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    Controller Synthesis Methodology for Multivariable Nonlinear Systems With Application to Aerospace

    Source: Journal of Dynamic Systems, Measurement, and Control:;2004:;volume( 126 ):;issue: 003::page 595
    Author:
    Amir Nassirharand
    ,
    Technical Expert
    ,
    Hassan Karimi
    DOI: 10.1115/1.1789975
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, a new systematic controller synthesis methodology for use with highly nonlinear multivariable and nonautonomous systems with application to a class of multivariable nonlinear aerospace systems is presented. The procedure is applied to a typical liquid propellant engine, and the performance of the resulting new control system is presented. In this research, the nonlinear dynamic model of the engine, which includes both soft and hard nonlinearities, is developed. The systematic controller design procedure is based on describing function models of the engine coupled with a new multivariable exact model matching procedure.
    keyword(s): Control equipment , Engines , Design , Nonlinear systems , Propellants , Aerospace industry AND Control systems ,
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      Controller Synthesis Methodology for Multivariable Nonlinear Systems With Application to Aerospace

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/129768
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    • Journal of Dynamic Systems, Measurement, and Control

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    contributor authorAmir Nassirharand
    contributor authorTechnical Expert
    contributor authorHassan Karimi
    date accessioned2017-05-09T00:12:36Z
    date available2017-05-09T00:12:36Z
    date copyrightSeptember, 2004
    date issued2004
    identifier issn0022-0434
    identifier otherJDSMAA-26333#595_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/129768
    description abstractIn this paper, a new systematic controller synthesis methodology for use with highly nonlinear multivariable and nonautonomous systems with application to a class of multivariable nonlinear aerospace systems is presented. The procedure is applied to a typical liquid propellant engine, and the performance of the resulting new control system is presented. In this research, the nonlinear dynamic model of the engine, which includes both soft and hard nonlinearities, is developed. The systematic controller design procedure is based on describing function models of the engine coupled with a new multivariable exact model matching procedure.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleController Synthesis Methodology for Multivariable Nonlinear Systems With Application to Aerospace
    typeJournal Paper
    journal volume126
    journal issue3
    journal titleJournal of Dynamic Systems, Measurement, and Control
    identifier doi10.1115/1.1789975
    journal fristpage595
    journal lastpage604
    identifier eissn1528-9028
    keywordsControl equipment
    keywordsEngines
    keywordsDesign
    keywordsNonlinear systems
    keywordsPropellants
    keywordsAerospace industry AND Control systems
    treeJournal of Dynamic Systems, Measurement, and Control:;2004:;volume( 126 ):;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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