改进CKF在SINS大不对准角初始对准中的应用

Y. Liu, Tijing Cai, Li-Ming Wu
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引用次数: 1

摘要

为了提高捷联惯导系统的对准精度,减少初始对准时间,提出了一种改进的CKF方法。建立了具有较大初始不对准角的捷联惯导系统非线性误差模型。在CKF基本算法的基础上,在预测误差的协方差矩阵中引入多个衰落因子,实时在线调制各数据通道的增益矩阵,提高了算法的精度和鲁棒性;采用奇异值分解代替传统的CKF的Cholesky分解,提高了算法的稳定性。实验结果表明,改进的CKF对方位角的对准时间比CKF短100 s,对准精度比CKF提高40%,方位角对准精度小于0.1°。实验结果表明,改进后的CKF在提高速度的前提下,有效地提高了对准精度,更好地适应惯导系统初始对准时较大的不对准角。
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Application of Improved CKF in SINS Initial Alignment with Large Misalignment Angles
In order to improve the alignment accuracy and reduce time for the initial alignment of SINS, an improved CKF method is proposed. SINS nonlinear error model with large initial misalignment angles is built up. Based on the basic algorithm of CKF, multiple fading factors are introduced to the covariance matrix of the prediction errors to modulate gain matrix online in real-time for each data channel, which can improve the accuracy and robustness of the algorithm; Singular Value Decomposition is used instead of the traditional Cholesky decomposition of CKF to improve the stability of the algorithm. Experiment results show that the alignment time for azimuth angle of improved CKF is 100 seconds shorter than CKF, the alignment accuracy improved by 40% compared with CKF, and the alignment accuracy of azimuth angle is less than 0.1°. The experimental results show that the improved CKF effectively improves the alignment accuracy under the premise of higher speed, which better fits SINS initial alignment for large misalignment angles.
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