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