• DocumentCode
    506621
  • Title

    Nonlinear adaptive inversion control with neural network compensation for a longitudinal hypersonic vehicle model

  • Author

    Liu, Yan-bin ; LU, Yu-ping

  • Author_Institution
    Coll. of Astronaut., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
  • Volume
    2
  • fYear
    2009
  • fDate
    20-22 Nov. 2009
  • Firstpage
    264
  • Lastpage
    268
  • Abstract
    The focus of this paper is on nonlinear adaptive inversion control system of a longitudinal hypersonic vehicle model with neural network compensation for uncertain effects. Considering the partially unknown model dynamic for hypersonic vehicle, and the adaptive dynamic inversion control method with neural network compensation is presented, which can compensate the hypersonic vehicle model errors by the neural network output adjusted on line. Simulation results demonstrate that the nonlinear adaptive inversion control can guarantee the flight stability and also maintain the tracking performance.
  • Keywords
    adaptive control; aerospace control; compensation; neurocontrollers; nonlinear control systems; adaptive dynamic inversion control; flight control; longitudinal hypersonic vehicle model; neural network compensation; nonlinear adaptive inversion control system; partially unknown model dynamics; uncertain effects; Adaptive control; Adaptive systems; Aerospace simulation; Control system synthesis; Error correction; Neural networks; Nonlinear control systems; Nonlinear dynamical systems; Programmable control; Vehicle dynamics; flight control; hypersonic vehicle; inversion control; neuralnetwork compension;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Computing and Intelligent Systems, 2009. ICIS 2009. IEEE International Conference on
  • Conference_Location
    Shanghai
  • Print_ISBN
    978-1-4244-4754-1
  • Electronic_ISBN
    978-1-4244-4738-1
  • Type

    conf

  • DOI
    10.1109/ICICISYS.2009.5357959
  • Filename
    5357959