008. IEEE International Workshop on...47th Design Automation Conference, pp. 633–634. Potkonjak, M., Nahapetian, A., Nelson, M. & Massey, T. (2009) Hardware trojan horse de- tection using

  19. Smart command recognizer (SCR) - For development, test, and implementation of speech commands

    NASA Technical Reports Server (NTRS)

    Simpson, Carol A.; Bunnell, John W.; Krones, Robert R.

    1988-01-01

    The SCR, a rapid prototyping system for the development, testing, and implementation of speech commands in a flight simulator or test aircraft, is described. A single unit performs all functions needed during these three phases of system development, while the use of common software and speech command data structure files greatly reduces the preparation time for successive development phases. As a smart peripheral to a simulation or flight host computer, the SCR interprets the pilot's spoken input and passes command codes to the simulation or flight computer.

  20. Positive commandable oiler for satellite bearing lubrication

    NASA Technical Reports Server (NTRS)

    James, G. E.

    1977-01-01

    On-orbit commandable lubrication of ball bearings accomplished by direct oil application to the moving ball surfaces was studied. Test results for the lubricant applicator portion of the system are presented in conjunction with a design approach for the reservoir and metering components.