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航天器主动姿态控制系统
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航天器主动姿态控制系统
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航天器主动姿态控制系统
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spacecraft active attitude control system
航天器主动姿态控制系统
根据姿态误差(测量值与标称值之差)形成控制指令,产生控制力矩来实现航天器姿态控制的系统。
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