DocumentCode
2638777
Title
Design and development of an integrated test system for avionics ground experiment system
Author
Dong, Song ; Lin, Li
Author_Institution
Aeronaut. Sch., Northwestern Polytech. Univ., Xian
fYear
2008
fDate
10-12 Dec. 2008
Firstpage
1
Lastpage
5
Abstract
The integrated test system for an avionics ground experiment system is designed based on full requirements analysis to signals tested. Complex bus signals and functional signals are tested, analyzed and diagnosed in test system so as to guarantee ground experiment of integrated avionics system right. The multithreading technique is adopted in test software development and implementation. Finally, the test results are analyzed to verify the test system developed correct.
Keywords
aircraft testing; avionics; ground support systems; multi-threading; program testing; program verification; software engineering; system buses; avionics ground experiment system; complex bus signal; functional signal; integrated test system; multithreading technique; requirements analysis; software development testing; Aerospace electronics; Multithreading; Programming; Signal analysis; Signal design; Software testing; System testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems and Control in Aerospace and Astronautics, 2008. ISSCAA 2008. 2nd International Symposium on
Conference_Location
Shenzhen
Print_ISBN
978-1-4244-3908-9
Electronic_ISBN
978-1-4244-2386-6
Type
conf
DOI
10.1109/ISSCAA.2008.4776335
Filename
4776335
Link To Document