空中监视雷达中飞机旋转结构调制特性的建模与验证

Ding Jianjiang, Yu Zhiqiang, Yan Da-zhi, R. Chongji
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引用次数: 1

摘要

提出了一种实用的参数化模型(PPM),描述了空中监视雷达中飞机旋转结构的调制特性,并进行了验证。首先,基于光电磁散射理论,系统地描述了飞机旋转结构调制信号的散射机理。其次,在理论参数模型、雷达系统和飞机旋转结构的基础上,提出了PPM。分析了空中监视雷达回波调制特征与飞机物理旋转结构之间的关系。第三,通过分析飞机构型和方位、雷达参数和运行情况等不同条件回波,对PPM进行了验证。结果表明,PPM可以描述直升机和螺旋桨的旋转结构所对应的相对不变的调制特征,并且可以可靠、稳定地从空中监视雷达回波中提取调制特征。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Modeling and validation of modulated characteristics for aircraft rotating structure in the air surveillance radars
A practical parametric model (PPM), described the modulated characteristics for aircraft rotating structure in the air surveillance radars is presented and validated. Firstly, the scattering mechanism of the modulated signatures generated by aircraft rotating structure is described systematically based on the optical electromagnetism scattering theories. Secondly, the PPM is proposed based on some theoretical parametric models, the radar system and aircraft rotating structure. The relationships between the modulated signatures of the air surveillance radar echoes and the physical rotating structures of aircraft are analyzed. Thirdly, the PPM is validated by analysis of different conditions echoes including aircraft configuration and orientation, radar parameters and operation. The results demonstrate that the relatively unchangeable modulated feature, which is corresponding to the rotating structure of helicopters and propellers, can be described with the PPM, and can be reliably and steadily extracted from the echoes of the air surveillance radars.
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