タイトル | Orbiter attitude design for the Astro-1 Spacelab mission |
著者(英) | Echols, R. T.; Stewart, R. L.; Olsen, C. D.; Onken, J. F.; Horvath, T. J.; Woods, W. K. |
著者所属(英) | NASA Marshall Space Flight Center |
発行日 | 1992-03-01 |
言語 | eng |
内容記述 | The methods utilized to design orbiter attitudes that satisfied the various Space Shuttle program and payload constraints of the Astro-1 Spacelab astronomy mission are described. The premission methods developed for attitude design and how those methods were applied to accomplish the large amount of real-time replanning required during the flight are presented. Some of the attitude concerns for Astro-1 included orbiter window thermal constraints, two separate telescope fields-of-view, tracking and data relay satellite Ku-band access, and telescope sun avoidance. |
NASA分類 | ASTRONOMY |
レポートNO | 92A38587 AIAA PAPER 92-1466 |
権利 | Copyright |
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