研究了基于偏航观测器的三轴稳定偏置动量对地定向卫星姿态控制问题。

Attitude control problem of a three-axis stabilized, momentum biased, and nadir-pointing satellite is investigated based on yaw observer.

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对三轴稳定地球同步卫星中用于姿态控制的偏置动量轮转速变化问题进行研究。

This paper researches the variation of the Momentum Wheel(MW) rotation rate which is applied to attitude control in three-axis stabilized GEO satellites.

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如果可能的话，不要使用偏置补偿(脉冲电流)。因为对脉冲电流的感抗可能会使测量不稳定，或者使自动量程功能难于工作。

If possible, do not use offset compensation (pulsed current) because inductive reaction to the current pulse may cause unstable measurements or make autoranging difficult.

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