| タイトル | Precision orbit raising trajectories |
| 著者（英） | Flanagan, P. F.; Horsewood, J. L.; Pines, S. |
| 発行日 | 1975-03-01 |
| 言語 | eng |
| 内容記述 | A precision trajectory program has been developed to serve as a test bed for geocentric orbit raising steering laws. The steering laws to be evaluated have been developed using optimization methods employing averaging techniques. This program provides the capability of testing the steering laws in a precision simulation. The principal system models incorporated in the program are described, including the radiation environment, the solar array model, the thrusters and power processors, the geopotential, and the solar system. Steering and array orientation constraints are discussed, and the impact of these constraints on program design is considered. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 75A24960
AIAA PAPER 75-354 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/448817 |
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