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Bearings / Gyroscopes / Rigid bodies / Aerospace engineering / SPHERES / Axes conventions / Slosh dynamics / Spacecraft design / Degrees of freedom / Spaceflight / Physics / Space technology


Document Date: 2003-01-22 08:51:33

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City

Blacksburg / Glendale / /

Company

United Aircraft Corporation / North American Rockwell Group / Lockheed Martin / Boeing Satellite Systems / Jet Propulsion Laboratory / TRW Systems / Naval Research Laboratory / Air Force Research Laboratory / Specialty Components Incorporated / Optical Relay Spacecraft Laboratory / Stanford University’s Aerospace Robotics Laboratory / Space Electronics Incorporated. / Hughes Missile Systems Company / General Electric Company / NASA Langley Research Center / Guidance Dynamics Corporation / Grumman Aircraft Engineering Corporation / Honeywell Space Systems / Space Dynamics Laboratory / /

Country

United States / /

Currency

GBP / /

/

Event

Product Issues / Reorganization / /

Facility

University of Michigan’s Triaxial Air Bearing Testbed / Jet Propulsion Laboratory / Orbiting Astronomical Observatory / Stanford University / The University of Victoria / NASA Ames Research Center / Tokyo Institute of Technology / The ASTREX facility / Optical Relay Spacecraft Laboratory of NPS’s Spacecraft Research / University of Washington / Utah State University / Space Station Remote Manipulator System / International Space Station / The Air Force Institute of Technology’s SIMSAT / Massachusetts Institute of Technology / British Royal Military College of Science / Virginia Polytechnic Institute / State University / /

IndustryTerm

energy dissipation processes / rigorous systems / generation weather satellite / formation flying algorithms / planar air-bearing systems / damaged satellite / preferred technology / dumbbell systems / coupled attitude control/energy storage schemes / tethered satellite system / satellite attitude determination / planar systems / software development / manufacturing processes / manufacturing information / real-time position / precision systems / Umbrella systems / energy dissipation / tested control algorithms / reach hardware / closed-form solutions / pedagogical tools / radar satellite / strain energy / regulated cold gas / satellite attitude dynamics / electronics / diverse capabilities current systems / early systems / twin-mirror bifocal relay satellite / software architectures / air-bearing systems / /

Organization

University of Washington / NPS’s Spacecraft Research and Design Center / National Science Foundation / School of Aerospace Engineering / Space Shuttle mission / Massachusetts Institute of Technology / Naval Postgraduate School / Army Ballistic Missile Agency / Polytechnic Institute / State University / Air Force Institute of Technology / Virginia Tech / College of Science / University of Victoria / NASA Ames Research Center / Stanford University / Department of Mathematics and Ballistics / National Aeronautics and Space Administration / Utah State University / Space Division of North American Rockwell Group / Tokyo Institute of Technology / Department of Aerospace & Ocean Engineering / The University of Michigan / /

Person

Marcello Romano / Marshall Space / Mason A. Peck / Rear Admiral David / David R. Ellison / /

Position

astronaut / superintendent / Rear Admiral / Senior Staff Engineer / Skipper / representative / Marshall / controller / Associate Professor / /

Product

ORION / Momentum Control System / satellite / /

ProvinceOrState

Virginia / Michigan / Victoria / Massachusetts / Arizona / /

SportsLeague

Stanford University / /

Technology

formation flying algorithms / GPS / laser / MEMS / tested control algorithms / simulation / preferred technology / /

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