航天器环境工程2013，Vol.30Issue(3)：286-291,6.DOI:10.3969/j.issn.1673-1379.2013.03.012
基于统一建模语言(UML)的航天器真空热试验测控系统电气建模
UML-based electrical modeling of the measurement and control system for spacecraft vacuum thermal test
摘要
Abstract
With the bulk and scale production of spacecraft and the accelerated proces;s of the new model development,the spacecraft vacuum thermal tests are required in more and more diverse conditions.For example,the temperature measurement and control is becoming more and more complicated,and the existing system gradually shows its inherent inadequacy.This paper focuses on the measurement and control electrical system,based on the united modeling language(UML) analysis and a system model is proposed to increase the information processing capability of the test equipment,to enhance the system design human-computer interaction level,and thus to improve the state tracking functions during the test.It is demonstrated through the actual case application that the reliability of the test is enhanced by the electric model.关键词
航天器/真空热试验/测控系统/统一建模语言/电气模型Key words
spacecraft/ vacuum thermal test/ measurement and control system/ united modeling language (UML)/ electrical model分类
信息技术与安全科学引用本文复制引用
龚喆,刘国青,裴一飞,刘畅,姚乃明..基于统一建模语言(UML)的航天器真空热试验测控系统电气建模[J].航天器环境工程,2013,30(3):286-291,6.基金项目
北京卫星环境工程研究所自主研发项目"航天器真空热试验集群测控平台方案研究" （）
