• DocumentCode
    1111439
  • Title

    Adaptive Neural Network Control for Helicopters in Vertical Flight

  • Author

    Tee, Keng Peng ; Ge, Shuzhi Sam ; Tay, Francis E H

  • Author_Institution
    Dept. of Electr. & Comput. Eng., Nat. Univ. of Singapore, Singapore
  • Volume
    16
  • Issue
    4
  • fYear
    2008
  • fDate
    7/1/2008 12:00:00 AM
  • Firstpage
    753
  • Lastpage
    762
  • Abstract
    In this brief, robust adaptive neural network (NN) control is presented for helicopters in vertical flight, with dynamics in single-input-single-output (SISO) nonlinear nonaffine form. Based on the use of the implicit function theorem and the mean value theorem, we propose a constructive approach for adaptive NN control design with guaranteed stability. Considering both full-state and output feedback cases, it is shown that the output tracking error converges to a small neighborhood of the origin, while the remaining closed-loop signals remain bounded. The simulation study demonstrates the effectiveness of the proposed control.
  • Keywords
    adaptive control; aircraft control; closed loop systems; control system synthesis; helicopters; neurocontrollers; nonlinear control systems; robust control; state feedback; vehicle dynamics; full-state feedback; guaranteed stability; helicopter control; output feedback; robust adaptive neural network control; single-input-single-output nonlinear nonaffine form; tracking error; vertical flight; Adaptive control; helicopters; neural networks (NNs); output feedback; uncertain systems;
  • fLanguage
    English
  • Journal_Title
    Control Systems Technology, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    1063-6536
  • Type

    jour

  • DOI
    10.1109/TCST.2007.912242
  • Filename
    4476154