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    Aeroengine Multivariable Nonlinear Tracking Control Based on Uncertainty and Disturbance Estimator

    Source: Journal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;issue: 012::page 121601
    Author:
    Xiao, Lingfei
    DOI: 10.1115/1.4027820
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The multivariable robust tracking control problem for aeroengine is considered in this paper. On the basis of the aeroengine nonlinear affine uncertain dynamic model, and according to uncertainty and disturbance estimator (UDE) control approach, a novel aeroengine multivariable robust nonlinear tracking control method is presented in order to provide favorable tracking and disturbance rejection performance. After getting a generalization form of UDEbased aeroengine multivariable controller, a simplification form of control law is obtained when a specified form of lowpass filter is applied. Reference model of the aeroengine system should have satisfying dynamic, thus an optional reference model is provided. Simulation on a twinshaft aeroengine with two inputs, verifies the effectiveness of the proposed method.
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      Aeroengine Multivariable Nonlinear Tracking Control Based on Uncertainty and Disturbance Estimator

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/154864
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    contributor authorXiao, Lingfei
    date accessioned2017-05-09T01:08:10Z
    date available2017-05-09T01:08:10Z
    date issued2014
    identifier issn1528-8919
    identifier othergtp_136_12_121601.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/154864
    description abstractThe multivariable robust tracking control problem for aeroengine is considered in this paper. On the basis of the aeroengine nonlinear affine uncertain dynamic model, and according to uncertainty and disturbance estimator (UDE) control approach, a novel aeroengine multivariable robust nonlinear tracking control method is presented in order to provide favorable tracking and disturbance rejection performance. After getting a generalization form of UDEbased aeroengine multivariable controller, a simplification form of control law is obtained when a specified form of lowpass filter is applied. Reference model of the aeroengine system should have satisfying dynamic, thus an optional reference model is provided. Simulation on a twinshaft aeroengine with two inputs, verifies the effectiveness of the proposed method.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAeroengine Multivariable Nonlinear Tracking Control Based on Uncertainty and Disturbance Estimator
    typeJournal Paper
    journal volume136
    journal issue12
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4027820
    journal fristpage121601
    journal lastpage121601
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;issue: 012
    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
    yabeshDSpacePersian