| 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 |
|
