• DocumentCode
    736442
  • Title

    Fuzzy self-tuning PID controller for an unmanned helicopter

  • Author

    Xing, Gong ; Lifeng, Wang ; Zhijun, Meng

  • Author_Institution
    School of Aeronautic Science and Engineering, Beihang University, Beijing 100191
  • fYear
    2015
  • fDate
    28-30 July 2015
  • Firstpage
    3635
  • Lastpage
    3641
  • Abstract
    A fuzzy self-tuning PID controller is proposed for the path following of an unmanned helicopter. Generally, helicopter control system contains two control loops; the inner loop is an attitude controller and the outer loop is a path following controller. This paper adopts conventional PID controller to control attitude whilst fuzzy self-tuning PID controller to achieve the goal of path following. Moreover, the latter is the focus of this paper. The fuzzy self-tuning PID controller works as follows. When deviations from desired trajectory emerge and change over time, fuzzy controller will tune the parameters of PID controller accordingly. Furthermore, the navigation algorithm for the great circle flight path on the earth surface is designed. Finally, the simulation results of tracking a desired great circle flight path demonstrate the performance of the controller.
  • Keywords
    Aircraft navigation; Attitude control; Helicopters; Niobium; PD control; Rotors; Trajectory; Fuzzy self-tuning PID control; Great circle flight path; Path following;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2015 34th Chinese
  • Conference_Location
    Hangzhou, China
  • Type

    conf

  • DOI
    10.1109/ChiCC.2015.7260201
  • Filename
    7260201