2007Journal of Chinese Inertial TechnologyRequires access

Integrated navigation system of three-star passive Beidou/SINS based on pseudo-range difference

Xiaodong Zhang

Open publisher page 1 citations

Abstract

Since the Beidou is in the orbit far from the earth, the error of the pseudo-range of the Beidou receiver is large enough to affect the performance of passive Beidou three-star/SINS system. Considering the complexity of Beidou pseudo-range error model and the precision of the error estimation model in Kalman filtering, the method of pseudo-range difference on a single receiver was presented to reduce the measurement error. The model of three-star/SINS integrated navigation system based on the pseudo-range difference was built based on the theory analysis. The field experiment shows that this algorithm improves the localization precision of the integrated navigation system and simplifies the filtering parameter.

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What this paper is about

Since the Beidou is in the orbit far from the earth, the error of the pseudo-range of the Beidou receiver is large enough to affect the performance of passive Beidou three-star/SINS system. Considering the complexity of Beidou pseudo-range error model and the precision of the error estimation model in Kalman filtering, the method of pseudo-range difference on a single receiver was presented to reduce the measurement error. The model of three-star/SINS integrated navigation system based on the pseudo-range difference was built based on the theory analysis. The field experiment shows that this algorithm improves the localization precision of the integrated navigation system and simplifies the filtering parameter.

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Available abstract

Since the Beidou is in the orbit far from the earth, the error of the pseudo-range of the Beidou receiver is large enough to affect the performance of passive Beidou three-star/SINS system. Considering the complexity of Beidou pseudo-range error model and the precision of the error estimation model in Kalman filtering, the method of pseudo-range difference on a single receiver was presented to reduce the measurement error. The model of three-star/SINS integrated navigation system based on the pseudo-range difference was built based on the theory analysis. The field experiment shows that this algorithm improves the localization precision of the integrated navigation system and simplifies the filtering parameter.

Key concepts: Kalman filter, Pseudorange, Range (aeronautics), Computer science, Celestial navigation, BeiDou Navigation Satellite System, Orbit determination, Navigation system

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