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Multiple model adaptive estimation algorithm for SINS/CNS integrated navigation system

机译:SINS / CNS组合导航系统的多模型自适应估计算法

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In this paper, we investigate the Multiple Model Adaptive Estimation (MMAE) and present a new filtering method based on MMAE algorithm. This method is applied to the SINS/CNS integrated navigation system under the motion of ballistic missile. In this proposed algorithm, we use improved Kalman filters rather than traditional Kalman filters, such as Extended Kalman Filter (EKF), Unscented Kalman Filter (UKF). And EKF and UKF are used as sub filters in MMAE algorithm to realize the state estimation of nonlinear system. Single model filters have poor adaptability, when system parameters are unknown or uncertainty. The proposed multiple model filters can solve this problem. As the simulation result shows, the improved filtering methods have better navigation accuracy, and can be more flexible when compared with traditional EKF and UKF algorithms, but pay for heavier computational burden.
机译:在本文中,我们研究了多模型自适应估计(MMAE),并提出了一种基于MMAE算法的新滤波方法。该方法适用于弹道导弹运动下的SINS / CNS组合导航系统。在该算法中,我们使用改进的卡尔曼滤波器,而不是传统的卡尔曼滤波器,例如扩展卡尔曼滤波器(EKF),无味卡尔曼滤波器(UKF)。 EKF和UKF作为MMAE算法的子滤波器,实现了非线性系统的状态估计。当系统参数未知或不确定时,单模型滤波器的适应性较差。提出的多模型滤波器可以解决这个问题。仿真结果表明,改进的滤波方法具有更好的导航精度,与传统的EKF和UKF算法相比具有更高的灵活性,但付出了较大的计算负担。

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