A Stability Guaranteed Variational Bayesian Converted Measurement Kalman Filter for Radar Tracking With Unknown Noise Covariances

IF 5.7 2区 计算机科学 Q1 ENGINEERING, AEROSPACE IEEE Transactions on Aerospace and Electronic Systems Pub Date : 2024-10-30 DOI:10.1109/TAES.2024.3488679
Songzhou Li;Di Zhou;Yutang Li;Runle Du;Jiaqi Liu
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Abstract

Tracking with radar measurements is challenging due to the nonlinear relationship between the measurements and the target Cartesian state. Besides, the unknown noise covariances also trouble the design of the tracking filter. In this article, a variational Bayesian converted measurement Kalman filter (VBCMKF) is proposed to tackle the radar tracking problem with unknown process and measurement covariance matrixes. Aiming to gain better estimation accuracy, the idea of moving horizon estimation is adopted, namely, the states over a moving window of fixed length and the unknown process and measurement covariance matrixes are iteratively extracted from the collected measurements by exploiting variational Bayesian inference. During the iteration, the original measurement model is converted to an equivalent linear form in Cartesian coordinates by utilizing the measurement conversion technique, making the measurement update for the augmented state able to be conducted in an analytical style rather than by resorting to complex numerical approximations for high-dimension nonlinear Gaussian integral. Moreover, a stability guaranteed strategy is integrated into the filter to constrain the noise covariances within preset ranges through boundary overflow checks. It is proven that the obtained state estimation error is exponentially bounded in mean square. The effectiveness of the proposed VBCMKF is verified through simulations. The results demonstrate its outperformance in tracking accuracy and consistency.
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用于未知噪声协方差雷达跟踪的稳定性保证变异贝叶斯转换测量卡尔曼滤波器
由于测量值与目标笛卡尔状态之间的非线性关系,用雷达测量进行跟踪具有挑战性。此外,未知的噪声协方差也影响了跟踪滤波器的设计。本文提出了一种变分贝叶斯转换测量卡尔曼滤波器(VBCMKF),用于处理具有未知过程和测量协方差矩阵的雷达跟踪问题。为了获得更好的估计精度,采用了移动地平线估计的思想,即利用变分贝叶斯推理,从收集到的测量数据中迭代提取固定长度运动窗口上的状态和未知过程和测量协方差矩阵。在迭代过程中,利用测量转换技术将原始测量模型转换为笛卡尔坐标下的等效线性形式,使增广状态的测量更新能够以解析的方式进行,而不是依靠复杂的高维非线性高斯积分的数值近似。此外,在滤波器中引入稳定性保证策略,通过边界溢出检查将噪声协方差限制在预设范围内。证明了所得到的状态估计误差在均方上呈指数有界。仿真结果验证了该方法的有效性。结果表明,该方法在跟踪精度和一致性方面具有优异的性能。
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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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