| タイトル | Mechanism test bed. Flexible body model report |
| 本文（外部サイト） | http://hdl.handle.net/2060/19910020847 |
| 著者（英） | Compton, Jimmy |
| 著者所属（英） | Control Dynamics Co. |
| 発行日 | 1991-07-01 |
| 言語 | eng |
| 内容記述 | The Space Station Mechanism Test Bed is a six degree-of-freedom motion simulation facility used to evaluate docking and berthing hardware mechanisms. A generalized rigid body math model was developed which allowed the computation of vehicle relative motion in six DOF due to forces and moments from mechanism contact, attitude control systems, and gravity. No vehicle size limitations were imposed in the model. The equations of motion were based on Hill's equations for translational motion with respect to a nominal circular earth orbit and Newton-Euler equations for rotational motion. This rigid body model and supporting software were being refined. |
| NASA分類 | RESEARCH AND SUPPORT FACILITIES (AIR) |
| レポートNO | 91N30161
NASA-CR-184189
NAS 1.26:184189 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/131255 |
