• DocumentCode
    1363166
  • Title

    Computation of a Flexible Aircraft LPV/LFT Model Using Interpolation

  • Author

    Ferreres, Gilles

  • Author_Institution
    Syst. Control & Flight Dynamics Dept., ONERA-CERT/DCSD, Toulouse, France
  • Volume
    19
  • Issue
    1
  • fYear
    2011
  • Firstpage
    132
  • Lastpage
    139
  • Abstract
    The issue of this paper is to compute an LPV/LFT aircraft model, i.e., a continuum of models, by approximately interpolating a finite gridding of very high-order models. Reduced-order models of the flexible part are computed and interpolated using a rescaled companion state-space representation.
  • Keywords
    aircraft control; flexible structures; interpolation; reduced order systems; state-space methods; LPV/LFT aircraft model; finite gridding; flexible aircraft LPV/LFT model; interpolation; reduced-order models; rescaled companion state-space representation; Aircraft; Atmospheric modeling; Computational modeling; Eigenvalues and eigenfunctions; Interpolation; Mathematical model; Reduced order systems; Companion form; flexible aircraft; interpolation;
  • fLanguage
    English
  • Journal_Title
    Control Systems Technology, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    1063-6536
  • Type

    jour

  • DOI
    10.1109/TCST.2010.2078510
  • Filename
    5611633
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=1363166