| タイトル | A preliminary study of the attitude control for the Shuttle Tethered Satellite System |
| 著者（英） | Gresham, L. L.; Rupp, C. C. |
| 著者所属（英） | Mississippi State Univ.|NASA Marshall Space Flight Center |
| 発行日 | 1979-01-01 |
| 言語 | eng |
| 内容記述 | The objective of this investigation is to determine the equations of motion governing the attitude of a tethered satellite and subsequently to gain insight toward obtaining an appropriate control law. This study relates the coupling of the rotational dynamics of the satellite with the dynamical system of the Orbiter already constructed. In particular, a simplified approach is utilized to describe the satellite as constrained to planar motion. Modifications to the existing tethered satellite trajectory simulation provide a conceptual study of the satellite's behavior and its effect on the overall system. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 79A50032 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/425557 |
