This thesis designed an universal test system for missiles 'launch and control system, which based on VXIbus.
现有的检测装置多为针对某一特定型号发控系统的专用设备，通用性差、研制周期长。
The "VXIbus synchronous Data acquisition Module" presented in this dissertation supports real-time synchronous acquisition, storage and processing of the multi-channel inputs.
本文设计的VXI同步数据采集模块是一种支持多个通道以同步的方式对输入信号进行实时采集、存储和处理的测量模块。
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