航天器环境工程2017，Vol.34Issue(6)：679-684,6.DOI:10.3969/j.issn.1673-1379.2017.06.018
大型航天器真空热试验过程管理系统设计与实现
Design and implementation of vacuum thermal test process management
system for large spacecraft
吴东亮 1韩放 1刘阳 1刘畅 1王晶1
作者信息
- 1. 北京卫星环境工程研究所,北京 100094
- 折叠
摘要
Abstract
In view of great difficulties of management, control and traceability of the test process data in a large-scale spacecraft vacuum thermal test caused by the complexity of the test process and the test unit interface, and a large number of printing process sheets, etc., a vacuum thermal process management system for large spacecraft is designed based on the service-oriented architecture (SOA), a systematic approach to business process management and a flexible process engine. The system is deployed in the largest space environment simulator KM8 in China, and is successfully applied to a spacecraft thermal test. It is shown that the system improves the efficiency of the test by its digitization, visualization and fine dynamic control.关键词
大型航天器/面向服务架构/真空热试验/过程管理Key words
large spacecraft/service-oriented architecture/vacuum thermal test/process management分类
信息技术与安全科学引用本文复制引用
吴东亮,韩放,刘阳,刘畅,王晶..大型航天器真空热试验过程管理系统设计与实现[J].航天器环境工程,2017,34(6):679-684,6.
