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    Integrated in-Flight Fault Detection and Accommodation: A Model-Based Study

    Source: Journal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 004::page 962
    Author:
    Randal T. Rausch
    ,
    Kai F. Goebel
    ,
    Neil H. Eklund
    ,
    Brent J. Brunell
    DOI: 10.1115/1.2720517
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In-flight fault accommodation of safety-critical faults requires rapid detection and remediation. Indeed, for a class of safety-critical faults, detection within a millisecond range is imperative to allow accommodation in time to avert undesired engine behavior. We address these issues with an integrated detection and accommodation scheme. This scheme comprises model-based detection, a bank of binary classifiers, and an accommodation module. The latter biases control signals with pre-defined adjustments to regain operability while staying within established safety limits. The adjustments were developed using evolutionary algorithms to identify optimal biases off-line for multiple faults and points within the flight envelope. These biases are interpolated online for the current flight conditions. High-fidelity simulation results are presented showing accommodation applied to a high-pressure compressor fault on a commercial, high-bypass, twin-spool, turbofan engine throughout the flight envelope.
    keyword(s): Engines , Compressors , Flight , Flaw detection , High pressure (Physics) AND Sensors ,
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      Integrated in-Flight Fault Detection and Accommodation: A Model-Based Study

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    https://yetl.yabesh.ir/yetl1/handle/yetl/135662
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    contributor authorRandal T. Rausch
    contributor authorKai F. Goebel
    contributor authorNeil H. Eklund
    contributor authorBrent J. Brunell
    date accessioned2017-05-09T00:23:34Z
    date available2017-05-09T00:23:34Z
    date copyrightOctober, 2007
    date issued2007
    identifier issn1528-8919
    identifier otherJETPEZ-26973#962_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/135662
    description abstractIn-flight fault accommodation of safety-critical faults requires rapid detection and remediation. Indeed, for a class of safety-critical faults, detection within a millisecond range is imperative to allow accommodation in time to avert undesired engine behavior. We address these issues with an integrated detection and accommodation scheme. This scheme comprises model-based detection, a bank of binary classifiers, and an accommodation module. The latter biases control signals with pre-defined adjustments to regain operability while staying within established safety limits. The adjustments were developed using evolutionary algorithms to identify optimal biases off-line for multiple faults and points within the flight envelope. These biases are interpolated online for the current flight conditions. High-fidelity simulation results are presented showing accommodation applied to a high-pressure compressor fault on a commercial, high-bypass, twin-spool, turbofan engine throughout the flight envelope.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleIntegrated in-Flight Fault Detection and Accommodation: A Model-Based Study
    typeJournal Paper
    journal volume129
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2720517
    journal fristpage962
    journal lastpage969
    identifier eissn0742-4795
    keywordsEngines
    keywordsCompressors
    keywordsFlight
    keywordsFlaw detection
    keywordsHigh pressure (Physics) AND Sensors
    treeJournal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 004
    contenttypeFulltext
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