• DocumentCode
    2224921
  • Title

    Small unmanned helicopter longitudinal control PID parameter optimization based on genetic algorithm

  • Author

    Ping, Zhao Wei ; Chao, Du Yun ; Zhou, Yu Dong

  • Author_Institution
    Shen Yang Aerosp. Univ., Shenyang, China
  • Volume
    6
  • fYear
    2010
  • fDate
    20-22 Aug. 2010
  • Abstract
    The PID control as a popularly control method that is used in the control system, this control method is still adopted in many practical applications of the process currently. The paper mainly discusses the classical PID tuning methods, and on the basis of the method, which achieve a small unmanned helicopter longitudinal PID control parameters optimization by introducing the idea of genetic algorithm. The performance of control system is assured when adopting genetic algorithms. The simulation results comparing with the classical PID tuning methods shows that PID controller that is designed with genetic algorithms is better flexibility, and can obtain the better control effect.
  • Keywords
    aircraft control; attitude control; genetic algorithms; helicopters; remotely operated vehicles; three-term control; PID control; PID parameter optimization; PID tuning methods; control system performance; genetic algorithm; unmanned helicopter longitudinal control; Computer languages; Helicopters; Genetic algorithm; PID; optimization;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Advanced Computer Theory and Engineering (ICACTE), 2010 3rd International Conference on
  • Conference_Location
    Chengdu
  • ISSN
    2154-7491
  • Print_ISBN
    978-1-4244-6539-2
  • Type

    conf

  • DOI
    10.1109/ICACTE.2010.5579403
  • Filename
    5579403