Design and Application of Test Process Management System for Spacecraft Vacuum Thermal Test

被引:0
|
作者
Su, Xinming [1 ]
Wu, Dongliang [2 ]
Fei, Zelin [2 ]
Wang, Jing [2 ]
Liu, Chang [2 ]
机构
[1] Beihang Univ, Sch Aeronaut Sci & Engn, Beijing, Peoples R China
[2] Beijing Inst Satellite Environm Engn, Youyi Rd 104, Beijing, Peoples R China
关键词
Spacecraft thermal test; Process management; Service-oriented architecture; Process flow;
D O I
10.1007/978-981-13-8779-1_65
中图分类号
TP3 [计算技术、计算机技术];
学科分类号
0812 ;
摘要
Spacecraft vacuum thermal test is a complex system engineering with the combination of operator and mechanical equipment. In order to ensure that the environmental simulation meets the requirements, the staff needs to operate the test equipment frequently during the test. The original management method of spacecraft thermal test process relies on a large number of paper forms, which is used to adjust and confirm the parameters during the test; this kind of operation is complicated and there are risks of operations. Based on service-oriented architecture and business-process management, a new generation of spacecraft thermal test process management system is designed and implemented. The system has been successfully deployed and applied in KM8. The operation results show that the system greatly improves the efficiency in the test process and realizes the digitalization and visualization control of spacecraft thermal test.
引用
收藏
页码:567 / 575
页数:9
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