• DocumentCode
    2086875
  • Title

    Adaptive nonlinear dynamic inversion control for airborne dispenser uncertain system

  • Author

    Sun Xiaoxu ; Shan Jiayuan

  • Author_Institution
    Sch. of Aerosp. Eng., Beijing Inst. of Technol., Beijing, China
  • fYear
    2010
  • fDate
    29-31 July 2010
  • Firstpage
    575
  • Lastpage
    578
  • Abstract
    This An approach to design dynamic inversion controller with adaptive compensator for airborne dispenser has been presented in this paper. The basic control law is designed using the dynamic inversion method, and the online learning neural networks are used to compensate the system errors and external disturbance. The online weights and thresholds tuning rules are deduced according to the tracking error performance functions by Lyapunov method. And it can guarantee the system to keep stable. With the changes of the flying states, the controller can adapt to the fast varying states of the system, and has preferable performance. Simulation results show that limitation of needing accurate mathematical model in dynamic inversion can be released. And the robustness of the whole system is greatly improved.
  • Keywords
    Lyapunov methods; adaptive control; learning (artificial intelligence); missile control; neurocontrollers; nonlinear control systems; stability; uncertain systems; Lyapunov method; adaptive compensator; adaptive control; airborne dispenser; dynamic inversion control; nonlinear control; online learning neural networks; uncertain system; Adaptation model; Aerodynamics; Artificial neural networks; Mathematical model; Missiles; Nonlinear dynamical systems; Simulation; Adaptive Nonlinear Controller; Dynamic Inversion; Inverse Error; Neural Network;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2010 29th Chinese
  • Conference_Location
    Beijing
  • Print_ISBN
    978-1-4244-6263-6
  • Type

    conf

  • Filename
    5572643