DocumentCode :
593079
Title :
Investigation of Injury Effects to Strong Electromagnetic Pulse on Typical Flying Control System
Author :
Lin Jin-Yong ; Dong Wen-Jie ; Zhou Chun-Mei ; Zhang Chun-xia ; Ma Ji-Feng
Author_Institution :
Nat. Key Lab. of Sci. & Technol. on Aerosp. Intell. Control, Beijing Aerosp. Autom. Control Inst., Beijing, China
fYear :
2012
fDate :
8-10 Dec. 2012
Firstpage :
1532
Lastpage :
1535
Abstract :
Flying control system is the core fabrication division of aircraft", "and its working reliability and the performance sticking up to strong electromagnetic pulse(SEMP) can directly affect the success or fail of flying mission. Aiming at the protecting problems of flying control system under strong electromagnetic pulse environment, injury effect and latent threat to aircraft as well as hurt modes to flying control system from strong EMP were firstly analyzed, then the electric current injection experiment on the data communication interface of typical flying control system were investigated, lastly the relevant results of electric current injection experiment were presented, which will support the protecting method study sticking up to strong electromagnetic pulse for flying control system.
Keywords :
aircraft control; electromagnetic pulse; injuries; reliability; SEMP; aircraft core fabrication division; data communication interface; electric current injection experiment; flying control system; flying mission; injury effect investigation; reliability; strong electromagnetic pulse; Aerospace control; Aerospace electronics; Cable shielding; Computers; Control equipment; Radiation effects; electric current injection experimentc; flying control system interface; injury effect; strong electromagnetic pulse/SEMP;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Instrumentation, Measurement, Computer, Communication and Control (IMCCC), 2012 Second International Conference on
Conference_Location :
Harbin
Print_ISBN :
978-1-4673-5034-1
Type :
conf
DOI :
10.1109/IMCCC.2012.358
Filename :
6429194
Link To Document :
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