• DocumentCode
    3394770
  • Title

    Research on the fault diagnosis of flight control system

  • Author

    Xu Xin-li ; Jiang Zhen ; Fan Bing-Xiao

  • Author_Institution
    Coll. of Mech. Electr. Eng. & Autom., Shanghai Univ., Shanghai, China
  • fYear
    2011
  • fDate
    19-22 Aug. 2011
  • Firstpage
    1427
  • Lastpage
    1431
  • Abstract
    As the core of aircraft, the state of flight control system can impact the survivability and mission effectiveness of the aircraft obviously. The fault diagnosis of flight control system when it breaks down can provide some essential information for subsequent reconfigurable control, which can guarantee the system stability. In this paper, the history and current state of fault diagnosis methods about flight control system are introduced, and then some important methods for fault diagnosis are analysed. Some focus problems on fault diagnosis are also summarized. Finally, an outlook is did for the development tendency of fault diagnosis about flight control system.
  • Keywords
    aircraft control; stability; aircraft; fault diagnosis; flight control system; subsequent reconfigurable control; system stability; Aerospace control; Artificial intelligence; Fault detection; Fault diagnosis; Mathematical model; Signal processing; State estimation; fault and damage; fault diagnosis; flight control system; reconfigurable control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Mechatronic Science, Electric Engineering and Computer (MEC), 2011 International Conference on
  • Conference_Location
    Jilin
  • Print_ISBN
    978-1-61284-719-1
  • Type

    conf

  • DOI
    10.1109/MEC.2011.6025739
  • Filename
    6025739