... This is the EPS SMS SA angle following the SA slew. ... Calendar 120167B1 Start Stop V1-SUN Beta Bay 5 Bay 8 Bay 10 ddd:hh:mm:ss ddd:hh:mm:ss RA DEC PA OR Angle Angle Incid Incid Incid 016 :00:00:00 016 :00:27:24 188 -31 118 0 94 1.8 80 15 75 ...
... This is the EPS SMS SA angle following the SA slew. ... 2 92.293 24.390 SMS037Q 2003.110 :03:44:55 92.485 24.239 13.9 WFPC2 AP17 Controlled Exposures in SC105N00 Start Time Duration(sec) End Time(approx) SCAP --------------------------------------...
... This is the EPS SMS SA angle following the SA slew. ... Calendar 100327A5 Start Stop V1-SUN Beta Bay 5 Bay 8 Bay 10 ddd:hh:mm:ss ddd:hh:mm:ss RA DEC PA OR Angle Angle Incid Incid Incid 032 :00:00:00 032 :00:41:01 84 -69 228 0 86 11.2 80 15 75 ...
... limited by the accuracy of the guide star acquisition positional uncertainty ... 60" on the largest spacecraft move that can be done while using the same guide star ...
[
Текст
]
Ссылки http://www.stsci.edu/jwst/instruments/miri/docarchive/JWST-STScI-001407.pdf -- 489.4 Кб -- 05.02.2013 Похожие документы
... uncertainty within any science instrument and the guider shall not exceed 0.005 ... any JWST observation anyway because of the finite accuracy of its guide star catalog ...