Funder
Beijing Institute of Aerospace Control Technology and the National Natural Science Foundation
Reference21 articles.
1. Active vibration suppression in flexible spacecraft attitude tracking;Di Gennaro;J. Guid. Control Dyn.,1998
2. Adaptive variable structure and commanding shaped vibration control of flexible spacecraft;Hu;J. Guid. Control Dyn.,2007
3. L1 adaptive control of flexible spacecraft despite disturbances;Lee;Acta Astronaut.,2012
4. Robust control of flexible spacecraft during large-angle attitude maneuver;Yu;J. Guid. Control Dyn.,2014
5. Chokri Sendi, Mohammad A. Ayoubi, Robust Fuzzy Logic-Based Tracking Control of a Flexible Spacecraft with H1 Performance Criteria, in: AIAA SPACE 2014 Conference and Exposition, 4–7 August 2014, San Diego, CA.
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