Numerical simulation of RCS for carrier electronic warfare airplanes

被引:0
作者
Yue Kuizhi [1 ,2 ]
Liu Wenlin [1 ]
Li Guanxiong [2 ]
Ji Jinzu [2 ]
Yu Dazhao [1 ]
机构
[1] Department of Airborne Vehicle Engineering, Naval Aeronautical and Astronautical University
[2] School of Aeronautic Science and Engineering, Beihang University
基金
中国国家自然科学基金;
关键词
Carrier aircraft; Configuration design; Electronic warfare; Physical optics method; Stealth;
D O I
暂无
中图分类号
V271.492 [];
学科分类号
082503 ;
摘要
This paper studies the radar cross section(RCS) of carrier electronic warfare airplanes.Under the typical naval operations section, the mathematical model of the radar wave’s pitch angle incidence range analysis is established. Based on the CATIA software, considering dynamic deflections of duck wing leading edge flaps, flaperons, horizontal tail, and rudder, as well as aircraft with air-to-air missile, anti-radiation missile, electronic jamming pod, and other weapons, the 3D models of carrier electronic warfare airplanes Model A and Model B with weapons were established. Based on the physical optics method and the equivalent electromagnetic flow method, by the use of the RCSAnsys software, the characteristics of carrier electronic warfare airplanes’ RCS under steady and dynamic flights were simulated under the UHF, X, and S radar bands. This paper researches the detection probability of aircraft by radars under the condition of electronic warfare, and completes the mathematical statistical analysis of the simulation results. The results show that: The Model A of carrier electronic warfare airplane is better than Model B on stealth performance and on discover probability by radar detection effectively.
引用
收藏
页码:545 / 555
页数:11
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