Abstract
Under the extensive application of the spacecraft, an adaptive sliding mode fault tolerant controller is proposed for a spacecraft with the actuator effectiveness and external disturbance. In this approach, the attitude fault-tolerant control scheme based on the sliding mode control theory is design to achieve fault-tolerant control and external disturbance rejection. Then, considering the unknown parameters problem of the actuator and disturbance, adaptive methods is introduced to real-time estimate the unknown parameters, which improve the robustness and practicality of the controller. Finally, the stability of the proposed controller is proved based on the Lyapunov theory and the simulation results show the method with strong fault tolerance for spacecraft actuator failure.
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Li, A. et al. (2020). Adaptive Sliding Mode Fault Tolerant Control of Spacecraft with Actuator Effectiveness. In: Xu, Z., Parizi, R., Hammoudeh, M., Loyola-González, O. (eds) Cyber Security Intelligence and Analytics. CSIA 2020. Advances in Intelligent Systems and Computing, vol 1146. Springer, Cham. https://doi.org/10.1007/978-3-030-43306-2_59
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DOI: https://doi.org/10.1007/978-3-030-43306-2_59
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