DocumentCode :
1792303
Title :
Automatic testing equivalent system design of manned spacecraft
Author :
Fusheng Zhang ; Zhiyong Xie
Author_Institution :
Inst. of Manned Space Syst. Eng., China Acad. of Space Technol., Beijing, China
fYear :
2014
fDate :
3-6 Aug. 2014
Firstpage :
1962
Lastpage :
1966
Abstract :
Interface test between spacecraft and electrical ground testing system(EGTS) before assembly integration and testing (AIT) is time-consuming and over ties up manpower. An equivalent system has been designed based on PXI instrument and auto-test programming in order to increase the system efficiency and automation. The system could simulate actual spacecraft to send pyrotechnic device state signal, analog signal, and execute the result of ground controlling order, and exchange testing data with EGTS to realize the user-defined automatic test. A typical application result shows that the consuming time of the automatic system falls to 6 minutes from 65 minutes and tied-up manpower declines from 4 to 2 compared with conventional equivalent system, which achieves a big step forward in system efficiency and configuration.
Keywords :
aerospace computing; automatic programming; automatic testing; space vehicles; EGTS; PXI instrument; analog signal; assembly integration and testing; automatic testing equivalent system design; autotest programming; electrical ground testing system; interface test; manned spacecraft; pyrotechnic device state signal; user-defined automatic test; Extraterrestrial measurements; Instruments; Power supplies; Signal processing; Software; Space vehicles; Testing; Automatic testing; Equivalent system; Manned spacecraft; PXI;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Mechatronics and Automation (ICMA), 2014 IEEE International Conference on
Conference_Location :
Tianjin
Print_ISBN :
978-1-4799-3978-7
Type :
conf
DOI :
10.1109/ICMA.2014.6886003
Filename :
6886003
Link To Document :
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