• DocumentCode
    2106087
  • Title

    An FDIA approach for aircraft based on the Kalman filter

  • Author

    Jiang, Caihong ; Wang, Xi ; He, Ai ; Kong, Xiangxin

  • Author_Institution
    Sch. of Jet Propulsion, Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
  • fYear
    2010
  • fDate
    17-19 Dec. 2010
  • Firstpage
    466
  • Lastpage
    469
  • Abstract
    The fault diagnosis, isolation and accommodation techniques (FDIA) play an important role in the advance engine control system, and also can highly improve the reliability of the whole control system. In this paper, we build the engine realtime dynamic linear model in the framework of gain scheduling. Meanwhile, a fast recursive Kalman algorithm has been proposed to build the Kalman filter in order to raise the estimation computation speed of the dynamic system. Finally, this algorithm has been applied to an aeroengine, and experimental result demonstrates the effectiveness of the proposed design approach.
  • Keywords
    Kalman filters; aerospace engines; aircraft; time-varying systems; FDIA approach; Kalman filter; accommodation technique; advance engine control system; aeroengine; aircraft; engine realtime dynamic linear model; fault diagnosis technique; gain scheduling; isolation technique; recursive Kalman algorithm; Aircraft propulsion; Atmospheric modeling; Dynamic scheduling; Engines; Kalman filters; Mathematical model; Steady-state; Analytical redundancy; Fault detection; Kalman filter; isolation and accommodation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Information Theory and Information Security (ICITIS), 2010 IEEE International Conference on
  • Conference_Location
    Beijing
  • Print_ISBN
    978-1-4244-6942-0
  • Type

    conf

  • DOI
    10.1109/ICITIS.2010.5689561
  • Filename
    5689561