• DocumentCode
    3133789
  • Title

    Neural network based adaptive dynamic inversion flight control system design

  • Author

    Lili ; Hua-min, Zhang

  • Author_Institution
    Dept. of Aerial Instrum. & Electr. Eng., First Aeronaut. Inst. of Air Force, Xin Yang, China
  • Volume
    1
  • fYear
    2011
  • fDate
    25-28 July 2011
  • Firstpage
    135
  • Lastpage
    137
  • Abstract
    This paper introduces a neutral network(NN) based adaptive dynamic inversion flight control system. Super-maneuverable flight control law adapts nonlinear inversion design; on-line learning neural networks are implemented to compensate inversion errors due to modeling error or actuator faults. Simulation results show that through adaptively compensating inversion error by neutral networks, the limitation of needing accurate mathematical model in dynamic inversion method is released and the robustness of the whole system is greatly enhanced.
  • Keywords
    adaptive control; aerospace control; control engineering computing; control system synthesis; neurocontrollers; nonlinear control systems; robust control; adaptive dynamic inversion flight control system; nonlinear inversion design; online learning neural networks; robustness; super-maneuverable flight control law; Adaptive systems; Aerodynamics; Aerospace control; Atmospheric modeling; Biological neural networks; Mathematical model; Nonlinear dynamical systems; adaptive control; dynamic inversion; flight control; neural network;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Control and Information Processing (ICICIP), 2011 2nd International Conference on
  • Conference_Location
    Harbin
  • Print_ISBN
    978-1-4577-0813-8
  • Type

    conf

  • DOI
    10.1109/ICICIP.2011.6008215
  • Filename
    6008215