• DocumentCode
    622584
  • Title

    Super-twisting sliding mode control based on Lyapunov analysis for the cursing flight of hypersonic vehicles

  • Author

    Chaoxu Mu ; Changyin Sun ; Chengshan Qian ; Ruimin Zhang

  • Author_Institution
    Dept. of Electr. Eng. & Autom., Tianjin Univ., Tianjin, China
  • fYear
    2013
  • fDate
    12-14 June 2013
  • Firstpage
    522
  • Lastpage
    527
  • Abstract
    In this paper, the tracking control for air-breathing hypersonic vehicles in cruising flight is studied, where the super-twisting algorithm is utilized to design a continuous controller. The nonlinear transformation is used to clarify a control-oriented model for hypersonic vehicles. A second order sliding mode controller based on the super-twisting algorithm is designed for the tracking of velocity and altitude, and Lyapunov approach is involved to analyze the stability of closed loop system, which also demonstrates that sliding mode surfaces converge in a finite time. The super-twisting sliding mode control has the ability to reduce chattering and also is robust against varying parameters. Simulations are shown to validate that the proposed method has reduced chattering efficiently and the robustness has been also guaranteed.
  • Keywords
    Lyapunov methods; aerospace control; aircraft; closed loop systems; control system synthesis; nonlinear control systems; variable structure systems; Lyapunov analysis; Lyapunov approach; air breathing hypersonic vehicles; closed loop system; continuous controller design; cursing flight; hypersonic vehicles; nonlinear transformation; stability analysis; super twisting sliding mode control; super-twisting algorithm; Aerodynamics; Atmospheric modeling; Lyapunov methods; Robustness; Sliding mode control; Vehicle dynamics; Vehicles;
  • 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.2013.6565017
  • Filename
    6565017