DocumentCode :
1870238
Title :
Cockpit Protection Analysis against High Power Microwave
Author :
Huang, Jun ; Hu, Yun-an ; Zhang, Hao-ran ; Jin, Yan
Author_Institution :
Grad. Students´´ Brigade, Naval Aeronaut. Eng. Inst., Yantai, China
fYear :
2010
fDate :
10-12 Dec. 2010
Firstpage :
1
Lastpage :
4
Abstract :
A model of high power microwave (HPM) with multiple parameters is brought forward, a calculation method of electromagnetic transmission rate and reflectivity is proposed, a finite-difference time-domain (FDTD) film algorithm is set forth, a shielded cockpit glass construction is designed by a new flow, and protective effect analysis on military aircraft´s cockpit against HPM is carried out on a 3D plane, airborne equipments and pilot model with a scale of 1:1. The simulation tests show the soft kill protective efficiency in the range of carrier frequencies and protective limits of the glass construction with incident angles.
Keywords :
aircraft communication; electromagnetic wave transmission; protection; calculation method; carrier frequencies; cockpit glass construction; cockpit protection analysis; electromagnetic transmission rate; finite difference time domain film algorithm; high power microwave; multiple parameters; protective effect analysis; reflectivity; Atmospheric modeling; Attenuation; Finite difference methods; Glass; Reflectivity; Time domain analysis;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computational Intelligence and Software Engineering (CiSE), 2010 International Conference on
Conference_Location :
Wuhan
Print_ISBN :
978-1-4244-5391-7
Electronic_ISBN :
978-1-4244-5392-4
Type :
conf
DOI :
10.1109/CISE.2010.5676773
Filename :
5676773
Link To Document :
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