• DocumentCode
    2924734
  • Title

    Redundancy design philosophy for catastrophic loss protection

  • Author

    Eagle, Kenneth H. ; Agarwala, Ajay S.

  • Author_Institution
    Boeing Helicopters, Philadelphia, PA, USA
  • fYear
    1992
  • fDate
    21-23 Jan 1992
  • Firstpage
    1
  • Lastpage
    4
  • Abstract
    To ensure high flight safety and mission reliability in flight-critical electronics of aerospace vehicles, a redundancy design technique named brick wall is discussed. Basically, the technique proposes triplex redundant, independent paths where each path can self-monitor its own health (by using a comparison scheme within each path). Upon a fault detection, the whole path is taken offline. The inherent high redundancy allows the achievement of stringent flight safety and mission reliability goals. The design also protects against hidden/unknown failure modes and sneak circuits. The design tradeoffs are made against higher maintenance rates, cost, and weight
  • Keywords
    aircraft; design engineering; reliability; safety; aerospace vehicles; brick wall; catastrophic loss protection; failure modes; fault detection; redundancy design; reliability; safety; sneak circuits; Aerospace control; Aerospace electronics; Aerospace safety; Automatic frequency control; Circuits; FCC; Helicopters; Maintenance; Protection; Redundancy;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Reliability and Maintainability Symposium, 1992. Proceedings., Annual
  • Conference_Location
    Las Vegas, NV
  • Print_ISBN
    0-7803-0521-3
  • Type

    conf

  • DOI
    10.1109/ARMS.1992.187791
  • Filename
    187791