| タイトル | Mechanisms of the Space Active Vibration Isolation (SAVI) |
| 著者（英） | Schmitt, Frank |
| 著者所属（英） | Honeywell, Inc. |
| 発行日 | 1992-05-01 |
| 言語 | eng |
| 内容記述 | The Space Active Vibration Isolation (SAVI) is a concept for vibration isolation of one body from another with simultaneous precise control in 6 Degrees Of Freedom (DOF). SAVI achieves this using a combination of electromechanical linear actuators and magnetic actuators. Other mechanisms of interest include a structure for simulating the body being pointed, an apparatus to simulate the body that is the vibration source, and mechanisms to off-load the weight of each of these two bodies from the experiment to approximate a zero-g condition. A SAVI was built and tested to demonstrate these capabilities. |
| NASA分類 | STRUCTURAL MECHANICS |
| レポートNO | 92N25084 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/231567 |
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