Auto test system (ATS) of missile conducting instrument was introduced based on virtual instrument structure, its hardware allocation and software module design under Lab Windows/CVI were discussed in detail.
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介绍了一种基于虚拟仪器结构的导弹指挥仪自动测试系统 ,详细讨论了该系统的硬件配置和在LabWindows/CVI环境下的软件模块化设计
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