某型导弹发控设备自动测试系统设计

Design of missile inertial guidance equipment automatic test system

阐述了某型导弹发控设备自动测试系统的设计思想、硬件组成和软件设计。系统采用基于网络数据采集卡的虚拟仪器结构,实现了对某型导弹发控设备的自动测试,具有较高的可靠性、可维修性和良好的使用性。

This paper describes a type of missile launch and control equipment, automatic test system design, hardware components and software design. System uses a Web-based virtual instrument data acquisition card of the structure, the realization of a missile launch and control equipment, automatic test, with high reliability, maintainability and good usability.