Application of Square-Root Information Kalman Filtering to Combined Navigation Systems

With the rapid development of modern science and technology, navigation technology plays a crucial role in transportation, aerospace, military and other fields. At present, a single navigation technology has been difficult to meet the complex navigation needs of high mobility carriers or special environments. Aiming at the above problems, this paper carries out an in-depth study on the tightly coupled navigation system of Strapdown Inertial Navigation System (SINS) and Global Navigation Satellite System (GNSS), and introduces the square-root information Kalman filtering algorithm. The algorithm takes the information matrix (the inverse of the mean square error matrix) as the updating object, which effectively avoids the numerical instability and non-positive characterization problems that may occur in the iterative process of the mean square error matrix. Compared with the traditional extended Kalman filter, the square-root information Kalman filter has higher numerical stability and computational efficiency in dealing with nonlinear systems, which is especially suitable for multi-sensor fusion scenarios.

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Publication Details

Journal
Academic Journal of Science and Technology
Published
2025-03-26
DOI
https://doi.org/10.54097/2kdp2109
Primary Topic
Inertial Sensor and Navigation
Type
article
Field-Weighted Citation Impact
0.00
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article

Application of Square-Root Information Kalman Filtering to Combined Navigation Systems

Yifan Yang, Luo Yanmin
Academic Journal of Science and Technology
Inertial Sensor and Navigation
article

Application of Square-Root Information Kalman Filtering to Combined Navigation Systems

Yifan Yang, Luo Yanmin
article en

Abstract

With the rapid development of modern science and technology, navigation technology plays a crucial role in transportation, aerospace, military and other fields. At present, a single navigation technology has been difficult to meet the complex navigation needs of high mobility carriers or special environments. Aiming at the above problems, this paper carries out an in-depth study on the tightly coupled navigation system of Strapdown Inertial Navigation System (SINS) and Global Navigation Satellite System (GNSS), and introduces the square-root information Kalman filtering algorithm. The algorithm takes the information matrix (the inverse of the mean square error matrix) as the updating object, which effectively avoids the numerical instability and non-positive characterization problems that may occur in the iterative process of the mean square error matrix. Compared with the traditional extended Kalman filter, the square-root information Kalman filter has higher numerical stability and computational efficiency in dealing with nonlinear systems, which is especially suitable for multi-sensor fusion scenarios.

Academic Journal of Science and TechnologyVol. 14(3)
Openalex Percentile: Top 92%
Inertial Sensor and Navigation
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