| タイトル | Seasat-A attitude control system |
| 著者（英） | Rodden, J. J.; Weiss, R.; Hendricks, R. J. |
| 著者所属（英） | Lockheed Missiles and Space Co. |
| 発行日 | 1977-01-01 |
| 言語 | eng |
| 内容記述 | The Seasat-A attitude control system controls the attitude of the satellite system during injection into final circular orbit after Atlas boost, during orbit adjust and trim phases, and throughout the 3-year mission. Ascent and injection guidance and attitude control are provided by the Agena spacecraft with a gyrocompassed mass expulsion system. On-orbit attitude control functions are performed by a system that has its functional roots in the gravity-gradient momentum bias technology. The paper discusses hardware, control laws, and simulation results. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 77A42769
AIAA PAPER 77-1057 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/437048 |
