基于Tikhonov正则化参数优化的北斗多径误差减小方法

Remote. Sens. Pub Date : 2023-07-04 DOI:10.3390/rs15133400
Xinzhong Li, Yongliang Xiong, Shaoguang Xu, Weiwei Chen, Ban Zhao, Rui Zhang
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摘要

多径误差是制约北斗卫星导航系统相对定位精度的重要因素。由于反射环境的复杂性,多径误差的数学建模相当困难。恒星滤波算法利用周期重复的特性对多径误差进行校正,大大降低了多径误差的影响,提高了定位和姿态测量的精度。由于北斗系统的星座非均质性,侧滤波的应用比较复杂。基于重构的载波相位单差残差,采用分割思想估计北斗卫星的多径重复时间。利用Tikhonov正则化方法和经典小波方法提取载波相位单差残差的多径,得到单差残差的“干净”序列。实验结果表明,采用Tikhonov正则化方法正确提取多径误差是可行的,且多径误差比原始残差测量更平滑。进一步优化了正则化参数的估计方法。采用优化的带恒星滤波的Tikhonov正则化方法后,GEO、IGSO和MEO卫星的平均RMS分别提高了45.9%、38.2%和37.5%。E、N、U组件的定位精度分别提高24.8%、26.3%、42.7%。在横摆角和俯仰角分别提高了22.9%和12.6%的姿态分辨精度。所提出的方法可以作为备选的北斗系统多径误差建模和缓解方法。
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A Multipath Error Reduction Method for BDS Using Tikhonov Regularization with Parameter Optimization
Multipath error is an important factor restricting the relative positioning accuracy of the Beidou Navigation Satellite System (BDS). Because of the complexity of the reflection environment, the mathematical modeling of multipath errors is quite difficult. The sidereal filtering algorithm corrects multipath errors by using the feature of period repetition, which can greatly reduce its influence and improve the accuracy of positioning and attitude measurement. In view of the constellation heterogeneity of BDS, it is more complicated to apply sideral filtering. Based on the reconstructed single-difference residual of the carrier phase, the multipath repetition time of the Beidou satellite is estimated using the idea of segmentation. The Tikhonov regularization method and the classical wavelet method are used to extract the multipath of the single-difference residual of the carrier phase, and the “clean” sequence of the single-difference residual is obtained. The experimental results show that it is feasible to extract the multipath error correctly by Tikhonov regularization, and the multipath error is smoother than the original residual measurement. Furthermore, the estimation method of the regularization parameter is further optimized. After using the optimized Tikhonov regularization method with sidereal filtering, the mean RMS improvements of GEO, IGSO, and MEO satellites are 45.9%, 38.2%, and 37.5%, respectively. The positioning accuracy on E, N, and U components is improved by 24.8%, 26.3%, and 42.7%, respectively. The attitude resolution accuracy is improved by 22.9% in the yaw angle and 12.6% in the pitch angle. The proposed method can be an alternative BDS multipath error modeling and mitigation approach.
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