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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


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