• DocumentCode
    1794987
  • Title

    Quadrotor unmanned helicopter attitude control based on improved ADRC

  • Author

    Guo-Yan Xia ; Zheng-Hua Liu

  • Author_Institution
    Sch. of Autom. Sci. & Electr. Eng., Beihang Univ., Beijing, China
  • fYear
    2014
  • fDate
    8-10 Aug. 2014
  • Firstpage
    916
  • Lastpage
    921
  • Abstract
    A kind of attitude control method for the quadrotor unmanned helicopter based on improved active disturbance rejection control (ADRC) is proposed in this paper. The dynamic model of the quadrotor unmanned helicopter is built, and the virtual control is introduced, then the non-linear model is decomposed into height, yaw, roll and pitch of the four independent channels and the disturbance rejection control technology is applied into the various channels. The simulation results show that ADRC can achieve the attitude augmentation control of the helicopter and have a good robustness. Also the results show that the improved ADRC is superior to classical ADRC both on performance and adaptability.
  • Keywords
    active disturbance rejection control; aircraft control; attitude control; helicopters; nonlinear control systems; ADRC; active disturbance rejection control; attitude augmentation control; attitude control method; disturbance rejection control technology; dynamic model; nonlinear model; quadrotor unmanned helicopter attitude control; virtual control; Attitude control; Educational institutions; Force; Helicopters; Mathematical model; Robustness; Rotors; attitude control; improved ADRC; quadrotor unmanned helicopter; robustness;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
  • Conference_Location
    Yantai
  • Print_ISBN
    978-1-4799-4700-3
  • Type

    conf

  • DOI
    10.1109/CGNCC.2014.7007331
  • Filename
    7007331