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Research on Initial Alignment Method of SINS with Improved CKF

机译:改进CKF的捷联惯导系统初始对准方法研究

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摘要

The initial alignment model of Strapdown Inertial Navigation System (SINS) with large misalignment angle is a linear and nonlinear mixed system model. Aiming at the model, an improved Cubature Kalman Filter(CKF) algorithm is adopted. Firstly, the initial alignment model of SINS is established and analyzed. Then, singular value decomposition (SVD) is used to assist Cholesky decomposition to ensure numerical stability in the time update phase of the algorithm, while adjusting the modified covariance, and performing Kalman in the measurement update phase. Finally, the experimental results of initial alignment show that the improved CKF can deal with the SINS initial alignment problem well. The filtering accuracy is comparable to the CKF estimation accuracy, and the solving speed is better than the CKF.
机译:大失准角捷联惯导系统的初始对准模型是线性和非线性混合系统模型。针对该模型,本文提出了一种改进的库伯卡尔曼滤波算法。首先,建立并分析了捷联惯导系统的初始对准模型。然后,使用奇异值分解(SVD)协助Cholesky分解,以确保算法时间更新阶段的数值稳定性,同时调整修正的协方差,并在测量更新阶段执行Kalman。最后,初始对准实验结果表明,改进的CKF可以很好地解决SINS初始对准问题。滤波精度与CKF估计精度相当,并且求解速度优于CKF。

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