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    Optimal Command Generation for Tracking a Class of Discontinuous Trajectories

    Source: Journal of Dynamic Systems, Measurement, and Control:;1976:;volume( 098 ):;issue: 002::page 167
    Author:
    S. Weissenberger
    DOI: 10.1115/1.3427005
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Commands are found to drive a linear system to optimally track a class of prescribed trajectories, each of which contains a point of discontinuity. The paper focuses on the guidance problem of command generation, to be implemented in a feedforward fashion; the necessary additional control or feedback regulation structure is not studied in detail, but assumed to be provided in applications as a conventional error-feedback regulator. Solutions are found for the infinite-time problem which are optimal with respect to a quadratic performance criterion; suboptimal controls which satisfy a continuity condition are also found. The controls have applications to certain problems in aircraft guidance where command trajectories are piecewise continuous. Several examples are worked out in detail, with comparisons with conventional, nonfeedforward solutions to the problem, and a brief discussion of a simpler, suboptimal solution.
    keyword(s): Aircraft , Errors , Feedback , Feedforward control AND Linear systems ,
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      Optimal Command Generation for Tracking a Class of Discontinuous Trajectories

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    https://yetl.yabesh.ir/yetl1/handle/yetl/88491
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    • Journal of Dynamic Systems, Measurement, and Control

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    contributor authorS. Weissenberger
    date accessioned2017-05-08T23:00:25Z
    date available2017-05-08T23:00:25Z
    date copyrightJune, 1976
    date issued1976
    identifier issn0022-0434
    identifier otherJDSMAA-26037#167_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/88491
    description abstractCommands are found to drive a linear system to optimally track a class of prescribed trajectories, each of which contains a point of discontinuity. The paper focuses on the guidance problem of command generation, to be implemented in a feedforward fashion; the necessary additional control or feedback regulation structure is not studied in detail, but assumed to be provided in applications as a conventional error-feedback regulator. Solutions are found for the infinite-time problem which are optimal with respect to a quadratic performance criterion; suboptimal controls which satisfy a continuity condition are also found. The controls have applications to certain problems in aircraft guidance where command trajectories are piecewise continuous. Several examples are worked out in detail, with comparisons with conventional, nonfeedforward solutions to the problem, and a brief discussion of a simpler, suboptimal solution.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOptimal Command Generation for Tracking a Class of Discontinuous Trajectories
    typeJournal Paper
    journal volume98
    journal issue2
    journal titleJournal of Dynamic Systems, Measurement, and Control
    identifier doi10.1115/1.3427005
    journal fristpage167
    journal lastpage172
    identifier eissn1528-9028
    keywordsAircraft
    keywordsErrors
    keywordsFeedback
    keywordsFeedforward control AND Linear systems
    treeJournal of Dynamic Systems, Measurement, and Control:;1976:;volume( 098 ):;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
    yabeshDSpacePersian