• DocumentCode
    2656532
  • Title

    Hybrid PID velocity control for an unmanned helicopter based on single neuron

  • Author

    Jiande, Wu ; Zhou, Wan ; Xin, Xiong

  • Author_Institution
    Sch. of Inf. Eng. & Autom., Kunming Univ. of Sci. & Technol., Kunming
  • fYear
    2008
  • fDate
    16-18 July 2008
  • Firstpage
    295
  • Lastpage
    299
  • Abstract
    The miniature unmanned helicopter exhibits a complex and nonlinear dynamic behavior, open- loop unstable and a high degree of inter-axis coupling. This paper describes a hybrid PID velocity control method based on single neuron for an unmanned helicopter. This method possesses both the simple structure of PID controller, and adjusting papameters on-line by intelligent technique. The application results of an unmanned helicopter show that the proposed controller can have helicopter achieve stable attitude in hover and improve the stability of the attitude control system. And the fine robustness for imprecise helicopter model is accounted for.
  • Keywords
    aircraft control; attitude control; helicopters; mobile robots; neurocontrollers; remotely operated vehicles; stability; three-term control; velocity control; attitude control system; hybrid PID velocity control; intelligent technique; nonlinear dynamic behavior; single neuron; unmanned helicopter; Attitude control; Control systems; Couplings; Helicopters; Intelligent structures; Neurons; Open loop systems; Stability; Three-term control; Velocity control; Adjusting paramenters on-line; Hybrid PID velocity control; Robustness; Unmanned helicopter;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference, 2008. CCC 2008. 27th Chinese
  • Conference_Location
    Kunming
  • Print_ISBN
    978-7-900719-70-6
  • Electronic_ISBN
    978-7-900719-70-6
  • Type

    conf

  • DOI
    10.1109/CHICC.2008.4604954
  • Filename
    4604954