• DocumentCode
    622693
  • Title

    Nonlinear control design and stability analysis of a small-scale unmanned helicopter

  • Author

    Lin Zhang ; Zhengtao Ding

  • Author_Institution
    Control Syst. Centre, Univ. of Manchester, Manchester, UK
  • fYear
    2013
  • fDate
    12-14 June 2013
  • Firstpage
    1662
  • Lastpage
    1667
  • Abstract
    The main focus of this paper is to design nonlinear controllers and analyse stability for a miniature unmanned helicopter. Our work is to utilize nonlinear control methodology to command dynamics of unmanned helicopter which has been divided into slower translational dynamics (outer-loop) and faster orientation dynamics (inner-loop), thus exhibiting hierarchical structure. The attitude angles and position which separately belong to the inner-loop and the outer-loop can be independently controlled by backstepping control strategy. Stability analysis of the helicopter system including flapping dynamics has been presented after designing controllers.
  • Keywords
    attitude control; autonomous aerial vehicles; control system synthesis; helicopters; nonlinear control systems; stability; vehicle dynamics; attitude angles; backstepping control strategy; flapping dynamics; helicopter system; hierarchical structure; miniature unmanned helicopter; nonlinear control design; orientation dynamics; small-scale unmanned helicopter; stability analysis; translational dynamics; Dynamics; Equations; Helicopters; Mathematical model; Rotors; Stability analysis; Tunneling magnetoresistance;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control and Automation (ICCA), 2013 10th IEEE International Conference on
  • Conference_Location
    Hangzhou
  • ISSN
    1948-3449
  • Print_ISBN
    978-1-4673-4707-5
  • Type

    conf

  • DOI
    10.1109/ICCA.2013.6565166
  • Filename
    6565166