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    Next Generation Space Telescope. I: Design Considerations

    Source: Journal of Aerospace Engineering:;1994:;Volume ( 007 ):;issue: 004
    Author:
    B. Scott May
    ,
    Nicholas P. Jones
    DOI: 10.1061/(ASCE)0893-1321(1994)7:4(355)
    Publisher: American Society of Civil Engineers
    Abstract: The pointing control system of the Hubble Space Telescope (HST) represents the current state of the art for the precision control of a large spacecraft. The proposed Next Generation Space Telescope (NGST) will require an order‐of‐magnitude increase in pointing resolution over that of HST. The use of active optics in the form of a steerable secondary mirror has been proposed for NGST in order to satisfy these requirements. An introduction to some of the design concepts associated with the design of the NGST, including a description of the proposed vehicle, a description of the pertinent design parameters, and a description of the types of disturbances to which it may be subjected, is given herein. A companion paper provides a description of a feasibility study conducted to evaluate the use of a control system for the implementation of “beam steering” to compensate for the motion of the vehicle without necessitating the reorientation of the whole structure.
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      Next Generation Space Telescope. I: Design Considerations

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    http://yetl.yabesh.ir/yetl1/handle/yetl/79795
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    contributor authorB. Scott May
    contributor authorNicholas P. Jones
    date accessioned2017-05-08T22:24:12Z
    date available2017-05-08T22:24:12Z
    date copyrightOctober 1994
    date issued1994
    identifier other44093518.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/79795
    description abstractThe pointing control system of the Hubble Space Telescope (HST) represents the current state of the art for the precision control of a large spacecraft. The proposed Next Generation Space Telescope (NGST) will require an order‐of‐magnitude increase in pointing resolution over that of HST. The use of active optics in the form of a steerable secondary mirror has been proposed for NGST in order to satisfy these requirements. An introduction to some of the design concepts associated with the design of the NGST, including a description of the proposed vehicle, a description of the pertinent design parameters, and a description of the types of disturbances to which it may be subjected, is given herein. A companion paper provides a description of a feasibility study conducted to evaluate the use of a control system for the implementation of “beam steering” to compensate for the motion of the vehicle without necessitating the reorientation of the whole structure.
    publisherAmerican Society of Civil Engineers
    titleNext Generation Space Telescope. I: Design Considerations
    typeJournal Paper
    journal volume7
    journal issue4
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(1994)7:4(355)
    treeJournal of Aerospace Engineering:;1994:;Volume ( 007 ):;issue: 004
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    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