| 发明名称 |
Fully redundant spacecraft power and attitude control system |
| 摘要 |
An energy storage flywheel (106) system for a spacecraft is implemented with a fully redundant rotating group and gimbal actuator (324). In particular, the gimbal actuator (324), motor/generator (330), primary bearings (342), and secondary bearing actuator (354) are each implemented with a pair of redundant coils or motors. |
| 申请公布号 |
EP1912312(A3) |
申请公布日期 |
2009.09.02 |
| 申请号 |
EP20070112367 |
申请日期 |
2007.07.12 |
| 申请人 |
HONEYWELL INTERNATIONAL INC. |
发明人 |
POTTER, CALVIN C;CORCINO, DAVID;WINGETT, PAUL T.;HANLON, CASEY |
| 分类号 |
H02K7/09;H02K7/02 |
主分类号 |
H02K7/09 |
| 代理机构 |
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代理人 |
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| 主权项 |
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| 地址 |
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