• DocumentCode
    2543979
  • Title

    Prognostics, the real issues involved with predicting life remaining

  • Author

    Engel, Stephen J. ; Gilmartin, Barbara J. ; Bongort, Kenneth ; Hess, Andrew

  • Author_Institution
    Northrop Grumman Corp., Bethpage, NY, USA
  • Volume
    6
  • fYear
    2000
  • fDate
    2000
  • Firstpage
    457
  • Abstract
    This paper reviews the fundamentals of prognostics with emphasis on the estimation of remaining life and the interrelationships between accuracy, precision and confidence. A distinction is made between the static view of failure distributions derived from historical data and the dynamic view of remaining life derived from condition. The nonstationary nature of prognoses is illustrated using data from a failing SH-60 helicopter gearbox. A method is demonstrated that measures the accuracy and uncertainty of remaining life estimates using example prognostic features. This method isolates the uncertainty attributable to features and their interpretation from the uncertainty due to the random variables that govern the physics of component failure. Results from the example features support a hypothesized trend of improved accuracy and lower uncertainty as remaining life decreases
  • Keywords
    aerospace expert systems; aircraft maintenance; aircraft testing; condition monitoring; fault diagnosis; helicopters; uncertainty handling; PDF; SH-60 helicopter gearbox; accuracy; component failure; condition-based maintenance; confidence; failure distributions; fused predictions; just-in-time line; nonstationary nature; precision; prognostics; random variables; remaining life prediction; uncertainty; Aerodynamics; Biographies; Extrapolation; Helicopters; Life estimation; Physics; Propulsion; Random variables; Rivers; Uncertainty;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference Proceedings, 2000 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    0-7803-5846-5
  • Type

    conf

  • DOI
    10.1109/AERO.2000.877920
  • Filename
    877920