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    Helicopter Track and Balance With Artificial Neural Nets

    Source: Journal of Dynamic Systems, Measurement, and Control:;1995:;volume( 117 ):;issue: 002::page 226
    Author:
    Howard J. Taitel
    ,
    David Gauthier
    ,
    Kourosh Danai
    DOI: 10.1115/1.2835183
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Before 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.
    keyword(s): Artificial neural networks , Flight , Vibration , Aircraft , Assembly lines , Maintenance , Reliability , Feedforward control AND Industrial plants ,
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      Helicopter Track and Balance With Artificial Neural Nets

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/115100
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    • Journal of Dynamic Systems, Measurement, and Control

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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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