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基于游标测距的螺旋桨桨叶参数提取方法

A Parameter Extraction Method for Propeller Blades Based on Range Vernier

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针对螺旋桨飞机微动特征检测问题,提出了游标测距检测方法,首先假设目标运动模型,得到其回波表达式,通过雷达游标测距方法获取飞机运动轨迹测量数据,其中包含平动和微动分量,由于目标常规测距增量不包含微动分量,采用其补偿多普勒距离增量,去除平动分量,从而得到目标微动检测结果,最后结合雷达RCS测量数据进行分析,得到螺旋桨参数,实测数据表明,该方法能有效估计出螺旋桨的转速、叶片数等参数.
Aiming at the problem of propeller aircraft micro-motion feature detection,a method for detecting the mi-cro-motion characteristics of a propeller was proposed.Firstly,the target motion model was assumed and its echo expression was obtained.The measurement data of aircraft's motion trajectory were obtained by radar vernier ranging method.Since the regular ranging increment of the target did not contain the micro-motion component,it compen-sated the Doppler distance increment and removed the translation component,thus obtaining the detection result of the target micro motion.Finally,combining with the radar RCS measurement data,the propeller parameters and the measured data were obtained.The method can effectively estimate parameters such as the propeller rotation speed,micro-motion component,and blade number.

radarvernier rangingmicro motionpropeller

全刚、郑国毅、李强、贾润熙、何晓毛

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中国酒泉卫星发射中心 甘肃酒泉 732750

雷达 游标测距 微动 螺旋桨

2024

火控雷达技术
西安电子工程研究所

火控雷达技术

影响因子:0.234
ISSN:1008-8652
年,卷(期):2024.53(3)
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