| タイトル | Advanced actuators for the control of large space structures |
| 本文（外部サイト） | http://hdl.handle.net/2060/19930018383 |
| 著者（英） | Johnson, Bruce; Hockney, Richard; Misovec, Kathleen; Downer, James |
| 著者所属（英） | SatCon Technology Corp. |
| 発行日 | 1993-01-01 |
| 言語 | eng |
| 内容記述 | The objective of this research was to develop advanced six-degree-of-freedom actuators employing magnetic suspensions suitable for the control of structural vibrations in large space structures. The advanced actuators consist of a magnetically suspended mass that has three-degrees-of-freedom in both translation and rotation. The most promising of these actuators featured a rotating suspended mass providing structural control torques in a manner similar to a control moment gyro (CMG). These actuators employ large-angle-magnetic suspensions that allow gimballing of the suspended mass without mechanical gimbals. Design definitions and sizing algorithms for these CMG type as well as angular reaction mass actuators based on multi-degree-of-freedom magnetic suspensions were developed. The performance of these actuators was analytically compared with conventional reaction mass actuators for a simple space structure model. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 93N27572 |
| 権利 | No Copyright |
