• DocumentCode
    1585374
  • Title

    Design of fuzzy sliding mode controller for supersonic anti-ship missile

  • Author

    Zhang, Yifei ; Deng, Fanglin ; Shi, Xusheng

  • Author_Institution
    Dept. of Autom., The Second Artillery Eng. Acad., Xi´´an, China
  • Volume
    6
  • fYear
    2004
  • Firstpage
    5402
  • Abstract
    Supersonic anti-ship missile flies with the special trajectory that initially cruises at high altitude, and cruises at low altitude at the end of its trajectory. As the difference of aerodynamic parameters between high altitude and low altitude is great, the missiles´ control performance must be very good. Sliding mode control can strengthen system´s robustness and sensitivity, so it is appropriate to control missile´s flight trajectory. But the chattering caused by SMC may badly affect system´s stabilization. To overcome the shortcoming, a fuzzy sliding mode controller combined fuzzy control with SMC was designed. Not only the controller keeps good robustness and sensitivity, but also it can efficiently reduce the chattering. Simulation results show that the method is effective.
  • Keywords
    control system synthesis; fuzzy control; missile control; position control; stability; variable structure systems; fuzzy control; missile control; sliding mode controller; supersonic antiship missile; Aerodynamics; Control systems; Design engineering; Fuzzy control; Missiles; Robust control; Sliding mode control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Control and Automation, 2004. WCICA 2004. Fifth World Congress on
  • Print_ISBN
    0-7803-8273-0
  • Type

    conf

  • DOI
    10.1109/WCICA.2004.1343760
  • Filename
    1343760