The rapid speed attitude maneuver based on SGCMG for small satellite is also studied.
研究了使用SGCMG的航天器的快速姿态机动问题。
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。
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