本文探讨振动陀螺的工作原理，包括其构造，运动方程序，误差分析。
This paper approaches the principle of operation for a vibratory gyro, as well as its configuration, movement equation and error analysis.
发动机喷管与火箭固联时的横向运动方程序及其相应的边界条件是分析工作的基础。
The equations of transverse movement when nozzle connected rigidly with rocket and related boundary conditions form the basis for analyses.
本文直接以双万向联轴器为研究对象，应用矢量分析法，列出了双万向联轴器的运动方程序。
In this paper, motion equations of the double universal joint are given by using the vector analysis.
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