Roll/yaw control of a flexible spacecraft using skewed bias momentumwheels
- 1 July 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 8 (4) , 447-453
- https://doi.org/10.2514/3.20004
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Attitude stabilization of flexible spacecraft during stationkeeping maneuversJournal of Guidance, Control, and Dynamics, 1984
- Attitude Control of a Flexible SpacecraftJournal of Guidance and Control, 1980
- Control System Design in the Presence of Severe Structural Dynamics InteractionsJournal of Guidance and Control, 1978
- Attitude Stabilization of Synchronous Communications Satellites Employing Narrow-Beam AntennasJournal of Spacecraft and Rockets, 1971
- Results of flexible spacecraft attitude control studies utilizing hybrid coordinatesJournal of Spacecraft and Rockets, 1971