A fault-tolerant adaptive control scheme is developed for attitude tracking of flexible spacecraft with unknown inertia parameters, external disturbance, and actuator faults. The uncertainties of flexibility and dynamics are parameterized, and the control gain matrix uncertainty is handled using an uncertainty decomposition. The control scheme, with adaptive laws of the overall system uncertain parameter estimates, guarantees the system stability and asymptotic attitude tracking properties. Simulation results illustrate the effectiveness of the proposed control scheme.
Uncertainty decomposition-based fault-tolerant adaptive control of flexible spacecraft
IEEE Transactions on Aerospace and Electronic Systems ; 51 , 2 ; 1053-1068
2015-04-01
1489201 byte
Article (Journal)
Electronic Resource
English
Robust constrained fault-tolerant attitude control for flexible spacecraft
SAGE Publications | 2018
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