Stability of Proportional-Plus-Derivative-Plus-Integral Control of Flexible Spacecraft
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
General Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.55915
Reference15 articles.
1. Attitude Dynamics of Satellites with Flexible Appendages- A Brief Review
2. 2Likins, P.W. "Dynamics and Control of Flexible Space Vehicles," Jet Propulsion Laboratory Report 32-1329, Rev. 1,Jan. 1970.
3. Flexible spacecraft control design using pole allocation technique
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