• DocumentCode
    381333
  • Title

    Maneuver simulation of a non-linear system using membership function optimization of a fuzzy logic controller

  • Author

    Zadeh, Hossein S.

  • Author_Institution
    Sch. of Bus. Inf. Technol., R. Melbourne Inst. of Technol., Vic., Australia
  • Volume
    5
  • fYear
    2002
  • fDate
    2002
  • Firstpage
    146584
  • Abstract
    This work is an ongoing investigation of attitude control (π/2 rad rotation) as well as vibration suppression of a very flexible structure. A nominal fuzzy logic controller had been designed and used as a basis for design of an optimized fuzzy controller. The optimization algorithm and procedure have been explained in an earlier paper. This paper presents simulation results of both the nominal and optimized systems. Clear improvement in the performance of the optimized controller in comparison to that of the nominal system is evident. A computer program is developed to animate results of the simulation in a three dimensional space. The program runs under GNU/Linux and uses GTK and OpenGL for visualization.
  • Keywords
    aerospace computing; artificial satellites; attitude control; control system synthesis; digital simulation; flexible structures; fuzzy control; nonlinear control systems; optimisation; vibration control; GNU/Linux; GTK; OpenGL; attitude control; computer program; flexible structure; fuzzy logic controller design; membership function optimization; nonlinear system; satellite maneuver simulation; simulation; solar panel deployment; spacecraft; vibration suppression; visualization; Animation; Computational modeling; Computer simulation; Control systems; Design optimization; Flexible structures; Fuzzy control; Fuzzy logic; Nonlinear control systems; Vibration control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference Proceedings, 2002. IEEE
  • Print_ISBN
    0-7803-7231-X
  • Type

    conf

  • DOI
    10.1109/AERO.2002.1035399
  • Filename
    1035399