摘要
介绍了一种采用PC/AT总线微机的液体火箭发动机热试车数据自动采集系统。该系统能同时完成模拟和脉冲两类信号的自动采集,采集软件由汇编语言编写,定时采集由计算机内部时钟中断实现,软件设计考虑了不同信号对采样时间的特殊要求。
This paper describes a data auto-acquisition system of PC/AT buscomputer in liquid rocket engine firing tests. This system can be able to deal withboth analog information and frequency inputs, the acqusition software is written inassemble language. The sampling time is provided by internal timer interrupt ofcomputer. The special requirements of different signals for sampling periods aretaken in account of the software design.
出处
《推进技术》
EI
CAS
CSCD
北大核心
1994年第2期68-71,共4页
Journal of Propulsion Technology
关键词
数据采集
发动机试验
火箭发动机
Data acquisition system,Engine test,Liquid Propellant rocket enging,Automatic data processing,Microcomputer