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Space / Control moment gyroscope / Rotation / Ordinal number / Angular momentum / Gimbal / Symbol / Attitude control / Physics / Gyroscopes / Classical mechanics


JOURNAL OF GUIDANCE, CONTROL, AND DYNAMICS Vol. 27, No. 4, July–August 2004 Attitude Dynamics/Control of Dual-Body Spacecraft with Variable-Speed Control Moment Gyros Marcello Romano and Brij N. Agrawal
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Document Date: 2009-05-29 13:30:28


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City

Monterey / Danvers / /

Company

Optical Relay Spacecraft Laboratory / Ford / Clearance Center Inc. / Aeronautics and Astronautics Inc. / /

Country

Italy / /

Currency

USD / /

Facility

Syracuse University / Optical Relay Spacecraft Laboratory / McMaster University / /

IndustryTerm

control law design / guidance algorithm / aerospace engineering / gimbal rate steering law / feedback law / vector product / rate steering law / acceleration steering law / acceleration-based steering law / proposed control law / feedback control law / momentum exchange devices / nonlinear feedback control law / nonlinear control law / nonlinear feedback law / control law / energy / /

Organization

Copyright Clearance Center / McMaster University / American Institute of Aeronautics and Astronautics / Spacecraft Research and Design Center / Politecnico di Milano / Syracuse University / Naval Postgraduate School / U.S. Securities and Exchange Commission / /

Position

hb / Professor and Director / Director / rT / absolute angular momentum hb / /

Product

Cowon D2+ Portable Audio Device / /

ProgrammingLanguage

MATLAB / L / Simulink / /

ProvinceOrState

California / Massachusetts / /

Technology

guidance algorithm / laser / preceding algorithm / simulation / /

URL

http /

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