Uncertainty decomposition-based fault-tolerant adaptive control of flexible spacecraft

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...

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Veröffentlicht in:IEEE transactions on aerospace and electronic systems 2015-04, Vol.51 (2), p.1053-1068
Hauptverfasser: Ma, Yajie, Jiang, Bin, Tao, Gang, Cheng, Yuehua
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Cheng, Yuehua
description 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.
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subjects Actuators
Attitude control
Fault tolerance
Fault tolerant systems
Space vehicles
Symmetric matrices
Uncertainty
title Uncertainty decomposition-based fault-tolerant adaptive control of flexible spacecraft
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