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    Singular Direction Escape Steering Law for Control Moment Gyros

    Source: Journal of Aerospace Engineering:;2017:;Volume ( 030 ):;issue: 005
    Author:
    Yanning Guo
    ,
    Hutao Cui
    ,
    Guangfu Ma
    ,
    Chuanjiang Li
    DOI: 10.1061/(ASCE)AS.1943-5525.0000724
    Publisher: American Society of Civil Engineers
    Abstract: This paper proposes a new singularity direction escape steering law for control moment gyros (CMG) using singular value decomposition (SVD). The proposed steering law differs from the classical singular direction avoidance (SDA) steering law in two respects. First, torque errors are introduced in the direction of the smallest two singular values through modification of the diagonal matrix. This is done by tuning parameters related to the magnitude of torque error so that both singularity avoidance and escape performance can be achieved. Second, instead of using a conventional singularity measure, new output torque metrics of the CMG cluster along the torque command direction are introduced and adopted in this steering law, so as to reduce unnecessary torque error for certain near-singular circumstances. Several numerical simulations are provided at last, and comparisons with existing steering laws are presented to demonstrate the superior performance of the proposed method.
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      Singular Direction Escape Steering Law for Control Moment Gyros

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4242017
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    contributor authorYanning Guo
    contributor authorHutao Cui
    contributor authorGuangfu Ma
    contributor authorChuanjiang Li
    date accessioned2017-12-16T09:22:24Z
    date available2017-12-16T09:22:24Z
    date issued2017
    identifier other%28ASCE%29AS.1943-5525.0000724.pdf
    identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4242017
    description abstractThis paper proposes a new singularity direction escape steering law for control moment gyros (CMG) using singular value decomposition (SVD). The proposed steering law differs from the classical singular direction avoidance (SDA) steering law in two respects. First, torque errors are introduced in the direction of the smallest two singular values through modification of the diagonal matrix. This is done by tuning parameters related to the magnitude of torque error so that both singularity avoidance and escape performance can be achieved. Second, instead of using a conventional singularity measure, new output torque metrics of the CMG cluster along the torque command direction are introduced and adopted in this steering law, so as to reduce unnecessary torque error for certain near-singular circumstances. Several numerical simulations are provided at last, and comparisons with existing steering laws are presented to demonstrate the superior performance of the proposed method.
    publisherAmerican Society of Civil Engineers
    titleSingular Direction Escape Steering Law for Control Moment Gyros
    typeJournal Paper
    journal volume30
    journal issue5
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000724
    treeJournal of Aerospace Engineering:;2017:;Volume ( 030 ):;issue: 005
    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