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Adaptive Finite-Time Command Filtered Fault-Tolerant Control for Uncertain Spacecraft with Prescribed Performance

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  • Zhongtian Chen
  • Qiang Chen
  • Xiongxiong He
  • Mingxuan Sun

Abstract

In this paper, an adaptive finite-time fault-tolerant control scheme is proposed for the attitude stabilization of rigid spacecrafts. A first-order command filter is presented at the second step of the backstepping design to approximate the derivative of the virtual control, such that the singularity problem caused by the differentiation of the virtual control is avoided. Then, an adaptive fuzzy finite-time backstepping controller is developed to achieve the finite-time attitude stabilization subject to inertia uncertainty, external disturbance, actuator saturation, and faults. Through using an error transformation, the prescribed performance boundary is incorporated into the controller design to guarantee the prescribed performance of the system output. Numerical simulations demonstrate the effectiveness of the proposed scheme.

Suggested Citation

  • Zhongtian Chen & Qiang Chen & Xiongxiong He & Mingxuan Sun, 2018. "Adaptive Finite-Time Command Filtered Fault-Tolerant Control for Uncertain Spacecraft with Prescribed Performance," Complexity, Hindawi, vol. 2018, pages 1-12, November.
    • Handle: RePEc:hin:complx:4912483
    DOI: 10.1155/2018/4912483
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    References listed on IDEAS

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    1. Ruisheng Sun & Jing Na & Bin Zhu, 2018. "Robust approximation-free prescribed performance control for nonlinear systems and its application," International Journal of Systems Science, Taylor & Francis Journals, vol. 49(3), pages 511-522, February.
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    Cited by:

    1. Linwu Shen & Qiang Chen & Meiling Tao & Xiongxiong He, 2019. "Adaptive Fixed-Time Sliding Mode Control for Uncertain Twin-Rotor System with Experimental Validation," Complexity, Hindawi, vol. 2019, pages 1-11, October.

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