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    Initial Condition Sensitivity Functions and Their Applications

    Source: Journal of Dynamic Systems, Measurement, and Control:;1971:;volume( 093 ):;issue: 002::page 116
    Author:
    Cornelius T. Leondes
    ,
    C. A. Wu
    DOI: 10.1115/1.3426469
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The well-known method of obtaining sensitivity functions is usually restricted by the condition of continuity imposed on the functions of the coordinates in system equations. For the case of discontinuous functions, more elaborate procedures are required to give a good linear approximation. It is shown that sensitivity functions are discontinuous at the discontinuous points. Also, relations between elements of sensitivity functions at these points are shown to be linear for a given nominal solution of the system. The switching time of the desired Bang-Bang control can be estimated if variations in initial conditions are known. The changes in terminal states and cost function due to deviations in initial conditions can be determined, to first order, by the use of sensitivity functions. Bounds on the deviations in initial conditions can be found by a worst case approach so that the desired terminal conditions are satisfied within given tolerances. The fundamental importance of these techniques in a number of areas of application, for instance, guidance and control of aerospace vehicles, is well known.
    keyword(s): Functions , Aircraft , Approximation AND Equations ,
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      Initial Condition Sensitivity Functions and Their Applications

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/150534
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    contributor authorCornelius T. Leondes
    contributor authorC. A. Wu
    date accessioned2017-05-09T00:55:20Z
    date available2017-05-09T00:55:20Z
    date copyrightJune, 1971
    date issued1971
    identifier issn0022-0434
    identifier otherJDSMAA-25979#116_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/150534
    description abstractThe well-known method of obtaining sensitivity functions is usually restricted by the condition of continuity imposed on the functions of the coordinates in system equations. For the case of discontinuous functions, more elaborate procedures are required to give a good linear approximation. It is shown that sensitivity functions are discontinuous at the discontinuous points. Also, relations between elements of sensitivity functions at these points are shown to be linear for a given nominal solution of the system. The switching time of the desired Bang-Bang control can be estimated if variations in initial conditions are known. The changes in terminal states and cost function due to deviations in initial conditions can be determined, to first order, by the use of sensitivity functions. Bounds on the deviations in initial conditions can be found by a worst case approach so that the desired terminal conditions are satisfied within given tolerances. The fundamental importance of these techniques in a number of areas of application, for instance, guidance and control of aerospace vehicles, is well known.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInitial Condition Sensitivity Functions and Their Applications
    typeJournal Paper
    journal volume93
    journal issue2
    journal titleJournal of Dynamic Systems, Measurement, and Control
    identifier doi10.1115/1.3426469
    journal fristpage116
    journal lastpage122
    identifier eissn1528-9028
    keywordsFunctions
    keywordsAircraft
    keywordsApproximation AND Equations
    treeJournal of Dynamic Systems, Measurement, and Control:;1971:;volume( 093 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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