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CMG(控制力矩陀螺)用于低轨道三轴稳定对地定向卫星时,会受到卫星轨道角速度引起的陀螺力矩扰动.本文从工程实现的简单性和软硬件的利用性考虑,推导了一种能够补偿卫星轨道角速度影响的DGCMG(双框架控制力矩陀螺)控制规律.
CMG (Control Moment Gyro) is used in low-orbit three-axis stable earth-oriented satellite, it will be subject to the satellite orbit angular velocity caused by the gyroscopic torque disturbance.This article from the engineering realization of the simplicity and hardware and software considerations, derived a can DGCMG (Double Frame Control Moment Gyro) Control Law to Compensate for the Influence of Orbit Angular Velocity.