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contributor authorHoward J. Taitel
contributor authorDavid Gauthier
contributor authorKourosh Danai
date accessioned2017-05-08T23:46:50Z
date available2017-05-08T23:46:50Z
date copyrightJune, 1995
date issued1995
identifier issn0022-0434
identifier otherJDSMAA-26215#226_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/115100
description abstractBefore a helicopter leaves the plant, it needs to be tuned so that its vibrations meet the required specifications. Helicopter track and balance is currently performed based on “sensitivity coefficients” which have been developed statistically after years of production experience. The fundamental problem with using these sensitivity coefficients, however, is that they do not account for the nonlinear coupling between modifications or their effect on high amplitude vibrations. In order to ensure the reliability of these sensitivity coefficients, only a limited number of modifications are simultaneously applied. As such, a number of flights are performed before the aircraft is tuned, resulting in increased production and maintenance cost. In this paper, the application of feedforward neural nets coupled with back-propagation training is demonstrated to learn the nonlinear effect of modifications, so that the appropriate set of modifications can be selected in fewer iterations (flights). The effectiveness of this system of neural nets for track and balance is currently being investigated at the Sikorsky production line.
publisherThe American Society of Mechanical Engineers (ASME)
titleHelicopter Track and Balance With Artificial Neural Nets
typeJournal Paper
journal volume117
journal issue2
journal titleJournal of Dynamic Systems, Measurement, and Control
identifier doi10.1115/1.2835183
journal fristpage226
journal lastpage231
identifier eissn1528-9028
keywordsArtificial neural networks
keywordsFlight
keywordsVibration
keywordsAircraft
keywordsAssembly lines
keywordsMaintenance
keywordsReliability
keywordsFeedforward control AND Industrial plants
treeJournal of Dynamic Systems, Measurement, and Control:;1995:;volume( 117 ):;issue: 002
contenttypeFulltext


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