This paper proposes an angular velocity bounded robust adaptive control design for attitude maneuver and vibration reduction in the presence of external disturbances and uncertainties in the inertia matrix. The control design is Lyapunov based to ensure closed-loop stability, boundedness of system s
Adaptive robust attitude control of a flexible spacecraft
β Scribed by Morteza Shahravi; Mansour Kabganian; Aria Alasty
- Publisher
- John Wiley and Sons
- Year
- 2006
- Tongue
- English
- Weight
- 507 KB
- Volume
- 16
- Category
- Article
- ISSN
- 1049-8923
- DOI
- 10.1002/rnc.1051
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β¦ Synopsis
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 dynamic coβordinates. The model of the spacecraft considered as rigid central hub and two elastic appendages. Collocated actuators and sensors are placed on the rigid central hub. Stability proof of the overall closedβloop system is given via Lyapunov analysis. Numerical simulations show that the attitude manoeuvres can be performed precisely and the elastic deformations of the flexible substructures are suppressed as well. Copyright Β© 2006 John Wiley & Sons, Ltd.
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