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