Show simple item record

contributor authorP. Dewallef
contributor authorC. Romessis
contributor authorO. Léonard
contributor authorK. Mathioudakis
date accessioned2017-05-09T00:19:51Z
date available2017-05-09T00:19:51Z
date copyrightApril, 2006
date issued2006
identifier issn1528-8919
identifier otherJETPEZ-26905#281_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/133685
description abstractA diagnostic method consisting of a combination of Kalman filters and Bayesian Belief Network (BBN) is presented. A soft-constrained Kalman filter uses a priori information derived by a BBN at each time step, to derive estimations of the unknown health parameters. The resulting algorithm has improved identification capability in comparison to the stand-alone Kalman filter. The paper focuses on a way of combining the information produced by the BBN with the Kalman filter. An extensive set of fault cases is used to test the method on a typical civil turbofan layout. The effectiveness of the method is thus demonstrated, and its advantages over individual constituent methods are presented.
publisherThe American Society of Mechanical Engineers (ASME)
titleCombining Classification Techniques With Kalman Filters for Aircraft Engine Diagnostics
typeJournal Paper
journal volume128
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2056507
journal fristpage281
journal lastpage287
identifier eissn0742-4795
keywordsAlgorithms
keywordsKalman filters
keywordsMeasurement AND Aircraft engines
treeJournal of Engineering for Gas Turbines and Power:;2006:;volume( 128 ):;issue: 002
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record