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VIRTUAL REACTION WHEEL ARRAY USING CONTROL MOMENT GYROS
VIRTUAL REACTION WHEEL ARRAY USING CONTROL MOMENT GYROS
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机译:使用控制力矩陀螺的虚拟反应轮阵列
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摘要
An attitude control system (ACS) for a spacecraft includes an attitude control assembly (ACA) interface, a control moment gyro (CMG) array and a reaction wheel assembly (RWA) control unit. The ACA interface converts torque commands received from the RWA control unit into CMG gimbal rates for the CMG array. The ACA interface receives CMG gimbal angles from the CMGs and converts the CMG gimbals angles into RWA speeds, which are then provided to the RWA control unit.
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