Transactions of Nanjing University of Aeronautics & Astronautics
Sliding Mode Fault Tolerant Attitude Control Scheme for Spacecraft with Actuator Faults
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Abstract:
An active fault tolerant control scheme is investigated for the attitude control systems of spacecraft with external disturbance and actuator faults by using the sliding mode technique. Firstly, the dynamic equations and kinematic equations of spacecraft are given. For the dynamic mode of spacecraft in faulty case, a fault diagnosis component is used for fault detection and estimation by using a nonlinear observer. According to the fault estimation information obtained during the fault diagnosis, the fault tolerant control scheme is developed by adopting the backstepping sliding mode control technique. Meanwhile, the Lyapunov theory is used to analyze the stability of the closed-loop attitude systems. Finally, simulation results for the attitude dynamics models show the feasibility of the proposed fault tolerant scheme.
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Clc Number:
V249
CHINA AERO-SCIENCES
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