| タイトル | Docking of a rigid spacecraft with unrestrained orbiting flexible structure |
| 本文（外部サイト） | http://hdl.handle.net/2060/19830013989 |
| 著者（英） | Kane, T. R. |
| 著者所属（英） | Stanford Univ. |
| 発行日 | 1983-04-01 |
| 言語 | eng |
| 内容記述 | A methodology for producing simulations of the docking of a rigid spacecraft with any unrestrained flexible structure was studied. A detailed algorithm for the simulation of the docking of a rigid body with a nonuniform unrestrained beam was sought. The values acquired during docking by the variables characterizing the motions of the rigid body and the unrestrained beam were sought. |
| NASA分類 | ASTRONAUTICS (GENERAL) |
| レポートNO | 83N22260 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/567486 |
