• DocumentCode
    2197146
  • Title

    Validation of autonomous fault diagnostic software

  • Author

    Kolcio, K. ; Hanson, M. ; Fesq, L.

  • Author_Institution
    TRW Inc., Redondo Beach, CA, USA
  • Volume
    4
  • fYear
    1998
  • fDate
    21-28 Mar 1998
  • Firstpage
    251
  • Abstract
    A model based diagnostic engine called Marple, developed at TRW, relies on nominal models to perform fault detection and isolation. Nominal model-building and validation and verification play a critical role in Marple´s ability to correctly isolate faults and to report nominal system behavior. Recently developed Marple models of a portion of the Attitude Control Subsystem of the Total Ozone Mapping Spectrometer-Earth Probe satellite have been validated with both simulated and flight data. Sensitivity studies performed with simulated data show that the models are particularly sensitive to sensor noise. Initial comparison of Marple models to fault-free measured data revealed the need for additional model parameter tuning to eliminate diagnoses of faults when none actually occur in the data. This paper develops a methodology for building Marple models and describes experiences with using simulated and measured data to validate models
  • Keywords
    aerospace computing; attitude control; fault diagnosis; fault tolerant computing; sensitivity analysis; Attitude Control Subsystem; Earth Probe satellite; Marple models; TRW; Total Ozone Mapping Spectrometer; autonomous fault diagnostic software; diagnostic engine; fault detection; fault-free measured data; flight data; isolation; nominal model-building; nominal models; sensor noise; simulated data; validation; verification; Costs; Engines; Fault detection; Friction; Hardware; Satellites; Space technology; Space vehicles; Torque; Wheels;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 1998 IEEE
  • Conference_Location
    Snowmass at Aspen, CO
  • ISSN
    1095-323X
  • Print_ISBN
    0-7803-4311-5
  • Type

    conf

  • DOI
    10.1109/AERO.1998.682197
  • Filename
    682197