Precision attitude control with a single body-fixed momentum wheel-Reference-Cited by-同舟云学术

Precision attitude control with a single body-fixed momentum wheel

Published:1974-08-05 Issue: Volume: Page:
ISSN:
Container-title:Mechanics and Control of Flight Conference
language:
Short-container-title:

Author:

IWENS R.,FLEMING A.,SPECTOR V.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1974-894

Reference6 articles.

1. H. J. Dougherty, E. D. Scott and 3. J. d d "Analysis and Design of WHECON - An Attit& Control Concept," A m 2nd Communications Satellite Systems Conference, San Francis- April8-10,1968.

2. C. A. Franklin and E. H. Davison, "A Hi Communications Technology Satellite for and 14 GHz Bands," AIAA 4th Connnunicatio Satellite Systems Conference, Washington, April24-26,1972.

3. F. R. Vigneron, D. V. McMillen and J. R. Kettlewell, "The Attitude Stabili and Cmtrol System for the Communicati Technology Satellite," The 1972 Natio communications Conference, Houston, Tea December4-6,1972.

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2. Roll/yaw control of flexible spacecraft using skewed bias momentum wheels;17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference;1984-06-25

3. A DELAYED PULSE ROLL/YAW CONTROLLER FOR A MOMENTUM BIASED SPACECRAFT;Automatic Control in Space 1982;1983

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5. A new concept for attitude control of communication satellites usingResidual Pitch Momentum /RPM/;6th Communications Satellite Systems Conference;1976-04-05