• DocumentCode
    3558470
  • Title

    Performance enhancement of a multiple model adaptive estimator

  • Author

    Maybeck, Peter S. ; Hanlon, Peter D.

  • Author_Institution
    US Air Force Inst. of Technol., Wright-Patterson AFB, OH, USA
  • Volume
    31
  • Issue
    4
  • fYear
    1995
  • Firstpage
    1240
  • Lastpage
    1254
  • Abstract
    We describe performance improvement techniques for a multiple model adaptive estimator (MMAE) used to detect and identify control surface and sensor failures on an unmanned flight vehicle. Initially failure identification was accomplished within 4 s of onset, but by removing the "β dominance" effects, bounding the hypothesis conditional probabilities, retuning the Kalman filters, increasing the penalty for measurement residuals, decreasing the probability smoothing, and increasing residual propagation, the identification time was reduced to 2 s.<>
  • Keywords
    adaptive Kalman filters; adaptive estimation; aircraft control; failure analysis; probability; smoothing methods; /spl beta/ dominance effects; Kalman filter retuning; control surface failures; failure identification; hypothesis conditional probabilities; identification time; measurement residuals penalty; multiple model adaptive estimator; performance improvement techniques; probability smoothing; residual propagation; sensor failures; unmanned flight vehicle; Adaptive control; Aerospace control; Aircraft; Filters; Force sensors; Noise measurement; Programmable control; Smoothing methods; State estimation; Vehicle detection;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/7.464348
  • Filename
    464348