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contributor authorH. S. Tan
date accessioned2017-05-09T00:19:44Z
date available2017-05-09T00:19:44Z
date copyrightOctober, 2006
date issued2006
identifier issn1528-8919
identifier otherJETPEZ-26926#773_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/133625
description abstractThe conventional approach to neural network-based aircraft engine fault diagnostics has been mainly via multilayer feed-forward systems with sigmoidal hidden neurons trained by back propagation as well as radial basis function networks. In this paper, we explore two novel approaches to the fault-classification problem using (i) Fourier neural networks, which synthesizes the approximation capability of multidimensional Fourier transforms and gradient-descent learning, and (ii) a class of generalized single hidden layer networks (GSLN), which self-structures via Gram-Schmidt orthonormalization. Using a simulation program for the F404 engine, we generate steady-state engine parameters corresponding to a set of combined two-module deficiencies and require various neural networks to classify the multiple faults. We show that, compared to the conventional network architecture, the Fourier neural network exhibits stronger noise robustness and the GSLNs converge at a much superior speed.
publisherThe American Society of Mechanical Engineers (ASME)
titleFourier Neural Networks and Generalized Single Hidden Layer Networks in Aircraft Engine Fault Diagnostics
typeJournal Paper
journal volume128
journal issue4
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2179465
journal fristpage773
journal lastpage782
identifier eissn0742-4795
keywordsArtificial neural networks
keywordsNetworks
keywordsAircraft engines AND Engines
treeJournal of Engineering for Gas Turbines and Power:;2006:;volume( 128 ):;issue: 004
contenttypeFulltext


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