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    Combining Classification Techniques With Kalman Filters for Aircraft Engine Diagnostics

    Source: Journal of Engineering for Gas Turbines and Power:;2006:;volume( 128 ):;issue: 002::page 281
    Author:
    P. Dewallef
    ,
    C. Romessis
    ,
    O. Léonard
    ,
    K. Mathioudakis
    DOI: 10.1115/1.2056507
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A 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.
    keyword(s): Algorithms , Kalman filters , Measurement AND Aircraft engines ,
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      Combining Classification Techniques With Kalman Filters for Aircraft Engine Diagnostics

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/133685
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    • Journal of Engineering for Gas Turbines and Power

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    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
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