摘要
在介绍CPC I总线的基础上,提出了一种基于该总线的导弹新型测发控系统,研究了其总体结构和功能,讨论了其主要模块电路和系统软件的设计。通过调试和应用证明,该系统具有可靠性高、测试准确、操作简便和快捷的特点。
On the basis of introducing CPCI-bus, based on the CPCI-bus is put forward. The construction a new checkout-launch-control system of missile and function of such system as well as the design of the main circuits and software are studied. Through debugging system and application in reality, the system based on CPCI-bus is of high reliability, accurate measurement, simplicity of operator and shortcut.
出处
《宇航计测技术》
CSCD
2006年第6期35-38,47,共5页
Journal of Astronautic Metrology and Measurement
关键词
CPCI总线
导弹测发控系统
模块化设计
CPCI-bus, Checkout-launch-control system of missiles ,Modularized design