• DocumentCode
    3479767
  • Title

    Real-time fault detection of the Space Shuttle Main Engine

  • Author

    Panossian, H.V. ; Kemp, V.R.

  • Author_Institution
    Rockwell Int., Canoga Park, CA, USA
  • fYear
    1991
  • fDate
    11-13 Dec 1991
  • Firstpage
    2609
  • Abstract
    The authors present a real-time failure-detection algorithm that will soon be implemented on the Space Shuttle Main Engine, (SSME) on an online basis. It is referred to as the real-time failure control (RTFC) algorithm, and it entails signal-based limit and trend checking based on information from complex model-based estimates. Thus, the SSME digital transient model and the power balance model are used to provide the algorithm with precomputed initial values, expected values, and standard deviations that serve as baselines for nominal operation
  • Keywords
    aerospace computing; aerospace engines; failure analysis; online operation; real-time systems; space vehicles; Space Shuttle Main Engine; digital transient model; expected values; fault detection; online algorithm; power balance model; real-time failure control algorithm; real-time failure-detection algorithm; standard deviations; Condition monitoring; Costs; Engines; Fault detection; Frequency; Real time systems; Redundancy; Safety; Space shuttles; Testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 1991., Proceedings of the 30th IEEE Conference on
  • Conference_Location
    Brighton
  • Print_ISBN
    0-7803-0450-0
  • Type

    conf

  • DOI
    10.1109/CDC.1991.261822
  • Filename
    261822