DocumentCode :
3576140
Title :
Design of a new universal testing system for space vehicle control system
Author :
Qi Lichun ; Zhu Xufeng ; Zhan Lailong
Author_Institution :
Beijing Aerosp. Autom. Control Inst., Beijing, China
fYear :
2014
Firstpage :
2173
Lastpage :
2176
Abstract :
In order to meet the requirements of unit equipment testing system applied to space vehicle control system, a universal testing system is designed. It consists of hardware architecture based on Compact PCI and software architecture based on VxWorks. It can meet the demand of the mission-critical applications totally. It has the advantages of well-run, high reliability, multipurpose testing, low-cost, and fast response over the conventional card. Design of hardware platform, implement of software testing flow and structure design are presented in detail.
Keywords :
aerospace computing; control engineering computing; program testing; software architecture; space vehicles; test equipment; Compact PCI; VxWorks; hardware architecture; mission-critical applications; software architecture; software testing flow; space vehicle control system; structure design; unit equipment testing system; universal testing system; Computers; Hardware; Reliability engineering; Switches; Testing; Compact PCI; VxWorks; high reliability; universal testing system;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Mechatronics and Control (ICMC), 2014 International Conference on
Print_ISBN :
978-1-4799-2537-7
Type :
conf
DOI :
10.1109/ICMC.2014.7231954
Filename :
7231954
Link To Document :
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