Model-Based Signal Processing for Joint Drones Detection, Tracking, and Parameters Estimation

Oleg A. Krasnov;Xingzhuo Li;Alexander Yarovoy
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Abstract

The problem of multicopter (multirotor drone) classification is considered. A two-stage approach for multicopter joint detection, tracking, and parameter estimation is proposed. A previously published particle filter (PF)-based track-before-detect (TBD) algorithm with a single-rotor drone is used in the first stage to detect, localize, and track the target. The algorithm is, however, modified by the utilization of a new drone model, which is based on a simplified representation of a rotated propeller as a bunch of thin wires. Using this model, closed-form analytical equations for the radar signal temporal dependence and micro-Doppler spectrum are derived for each rotor. Significant improvement in micro-Doppler spectrum prediction due to the implementation of this model has been observed. The actual number of multicopter rotors and their independent parameters, such as rotation velocity and initial orientation angle, are estimated in the second processing stage. The estimation problem is formulated as a maximum likelihood (ML) search in a multidimensional space of parameters. This computationally expensive optimization problem is converted to the problem of multiple likelihood function peaks detection in 2-D space “rotational velocity-initial orientation angle” for each propeller. The latter is solved by a computationally efficient 2-D grid search algorithm, which is followed by a few extra processing steps to remove the residual false alarms by analyzing detections over multiple consecutive coherence processing intervals. The proposed approach for multicopter detection and classification has been verified using simulated and experimental data.
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基于模型的信号处理用于无人机联合探测、跟踪和参数估计
研究考虑了多旋翼无人机的分类问题。提出了一种两阶段的多旋翼联合检测、跟踪和参数估计方法。第一阶段使用之前发布的基于粒子滤波器(PF)的单旋翼无人机先跟踪后检测(TBD)算法来检测、定位和跟踪目标。不过,该算法通过使用新的无人机模型进行了修改,该模型基于将旋转的螺旋桨简化表示为一束细线。利用该模型,可为每个旋翼推导出雷达信号时间依赖性和微多普勒频谱的闭式分析方程。由于采用了这一模型,微多普勒频谱预测有了显著改善。多旋翼飞行器旋翼的实际数量及其独立参数(如旋转速度和初始方向角)在第二处理阶段进行估算。估算问题是在多维参数空间中进行最大似然(ML)搜索。这个计算成本高昂的优化问题被转换为每个螺旋桨在二维空间 "旋转速度-初始方向角 "中的多重似然函数峰值检测问题。后者通过一种计算效率高的二维网格搜索算法来解决,然后再经过几个额外的处理步骤,通过分析多个连续相干处理区间的检测结果来消除残余误报。所提出的多旋翼飞机检测和分类方法已通过模拟和实验数据得到验证。
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