• DocumentCode
    3178415
  • Title

    Modelling and control of oblique cross quadrotors vehicle

  • Author

    Hao, Wang ; Xiaoxing, Fang ; Zhihao, Cai ; Yingxun, Wang

  • Author_Institution
    Sch. of Autom. Sci. & Electr. Eng., Beihang Univ., Beijing, China
  • fYear
    2011
  • fDate
    8-10 Aug. 2011
  • Firstpage
    3113
  • Lastpage
    3117
  • Abstract
    Oblique cross quadrotors vehicle is a variant of quadrotors, which is more suitable for take photos in the air compared to the conventional cross-shaped quadrotors and the rotary-wing state of Quad Tilt Rotor(QTR) have to take this flight mode. A lot of research work have done about the conventional cross-shaped quadrotors but little about oblique cross quadrotors vehicle. The mathematics model of the oblique cross quadrotors vehicle was built up according Newton-Euler formalism and an experimental identification of dynamic parameters is presented. After that, PD was applied to design the control laws. The simulation results demonstrate that the designed control laws can accurately track the given trajectory and have a good performance.
  • Keywords
    aircraft control; helicopters; rotors; Newton-Euler formalism; control law design; dynamic parameter identification; flight mode; mathematics model; oblique cross-shaped quadrotor vehicle control; oblique cross-shaped quadrotor vehicle modelling; quad tilt rotor; rotary-wing state; Atmospheric modeling; Helicopters; MATLAB; Mathematical model; Rotors; Stability analysis; Vehicles; PD; identification; model; oblique cross; quadrotors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Artificial Intelligence, Management Science and Electronic Commerce (AIMSEC), 2011 2nd International Conference on
  • Conference_Location
    Deng Leng
  • Print_ISBN
    978-1-4577-0535-9
  • Type

    conf

  • DOI
    10.1109/AIMSEC.2011.6010829
  • Filename
    6010829