1.A technique for estimation of gyro installation errors in gimbaled INS was presented based on the oscillation around gyro input axis.
介绍了一种用于测量平台式惯性导航系统陀螺安装误差的陀螺轴扰动技术。
2.The S-IVB stage has its single engine gimbaled in pitch and yaw .
IVB级有一个单独摆动发动机来作俯仰和偏航。
3.Spacecraft attitude control using parallel-gimbaled variable speed control moment gyros group
采用平行构型变速控制力矩陀螺群的航天器姿态控制