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An investigation into the milliarcsecond attitude control errors of Hubble Space TelescopeAn analysis of the fine pointing errors of the Hubble Space Telescope (HST), in the range from 1 to 15 milliarcsecs, is reported on. The emphasis is on the study of the performance characteristics of the pointing control system, fine guidance sensors and the optical telescope assembly, which produce relative attitude and astrometric measurement errors. Since the first servicing mission in December 1993, the HST relative short term position stability is of the order of 3 milliarcsecs RMS when averaged over 1 min intervals. At this level of accuracy, longer term systematic attitude errors in this range can have a noticeable impact on the telescope's observations. The various error sources are described, including: internal temperature effects; spacecraft structure temperature effects; calibration procedures, and computational inaccuracies.
Document ID
19980137219
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Bradley, A. J.
(Allied-Signal Aerospace Co. Seabrook, MD United States)
Chapman, R. D.
(Allied-Signal Technical Services Corp. Lanham, MD United States)
Kalinowski, J. K.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Kimmer, E.
(Allied-Signal Technical Services Corp. Lanham, MD United States)
Welter, G.
(Computer Sciences Corp. Laurel, MD United States)
Whittier, W.
(Lockheed Missiles and Space Co. Greenbelt, MD United States)
Date Acquired
August 18, 2013
Publication Date
August 1, 1997
Subject Category
Astronomy
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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