• DocumentCode
    3268504
  • Title

    Global stabilization of a PVTOL aircraft with bounded thrust

  • Author

    Fantoni, I. ; Zavala, A. ; Lozano, R.

  • Author_Institution
    Heudiasyc, Univ. de Technol. de Compiegne, France
  • Volume
    4
  • fYear
    2002
  • fDate
    10-13 Dec. 2002
  • Firstpage
    4462
  • Abstract
    A global stabilizing control design is proposed for the planar vertical takeoff and landing (PVTOL) aircraft. The methodology is based on the use of nonlinear combinations of saturation functions bounding the thrust input to arbitrary saturation limits. The algorithm is simple and provides global convergence of the state to the origin.
  • Keywords
    aircraft control; convergence; nonlinear control systems; nonlinear functions; stability; PVTOL aircraft; arbitrary saturation limits; bounded thrust; global convergence; global stabilization; nonlinear control systems; nonlinear saturation functions; planar vertical takeoff and landing aircraft; Aerospace control; Aircraft; Control design; Control systems; Convergence; Equations; Gain; Linear approximation; Nonlinear control systems; State feedback;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 2002, Proceedings of the 41st IEEE Conference on
  • ISSN
    0191-2216
  • Print_ISBN
    0-7803-7516-5
  • Type

    conf

  • DOI
    10.1109/CDC.2002.1185076
  • Filename
    1185076
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=3268504