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UD factorization applied to airborne Kalman-filter-based fusion

机译:应用于机载卡尔曼 - 滤波器的融合的UD分解

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To ensure numerical accuracy and stability for real-time Kalman filter implementation, Bierman's upper diagonal (UD) factorization is used. The use of multiple sensors to form a more accurate state vector has included combining infrared search and track (IRST), electronic support measures (ESM), and radar sensor data, with applications to track initialization/deletion, association correlation, and track-update fusion functions. Each area of fusion is discussed and the interfaces between sensors and fusion are given. Different fusion architectures are shown and their impact on state vector estimation accuracy is shown to vary. All three methods use the extended Kalman filter (EKF) as the base. Correlation, association, and track initialization are examined relative to the different fusion architectures. The correlated process noise which exists for the multisensor application is examined. Root-mean-square position and velocity plots versus time for aircraft are given which incorporate a six-state EKF.
机译:为确保实时卡尔曼滤波器实现的数值准确性和稳定性,使用BierMan的上对角线(UD)分解。使用多个传感器以形成更准确的状态向量,包括结合红外搜索和轨道(IRST),电子支持措施(ESM)和雷达传感器数据,其中包含用于跟踪初始化/删除,关联相关性和跟踪更新的应用程序融合功能。讨论了每个融合区域,并给出了传感器和融合之间的接口。示出了不同的融合架构,并显示其对状态矢量估计精度的影响变化。所有三种方法都使用扩展的卡尔曼滤波器(EKF)作为基础。相对于不同的融合架构检查相关性,关联和跟踪初始化。检查了用于多传感器应用程序的相关过程噪声。给出了根均方位置和速度绘制飞机的时间,其包括六州EKF。

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