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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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