天线热真空测试多参数测试系统的设计与实现

2018 3rd International Conference on Mechanical, Control and Computer Engineering (ICMCCE) Pub Date : 2018-09-01 DOI:10.1109/ICMCCE.2018.00066

Xi Zhu, W. An, Bin Shen, Qingyu Wang, Yang Liu

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引用次数: 0

摘要

介绍了一种可用于天线热真空测试的多参数测试系统。该系统由一维旋转平台、信号采集、信号传输和伺服控制系统组成。测试中的温度等信号通过信号采集系统进行采集。采集后通过信号传输系统传输到主控系统，并通过以太网与远程计算机连接。给出了天线热真空测试多参数测试系统的硬件结构、通信协议和软件设计。通过在真空热环境下的测试，结果表明该系统测量精度高，稳定性好，能够满足真空热环境条件下天线热测试的要求。

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 and Implementation of Multi-parameter Test System for Antenna Thermal Vacuum Test

This paper introduces a multi-parameter test system that can be used for antenna thermal vacuum test. The system consists of a one-dimensional rotating platform, signal acquisition, signal transmission and servo control system. The temperature and other signals in the test are carried out through the signal acquisition system. It is collected and transmitted to the master control system via a signal transmission system and connected to a remote computer via Ethernet. The hardware structure, communication protocol and software design of the antenna thermal vacuum test multi-parameter test system are given. Through the test in the vacuum heat environment, the results show that the system has high measurement accuracy and good stability, and can meet the requirements of the antenna thermal test under the condition of vacuum heat environment.

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来源期刊

2018 3rd International Conference on Mechanical, Control and Computer Engineering (ICMCCE)

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