• DocumentCode
    2241859
  • Title

    Attitude stability control of Quad-rotor aerial robot base on controlled Lagrangian method

  • Author

    Xun, Gong ; Dongfu, Xu

  • Author_Institution
    Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, Changchun 130033, P.R. China
  • fYear
    2015
  • fDate
    28-30 July 2015
  • Firstpage
    963
  • Lastpage
    966
  • Abstract
    Over the last decade, a kind of Quad-rotor aerial robot, with its characteristics such as simple structure and flexible control, has become the hotspot in the field of small aerial robots research content. In this paper, based on the energy shaping theory, the controlled Lagrangians method will be introduced into the attitude stability control system of Qaud-rotor aerial robot in order to predigest the design procedure and guarantee the exact tracking to the desired angle signals. At finally, the availability of the proposed scheme is verified through numerical simulation with different initial state.
  • Keywords
    Aircraft; Angular velocity; Attitude control; Control systems; DC motors; Stability analysis; Controlled Lagrangians; Energy Shaping; Quad-rotor Robot;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2015 34th Chinese
  • Conference_Location
    Hangzhou, China
  • Type

    conf

  • DOI
    10.1109/ChiCC.2015.7259764
  • Filename
    7259764