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