Optimal feedback slewing of flexible spacecraft
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
General Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.19749
Reference1 articles.
Cited by 95 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
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3. Attitude Control and Vibration Suppression for Flexible Spacecraft Using Control Moment Gyroscopes;Journal of Aerospace Engineering;2016-01
4. A composite anti-disturbance control scheme for attitude stabilization and vibration suppression of flexible spacecrafts;Journal of Vibration and Control;2015-12-09
5. Analytic Transfer Functions for the Dynamics & Control of Flexible Rotating Spacecraft Performing Large Angle Maneuvers;The Journal of the Astronautical Sciences;2015-06
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