给出了反馈力矩系数，分析了力矩系数对提高加速度表量程和保证精度的作用。
The moment reactive coefficient is given, and the effect of moment reactive coefficient on expanding the measurement range and improving the accuracy of force-balance accelerometer is analyzed.
卫星姿控飞轮是由三相轮流换向无刷直流电动机驱动的，采用力矩控制(电流反馈)模式。
Satellite attitude control flywheel is driven by three-phase alternate commutating brushless DC motor, schema of which is torque control model (current feedback).
本文给出了力矩反馈控制的实现方法。
This paper presents the realization method of the torque feedback control.
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