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    Nonlinear Control of Mismatched Uncertain Linear Systems and Application to Control of Aircraft

    Source: Journal of Dynamic Systems, Measurement, and Control:;1984:;volume( 106 ):;issue: 003::page 203
    Author:
    S. N. Singh
    ,
    Antônio A. R. Coelho
    DOI: 10.1115/1.3149673
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes an approach to control of nonzero set points of uncertain linear systems based on the theory of ultimate boundedness. We derive a nonlinear control which guarantees that every system response is ultimately bounded within a certain neighborhood of the desired nonzero set point. Analytical expressions for the bounds on variations in parameters for ultimate boundedness are obtained. These results are applied to control of a VTOL aircraft whose time-varying parameters are uncertain. Unlike previous works, arbitrary and fast variations in aircraft parameters are allowed. It is shown that the nonlinear controller is effective for larger variation in parameters than the reduced linear controller. Digital simulation results show that the aircraft can be precisely maneuvered in spite of uncertain parameter variations.
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      Nonlinear Control of Mismatched Uncertain Linear Systems and Application to Control of Aircraft

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    http://yetl.yabesh.ir/yetl1/handle/yetl/98215
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    contributor authorS. N. Singh
    contributor authorAntônio A. R. Coelho
    date accessioned2017-05-08T23:17:25Z
    date available2017-05-08T23:17:25Z
    date copyrightSeptember, 1984
    date issued1984
    identifier issn0022-0434
    identifier otherJDSMAA-26083#203_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/98215
    description abstractThis paper describes an approach to control of nonzero set points of uncertain linear systems based on the theory of ultimate boundedness. We derive a nonlinear control which guarantees that every system response is ultimately bounded within a certain neighborhood of the desired nonzero set point. Analytical expressions for the bounds on variations in parameters for ultimate boundedness are obtained. These results are applied to control of a VTOL aircraft whose time-varying parameters are uncertain. Unlike previous works, arbitrary and fast variations in aircraft parameters are allowed. It is shown that the nonlinear controller is effective for larger variation in parameters than the reduced linear controller. Digital simulation results show that the aircraft can be precisely maneuvered in spite of uncertain parameter variations.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleNonlinear Control of Mismatched Uncertain Linear Systems and Application to Control of Aircraft
    typeJournal Paper
    journal volume106
    journal issue3
    journal titleJournal of Dynamic Systems, Measurement, and Control
    identifier doi10.1115/1.3149673
    journal fristpage203
    journal lastpage210
    identifier eissn1528-9028
    treeJournal of Dynamic Systems, Measurement, and Control:;1984:;volume( 106 ):;issue: 003
    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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