• DocumentCode
    1795218
  • Title

    Fuzzy switched H∞ control for flexible air-breathing hypersonic vehicles

  • Author

    Changhua Hu ; Xiaoxiang Hu ; Shipeng Fang

  • Author_Institution
    302 Unit, Xi´an Res. Inst. of High-Technol., Xi´an, China
  • fYear
    2014
  • fDate
    8-10 Aug. 2014
  • Firstpage
    1895
  • Lastpage
    1899
  • Abstract
    The modeling, guidance and control of flexible air-breathing hypersonic vehicles (FAHVs) is highly challenging and still an open problem because of the complex inherent couplings, the strong flexibility effects, the big flight envelope, the varied parameters and external disturbance. A fuzzy switched H∞ control design method is addressed for FAHVs in this paper. The big flight envelope of FAHVs is divided into several regions with respect to the chosen switching signals, and the switched H∞ controller design method is presented. Fuzzy smooth switching condition is also introduced to avoid chattering of the plant at the switching boundaries. A numerical simulation is carried on the FAHVs´ original nonlinear dynamics to show the availability of the design methods.
  • Keywords
    H∞ control; aircraft control; control system synthesis; flexible structures; fuzzy control; nonlinear dynamical systems; time-varying systems; FAHV control; FAHV guidance; FAHV modeling; FAHV original nonlinear dynamics; external disturbance; flexibility effects; flexible air-breathing hypersonic vehicles; flight envelope; fuzzy smooth switching condition; fuzzy switched H∞ control design method; numerical simulation; plant chattering; switching boundaries; switching signals; Atmospheric modeling; Control design; Design methodology; Nonlinear dynamical systems; Switches; Vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
  • Conference_Location
    Yantai
  • Print_ISBN
    978-1-4799-4700-3
  • Type

    conf

  • DOI
    10.1109/CGNCC.2014.7007470
  • Filename
    7007470