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