反作用轮微振动是影响卫星姿态控制精度的重要因素。
Reaction wheel is one of the main disturbance sources for the attitude control system accuracy of spacecraft.
仿真结果表明，该方案可以保证卫星的姿态控制精度、结构振动抑制和控制系统鲁棒性。
Simulation results show that the presented control can ensure the precision of the attitude control performance, suppression of the structure vibrations and robustness of the control system.
数学仿真表明，变结构自动驾驶仪具有很好的快速性和很高的姿态控制精度，可以满足动能拦截器对姿态控制的要求。
The simulation result shows that the variable structure automatic pilot for KKV is fast and has high attitude control accuracy, which satisfies the requirements.
作为应用在航天器上的惯性执行机构，单框架控制力矩陀螺(SGCMG)的操纵性能对航天器姿态控制精度有着极大的影响。
As inertial actuators mounted on the spacecraft, Single Gimbal control Moment Gyroscopes (SGCMGs) can affect the attitude control accuracy to a great extent.
作为应用在航天器上的惯性执行机构，单框架控制力矩陀螺(SGCMG)的操纵性能对航天器姿态控制精度有着极大的影响。
As inertial actuators mounted on the spacecraft, Single Gimbal control Moment Gyroscopes (SGCMGs) can affect the attitude control accuracy to a great extent.
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