• DocumentCode
    550163
  • Title

    The control method within wind disturbance for MAV based on nonlinear model

  • Author

    Miao Cunxiao ; Fang Jiancheng ; Sun Dingsheng ; Gao Yanhao

  • Author_Institution
    Sch. of Instrum. Sci. & Opto-Electron. Eng., BeiHang Univ., Beijing, China
  • fYear
    2011
  • fDate
    22-24 July 2011
  • Firstpage
    3896
  • Lastpage
    3901
  • Abstract
    To solve the issues of nonlinear model and wind disturbance, it was proposed that the sliding mode control method based on vector field. Firstly, the nonlinear model for MAV(Micro Aerial Vehicle) was constructed. Secondly, the complexity tracking decomposed into straight line and arc segment by the proposed control method, the stable and convergent control law was constructed, and then the simulation experiment shows that MAV can complete the task of tracking in the windy condition through the navigation information. Finally, the proposed control method was compared with the traditional PID controller by flight experiments, and experimental results show that the proposed control method can guarantee the flight path control accuracy in the wind field for MAV.
  • Keywords
    aerospace control; nonlinear control systems; space vehicles; three-term control; variable structure systems; MAV based on nonlinear model; PID controller; arc segment; complexity tracking; convergent control; micro aerial vehicle; navigation information; sliding mode control method; straight line; vector field; wind disturbance; Control systems; Electronic mail; Global Positioning System; Micromechanical devices; Nonlinear dynamical systems; Vehicles; Wind; Micro Aerial Vehicle; Nonlinear dynamics model; Sliding mode; Vector field; Wind disturbance;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2011 30th Chinese
  • Conference_Location
    Yantai
  • ISSN
    1934-1768
  • Print_ISBN
    978-1-4577-0677-6
  • Electronic_ISBN
    1934-1768
  • Type

    conf

  • Filename
    6000500