主管单位:中华人民共和国工业和信息化部
主办单位:西北工业大学  中国航空学会
地       址:西北工业大学友谊校区航空楼
海上低空直升机RCS与隐身性能分析
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南京航空航天大学 航空学院

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中图分类号:

V218

基金项目:

江苏高校优势学科建设工程资助项目(PAPD)


RCS and stealth performance analyses of marine low-altitude helicopter
Author:
Affiliation:

College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics

Fund Project:

A Project Funded by the Priority Academic Program Development of Jiangsu Higher Education Institutions

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    摘要:

    海上低空直升机的雷达目标特性与隐身性能的研究可以为路径规划提供依据。本文建立随机粗糙海面模型,基于高频近似方法对海上低空飞行的直升机雷达目标特性进行分析,研究孤立直升机的雷达散射截面(RCS)以及直升机在海面环境背景下的复合电磁散射、海上直升机在不同飞行高度下的雷达隐身性能,并总结其影响规律。结果表明:在雷达波直射条件下,直升机表面的大曲率半径处形成强散射源,呈现出较高的RCS;当直升机在海上飞行时,随着飞行高度的增加,直升机与海面间的耦合效应减弱,复合电磁散射逐渐接近于孤立直升机;直升机在海上飞行时可以降低高度以缩短曝露距离,一定程度上能够躲避敌方的雷达追踪,实现隐身突防。

    Abstract:

    The study of radar target characteristics and stealth performance of low altitude helicopters at sea can provide a basis for path planning. a random rough sea surface model is established in this paper. Based on the high frequency approximation method, the radar target characteristics of helicopters flying at low altitude on the sea are analyzed. The radar cross section ( RCS ) of isolated helicopters, the composite electromagnetic scattering of helicopters in the background of sea surface environment, the radar stealth performance of offshore helicopters at different flight heights are studied, and the influence rules are summarized. The results show that under direct radar wave conditions, a strong scattering source is formed at the large curvature radius of the helicopter surface, exhibiting a high RCS; When helicopter is flying at sea, as the flying altitude increases, the coupling effect between the helicopter and the sea weakens, their composite electromagnetic scattering gradually approaches that an isolated helicopter; When helicopter fly at sea, it can lower their altitude to shorten the exposure distance and to some extent avoid enemy radar tracking, achieving stealth penetration.

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历史
  • 收稿日期:2024-08-26
  • 最后修改日期:2024-10-18
  • 录用日期:2024-11-06
  • 在线发布日期: 2025-05-08
  • 出版日期: