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Robust Finite-Time Control for Flexible Spacecraft Attitude Maneuver

✍ Scribed by Wu, Shunan; Radice, Gianmarco; Sun, Zhaowei


Book ID
121739871
Publisher
American Society of Civil Engineers
Year
2014
Tongue
English
Weight
820 KB
Volume
27
Category
Article
ISSN
0893-1321

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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