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Application of Improved 5th-Cubature Kalman Filter in Initial Strapdown Inertial Navigation System Alignment for Large Misalignment Angles

机译:改进的第五立方卡尔曼滤波器在大失准角初始捷联惯导系统对准中的应用

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In view of the fact the accuracy of the third-degree Cubature Kalman Filter (CKF) used for initial alignment under large misalignment angle conditions is insufficient, an improved fifth-degree CKF algorithm is proposed in this paper. In order to make full use of the innovation on filtering, the innovation covariance matrix is calculated recursively by an innovative sequence with an exponent fading factor. Then a new adaptive error covariance matrix scaling algorithm is proposed. The Singular Value Decomposition (SVD) method is used for improving the numerical stability of the fifth-degree CKF in this paper. In order to avoid the overshoot caused by excessive scaling of error covariance matrix during the convergence stage, the scaling scheme is terminated when the gradient of azimuth reaches the maximum. The experimental results show that the improved algorithm has better alignment accuracy with large misalignment angles than the traditional algorithm.
机译:鉴于在大偏心角条件下用于初始对准的三度Cubature卡尔曼滤波器(CKF)的精度不足,提出了一种改进的五度CKF算法。为了充分利用滤波的创新,通过具有指数衰落因子的创新序列递归计算创新协方差矩阵。然后提出了一种新的自适应误差协方差矩阵缩放算法。本文采用奇异值分解(SVD)方法提高了五阶CKF的数值稳定性。为了避免在收敛阶段由于误差协方差矩阵的过度缩放而导致的过冲,当方位角的梯度达到最大值时终止缩放方案。实验结果表明,与传统算法相比,改进算法具有较大的对准误差和较大的对准误差。

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