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
Link To Document :
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