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Volume 29 Issue 12
Dec.  2003
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Journal of Beijing University of Aeronautics and Astronautics  > 2003  >  29(12): 1130-1132.
Huang Ying. Helicopter pitch fly-by-wire control law design based on fuzzy control[J]. Journal of Beijing University of Aeronautics and Astronautics, 2003, 29(12): 1130-1132. (in Chinese)
Citation: Huang Ying. Helicopter pitch fly-by-wire control law design based on fuzzy control[J]. Journal of Beijing University of Aeronautics and Astronautics, 2003, 29(12): 1130-1132. (in Chinese)
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Helicopter pitch fly-by-wire control law design based on fuzzy control

  • Flight Automatic Control Research Institute, Xi'an 710065, China

  • Received Date: 20 Jun 2003
  • Publish Date: 31 Dec 2003
    Abstract
  • Because of the nonlinear properties of the helicopters, such as multivariable, strong couple, the conventional control methods can hardly provide the perfect manipulability for advanced helicopter. Fuzzy control is an effect control method, which deals with the control problems through the way similar to human problems solving, so it can control some uncertain systems by imitating the fuzzy concepts of human thoughts. Fuzzy control method was applied to designing the pitch ACAH control law of hovering for a helicopter. The effectiveness of the proposed method was provided by simulation.

     

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    • References(1)
  • [1] Michio Sugeno, Howard Winston, Isao Hirano, et al. Intelligent control of an unmanned helicopter based on fuzzy logic . In:51st American Helicopter Society Annual Forum ,1995. 791~803 [2] 章卫国,杨向忠.模糊控制理论与应用[M].西安:西北工业大学出版社,1999 Zhang Weiguo, Yang Xiangzhong.The theory and application of fuzzy control[M]. Xi'an:Northwestern Polytechnical University Press,1999(in Chinese)
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