The error between satellite attitude dynamics and its linearized model can affect the attitude control precision.

卫星姿态动力学系统与其线性化模型之间的误差会影响姿态控制的精度。

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And in the midcourse velocity correction segment, effects on the state error propagation caused by attitude errors and control system performance of the chasing satellite were studied.

在中途速度修正段，分析了追踪航天器姿态误差和控制系统性能误差对状态误差传播的影响。

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