2021
DOI: 10.3390/s21206930
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Using Multi-Antenna Trajectory Constraint to Analyze BeiDou Carrier-Phase Observation Error of Dynamic Receivers

Abstract: Appropriate cycle-slip and measurement-error models are essential for BeiDou carrier-phase-based integrity risk calculation. To establish the receiver’s measurement-error model, an accurate position reference of the GNSS antenna is fundamental for calculating the measurement error. However, it is still a challenge to acquire position references for dynamic BeiDou receivers, resulting in improper GNSS measurement-error models and unreliable integrity monitoring. This paper proposes an improved precise relative … Show more

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“…where j denotes the satellite number; E denotes the satellite elevation; Cycle slips are added into the carrier-phase observations with a certain probability corresponding to the value of 1  , 2  or 2  . The frequency of occurrence of cycle slips is obtained by statistically analyzing long-term data collected from the dynamic experiment with the same GNSS receiver (Xiong, Li, Wang, & Wu, 2021). In the simulation, the specific ratio is selected as 45.06% ( 1  ), 10.85% ( 2  ) and 44.09% ( 2  ).…”
Section: Simulation Settingsmentioning
confidence: 99%
“…where j denotes the satellite number; E denotes the satellite elevation; Cycle slips are added into the carrier-phase observations with a certain probability corresponding to the value of 1  , 2  or 2  . The frequency of occurrence of cycle slips is obtained by statistically analyzing long-term data collected from the dynamic experiment with the same GNSS receiver (Xiong, Li, Wang, & Wu, 2021). In the simulation, the specific ratio is selected as 45.06% ( 1  ), 10.85% ( 2  ) and 44.09% ( 2  ).…”
Section: Simulation Settingsmentioning
confidence: 99%