• DocumentCode
    3131621
  • Title

    Research on the reconfigurable technique of SUAV flight control system

  • Author

    Xin-li, Xu ; Zhen, Jiang ; Bing-xiao, Fan

  • Author_Institution
    Coll. of Mech. Electr. Eng. & Autom., Shanghai Univ., Shanghai, China
  • Volume
    2
  • fYear
    2011
  • fDate
    20-21 Aug. 2011
  • Firstpage
    45
  • Lastpage
    49
  • Abstract
    The research on a Small Unmaned Air Vehicle(SUAV) has developed with various kinds of advanced technology, such as micro-machine technology, micro-motor technology, micro-electronics technology, integrated technology, and especially the nanotechnology. As the core of SUAV systems, the reconfigurable technique of flight control system can apply to the unknown fault and damage, and enhance the survivability and mission effectiveness of the aircraft obviously. It has become one of the attractive research subjects in modern aircraft integration design area. In this paper, several important methods for reconfigurable flight control are introduced or analysed, and some focus problems on the reconfigurable flight control technique are summarized and proposed. Finally, an outlook is did about the development tendency of reconfigurable flight control technique.
  • Keywords
    aircraft control; micromechanical devices; mobile robots; reconfigurable architectures; reliability; remotely operated vehicles; SUAV flight control system; aircraft integration design; microelectronics technology; micromachine technology; mission effectiveness; reconfigurable technique; small unmanned air vehicle; Adaptation models; Adaptive systems; Aerospace control; Aircraft; Control systems; Fault diagnosis; Military aircraft; SUAV; fault and damage; flight control system; reconfigurable technique;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Computing, Control and Industrial Engineering (CCIE), 2011 IEEE 2nd International Conference on
  • Conference_Location
    Wuhan
  • Print_ISBN
    978-1-4244-9599-3
  • Type

    conf

  • DOI
    10.1109/CCIENG.2011.6008063
  • Filename
    6008063