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    Influence of Stored Angular Momentum on the Modal Characteristics of Spacecraft With Flexible Appendages

    Source: Journal of Applied Mechanics:;1975:;volume( 042 ):;issue: 004::page 785
    Author:
    P. C. Hughes
    ,
    H. N. Sharpe
    DOI: 10.1115/1.3423706
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The attitude dynamics and control of flexible spacecraft are more clearly understood if the natural frequencies of oscillation are known for these spacecraft. The influence of stored angular momentum hs (for example, dual-spin vehicles, or vehicles with a momentum wheel) on these natural frequencies is determined in terms of the appendage characteristics, the inertia distribution, and hs . Primary emphasis is placed on general qualitative results. The discussion is illustrated with an example.
    keyword(s): Angular momentum , Space vehicles , Vehicles , Frequency , Particle spin , Inertia (Mechanics) , Oscillations , Dynamics (Mechanics) , Momentum AND Wheels ,
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      Influence of Stored Angular Momentum on the Modal Characteristics of Spacecraft With Flexible Appendages

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    http://yetl.yabesh.ir/yetl1/handle/yetl/86970
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    contributor authorP. C. Hughes
    contributor authorH. N. Sharpe
    date accessioned2017-05-08T22:57:35Z
    date available2017-05-08T22:57:35Z
    date copyrightDecember, 1975
    date issued1975
    identifier issn0021-8936
    identifier otherJAMCAV-26047#785_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/86970
    description abstractThe attitude dynamics and control of flexible spacecraft are more clearly understood if the natural frequencies of oscillation are known for these spacecraft. The influence of stored angular momentum hs (for example, dual-spin vehicles, or vehicles with a momentum wheel) on these natural frequencies is determined in terms of the appendage characteristics, the inertia distribution, and hs . Primary emphasis is placed on general qualitative results. The discussion is illustrated with an example.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInfluence of Stored Angular Momentum on the Modal Characteristics of Spacecraft With Flexible Appendages
    typeJournal Paper
    journal volume42
    journal issue4
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.3423706
    journal fristpage785
    journal lastpage788
    identifier eissn1528-9036
    keywordsAngular momentum
    keywordsSpace vehicles
    keywordsVehicles
    keywordsFrequency
    keywordsParticle spin
    keywordsInertia (Mechanics)
    keywordsOscillations
    keywordsDynamics (Mechanics)
    keywordsMomentum AND Wheels
    treeJournal of Applied Mechanics:;1975:;volume( 042 ):;issue: 004
    contenttypeFulltext
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    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian