Abstract
The attitude fault-tolerant control problem for a satellite with reaction-wheel failures, uncertainties, and unknown external disturbances is investigated in this paper. Firstly, an iterative learning observer (ILO) is proposed to achieve fault detection, isolation, and estimation. Secondly, based on the ILO, a third-order sliding mode controller is proposed to stabilize the satellite attitude rapidly under unknown external disturbances and reaction-wheel faults. Thirdly, the asymptotically stability of the ILO and the third-order sliding mode controller is proved by using the Lyapunov stability theory. Finally, simulation results demonstrate that the proposed control scheme is more effective and feasible by comparing with other fault-tolerant control approach.
Original language | English |
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Pages (from-to) | 43-51 |
Number of pages | 9 |
Journal | Asian Journal of Control |
Volume | 21 |
Issue number | 1 |
DOIs | |
State | Published - Jan 2019 |
Keywords
- actuator fault
- fault-tolerant control
- iterative learning observer
- third-order sliding mode control
- uncertainty