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Adaptive fault tolerant control using integral sliding mode strategy with application to flexible spacecraft

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  • Qinglei Hu
  • Bing Xiao

Abstract

Adaptive-based integral sliding mode control scheme is developed to solve the actuator fault-tolerant compensation problem for linear time-invariant system in the presence of unknown actuator faults and external disturbances. A nonlinear integral-type sliding manifold is first presented that incorporates a virtual nominal control to achieve prescribed specifications of the perturbed system, and an adaptive sliding mode controller is constructed to automatically compensate for external disturbances and unknown time-invariant faults. It is shown that the proposed controller has the capability to guarantee that the resulting closed-loop system is asymptotically stable. Control design methodology is then extended to tackle with the unknown time-varying actuator faults. It is proved that any given level of gain attenuation from external disturbance/parametric estimation error to system output is achieved with the developed control law. The closed-loop performance of the new control solution derived here is evaluated extensively through numerical simulations in which the flexible spacecraft attitude control under both the external disturbances and actuator faults are considered.

Suggested Citation

  • Qinglei Hu & Bing Xiao, 2013. "Adaptive fault tolerant control using integral sliding mode strategy with application to flexible spacecraft," International Journal of Systems Science, Taylor & Francis Journals, vol. 44(12), pages 2273-2286.
    • Handle: RePEc:taf:tsysxx:v:44:y:2013:i:12:p:2273-2286
    DOI: 10.1080/00207721.2012.702236
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    Cited by:

    1. Xu, Xiaofeng & Chen, Mou & Li, Tao & Wu, Qingxian, 2021. "Composite fault tolerant attitude control for flexible satellite system under disturbance and input delay," Applied Mathematics and Computation, Elsevier, vol. 409(C).
    2. Zhiyao Ma & Yongming Li & Shaocheng Tong, 2017. "Observer-based fuzzy adaptive fault control for a class of MIMO nonlinear systems," International Journal of Systems Science, Taylor & Francis Journals, vol. 48(6), pages 1331-1346, April.
    3. Vimal Kumar, S. & Raja, R. & Marshal Anthoni, S. & Cao, Jinde & Tu, Zhengwen, 2018. "Robust finite-time non-fragile sampled-data control for T-S fuzzy flexible spacecraft model with stochastic actuator faults," Applied Mathematics and Computation, Elsevier, vol. 321(C), pages 483-497.
    4. Ngoc Phi Nguyen & Sung Kyung Hong, 2019. "Fault Diagnosis and Fault-Tolerant Control Scheme for Quadcopter UAVs with a Total Loss of Actuator," Energies, MDPI, vol. 12(6), pages 1-22, March.
    5. Ngoc Phi Nguyen & Sung Kyung Hong, 2018. "Fault-Tolerant Control of Quadcopter UAVs Using Robust Adaptive Sliding Mode Approach," Energies, MDPI, vol. 12(1), pages 1-15, December.

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