摘要
The wavefront distortion caused by the passage of radar echoes through the atmosphere, the external flow field of the aircraft, and the radome has a crucial influence on the angle measurement error of active radar single-pulse. The impact of the refractive index gradient caused by the turbulent structure on the wavefront distortion and the numerical solution accuracy of the weak form of the wave equation were analyzed. The “explicit” gradient term correction approach and the “gradient reconstruction” method of supplementing the small-scale structure of the density field with the turbulent vortex model for the weak form of the electromagnetic wave equation were proposed. Computer numerical simulation was conducted using the finite element method. The simulation results indicate that one of the significant causes of the radar angle measurement error is the electric field distortion induced by small-scale turbulence, and as the scale of the vortex structure decreases and the wavelength lengthens, the electric field distortion intensifies, and the angle measurement error increases.
| 投稿的翻译标题 | A method for analyzing angle measurement error of radar on hypersonic vehicle |
|---|---|
| 源语言 | 繁体中文 |
| 页(从-至) | 3666-3676 |
| 页数 | 11 |
| 期刊 | Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics |
| 卷 | 50 |
| 期 | 12 |
| DOI | |
| 出版状态 | 已出版 - 12月 2024 |
关键词
- electromagnetic wave equation
- finite element method
- hypersonic vehicles
- radar angle measurement
- weak form
指纹
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