• DocumentCode
    1378177
  • Title

    Real time failure detection algorithm for the Space Shuttle main engine

  • Author

    Panossian, H.V. ; Ewing, W.D.

  • Author_Institution
    Rocketdyne Div., Boeing North American, Canoga Park, CA, USA
  • Volume
    17
  • Issue
    4
  • fYear
    1997
  • fDate
    8/1/1997 12:00:00 AM
  • Firstpage
    16
  • Lastpage
    23
  • Abstract
    A real-time fault detection algorithm for the Space Shuttle main engine (SSME) is presented in this article. The system for anomaly and failure detection (SAFD) has been successfully tested on the NASA Technology Test Bed (TTB)engine at Marshall Space Flight Center in Alabama. It is currently being tested on the NASA Stennis test stand A-1, and has already proved its capability by detecting a failure earlier than a plume observer, while the redline system did not even detect the fault. It detects failures during steady-state and power throttling engine operation by monitoring 24 engine parameters in a real-time manner. The signal averages are compared with upper and lower safety limits, and if a multiple of sensor outputs violate the limits then a fault is flagged
  • Keywords
    aerospace engines; aerospace simulation; digital simulation; fault diagnosis; real-time systems; space vehicles; Marshall Space Flight Center; NASA Stennis test stand; NASA Technology Test Bed engine; Space Shuttle main engine; real time failure detection algorithm; safety limits; system for anomaly and failure detection; Condition monitoring; Detection algorithms; Engines; Fault detection; NASA; Safety; Space shuttles; Space technology; Steady-state; System testing;
  • fLanguage
    English
  • Journal_Title
    Control Systems, IEEE
  • Publisher
    ieee
  • ISSN
    1066-033X
  • Type

    jour

  • DOI
    10.1109/37.608337
  • Filename
    608337