| タイトル | Ground-based implementation and verification of control laws for tethered satellites |
| 著者（英） | Greene, Michael E.; Gwaltney, David A. |
| 著者所属（英） | NASA Langley Research Center|Auburn Univ. |
| 発行日 | 1992-02-01 |
| 言語 | eng |
| 内容記述 | Davis and Banerjee (1990) have developed a tethered-spacecraft system model in which out-of-plane librations are damped, using a length-rate control after the tether has been deployed. Attention is presently given to the implementation of such control schemes to prototype hardware designed for space flight. A prototype reel mechanism has been constructed for use in the Getaway Tether Experiment; both the Davis and Banerjee control scheme and a converted tension-control law have been implemented with tether length and length rate available as feedback. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 92A21185 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/329965 |
