Active damping control of flexible appendages for spacecraft
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference24 articles.
1. Vibration reduction for flexible spacecraft following momentum dumping with/without slewing;Banerjee;J. Guid. Control Dyn.,2001
2. H. Okubo, S. Kuwamoto, Agile attitude control and vibration suppression of flexible spacecraft using control moment gyros, in: 19th IFAC Symposium on Automatic Control in Aerospace, September 2–6, 2013, Würzburg, Germany.
3. M.Y. Cui, S.J. Xu, Optimal attitude control of flexible spacecraft with minimum vibration, in: AIAA Guidance, Navigation, and Control Conference, 2–5 August 2010, Toronto, Ontario, Canada.
4. R. Ikeda, M. Takahashi, Agile and precise attitude maneuver of flexible spacecraft based on nonstationary frequency-shaped robust control, in: AIAA Guidance, Navigation, and Control Conference, 2–5 August 2010, Toronto, Ontario, Canada.
5. Robust high-precision attitude control for flexible spacecraft with improved mixed H2/H∞ control strategy under poles assignment constraint;Liu;Acta Astronaut.,2017
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