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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 launch vehicle environmental temperature control system, developed a temperature control system based on the S7-200 programmable logic controller, and describes the PLC control principle and hardware and software design.