While gyro and trail effects can contribute to stability, other factors such as the distribution of mass and the bike's moment of inertia can play a role as well.
The design of a gradient singularity avoidance pseudo-inverse control law used for double gimbal control momentgyro (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 momentgyro (SGCMG) configuration of a large spacecraft is studied. First, the research object of analyzing configuration is restricted.