• DocumentCode
    1585551
  • Title

    Design of three-axis flight simulator controller based on genetic algorithm

  • Author

    Xu, Hongze ; Jin, Ling

  • Author_Institution
    Dept. of Autom., Beijing Jiaotong Univ., China
  • Volume
    6
  • fYear
    2004
  • Firstpage
    5430
  • Abstract
    The control system of three-axis flight simulator was required to have excellent dynamic tracing performance as well as fine noise-restrained property because the coupling in the frames of the flight simulator and the indeterminate time-invariant disturber in the hydraulic pressure system exists. Based on the characteristic of three-axis flight simulator, two-degree-of-freedom PID controller for outer-frame of flight simulator was designed. This type of controller had the capability of tracing target value as well as restraining noise. In addition, the outer-frame controller parameters were set based on improved genetic algorithm. Simulation results show the effectiveness of the controller. At the same time, the controller, which was designed based on the nominal model, is used on the other model. Simulation results show that the controller has the property of robustness.
  • Keywords
    aerospace simulation; control system synthesis; genetic algorithms; hydraulic systems; position control; robust control; three-term control; PID controller; genetic algorithm; hydraulic pressure system; indeterminate time-invariant disturber; outer-frame controller parameters; robust control; three-axis flight simulator controller; Aerospace simulation; Algorithm design and analysis; Control system synthesis; Genetic algorithms; Pressure control; Three-term 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.2004.1343768
  • Filename
    1343768