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    A Sensor-Fault-Tolerant Diagnosis Tool Based on a Quadratic Programming Approach

    Source: Journal of Engineering for Gas Turbines and Power:;2008:;volume( 130 ):;issue: 002::page 21605
    Author:
    S. Borguet
    ,
    O. Léonard
    DOI: 10.1115/1.2772637
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Kalman filters are widely used in the turbine engine community for health monitoring purpose. This algorithm gives a good estimate of the engine condition provided that the discrepancies between the model prediction and the measurements are zero-mean, white random variables. However, this assumption is not verified when instrumentation (sensor) faults occur. As a result, the identified health parameters tend to diverge from their actual values, which strongly deteriorates the diagnosis. The purpose of this contribution is to blend robustness against sensor faults into a tool for performance monitoring of jet engines. To this end, a robust estimation approach is considered and a sensor-fault detection and isolation module is derived. It relies on a quadratic program to estimate the sensor faults and is integrated easily with the original diagnosis tool. The improvements brought by this robust estimation approach are highlighted through a series of typical test cases that may be encountered on current turbine engines.
    keyword(s): Sensors , Patient diagnosis , Engines , Algorithms AND Noise (Sound) ,
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      A Sensor-Fault-Tolerant Diagnosis Tool Based on a Quadratic Programming Approach

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    http://yetl.yabesh.ir/yetl1/handle/yetl/137972
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    contributor authorS. Borguet
    contributor authorO. Léonard
    date accessioned2017-05-09T00:28:00Z
    date available2017-05-09T00:28:00Z
    date copyrightMarch, 2008
    date issued2008
    identifier issn1528-8919
    identifier otherJETPEZ-27001#021605_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/137972
    description abstractKalman filters are widely used in the turbine engine community for health monitoring purpose. This algorithm gives a good estimate of the engine condition provided that the discrepancies between the model prediction and the measurements are zero-mean, white random variables. However, this assumption is not verified when instrumentation (sensor) faults occur. As a result, the identified health parameters tend to diverge from their actual values, which strongly deteriorates the diagnosis. The purpose of this contribution is to blend robustness against sensor faults into a tool for performance monitoring of jet engines. To this end, a robust estimation approach is considered and a sensor-fault detection and isolation module is derived. It relies on a quadratic program to estimate the sensor faults and is integrated easily with the original diagnosis tool. The improvements brought by this robust estimation approach are highlighted through a series of typical test cases that may be encountered on current turbine engines.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Sensor-Fault-Tolerant Diagnosis Tool Based on a Quadratic Programming Approach
    typeJournal Paper
    journal volume130
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2772637
    journal fristpage21605
    identifier eissn0742-4795
    keywordsSensors
    keywordsPatient diagnosis
    keywordsEngines
    keywordsAlgorithms AND Noise (Sound)
    treeJournal of Engineering for Gas Turbines and Power:;2008:;volume( 130 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian