• DocumentCode
    1943703
  • Title

    Control strategy design based on fuzzy logic and LQR for 3-DOF helicopter model

  • Author

    Liu, Zhichao ; El haj, Zouhair Choukri ; Shi, Hongbo

  • Author_Institution
    East China Univ. of Sci. & Technol., Shanghai, China
  • fYear
    2010
  • fDate
    13-15 Aug. 2010
  • Firstpage
    262
  • Lastpage
    266
  • Abstract
    In this paper the elevation and traveling control strategy -fuzzy logic which is based on the LQR for a helicopter with three degrees of freedom is considered. The characteristic of channel coupling and nonlinearity of the system will be resolved by dividing the workplace into 4 phases which the system has a linear behavior, the phases are independently considered and LQR controllers are designed separately. It is then shown that fuzzy logic is used to combine all phases and chooses the appropriate controller parameters for the appropriate phase and so on can stabilize the whole nonlinear system. The performance of this strategy is shown by real response in the end of the paper compared to simple LQR.
  • Keywords
    aircraft control; control system analysis; fuzzy control; helicopters; linear systems; nonlinear control systems; stability; 3-DOF helicopter model; LQR controllers; channel coupling; control strategy design; degrees of freedom; elevation control strategy; fuzzy logic; linear system; nonlinear system; stability; traveling control strategy; Aerospace electronics; Control systems; Differential equations; Fuzzy logic; Helicopters; Mathematical model; Robustness;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Control and Information Processing (ICICIP), 2010 International Conference on
  • Conference_Location
    Dalian
  • Print_ISBN
    978-1-4244-7047-1
  • Type

    conf

  • DOI
    10.1109/ICICIP.2010.5564250
  • Filename
    5564250