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Robust Control of Flexible Spacecraft During Large-Angle Attitude Maneuver

✍ Scribed by Yu, Ya’nan; Meng, Xiuyun; Li, Keyong; Xiong, Fenfen


Book ID
121844327
Publisher
American Institute of Aeronautics and Astronautics
Year
2014
Tongue
English
Weight
537 KB
Volume
37
Category
Article
ISSN
0731-5090

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## Abstract A new attitude control strategy for rotational manoeuvre of an elastic spacecraft is presented. Adaptive sliding mode control with hybrid sliding surface (HSS) is used to minimize the effects of uncertainties, disturbances and the difficulties arising from measurement of flexible dynami