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