Information sensing is provided by transducers which detect relative angular displacements between the gyrogimbal and the supporting case.
信号的敏感是由能探测陀螺框架和支撑结构间的相对角位移的传感器来提供的。
2
The design of a gradient singularity avoidance pseudo-inverse control law used for double gimbal control moment gyro (DGCMG), its principle and calculation were introduced.
提出了一种用于双框架控制力矩陀螺的梯度型伪逆控制律,介绍了控制律的原理与计算方法。
3
The single gimbal control moment gyro (SGCMG) configuration of a large spacecraft is studied. First, the research object of analyzing configuration is restricted.