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Robust attitude synchronisation controllers design for spacecraft formation

โœ Scribed by Erdong, J.; Zhaowei, S.


Book ID
118681879
Publisher
The Institution of Engineering and Technology
Year
2009
Tongue
English
Weight
276 KB
Volume
3
Category
Article
ISSN
1751-8644

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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