摘要
本文介绍了运载火箭环境温度控制系统,研制开发了以S7-200可编程控制器为核心的温控系统,并阐述了PLC进行控制的原理及软硬件设计。
This paper introduces the temperature controlling system of the rocket environment,developes the temperature controlling system based on the S7 -200 PLC,describes the software and hardware designing and the principle of PLC controlling.
出处
《微计算机信息》
2000年第4期58-59,共2页
Control & Automation