Skewed Unscented Kalman Filter Using Gaussian Sum

IF 5.7 2区 计算机科学 Q1 ENGINEERING, AEROSPACE IEEE Transactions on Aerospace and Electronic Systems Pub Date : 2024-11-18 DOI:10.1109/TAES.2024.3501237
Hanyu Liu;Xiucong Sun;Jinghao Yang;Ming Xu;Shengzhou Bai
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Abstract

The unscented Kalman filter (UKF) finds extensive application in the state estimation of systems characterized by significant nonlinearity. A constraint of the UKF is its presumption that the probability density function (PDF) of the states maintains Gaussian distribution throughout the filter recursion, which restricts the estimation accuracy even though the UKF may still be applicable when the Gaussian assumption is not strictly met. To overcome this problem, a skewed unscented Kalman filter (SUKF) based on Gaussian sum is presented in this article. First, as the theoretical basis, the conventional UKF is reviewed. Then, the SUKF algorithm is presented in a manner analogous to the UKF, following a two-step process. In the time-update step, an approximation method, employing no additional sigma points compared to the UKF algorithm, has been proposed to obtain the skewness of the random variable after nonlinear transformation, which approximates the Taylor series of skewness up to fourth-order terms. In the measurement-update step, a Gaussian sum PDF matching the known mean, covariance, and skewness is constructed to represent the non-Gaussian joint PDF of states and measurements. Finally, taking one nonlinear transformation and three nonlinear systems with different dimensions as examples, the effectiveness of the proposed SUKF is verified through numerical simulations. The results demonstrate that the SUKF algorithm offers higher estimation accuracy compared to the conventional UKF while requiring similar computational time, which can provide a practical option for state estimation for highly nonlinear systems.
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使用高斯总和的偏斜无符号卡尔曼滤波器
无气味卡尔曼滤波器(UKF)在具有显著非线性特征的系统的状态估计中得到了广泛的应用。UKF的一个约束是它假设状态的概率密度函数(PDF)在整个滤波递归过程中保持高斯分布,这限制了估计的精度,即使在不严格满足高斯假设的情况下,UKF仍然可以适用。为了克服这一问题,本文提出了一种基于高斯和的偏斜无气味卡尔曼滤波器(SUKF)。首先,作为理论基础,对传统UKF进行了综述。然后,SUKF算法以类似于UKF的方式呈现,并遵循两个步骤的过程。在时间更新步骤中,提出了一种近似方法,与UKF算法相比,不使用额外的sigma点,以获得非线性变换后随机变量的偏度,该方法近似于四阶偏度的泰勒级数。在测量更新步骤中,构造一个匹配已知均值、协方差和偏度的高斯和PDF来表示状态和测量的非高斯联合PDF。最后,以一个非线性变换和三个不同维数的非线性系统为例,通过数值模拟验证了所提SUKF的有效性。结果表明,与传统的UKF算法相比,SUKF算法在计算时间相近的情况下具有更高的估计精度,为高度非线性系统的状态估计提供了一种实用的选择。
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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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