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Direct self-repairing control for a helicopter via quantum multi-model and disturbance observer

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  • Fuyang Chen
  • Ling Cai
  • Bin Jiang
  • Gang Tao

Abstract

In this paper, a new direct self-repairing control scheme is developed for a helicopter flight control system with unknown actuator faults and external disturbance. The design of multi-model-based adaptive control is used to accommodate the faulty system under different fault conditions. By appropriate switching based on quantum information technique, the system can be converted to the best model and the corresponding controller. Asymptotic model following performance and system stability is guaranteed. A disturbance observer is introduced to observe the disturbance of the system, which can produce corresponding control signals according to the disturbance. The results including a numerical simulation and a semi-physical verification demonstrate the effectiveness of the proposed self-repairing control approach for the helicopter flight control system.

Suggested Citation

  • Fuyang Chen & Ling Cai & Bin Jiang & Gang Tao, 2016. "Direct self-repairing control for a helicopter via quantum multi-model and disturbance observer," International Journal of Systems Science, Taylor & Francis Journals, vol. 47(3), pages 533-543, February.
    • Handle: RePEc:taf:tsysxx:v:47:y:2016:i:3:p:533-543
    DOI: 10.1080/00207721.2014.891669
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