• DocumentCode
    2581907
  • Title

    Robust actuator fault reconstruction for LPV systems using sliding mode observers

  • Author

    Alwi, Halim ; Edwards, Christopher

  • Author_Institution
    Dept. of Eng., Univ. of Leicester, Leicester, UK
  • fYear
    2010
  • fDate
    15-17 Dec. 2010
  • Firstpage
    84
  • Lastpage
    89
  • Abstract
    This paper presents a fault reconstruction method for LPV systems which is robust against uncertainty and corrupted measurements. The design is analyzed based on a virtual system resulting from factorizing the input distribution matrix associated with the monitored actuators. The key observer parameter (which is used to define the observer gains) is designed using LMIs to minimize the effect of the uncertainty and measurement corruption on the fault reconstruction. The output error injection signals are used to reconstruct the virtual faults, and the input distribution matrix factorization is used to map back to the actual faults. Simulations using an LPV model of a large transport aircraft are presented.
  • Keywords
    actuators; aircraft control; fault diagnosis; linear matrix inequalities; linear systems; matrix decomposition; observers; robust control; variable structure systems; LMI; LPV system; linear parameter varying model; matrix factorization; robust actuator fault reconstruction; sliding mode observer; transport aircraft model; virtual system; Actuators; Aircraft; Atmospheric modeling; Equations; Observers; Robustness; Uncertainty;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control (CDC), 2010 49th IEEE Conference on
  • Conference_Location
    Atlanta, GA
  • ISSN
    0743-1546
  • Print_ISBN
    978-1-4244-7745-6
  • Type

    conf

  • DOI
    10.1109/CDC.2010.5718014
  • Filename
    5718014