• DocumentCode
    566136
  • Title

    Robust model predictive controller design for a Hypersonic Flight Vehicle

  • Author

    Tao, Xiangyuan ; Hua, Chen ; Li, Ning ; Li, Shaoyuan

  • Author_Institution
    Department of Automation, Shanghai Jiao Tong University, and key laboratory of system control and information processing, ministry of education, 200240, China
  • fYear
    2012
  • fDate
    24-26 June 2012
  • Firstpage
    1299
  • Lastpage
    1304
  • Abstract
    This paper considers the control problem of cruising flight of Hypersonic Flight Vehicle (HFV). The dynamic characteristics of HFV can be addressed as a strong nonlinear, and parameter uncertain multivariable system with hard constraints, which is extremely difficult to design the controller. In this paper, the longitudinal dynamic model of HFV is studied. Subsequently, we propose a robust model predictive control (RMPC) strategy to handle constraints in a systematic manner and overcome the impact of parameter uncertainty on the control effect, and a robust model predictive controller is designed for cruising flight of HFV. Simulation results show that this method can provide sufficient robustness and handle constraints effectively.
  • Keywords
    Hypersonic flight vehicle; longitudinal flight control; robust predictive control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Modelling, Identification & Control (ICMIC), 2012 Proceedings of International Conference on
  • Conference_Location
    Wuhan, Hubei, China
  • Print_ISBN
    978-1-4673-1524-1
  • Type

    conf

  • Filename
    6260318