Adaptive IMM-UKF for Airborne Tracking

IF 0.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE
Alvaro Arroyo Cebeira, Mariano Asensio Vicente
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引用次数: 0

Abstract

In this paper, we propose a nonlinear tracking solution for maneuvering aerial targets based on an adaptive interacting multiple model (IMM) framework and unscented Kalman filters (UKFs), termed as AIMM-UKF. The purpose is to obtain more accurate estimates, better consistency of the tracker, and more robust prediction during sensor outages. The AIMM-UKF framework provides quick switching between two UKFs by adapting the transition probabilities between modes based on a distance function. Two modes are implemented: a uniform motion model and a maneuvering model. The experimental validation is performed with Monte Carlo simulations of three scenarios with ACAS Xa tracking logic as a benchmark, which is the next generation of airborne collision avoidance systems. The two algorithms are compared using hypothesis testing of the root mean square errors. In addition, we determine the normalized estimation error squared (NEES), a new proposed noise reduction factor to compare the estimation errors against the measurement errors, and an estimated maximum error of the tracker during sensor dropouts. The experimental results illustrate the superior performance of the proposed solution with respect to the tracking accuracy, consistency, and expected maximum error.
机载跟踪的自适应IMM-UKF
在本文中,我们提出了一种基于自适应交互多模型(IMM)框架和无气味卡尔曼滤波器(ukf)的机动空中目标非线性跟踪解决方案,称为AIMM-UKF。目的是在传感器中断期间获得更准确的估计,更好的跟踪器一致性和更稳健的预测。AIMM-UKF框架通过基于距离函数调整模式之间的转移概率,实现了两个ukf之间的快速切换。实现了两种模式:均匀运动模型和机动模型。以新一代机载避碰系统ACAS Xa跟踪逻辑为基准,通过蒙特卡罗模拟对三种场景进行了实验验证。采用均方根误差的假设检验对两种算法进行了比较。此外,我们确定了归一化估计误差平方(NEES),一种新的降噪因子,用于比较估计误差与测量误差,以及传感器丢失时跟踪器的估计最大误差。实验结果表明,该方法在跟踪精度、一致性和期望最大误差等方面具有较好的性能。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Aerospace America
Aerospace America 工程技术-工程:宇航
自引率
0.00%
发文量
9
审稿时长
4-8 weeks
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