DocumentCode
3513604
Title
Bayesian Extreme Value Statistics for Novelty Detection in Gas-Turbine Engines
Author
Clifton, David A. ; Tarassenko, Lionel ; McGrogan, Nicholas ; King, Dennis ; King, Steve ; Anuzis, Paul
Author_Institution
Dept. of Eng. Sci., Oxford Univ., Oxford
fYear
2008
fDate
1-8 March 2008
Firstpage
1
Lastpage
11
Abstract
We present a novel method for the identification of abnormal episodes in gas-turbine vibration data, in which we show 1) how a model of normal engine behaviour is constructed using signatures of "normal" engine vibration response; 2) how extreme value theory (EVT), a branch of statistics used to determine the expected value of extreme values drawn from a distribution, can be used to set novelty thresholds in the model, which, if exceeded, indicate an "abnormal" episode; 3) application to large data sets of modern gas-turbine flight data, which shows successful novelty detection results with low false-positive alarm rates. The advantages of this approach over previous work are 1) a very low false-positive alarm rate, while maintaining sufficient sensitivity to detect known abnormal events; 2) the use of a Bayesian framework such that uncertainty in the distribution of "normal" data is modelled, giving a principled, probabilistic interpretation of results; 3) an implementation that is sufficiently "lightweight" in processing and memory resources that real-time, on-line novelty detection is possible in an "on-wing" engine health-monitoring system.
Keywords
Bayes methods; condition monitoring; engines; gas turbines; statistical analysis; Bayesian extreme value statistics; engine health-monitoring system; engine vibration response; extreme value theory; false-positive alarm rates; gas-turbine engines; probabilistic interpretation; Bayesian methods; Condition monitoring; Data engineering; Engines; Event detection; Modems; Programmable control; Shafts; Statistics; Turbines;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2008 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4244-1487-1
Electronic_ISBN
1095-323X
Type
conf
DOI
10.1109/AERO.2008.4526423
Filename
4526423
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