An Improved Initial Alignment Method Based on SE<sub>2</sub>(3)/EKF for SINS/GNSS Integrated Navigation System with Large Misalignment Angles.

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作者： Jin,Sun ^[1] ; Yuxin,Chen ^[2] ; Bingbo,Cui ^[3]

作者单位： College of Internet of Things, Nanjing University of Posts and Telecommunications, Nanjing 210003, China. ^[1] State Key Laboratory of Ocean Engineering, Shanghai Jiao Tong University, Shanghai 200240, China. ^[2] Portland Institute, Nanjing University of Posts and Telecommunications, Nanjing 210003, China. ^[3] Key Laboratory of Modern Agricultural Equipment and Technology, Ministry of Education and Jiangsu Province, Jiangsu University, Zhenjiang 212013, China. ^[4] School of Agricultural Engineering, Jiangsu University, Zhenjiang 212013, China. ^[5]

关键词 Lie group SINS/GNSS integrated navigation system global navigation satellite system (GNSS)initial alignment large misalignment angles strap-down inertial navigation system (SINS)three-dimension special Euclidean group and extended Kalman filter (SE2(3)/EKF)

DOI 10.3390/s24092945

PMID 38733051

发布时间 2024-05-13

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