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Estimation of maneuvering target in the presence of non-Gaussian noise: A coordinated turn case study

机译:非高斯噪声存在下机动目标的估计:协调转弯案例研究

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HighlightsThe novel maximum-correntropy-criterion-based extended Kalman filters are devised for treating continuous-time nonlinear stochastic models with non-Gaussian noise.The radar tracking scenarios, where an aircraft executes a coordinated turn, are set up with impulsive and mixed-Gaussian noises.The maximum-correntropy-criterion-based extended Kalman filters are examined numerically and compared to the continuous-discrete extended, cubature and unscented Kalman filters.The contemporary cubature- and unscented-type Kalman filters outperform all their competitors in the accuracy of state estimation in the non-Gaussian target tracking case studies.AbstractThis paper explores performance of various methods for state estimation of radar tracking models. A coordinated turn case study of maneuvering target in the presence of non-Gaussian noise is of particular interest. We aim at evaluating the estimation potential of recently presented filters grounded in the Maximum Correntropy Criterion (MCC). Various investigations confirm the outstanding performance of such filters for treating stochastic systems disturbed with impulsive (shot) and mixed-Gaussian noises. However, those filters are intended for linear models, and the success of the MCC-based state estimation in a nonlinear continuous-time stochastic environment, which often underlies radar tracking modeling, is still debatable. First, we extend the MCC-based filters, which are designed presently for linear discrete-time stochastic models, to nonlinear continuous-discrete systems. We devise the conventional (non-square-root) filtering and its square-root version as well. Second, we fulfil a comprehensive examination of these new methods in severe conditions of tackling a seven-dimensional radar tracking problem, where an aircraft executes a coordinated turn, in the presence of both impulsive (shot) and mixed-Gaussian noises. In addition, the novel MCC-based filters are compared to various contemporary extended, cubature and unscented Kalman-like state estimators.
机译: 突出显示 基于新颖的基于最大熵准则的扩展卡尔曼滤波器设计用于处理具有非高斯噪声的连续时间非线性随机模型。 雷达跟踪设置飞机执行协调转弯的场景时,会设置脉冲和混合高斯噪声。 基于最大熵准则的扩展卡尔曼滤波对ters进行数字检查,并将其与连续离散的扩展,容积式和无味卡尔曼滤波器进行比较。 在非高斯目标跟踪情况下,当代的库尔曼型和无味型卡尔曼滤波器在状态估计的准确性方面优于所有竞争对手研究。 摘要 本文探讨了各种用于雷达跟踪模型状态估计的方法的性能。在非高斯噪声的情况下,机动目标的协调转弯案例研究尤为重要。我们旨在评估基于最大熵准则(MCC)的最新提出的滤波器的估计潜力。各种研究证实了这种滤波器在处理受脉冲(散粒)和混合高斯噪声干扰的随机系统方面的出色性能。但是,这些滤波器是用于线性模型的,在非线性连续时间随机环境中(通常是雷达跟踪建模的基础)基于MCC的状态估计的成功仍值得商bat。首先,我们将目前为线性离散时间随机模型设计的基于MCC的滤波器扩展到非线性连续离散系统。我们设计了常规(非平方根)过滤及其平方根版本。其次,我们在解决七维雷达跟踪问题的严酷条件下对这些新方法进行了全面检查,在这种情况下,飞机在存在脉冲(射击)噪声和混合高斯噪声的情况下执行协调的转弯。此外,将基于MCC的新型过滤器与各种当代扩展的,容积式的和无味的类似Kalman的状态估计器进行了比较。

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