Use of Cholesky square roots amidst the UD-factorization implementation of Kalman filters in real-time airborne tracking systems

R. Yannone
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Abstract

In airborne Track-While-Scan systems, target parameters are updated via individual Kalman Filters. To insure numerical stability and accuracy, UD-Factorization techniques are used. A preset number of individual tracks is typically maintained in dense target environments. In real-time application the processing load is of concern. The UD-Factorization algorithm for measurement updates operates on each measurement individually when the error covariance matrix of the measurements is diagonal. In the inertial X-Y-Z TWS Kalman Filter for each track, this matrix is inherently non-diagonal and consequently needs to be operated upon. The proposed algorithm utilizes the lower triangular Cholesky square root technique to determine the normalized measurement vector and observation matrix, and yields an identity measurement error covariance matrix. To perform all the computations necessary requires considerable effort, and this paper delineates what is involved. The computationally cost-effective way to operate reduces to only a few subsidiary calculations above what would be necessary had the measurement error covariance matrix been diagonal to begin with. This algorithm is invoked prior to performing the Kalman Measurement Update equations.
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在实时机载跟踪系统中卡尔曼滤波器的d分解实现中使用乔列斯基平方根
在机载随扫跟踪系统中,目标参数通过单独的卡尔曼滤波器进行更新。为了确保数值的稳定性和准确性,使用了ud分解技术。在密集的目标环境中,通常保持预设数量的单个轨道。在实时应用中,处理负载是一个值得关注的问题。当测量值的误差协方差矩阵为对角线时,测量值更新的UD-Factorization算法分别对每个测量值进行操作。在每个航迹的惯性X-Y-Z TWS卡尔曼滤波器中,该矩阵本身是非对角线的,因此需要对其进行运算。该算法利用下三角Cholesky平方根技术确定归一化的测量向量和观测矩阵,得到单位测量误差协方差矩阵。执行所有必要的计算需要相当大的努力,本文描述了所涉及的内容。如果测量误差协方差矩阵一开始是对角线的,那么计算成本效益的操作方法将只需要进行少量的辅助计算。在执行卡尔曼测量更新方程之前调用该算法。
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