| タイトル | Space station docking mechanism dynamic testing |
| 本文（外部サイト） | http://hdl.handle.net/2060/19890003225 |
| 著者（英） | Glaese, John R.; Howsman, Thomas G. |
| 著者所属（英） | Control Dynamics Co. |
| 発行日 | 1988-01-01 |
| 言語 | eng |
| 内容記述 | A prototype docking mechanism for the Space Station was designed and fabricated for NASA. This docking mechanism is actively controlled and uses a set of electromechanical actuators for alignment and load attenuation. Dynamic tests are planned using the Marshall Space Flight Center's 6-DOF Motion Simulator. The proposed tests call for basic functionality verification as well as complete hardware-in-the-loop docking dynamics simulations. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 89N12596 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/144738 |
