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Real-time computer control of a flexible spacecraft emulator

โœ Scribed by Crocker, G.W.; Hughes, P.C.; Hong, T.

Book ID
114560760
Publisher
IEEE
Year
1990
Tongue
English
Weight
570 KB
Volume
10
Category
Article
ISSN
1066-033X

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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