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    Balanced Model Reduction and Control of Rotor-Bearing Systems

    Source: Journal of Engineering for Gas Turbines and Power:;1997:;volume( 119 ):;issue: 002::page 456
    Author:
    J. T. Sawicki
    ,
    W. K. Gawronski
    DOI: 10.1115/1.2815596
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An effective technique is applied to the suppression of vibrations in flexible rotor-bearing systems with small gyroscopic effects. A balanced linear-quadratic-Gaussian (LQG) controller design procedure is implemented. The size of the controller is reduced in two stages by using (i) a balanced model reduction, and (ii) an LQG balanced reduction. The condition for a gyroscopic matrix is developed that allows one to ignore the rotor gyroscopic effects in the process of the controller design, although they are included in the rotor dynamics. The approach is illustrated on a typical rotor-bearing system represented by a 48 degree-of-freedom finite element model.
    keyword(s): Bearings , Rotors , Control equipment , Design , Rotordynamics , Degrees of freedom , Vibration AND Finite element model ,
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      Balanced Model Reduction and Control of Rotor-Bearing Systems

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/118705
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorJ. T. Sawicki
    contributor authorW. K. Gawronski
    date accessioned2017-05-08T23:53:30Z
    date available2017-05-08T23:53:30Z
    date copyrightApril, 1997
    date issued1997
    identifier issn1528-8919
    identifier otherJETPEZ-26764#456_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/118705
    description abstractAn effective technique is applied to the suppression of vibrations in flexible rotor-bearing systems with small gyroscopic effects. A balanced linear-quadratic-Gaussian (LQG) controller design procedure is implemented. The size of the controller is reduced in two stages by using (i) a balanced model reduction, and (ii) an LQG balanced reduction. The condition for a gyroscopic matrix is developed that allows one to ignore the rotor gyroscopic effects in the process of the controller design, although they are included in the rotor dynamics. The approach is illustrated on a typical rotor-bearing system represented by a 48 degree-of-freedom finite element model.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleBalanced Model Reduction and Control of Rotor-Bearing Systems
    typeJournal Paper
    journal volume119
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2815596
    journal fristpage456
    journal lastpage463
    identifier eissn0742-4795
    keywordsBearings
    keywordsRotors
    keywordsControl equipment
    keywordsDesign
    keywordsRotordynamics
    keywordsDegrees of freedom
    keywordsVibration AND Finite element model
    treeJournal of Engineering for Gas Turbines and Power:;1997:;volume( 119 ):;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
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