摘要
介绍了飞机排气活门控制系统的结构以及BIT技术分类,并将控制系统按其功能划分为核心数字电路、串行通信接口、输入通道和输出通道4个模块。通过对各个模块故障特征的分析,给出各个模块的BIT设计方法。
The structure of outflow valve control system for aircraft and the BIT technology classification were introduced. In accordance with the functions of the control system, it was divided into four modules, including the core digital circuit, the serial communication interface, the inputs channel and the output channel. Based on analyzing the fault characteristic of each module, BIT design methods were described.
出处
《机床与液压》
北大核心
2012年第1期99-102,共4页
Machine Tool & Hydraulics