首页 | 本学科首页   官方微博 | 高级检索  
     

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
引用本文: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
作者姓名:龚喆  刘国青  裴一飞  刘畅  姚乃明
作者单位:1.可靠性与环境工程技术重点实验室, 北京 100094
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"
摘    要:随着航天器批量化生产及新型号研制进程加快,航天器真空热试验需求越来越多样,试验温度测量与控制的复杂程度越来越高,现有测控系统逐渐暴露出固有缺陷。文章针对测控电气系统,基于统一建模语言(UML)分析并提出了系统模型,提高了试验设备信息的处理能力,增强了系统设计人机交互的规范性,改进了试验进行时状态跟踪效果。通过实际的案例应用,展示了通过电气模型提高试验可靠性的过程。

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

UML-based electrical modeling ofthe measurement and control system for spacecraft vacuum thermal test
Gong Zhe,Liu Guoqing,Pei Yifei,Liu Chang and Yao Naiming. UML-based electrical modeling ofthe measurement and control system for spacecraft vacuum thermal test[J]. Spacecraft Environment Engineering, 2013, 30(3): 286-291
Authors:Gong Zhe  Liu Guoqing  Pei Yifei  Liu Chang  Yao Naiming
Affiliation:1.Beijing Institute of Spacecraft Environment Engineering, Beijing 100094, China2.Science and Technology on Reliability and Environmental Engineering Laboratory
Abstract:With the bulk and scale production of spacecraft and the accelerated process 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.
Keywords:spacecraft  vacuum thermal test  measurement and control system  united modeling language (UML)  electrical model
本文献已被 CNKI 维普 万方数据 等数据库收录!
点击此处可从《航天器环境工程》浏览原始摘要信息
点击此处可从《航天器环境工程》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号