DocumentCode :
3286791
Title :
Design of an aeroplane ejection seat ATE system
Author :
Zhang Xingguo ; Yi Xiaoyu
Author_Institution :
Phys. & Inf. Eng. Coll., Henan Normal Univ., Xinxiang, China
fYear :
2011
fDate :
15-17 April 2011
Firstpage :
3156
Lastpage :
3158
Abstract :
An ATE system design based on many condition procedures control ejection seat is presented. This ATE system not only has BITE function, but also has the fault localization function which BITE does not has. Breakthrough tradition ATE design flaw, it can detect fault, as the ejection seat in the actual movement. This system can reduce the time of fault detection and services, and enhance the ejection seat lifesaving efficiency.
Keywords :
aircraft instrumentation; automatic test equipment; seats; ATE system; BITE function; airoplane ejection seat; breakthrough tradition; fault localization function; Aerospace electronics; Aircraft; Educational institutions; Microprocessors; Military aircraft; System analysis and design; ATE; ejection seat; fault detection; insurance;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electric Information and Control Engineering (ICEICE), 2011 International Conference on
Conference_Location :
Wuhan
Print_ISBN :
978-1-4244-8036-4
Type :
conf
DOI :
10.1109/ICEICE.2011.5777944
Filename :
5777944
Link To Document :
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