推进技术 ›› 1994, Vol. 15 ›› Issue (2): 68-71.

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液体火箭发动机热试车数据微机自动采集系统

杨乐平   

  1. 国防科技大学航天技术系
  • 发布日期:2021-08-15

A MICROCOMPUTER DATA AUTO-ACQUISITION SYSTEM IN LIQUID ROCKET ENGINE FIRING TESTS

  1. Department of Aerospace Technology, National Universityof Defense Technology, Changsha, 410073
  • Published:2021-08-15

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。

关键词: 数据采集系统;发动机试验;液体推进剂火箭发动机;自动数据处理;微型计算机

Abstract: 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.

Key words: Data acquisition system;Engine test;Liquid Propellant rocket enging;Automatic data processing;Microcomputer