摘要
分析飞机综合模块航电(IMA)系统的已有技术和计算机应用技术,研究飞机综合模块航电系统的物理拓扑,及典型系统接口,初步定义不同构型飞机综合模块航电电气系统的基本架构及接口。
Studying physical topology and typical interface of airplane IMA system based on analysis of existed air- plane IMA computer and its application technologies, then preXiminary definitions for fundamental electrical system architecture and its interface with different airplane IMA configurations are presented.
出处
《民用飞机设计与研究》
2013年第A02期13-18,共6页
Civil Aircraft Design & Research
