根据实际情况限定了大型航天器单框架控制力矩陀螺（SGCMG）构型分析研究的对象；
The single gimbal control moment gyro (SGCMG) configuration of a large spacecraft is studied. First, the research object of analyzing configuration is restricted.
综述了单框架控制力矩陀螺(SGCMG)系统操纵律研究概况，并对现存操纵律的性能进行了评价。
A survey of steering laws for Single Gimbal Control Moment Gyroscope (SGCMG) systems is made. Meanwhile, steering performance of the art is appreciated.
在单框架控制力矩陀螺(SGCMG)系统操纵律的设计中，通常假定框架伺服系统具有理想的伺服跟踪性能。
Gimbal servo systems of single gimbal control moment gyroscopes (SGCMGs) are often assumed to have ideal tracking performance during the steering law design.
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