The structure of the hardware and software of an aviation gyroscopic test system combined by industrial control computer, interface controller and test adapter is introduced.
介绍了工业控制计算机、接口控制箱、测试适配器组成的航空陀螺综合测试系统的硬件和软件结构。
The control flow of decreasing gyroscopic coupling is presented.
给出了减小陀螺效应耦合的控制流程。
It discusses the influence of ground control network, underground traverse survey, shaft orientation and gyroscopic orientation edge append-survey on breakthrough precision.
分析了地面控制网、井下导线测量、立井定向和加测陀螺定向边对贯通大型巷道精度的影响；讨论了提高测量精度的可行性方法。
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