摘要
本文介绍了PDP-11/03微型计算机在固体火箭发动机六分力试验中的数据采集和处理,论述了该系统的组成、功能和特点,最后给出了测试系统静态精度的测定值。
This paper describes a system using a PDP-11/03 microcomputer for the data acquisition and processing in six-component tests for solid rocket motors, and giving the chief techincal performance, structural components. function and features of the system. Relative experimental data are collected and a comparison made between those manually and computer processed. Static precision of the test system is given.
出处
《兵工学报》
EI
CAS
1987年第3期73-75,共3页
Acta Armamentarii
