A new detecting method of avoidability of singular states was proposed which was suitable for SGCMG systems.
在研究SGCMG系统的运动奇异机理及零运动的基础上，提出了一种判别奇异状态可回避性的新方法。
A survey of steering laws for Single Gimbal Control Moment Gyroscope (SGCMG) systems is made. Meanwhile, steering performance of the art is appreciated.
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。
The single gimbal control moment gyro (SGCMG) configuration of a large spacecraft is studied. First, the research object of analyzing configuration is restricted.
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 character of SGCMG system in the form of zero motion differential dynamic equation is given. The criterion of singularity escapable from reference 4 is improved.
给出了该零运动微分动力学下具有冗余度的单框架控制力矩陀螺系统奇异状态的性质，并改进了奇异可脱离性的判别方法。
In this paper, the Angle measuring system using in Single Gimbal Control Moment Gyroscope (SGCMG) is discussed after introducing the basic theory of resolver-to-angle converter.
在介绍集成轴角变换器的工作原理后，详细介绍了用于控制力矩陀螺速率控制系统中的测角系统。
In this paper, the Angle measuring system using in Single Gimbal Control Moment Gyroscope (SGCMG) is discussed after introducing the basic theory of resolver-to-angle converter.
在介绍集成轴角变换器的工作原理后，详细介绍了用于控制力矩陀螺速率控制系统中的测角系统。
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