• DocumentCode
    1639766
  • Title

    Design for BTT Missile Controller Base on the RBF Neural Networks

  • Author

    Shengjie, Huang ; Zhuwei, Zhao ; Qi, Luo

  • Author_Institution
    Sci. & Technol. Univ., Nanjing
  • fYear
    2007
  • Firstpage
    91
  • Lastpage
    95
  • Abstract
    In this paper, adaptive RBF neural networks are present for nonlinear BTT missile controller. Considering the unknown smooth function vectors and the uncertainty of pneumatic parameter , we introduce RBF neural networks to simulate this nonlinear vectors. It overcomes some limitations of robust control. Furthurmore, a systematic backstepping design method has been used to ultimately guarantee semileptonically uniformly bounded of closed loop signals, and the output of system can converge to a small neighborhood of the actual trajectory. Finally, the simulation result is presented to demonstrate the validity of the approach.
  • Keywords
    closed loop systems; control system synthesis; missile control; neurocontrollers; nonlinear control systems; pneumatic systems; radial basis function networks; vectors; adaptive RBF neural networks; backstepping design method; closed loop signals; nonlinear BTT missile controller design; nonlinear vectors; pneumatic parameter uncertainty; smooth function vectors; Adaptive control; Angular velocity; Backstepping; Control systems; Missiles; Neural networks; Nonlinear control systems; Programmable control; Robust control; Uncertainty; Adaptive control; BBT missile control systems; RBF neural control; backstepping;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference, 2007. CCC 2007. Chinese
  • Conference_Location
    Hunan
  • Print_ISBN
    978-7-81124-055-9
  • Electronic_ISBN
    978-7-900719-22-5
  • Type

    conf

  • DOI
    10.1109/CHICC.2006.4346857
  • Filename
    4346857