• DocumentCode
    3246443
  • Title

    Aircraft landing control based on adaptive CMAC

  • Author

    Yang, Teng-Chieh ; Juang, Jih-Gau

  • Author_Institution
    Dept. of Commun. & Guidance Eng., Nat. Taiwan Ocean Univ., Keelung, Taiwan
  • fYear
    2009
  • fDate
    14-17 July 2009
  • Firstpage
    791
  • Lastpage
    796
  • Abstract
    This paper presents an intelligent control scheme that uses an adaptive cerebellar model articulation controller (CMAC) in aircraft automatic landing system. The proposed intelligent controller can act as an experienced pilot and guide the aircraft to a safe landing in severe turbulence environment. Current flight control law is adopted in the intelligent design. Lyapunov theory is applied to obtain adaptive learning rule and stability analysis is also provided. Performance on tracking desired path and environment adaptive capability are demonstrated through software simulations.
  • Keywords
    Lyapunov methods; adaptive systems; aircraft landing guidance; cerebellar model arithmetic computers; neurocontrollers; stability; Lyapunov theory; adaptive cerebellar model articulation controller; adaptive learning rule; aircraft automatic landing system; aircraft landing control; flight control law; intelligent control scheme; intelligent design; software simulations; stability analysis; Accidents; Adaptive control; Aerospace control; Aerospace safety; Aircraft; Automatic control; FAA; Intelligent control; Neural networks; Programmable control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Advanced Intelligent Mechatronics, 2009. AIM 2009. IEEE/ASME International Conference on
  • Conference_Location
    Singapore
  • Print_ISBN
    978-1-4244-2852-6
  • Type

    conf

  • DOI
    10.1109/AIM.2009.5229913
  • Filename
    5229913