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A Second-Order Sliding Mode Controller Design for Spacecraft Tracking Control

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  • Yu-Xin Zhao
  • Tian Wu
  • Gang Li

Abstract

For spacecraft attitude tracking system, there exists the chattering phenomenon. In this paper, the spacecraft motion is decomposed into three-channel subsystems, and a second-order sliding mode control is proposed. This method has been proved to have good convergence and robustness. Combined with the proposed sliding surface, the three-channel controllers are designed. The control performance is confirmed by the simulation results, the approaching process is improved effectively, and a smooth transition is achieved without overshoot and buffeting.

Suggested Citation

  • Yu-Xin Zhao & Tian Wu & Gang Li, 2013. "A Second-Order Sliding Mode Controller Design for Spacecraft Tracking Control," Mathematical Problems in Engineering, Hindawi, vol. 2013, pages 1-9, September.
    • Handle: RePEc:hin:jnlmpe:429101
    DOI: 10.1155/2013/429101
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    Cited by:

    1. Mazare, Mahmood & Taghizadeh, Mostafa & Ghaf-Ghanbari, Pegah, 2021. "Fault tolerant control of wind turbines with simultaneous actuator and sensor faults using adaptive time delay control," Renewable Energy, Elsevier, vol. 174(C), pages 86-101.

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