• DocumentCode
    3279461
  • Title

    Efficient computation of a guaranteed stability domain for a high-order parameter dependent plant

  • Author

    Roos, C. ; Biannic, J.

  • Author_Institution
    Syst. Control & Flight Dynamics Dept., ONERA, Toulouse, France
  • fYear
    2010
  • fDate
    June 30 2010-July 2 2010
  • Firstpage
    3895
  • Lastpage
    3900
  • Abstract
    A practical method based on μ-analysis is proposed in this paper to compute a robustness margin for high-order LTI plants with highly repeated parametric uncertainties. This margin is guaranteed on a continuous frequency interval and there is no risk of missing a critical frequency. The resulting algorithm is then encompassed in a recursive procedure, which computes a guaranteed stability domain for possibly uncertain parameter dependent plants. Several extensions and variations to handle the trade-off between conservatism and computational time are also highlighted. The efficiency of the method is finally demonstrated on a challenging industrial problem: assessing the stability of a flexible passenger aircraft over its entire flight envelope and for all admissible mass configurations.
  • Keywords
    aircraft control; control system analysis; linear systems; stability; uncertain systems; μ-analysis; admissible mass configuration; continuous frequency interval; critical frequency; flexible passenger aircraft; flight envelope; guaranteed stability domain; high-order LTI plant; high-order parameter dependent plant; industrial problem; parametric uncertainty; recursive procedure; robustness margin; Aerospace industry; Constraint optimization; Frequency; Grid computing; High performance computing; Robust control; Robust stability; Robustness; Uncertainty; Upper bound;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference (ACC), 2010
  • Conference_Location
    Baltimore, MD
  • ISSN
    0743-1619
  • Print_ISBN
    978-1-4244-7426-4
  • Type

    conf

  • DOI
    10.1109/ACC.2010.5530661
  • Filename
    5530661