• DocumentCode
    2468158
  • Title

    A Poincaré map approach for the exact tracking of a nonlinear non-minimum phase system: the VTOL aircraft

  • Author

    Consolini, Luca ; Tosques, Mario

  • Author_Institution
    Dipt. di Ingegneria dell´´Informazione, Parco Area delle Sci., Parma
  • fYear
    2006
  • fDate
    13-15 Dec. 2006
  • Firstpage
    1788
  • Lastpage
    1793
  • Abstract
    This article considers the problem of open-loop exact tracking for the VTOL aircraft with respect to the nominal output. It is shown that if the norm of the acceleration of the reference curve is lower than k mg, where g is the gravity acceleration and km sime 0.2688, then there exists a special initial state such that the internal dynamics are bounded. The bounding term is directly proportional to the maximum norm of the acceleration of the reference trajectory
  • Keywords
    Poincare mapping; acceleration control; aircraft control; nonlinear control systems; open loop systems; position control; tracking; Poincare map approach; VTOL aircraft; gravity acceleration; internal dynamics; nonlinear nonminimum phase system; open-loop exact tracking; reference curve; reference trajectory; Acceleration; Aerospace control; Aircraft; Control nonlinearities; Control systems; Force control; Gravity; Nonlinear control systems; Trajectory; Velocity control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 2006 45th IEEE Conference on
  • Conference_Location
    San Diego, CA
  • Print_ISBN
    1-4244-0171-2
  • Type

    conf

  • DOI
    10.1109/CDC.2006.377775
  • Filename
    4177244
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=2468158