• DocumentCode
    1253917
  • Title

    Fuzzy guaranteed cost tracking control for a flexible air-breathing hypersonic vehicle

  • Author

    Hu, Xiaonan ; Wu, Liang ; Hu, Chuanmin ; Gao, Huijun

  • Author_Institution
    302 Unit, Xi´an Res. Inst. of Hi-Tech Hongqing Town, Xi´an, China
  • Volume
    6
  • Issue
    9
  • fYear
    2012
  • Firstpage
    1238
  • Lastpage
    1249
  • Abstract
    This study is concerned with the fuzzy guaranteed cost output tracking control design problem for a flexible air-breathing hypersonic vehicle (FAHV), which can be modelled in a Takagi-Sugeno (T-S) model form. Owing to the enormous complexity of the vehicle dynamics, only the longitudinal model is adopted for control design in the present paper. A T-S fuzzy model is first proposed to represent the non-linear dynamics of FAHV. Then, a new augmented system is developed and a fuzzy guaranteed cost output tracking control problem is studied by considering output tracking and performance cost simultaneously. A fuzzy guaranteed cost state feedback controller is designed for the obtained augmented system to guarantee that the closed-loop system is asymptotically stable and the proposed performance index has an upper bound. By utilising Lyapunov functional approach, sufficient solvability conditions for such a controller are also established in terms of linear matrix inequalities, which can be easily solved via standard numerical softwares. Numerical simulations are performed to show the excellent reference altitude and velocity tracking performance.
  • Keywords
    Lyapunov methods; aircraft; asymptotic stability; attitude control; computability; computational complexity; control system synthesis; flexible structures; fuzzy control; linear matrix inequalities; nonlinear dynamical systems; performance index; state feedback; tracking; vehicle dynamics; velocity control; FAHV; Lyapunov functional approach; T-S fuzzy model; T-S model form; Takagi-Sugeno model; asymptotically stable; augmented system; closed-loop system; enormous complexity; flexible air-breathing hypersonic vehicle; fuzzy guaranteed cost output tracking control design problem; fuzzy guaranteed cost output tracking control problem; fuzzy guaranteed cost state feedback controller; linear matrix inequality; longitudinal model; nonlinear dynamics; numerical simulations; performance cost; performance index; reference altitude; standard numerical softwares; sufficient solvability conditions; vehicle dynamics; velocity tracking performance;
  • fLanguage
    English
  • Journal_Title
    Control Theory & Applications, IET
  • Publisher
    iet
  • ISSN
    1751-8644
  • Type

    jour

  • DOI
    10.1049/iet-cta.2011.0065
  • Filename
    6252130