| contributor author | B. Scott May | |
| contributor author | Nicholas P. Jones | |
| date accessioned | 2017-05-08T22:24:12Z | |
| date available | 2017-05-08T22:24:12Z | |
| date copyright | October 1994 | |
| date issued | 1994 | |
| identifier other | 44093518.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/79795 | |
| description 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. | |
| publisher | American Society of Civil Engineers | |
| title | Next Generation Space Telescope. I: Design Considerations | |
| type | Journal Paper | |
| journal volume | 7 | |
| journal issue | 4 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)0893-1321(1994)7:4(355) | |
| tree | Journal of Aerospace Engineering:;1994:;Volume ( 007 ):;issue: 004 | |
| contenttype | Fulltext | |