Adaptive Kalman Filters With Small-Magnitude and Inaccurate Process Noise Covariance Matrix—Part I: Theoretical Results

IF 5.7 2区 计算机科学 Q1 ENGINEERING, AEROSPACE IEEE Transactions on Aerospace and Electronic Systems Pub Date : 2025-01-28 DOI:10.1109/TAES.2025.3535469
Fengchi Zhu;Siqing Zhang;Xiaofeng Li;Yulong Huang;Yonggang Zhang
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Abstract

There has been a great deal of attention on the online estimation of noise covariance matrices in Kalman filtering during recent decades. However, the existing methods face challenges in the estimation of small-magnitude process noise covariance matrices (PNCMs), which often occur in engineering applications. The purpose of this article, along with its companion article (Part II), is to tackle the aforementioned challenges encountered in practical applications. In this article, two adaptive Kalman filters are proposed to improve the estimation accuracy of small-magnitude PNCMs. We propose a nonadjacent state transition model to accumulate multiple small-magnitude PNCMs into a large-magnitude equivalent PNCM. Then, the adaptive Kalman filters are derived within the framework of variational Bayesian, where the cases are divided into two categories, i.e., single-coefficient estimation and multiple-coefficient estimation, based on the prior information of the PNCM. For the first case, the adaptive Kalman filter can be analytically derived. For the other case, the adaptive Kalman filter is developed based on numerical optimization, where the variational Bayesian and expectation maximization methods are integrated to address the absence of the conjugate prior distribution of the PNCM coefficients. The relative means and mean square errors of the estimated PNCM coefficients in the proposed filters are derived, and an optimal method for selecting the length of the nonadjacent state transition model is also given. Simulation results demonstrate the superior performance of the proposed adaptive filters compared with the existing state-of-the-art methods when the PNCM is small-magnitude and inaccurate. These two filters will be further applied to inertial-based integrated navigation in Part II.
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具有小幅度和不准确过程噪声协方差矩阵的自适应卡尔曼滤波器第一部分:理论结果
近几十年来,卡尔曼滤波中噪声协方差矩阵的在线估计受到了广泛的关注。然而,现有的方法在工程应用中经常遇到小幅度过程噪声协方差矩阵的估计问题。本文及其配套文章(第2部分)的目的是解决在实际应用程序中遇到的上述挑战。本文提出了两种自适应卡尔曼滤波器来提高小量级pncm的估计精度。我们提出了一个非相邻状态转换模型,将多个小量级的PNCM累积成一个大量级的等效PNCM。然后,在变分贝叶斯框架下推导了自适应卡尔曼滤波器,并将其分为单系数估计和多系数估计两类。对于第一种情况,可解析导出自适应卡尔曼滤波器。对于另一种情况,基于数值优化开发了自适应卡尔曼滤波器,该滤波器集成了变分贝叶斯和期望最大化方法,以解决PNCM系数缺乏共轭先验分布的问题。推导了滤波器估计的PNCM系数的相对均值和均方误差,并给出了选择非相邻状态转移模型长度的最优方法。仿真结果表明,在PNCM小幅度和不精确的情况下,与现有的自适应滤波方法相比,所提出的自适应滤波方法具有优越的性能。这两个过滤器将在第二部分中进一步应用于基于惯性的集成导航。
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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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