• DocumentCode
    582076
  • Title

    Adaptive exponential time-varying sliding mode control for hypersonic cruise vehicles

  • Author

    Liang Wang ; Xiangdong Liu ; Binglong Cong ; Zhen Chen

  • Author_Institution
    Sch. of Autom., Beijing Inst. of Technol., Beijing, China
  • fYear
    2012
  • fDate
    25-27 July 2012
  • Firstpage
    3160
  • Lastpage
    3165
  • Abstract
    This paper describes the design of an adaptive exponential time-varying sliding mode control (AETVSMC) with strong robustness for hypersonic cruise vehicles subject to parametric uncertainties on the inertial and aerodynamic coefficients. An adaptation scheme is adopted to deal with unknown but bounded system uncertainties. Thus, the selection of switching gains can be obtained on-line and the upper bounds of the model uncertainties are not required to be known in advance. Stability analysis of the closed-loop system is derived based on the Lyapunov theory. Finally, simulation results demonstrate the effectiveness and robustness of the proposed approach.
  • Keywords
    Lyapunov methods; adaptive control; aerodynamics; aircraft control; closed loop systems; control system synthesis; robust control; time-varying systems; uncertain systems; variable structure systems; AETVSMC; Lyapunov theory; adaptation scheme; adaptive exponential time-varying sliding mode control design; aerodynamic coefficients; closed-loop system; hypersonic cruise vehicles; inertial coefficients; model uncertainties; parametric uncertainties; robustness; stability analysis; switching gain selection; system uncertainties; Adaptation models; Aerodynamics; Robustness; Switches; Uncertainty; Vehicles; Adaptive; Exponential time-varying sliding mode; Hypersonic vehicle; Robustness;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2012 31st Chinese
  • Conference_Location
    Hefei
  • ISSN
    1934-1768
  • Print_ISBN
    978-1-4673-2581-3
  • Type

    conf

  • Filename
    6390465