• DocumentCode
    589415
  • Title

    Control of Hypersonic Vehicle Based on Improved QFT

  • Author

    Shi Zhen ; Wang Fei ; Ma Wen-qiao

  • Author_Institution
    Coll. of Autom., Harbin Eng. Univ., Harbin, China
  • Volume
    1
  • fYear
    2012
  • fDate
    28-29 Oct. 2012
  • Firstpage
    227
  • Lastpage
    230
  • Abstract
    Hypersonic vehicle has high military value in terms of real-time reconnaissance, remote rapid deployment and precision strike, especially the implementation of real-time reconnaissance mission has unique advantages. Efficient thrust, the aircraft must be flying high dynamic pressure conditions, in order to control the resulting aerodynamic heating and aerodynamic drag for the hypersonic vehicle angle of attack for precise control, at the same time, the dynamic characteristics of the hypersonic vehicle conventional aircraft are very different, the most critical aerodynamic characteristics are good enough stability of the pre-degree in terms of the control system must have a very strong robust feedback system. the QFT method, using an improved design of hypersonic flight longitudinal channel controller. Simulation results show that the robust controller design meets the system requirements.
  • Keywords
    aerodynamics; aircraft control; control system synthesis; drag; feedback; heating; military aircraft; robust control; QFT; aerodynamic drag control; aerodynamic heating control; dynamic characteristics; hypersonic flight longitudinal channel controller design; hypersonic vehicle control; hypersonic vehicle conventional aircraft; military value; precision strike; real-time reconnaissance mission; remote rapid deployment; robust controller design; robust feedback system; Aerodynamics; Aerospace control; Aircraft; Control systems; Robustness; Vehicle dynamics; Vehicles; QFT; control system; hepersonic; nonlinear;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Computational Intelligence and Design (ISCID), 2012 Fifth International Symposium on
  • Conference_Location
    Hangzhou
  • Print_ISBN
    978-1-4673-2646-9
  • Type

    conf

  • DOI
    10.1109/ISCID.2012.64
  • Filename
    6406959