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Satellite or spacecraft attitude control - has two layers each of four parallel gyros separately controlled and electrically driven to produce desired reaction forces
Satellite or spacecraft attitude control - has two layers each of four parallel gyros separately controlled and electrically driven to produce desired reaction forces
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机译：卫星或航天器姿态控制-四个平行陀螺仪各有两层，分别进行控制和电气驱动，以产生所需的反作用力
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摘要
The gyro attitude control for the satellite or spacecraft has two layers of four gyros each whose rotation is separately controlled in each direction to generate a controlled reaction force on the craft. The gyros are electrically driven so that no gas jets need to required. The electric drive is powered from solar or nuclear sources for a long life. Angular adjustment is obtained by selective drive of certain gyros.
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