| タイトル | Development of a magnetic acquisition and attitude control system for spinning rocket payloads |
| 著者（英） | Olney, D. J.; Shiftlett, L. F. |
| 著者所属（英） | NASA Goddard Space Flight Center |
| 発行日 | 1982-01-01 |
| 言語 | eng |
| 内容記述 | An attitude control system capable of pointing the roll principle axis of a spinning payload to within one degree of the magnetic field vector was flown successfully in 1981-82 aboard three Black Brant X payloads and one Terrier Malemute payload, and additional flights with the system have been requested. Using a filtered linear combination of signals provided by a single-axis rate gyro and a two-axis magnetometer, and control actuation from two cold-gas thrusters, the system can be assembled from standard rocket components and fitted to any payload size. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 82A48044
AIAA PAPER 82-1734 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/408548 |
