An Improved Robust Estimation Method for GNSS/SINS under GNSS-Challenged Environment

Junwei Wang, Xiyuan Chen, Chunfeng Shi, Jianguo Liu
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引用次数: 1

Abstract

The outlier measurement affects the accurate estimation effect of tightly coupled global navigation satellite system (GNSS) and strapdown inertial navigation system (SINS) integrated navigation parameters under GNSS-challenged environment. To improve the convergence speed and robustness of nonlinear filter used in tightly coupled GNSS/INS under GNSS-challenged environment, an iterated cubature Kalman filter (CKF) based on the improved robust estimation method is proposed. Firstly, the mind of nonlinear least squares regression is included into CKF framework, and multiple iterations are used to improve the convergence speed of the filter and the error compensation effect. Then, a simplified iterated update structure is developed to reduce the computational cost for integrated navigation system. Moreover, the Geman McClure (GM) loss function is introduced to reduce the weight of outlier measurement, which improves the robust estimation ability of the filter. The field experiment indicates that the proposed method has better compensation effect than traditional methods on navigation errors in the case of frequent signal outages.
GNSS挑战环境下改进的GNSS/SINS鲁棒估计方法
在全球卫星导航系统(GNSS)和捷联惯导系统(SINS)挑战环境下,离群值测量影响了紧密耦合卫星导航系统(GNSS)和捷联惯导系统(SINS)组合导航参数的准确估计效果。为了提高GNSS/INS紧耦合环境下非线性滤波器的收敛速度和鲁棒性,提出了一种基于改进鲁棒估计方法的迭代培养卡尔曼滤波器(CKF)。首先,将非线性最小二乘回归思想引入CKF框架,采用多次迭代的方法提高滤波的收敛速度和误差补偿效果;然后,提出了一种简化的迭代更新结构,以降低组合导航系统的计算成本。此外,引入了GM损失函数来降低离群值测量的权重,提高了滤波器的鲁棒估计能力。现场实验表明,在信号频繁中断的情况下,该方法对导航误差的补偿效果优于传统方法。
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