Motion Error Estimation and Coherent Integration for High-Speed Target With Airborne Bistatic Radar

IF 5.7 2区 计算机科学 Q1 ENGINEERING, AEROSPACE IEEE Transactions on Aerospace and Electronic Systems Pub Date : 2024-12-23 DOI:10.1109/TAES.2024.3520537
Xiaolong Li;Zerui Zhang;Fan Yang;Mingxing Wang;Tat Soon Yeo;Guolong Cui
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Abstract

With flexibility in maneuverability and remarkable adaptability, airborne bistatic radar system can obtain excellent detection performance for high-speed target by employing coherent integration. However, range migration (RM) and Doppler frequency migration (DFM) could become serious issues due to the relative motion characteristics of airborne platforms and high-speed target. Meanwhile, various unpredictable factors such as atmospheric turbulence and mechanical issues, etc., resulting in additional motion errors, would have further negative impacts on motion state and flight trajectory of airborne platforms. This phenomenon would cause serious consequence on coherent integration and target detection. Thus, we make contributions to tackle these limitations and enhance coherent integration and detection performance. First, we establish signal model with high-speed target in 3-D space for airborne bistatic radar system, along with motion error model which simultaneously includes translational error and rotational error. Next, we articulate range history's mathematical expression and further derive echo signal model. We then propose an improved generalized radon Fourier transform (IGRFT) method. More specifically, the purpose of IGRFT is achieving joint search for the parameters of the target motion and the parameters of motion error, to ensure high precision parameter estimation and high gain integration. However, the computational complexity surges due to the increasing of search dimensionality. To devise computationally feasible methods for practical applications, we split the high-dimensional maximization process into two disjoint problems by sequentially searching motion parameters and then motion error parameters, and this method is named generalized Radon transform (GRT)-IGRFT. Numerical simulations show that the proposed algorithms can correctly estimate parameters and achieve signal integration and target detection. Finally, we present performance analysis of two proposed strategies considering computational complexity, detection performance, and parameter estimation.
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机载双基地雷达高速目标运动误差估计与相干积分
机载双基地雷达系统具有机动灵活、自适应能力强的特点,采用相干积分对高速目标进行检测,可以获得优异的检测性能。然而,由于机载平台和高速目标的相对运动特性,距离偏移(RM)和多普勒频率偏移(DFM)可能成为严重的问题。同时,大气湍流、机械问题等各种不可预测因素导致的附加运动误差,将对机载平台的运动状态和飞行轨迹产生进一步的负面影响。这种现象会对相干积分和目标检测造成严重的影响。因此,我们为解决这些限制和提高相干集成和检测性能做出了贡献。首先,建立了机载双基地雷达系统的三维空间高速目标信号模型,同时建立了包含平移误差和旋转误差的运动误差模型。其次,给出了距离历史的数学表达式,并进一步推导了回波信号模型。然后,我们提出了一种改进的广义radon傅立叶变换(IGRFT)方法。更具体地说,IGRFT的目的是实现对目标运动参数和运动误差参数的联合搜索,以保证高精度的参数估计和高增益的积分。然而,随着搜索维数的增加,计算量急剧增加。为了设计计算可行的实际应用方法,我们将高维最大化过程分解为两个不相交的问题,先搜索运动参数,再搜索运动误差参数,并将该方法命名为广义Radon变换(GRT)-IGRFT。数值仿真结果表明,该算法能够正确估计参数,实现信号集成和目标检测。最后,我们从计算复杂度、检测性能和参数估计三个方面对两种策略进行了性能分析。
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来源期刊
CiteScore
7.80
自引率
13.60%
发文量
433
审稿时长
8.7 months
期刊介绍: IEEE Transactions on Aerospace and Electronic Systems focuses on the organization, design, development, integration, and operation of complex systems for space, air, ocean, or ground environment. These systems include, but are not limited to, navigation, avionics, spacecraft, aerospace power, radar, sonar, telemetry, defense, transportation, automated testing, and command and control.
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