An improved Kalman filter algorithm for tightly GNSS/INS integrated navigation system
The Kalman filter based on singular value decomposition (SVD) can sufficiently reduce the accumulation of rounding errors and is widely used in various applications with numerical calculations. However, in order to improve the filtering performance and adaptability in a tightly GNSS/INS (Global Navi...
| Published in: | Mathematical Biosciences and Engineering |
|---|---|
| Main Authors: | , , , , |
| Format: | Article |
| Language: | English |
| Published: |
AIMS Press
2024-01-01
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| Subjects: | |
| Online Access: | https://www.aimspress.com/article/doi/10.3934/mbe.2024040?viewType=HTML |
| _version_ | 1849988591108751360 |
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| author | Yuelin Yuan Fei Li Jialiang Chen Yu Wang Kai Liu |
| author_facet | Yuelin Yuan Fei Li Jialiang Chen Yu Wang Kai Liu |
| author_sort | Yuelin Yuan |
| collection | DOAJ |
| container_title | Mathematical Biosciences and Engineering |
| description | The Kalman filter based on singular value decomposition (SVD) can sufficiently reduce the accumulation of rounding errors and is widely used in various applications with numerical calculations. However, in order to improve the filtering performance and adaptability in a tightly GNSS/INS (Global Navigation Satellite System and Inertial Navigation System) integrated navigation system, we propose an improved robust method to satisfy the requirements. To solve the issue of large fluctuations in GNSS signals faced by the conventional method that uses a fixed noise covariance, the proposed method constructs a correction variable through the innovation and the new matrix which is obtained by performing SVD on the original matrix, dynamically correcting the noise covariance and has better robustness. In addition, the derived SVD form of the information filter (IF) extends its application. The proposed method has higher positioning accuracy and can be better applied to tightly coupled GNSS/INS navigation simulations and physical experiments. The experimental results show that, compared with the traditional Kalman algorithm based on SVD, the proposed algorithm*s maximum error is reduced by 45.77%. Compared with the traditional IF algorithm, the root mean squared error of the proposed IF algorithm in the form of SVD is also reduced by 4.7%. |
| format | Article |
| id | doaj-art-e1095f3b25f64a4ea4092be02e726aae |
| institution | Directory of Open Access Journals |
| issn | 1551-0018 |
| language | English |
| publishDate | 2024-01-01 |
| publisher | AIMS Press |
| record_format | Article |
| spelling | doaj-art-e1095f3b25f64a4ea4092be02e726aae2025-08-20T00:54:40ZengAIMS PressMathematical Biosciences and Engineering1551-00182024-01-0121196398310.3934/mbe.2024040An improved Kalman filter algorithm for tightly GNSS/INS integrated navigation systemYuelin Yuan0Fei Li 1Jialiang Chen2Yu Wang3Kai Liu41. School of Electronic Science, National University of Defense Technology, Changsha 410005, China2. School of Transportation and Logistics, Dalian University of Technology, Dalian 116024, China2. School of Transportation and Logistics, Dalian University of Technology, Dalian 116024, China3. School of Traffic and Transportation Engineering, Dalian Jiaotong University, Dalian 116028, China2. School of Transportation and Logistics, Dalian University of Technology, Dalian 116024, ChinaThe Kalman filter based on singular value decomposition (SVD) can sufficiently reduce the accumulation of rounding errors and is widely used in various applications with numerical calculations. However, in order to improve the filtering performance and adaptability in a tightly GNSS/INS (Global Navigation Satellite System and Inertial Navigation System) integrated navigation system, we propose an improved robust method to satisfy the requirements. To solve the issue of large fluctuations in GNSS signals faced by the conventional method that uses a fixed noise covariance, the proposed method constructs a correction variable through the innovation and the new matrix which is obtained by performing SVD on the original matrix, dynamically correcting the noise covariance and has better robustness. In addition, the derived SVD form of the information filter (IF) extends its application. The proposed method has higher positioning accuracy and can be better applied to tightly coupled GNSS/INS navigation simulations and physical experiments. The experimental results show that, compared with the traditional Kalman algorithm based on SVD, the proposed algorithm*s maximum error is reduced by 45.77%. Compared with the traditional IF algorithm, the root mean squared error of the proposed IF algorithm in the form of SVD is also reduced by 4.7%.https://www.aimspress.com/article/doi/10.3934/mbe.2024040?viewType=HTMLkalman filtersvdtightly coupled gnss/ins navigationcovariance matchinginformation filter |
| spellingShingle | Yuelin Yuan Fei Li Jialiang Chen Yu Wang Kai Liu An improved Kalman filter algorithm for tightly GNSS/INS integrated navigation system kalman filter svd tightly coupled gnss/ins navigation covariance matching information filter |
| title | An improved Kalman filter algorithm for tightly GNSS/INS integrated navigation system |
| title_full | An improved Kalman filter algorithm for tightly GNSS/INS integrated navigation system |
| title_fullStr | An improved Kalman filter algorithm for tightly GNSS/INS integrated navigation system |
| title_full_unstemmed | An improved Kalman filter algorithm for tightly GNSS/INS integrated navigation system |
| title_short | An improved Kalman filter algorithm for tightly GNSS/INS integrated navigation system |
| title_sort | improved kalman filter algorithm for tightly gnss ins integrated navigation system |
| topic | kalman filter svd tightly coupled gnss/ins navigation covariance matching information filter |
| url | https://www.aimspress.com/article/doi/10.3934/mbe.2024040?viewType=HTML |
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