基于MODBUS运载火箭热环境的远程群控系统设计

2021 3rd International Conference on Intelligent Control, Measurement and Signal Processing and Intelligent Oil Field (ICMSP) Pub Date : 2021-07-23 DOI:10.1109/ICMSP53480.2021.9513336

Yijie Li, Hong Li, Pu Li, Ying Cheng

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引用次数: 1

摘要

针对运载火箭地面仿真实验中区域划分多、装置长度不同、模型曲线不同等问题，设计并实现了火箭热环境远程群控方案。该系统以108台交直流转换电力电子设备为主要电源元件，采用以太网Modbus TCP/IP通信协议，采用组态软件WinCC和S7-200智能PLC作为执行终端。通过多端口开关，实现计算机对108台交直流转换电力电子设备的监控。该系统已在北京某科研院所成功应用，提高了工作效率，保证了运行的可靠性和稳定性。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Design of remote group control system based on thermal environment of MODBUS launch vehicle

Aiming at the problems of the ground simulation experiment of carrier rocket, such as the large number of regions divided, the different length of the device and the different model curve, the remote group control scheme of the rocket thermal environment was designed and realized. The system takes 108 sets of AC-DC conversion power electronic devices as the main power components, uses Ethernet Modbus TCP/IP communication protocol, and applies configuration software WinCC and S7-200 Smart PLC as the execution terminal. To be realized the monitoring of 108 AC - DC conversion power electronic equipment by a computer via multi-port switch. The system has been successfully applied in a research institute in Beijing, which improves the working efficiency and ensures the reliability and stability of the operation.

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来源期刊

2021 3rd International Conference on Intelligent Control, Measurement and Signal Processing and Intelligent Oil Field (ICMSP)

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