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Fully redundant spacecraft power and attitude control system
Fully redundant spacecraft power and attitude control system
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机译:完全冗余的航天器动力和姿态控制系统
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摘要
An energy storage flywheel system for a spacecraft is implemented with a fully redundant rotating group and gimbal actuator. In particular, the gimbal actuator, motor/generator, primary bearings, and secondary bearing actuator are each implemented with a pair of redundant coils or motors.
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