• DocumentCode
    2339770
  • Title

    Robust H-infinity controller with pole placement constrains in helicopter control

  • Author

    Xiuxia, Sun ; Jianqin, Mao ; Jiyang, Dai ; Yan, Lin

  • Author_Institution
    PLA Air Force Eng., Univ. Eng. Coll., Xi´´an, China
  • Volume
    5
  • fYear
    2000
  • fDate
    2000
  • Firstpage
    3372
  • Abstract
    In this paper, the H technique with pole placement constraints is used to design the CH-47 helicopter controller. The benefits from this are that the system not only has satisfied the H requirement but also can force the closed-loop poles into a suitable sub-region of the left-half plan. It avoids over fast dynamic responses for digital implementation and has satisfied damping. In our design, the following problems are considered: How to choose the controller structure? How to design the weighting functions? Should the uncertainty be defined in the input or output? The paper gives the answers to these questions. The simulation results show that the system designed satisfies the ADS-33 requirement and robustness stability
  • Keywords
    H control; aircraft control; closed loop systems; damping; dynamic response; helicopters; pole assignment; robust control; H control; closed-loop pole; damping; dynamic responses; helicopter control; pole placement; robust control; stability; Design engineering; Educational institutions; Force control; H infinity control; Helicopters; Programmable logic arrays; Robust control; Robust stability; State feedback; Sun;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Control and Automation, 2000. Proceedings of the 3rd World Congress on
  • Conference_Location
    Hefei
  • Print_ISBN
    0-7803-5995-X
  • Type

    conf

  • DOI
    10.1109/WCICA.2000.863161
  • Filename
    863161