| タイトル | Modeling and tachometer feedback in the control of an experimental single link flexible structure |
| 著者（英） | Inman, Daniel J.; Garcia, Ephrahim |
| 著者所属（英） | State Univ. of New York |
| 発行日 | 1990-01-01 |
| 言語 | eng |
| 内容記述 | In this work a formulation for the modeling of a single link flexible structure will be introduced that includes the effects of dynamic interaction between the actuator and structure. These effects are the rotational modal participation factors for the structure's vibratory motion that occurs at the slewing axis. It will be shown, both theoretically and experimentally, that this dynamic interaction can be advantageous for vibration suppression of the flexible modes of the system during slewing positioning maneuvers. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 91A35540 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/348479 |
