| タイトル | Validating GOES Instrument Thermal Deformations |
| 本文（外部サイト） | http://hdl.handle.net/2060/20010084974 |
| 著者（英） | Ghaffarian, Benny; Sayal, Chetan; Harter, Peter; Pugh, Brett; Chu, Don; Ng, Ray; Wilkin, Paul |
| 著者所属（英） | ITT Industries, Inc. |
| 発行日 | 2001-06-01 |
| 言語 | eng |
| 内容記述 | Comparison of the Geostationary Operational Environmental Satellite (GOES) instrument thermal model predictions with on-orbit data shows that the models capture the observed temperature and misalignment trends. Lack of precise knowledge as to spacecraft pointing precludes such comparison with instrument pointing predictions. Based on the models, thermally induced instrument attitude variation will dominate GOES N-Q Image Motion Compensation (IMC). Errors due to day-to-day changes in the attitude profiles are predicted to be under 10 microradians except for rapid scans where disturbances may reach 30 microradians. |
| NASA分類 | Spacecraft Instrumentation and Astrionics |
| 権利 | No Copyright |
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