Optimized Design for Cockpit Protective Glass Construction against High Power Microwave Using Genetic Algorithm

Jun Huang; Yan Jin; Yun An Hu; Hao Ran Zhang

doi:10.4028/www.scientific.net/AMR.403-408.3777

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Design, Modeling and Simulation of CMOS-MEMS Piezoresistive Cantilever Based Carbon Dioxide Gas Sensor for Capnometry
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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 403-408Optimized Design for Cockpit Protective Glass...

Optimized Design for Cockpit Protective Glass Construction against High Power Microwave Using Genetic Algorithm

Abstract:

According to main challenges to aircraft protection against high power microwave (HPM), the formula of electromagnetic transmission rate and reflectivity both for the perpendicularly and parallely polarized incident field are modified and simplified, a shielded cockpit glass construction is designed by a new optimized method on genetic algorithm, and protective efficiency analysis on military aircraft’s cockpit against HPM is carried out on a virtual 3D plane, airborne equipments and pilot model with a scale of 1:1. The verification simulation tests show the optimized construction has good protective efficiency in the range of carrier frequencies between 1-20 GHz, and protective intensity does not exceed limits of relevant international standard.

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Periodical:

Advanced Materials Research (Volumes 403-408)

Pages:

3777-3783

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.403-408.3777

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Online since:

November 2011

Authors:

Jun Huang, Yan Jin, Yun An Hu, Hao Ran Zhang

Keywords:

Cockpit Protective Glass Construction, Finite Difference Time Domain (FDTD), Genetic Algorithm (GA), High Power Microwave, Optimized Design, Soft Kill

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