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    Approximate Nonlinear Modeling and Feedback Linearization Control for Aeroengines

    Source: Journal of Engineering for Gas Turbines and Power:;2011:;volume( 133 ):;issue: 011::page 111601
    Author:
    Hui Zhao
    ,
    Jinfu Liu
    ,
    Daren Yu
    DOI: 10.1115/1.4003642
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper aims to develop an applicable nonlinear control technique for aeroengines. An approximate nonlinear model is presented and a rational identification procedure is given. Exact input-output feedback linearization can be easily performed on this model. The controller derived can approximately linearize the plant such that the close-loop system exhibits linear input-output dynamics locally. Modeling and controlling are exemplified and validated by a small turbofan engine. Simulation results illustrate that the modeling accuracy is good and linear close-loop system dynamics are achieved.
    keyword(s): Control equipment , Engines , Modeling , Feedback , Industrial plants , Design , Dynamics (Mechanics) , Robustness , Signals AND Errors ,
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      Approximate Nonlinear Modeling and Feedback Linearization Control for Aeroengines

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    http://yetl.yabesh.ir/yetl1/handle/yetl/145895
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorHui Zhao
    contributor authorJinfu Liu
    contributor authorDaren Yu
    date accessioned2017-05-09T00:43:26Z
    date available2017-05-09T00:43:26Z
    date copyrightNovember, 2011
    date issued2011
    identifier issn1528-8919
    identifier otherJETPEZ-27176#111601_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/145895
    description abstractThis paper aims to develop an applicable nonlinear control technique for aeroengines. An approximate nonlinear model is presented and a rational identification procedure is given. Exact input-output feedback linearization can be easily performed on this model. The controller derived can approximately linearize the plant such that the close-loop system exhibits linear input-output dynamics locally. Modeling and controlling are exemplified and validated by a small turbofan engine. Simulation results illustrate that the modeling accuracy is good and linear close-loop system dynamics are achieved.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleApproximate Nonlinear Modeling and Feedback Linearization Control for Aeroengines
    typeJournal Paper
    journal volume133
    journal issue11
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4003642
    journal fristpage111601
    identifier eissn0742-4795
    keywordsControl equipment
    keywordsEngines
    keywordsModeling
    keywordsFeedback
    keywordsIndustrial plants
    keywordsDesign
    keywordsDynamics (Mechanics)
    keywordsRobustness
    keywordsSignals AND Errors
    treeJournal of Engineering for Gas Turbines and Power:;2011:;volume( 133 ):;issue: 011
    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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