• DocumentCode
    3136768
  • Title

    On calculating flat outputs for Pfaffian systems by a reduction procedure - Demonstrated by means of the VTOL example

  • Author

    Schöberl, Markus ; Schlacher, Kurt

  • Author_Institution
    Inst. of Autom. Control & Control Syst. Technol., Univ. of Linz, Linz, Austria
  • fYear
    2011
  • fDate
    19-21 Dec. 2011
  • Firstpage
    477
  • Lastpage
    482
  • Abstract
    This paper addresses the problem of generating a flat system parametrization for Pfaffian systems in a constructive manner. The main idea behind the procedure is a subsequent application of transformations that decompose a given Pfaffian system into a sequence of systems. This splitting of a Pfaffian system possesses the property that a parametrization of the bottom part can be elementarily obtained provided a rank criterion is met and the parametrization for the upper part is known. Then (if possible) this procedure will be repeated with the upper system to generate a sequence of systems by gradual reduction of the complexity of the problem. The application of the whole machinery to the VTOL example will demonstrate the effectiveness of the procedure. In fact the well known flat output for the VTOL and an alternative one are derived using this constructive machinery in a systematic fashion.
  • Keywords
    aircraft control; machinery; partial differential equations; sequences; Pfaffian systems; VTOL example; complexity reduction; constructive machinery; flat system parametrization; rank criterion; system sequence; vertical take-off and landing aircraft; Differential equations; Machinery; Nonlinear control systems; Systematics; Vectors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control and Automation (ICCA), 2011 9th IEEE International Conference on
  • Conference_Location
    Santiago
  • ISSN
    1948-3449
  • Print_ISBN
    978-1-4577-1475-7
  • Type

    conf

  • DOI
    10.1109/ICCA.2011.6137922
  • Filename
    6137922