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Robust time-optimal control of uncertain flexible spacecraft

โœ Scribed by LIU, QIANG; WIE, BONG


Book ID
120835767
Publisher
American Institute of Aeronautics and Astronautics
Year
1992
Tongue
English
Weight
752 KB
Volume
15
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