• DocumentCode
    175568
  • Title

    Application of fuzzy optimization control in NSV anti-disturbance

  • Author

    Gao Qian ; He Nai-bao

  • Author_Institution
    Sch. of Comput. Eng., Jiangsu Univ. of Technol., Changzhou, China
  • fYear
    2014
  • fDate
    May 31 2014-June 2 2014
  • Firstpage
    552
  • Lastpage
    554
  • Abstract
    Variable universe fuzzy control based on intelligent control technology is proposed in this paper for the hypersonic flight process of nearspace vehicle (NSV) with severe changes of aero-dynamic parameters and susceptibility on the external disturbances. And the contraction-expansion factor of the fuzzy control is given to modify the scale of universe and reduce the computational cost. By adopting fast fuzzy terminal sliding mode with variable universe in the slow loop controller which is suffering the disturbance, its robustness, the speed of anti-disturbance and control accuracy are enhanced with the adaptively modified fuzzy universe. A demonstration with the Lyapunov function is given to proved that the errors of system could converge to zero in finite time.
  • Keywords
    adaptive control; aerodynamics; attitude control; control system synthesis; fuzzy control; nonlinear control systems; optimal control; space vehicles; variable structure systems; vehicle dynamics; Lyapunov function; NSV anti-disturbance; adaptively modified fuzzy universe; aerodynamic parameters; contraction-expansion factor; control accuracy; fast fuzzy terminal sliding mode; fuzzy optimization control; hypersonic flight process; intelligent control technology; nearspace vehicle; slow loop controller; variable universe fuzzy control; Adaptation models; Educational institutions; Equations; Fuzzy control; Interference; Mathematical model; Vehicles; Fuzzy Control; Nearspace Vehicle; Robust Control; Variable Universe;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control and Decision Conference (2014 CCDC), The 26th Chinese
  • Conference_Location
    Changsha
  • Print_ISBN
    978-1-4799-3707-3
  • Type

    conf

  • DOI
    10.1109/CCDC.2014.6852227
  • Filename
    6852227