振动翼微运动特性的详细特征建模

Jianzhou Li, Shuhui Chen, Haixuan Zhang, Chaoqun Fan, Lu Liu
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引用次数: 0

摘要

飞行目标的机翼由于受到外界因素的影响而产生振动。这种现象对于大机翼来说更为明显,并且会有影响微运动特性的细节特征。实际飞行中这种机翼微运动的电磁散射特性对目标识别和识别具有重要意义。本文着重对振动和变形引起的微运动特性和细部特征进行建模和分析。首先,建立了机翼振动的数学几何模型。然后对散射场进行仿真,并对仿真结果进行时频分析。结果观察到与常规结果不同的微多普勒特征。从机翼展向、弦向和翼型的详细特征出发,对机翼进行了振动建模研究。最终,人们发现是翼型的扭曲造成了这种现象。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Detailed Features Modeling of Vibrating Wing’s Micro-Motion Characteristics
Wings of flying targets vibrate due to the influence of external factors. This phenomenon is more pronounced for large wings and there will be detailed features that affect the micro-motion characteristics. The electromagnetic scattering characteristic of this kind of micro-motion of wings in actual flight is of great significance to target recognition and identification. This paper focuses on the modeling and analysis of the micro-motion characteristics and detailed features due to vibration and deformation. Firstly, the mathematical geometric model of wing vibration was established. Then the according to scattering field is simulated, and a time-frequency analysis was performed on the results. Micro-Doppler features different from conventional results were observed in the result. Starting from the detailed feature in spanwise, chordwise, and airfoil, the vibration modeling study of wings was carried out. Eventually, it was found that the twist of the airfoil caused this phenomenon.
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