In order to facilitate high-precision and real-time Precise Point Positioning(PPP),the International GNSS(Global Navigation Satellite System)Service(IGS),BDS-3(BeiDou-3 Navigation Satellite System),and Galileo navigat...In order to facilitate high-precision and real-time Precise Point Positioning(PPP),the International GNSS(Global Navigation Satellite System)Service(IGS),BDS-3(BeiDou-3 Navigation Satellite System),and Galileo navigation satellite system(Galileo)have provided real-time satellite clock correction,which is updated at a high-frequency.However,the frequent updates pose the challenges of increasing the computational burden and compromising the timeliness of these correction parameters.To address this issue,an improved Real-Time Service(RTS)method is developed using an extrapolation algorithm and a linear model.The results indicate that a 1 h arc length of the satellite clock correction series is optimal for fitting a linear model of the RTS.With this approach,the 1 h extrapolation results for BDS-3 and Galileo are superior to 0.09 ns.Moreover,when these model coefficients are transmitted and updated at the intervals of 1,2,5,and 10 min,the corresponding PPP can converge at the centimeter-level.It is evident that these improved RTS methods outperform the current approach with high-frequency interval transmission,as they effectively mitigate the challenges associated with maintaining the timeliness of correction parameters.展开更多
当前,在低轨导航增强、对地观测和科学应用等领域,低轨卫星对轨道参数的精度和实时性提出了更高的要求。利用国际GNSS服务组织实时服务(international global navigation satellite system service real-time service,IGS-RTS)播发的GP...当前,在低轨导航增强、对地观测和科学应用等领域,低轨卫星对轨道参数的精度和实时性提出了更高的要求。利用国际GNSS服务组织实时服务(international global navigation satellite system service real-time service,IGS-RTS)播发的GPS卫星轨道与钟差改正数,针对极区实时改正数接收中断情况下实现厘米级星载GPS实时定轨的关键问题开展研究。首先分析了实时改正数及其短时外推引起的星历综合误差的变化特性;然后以此为依据,在星载GPS实时精密定轨数学模型中构建分段随机游走的伪模糊度参数随机模型,以减小星历综合误差对实时精密定轨的影响,从而实现厘米级精度的实时定轨。采用自主研制的实时精密定轨软件SATODS,使用GPS广播星历与CLK93实时产品,对为期一周的重力场恢复和气候实验(gravity recovery and climate experiment,GRACE)C卫星的GPS双频实测数据模拟在轨实时精密定轨处理。实验结果表明,在考虑极区改正数接收中断的情况下,所提实时精密定轨方法可以达到7.04 cm的位置精度以及0.20 mm/s的速度精度,所提方法具有可行性和有效性。展开更多
基金This research is supported by the National Natural Science Foundation of China(NSFC)(Nos.42174019 and 41974025)the Fundamental Research Funds for the Central Universities.
文摘In order to facilitate high-precision and real-time Precise Point Positioning(PPP),the International GNSS(Global Navigation Satellite System)Service(IGS),BDS-3(BeiDou-3 Navigation Satellite System),and Galileo navigation satellite system(Galileo)have provided real-time satellite clock correction,which is updated at a high-frequency.However,the frequent updates pose the challenges of increasing the computational burden and compromising the timeliness of these correction parameters.To address this issue,an improved Real-Time Service(RTS)method is developed using an extrapolation algorithm and a linear model.The results indicate that a 1 h arc length of the satellite clock correction series is optimal for fitting a linear model of the RTS.With this approach,the 1 h extrapolation results for BDS-3 and Galileo are superior to 0.09 ns.Moreover,when these model coefficients are transmitted and updated at the intervals of 1,2,5,and 10 min,the corresponding PPP can converge at the centimeter-level.It is evident that these improved RTS methods outperform the current approach with high-frequency interval transmission,as they effectively mitigate the challenges associated with maintaining the timeliness of correction parameters.
文摘当前,在低轨导航增强、对地观测和科学应用等领域,低轨卫星对轨道参数的精度和实时性提出了更高的要求。利用国际GNSS服务组织实时服务(international global navigation satellite system service real-time service,IGS-RTS)播发的GPS卫星轨道与钟差改正数,针对极区实时改正数接收中断情况下实现厘米级星载GPS实时定轨的关键问题开展研究。首先分析了实时改正数及其短时外推引起的星历综合误差的变化特性;然后以此为依据,在星载GPS实时精密定轨数学模型中构建分段随机游走的伪模糊度参数随机模型,以减小星历综合误差对实时精密定轨的影响,从而实现厘米级精度的实时定轨。采用自主研制的实时精密定轨软件SATODS,使用GPS广播星历与CLK93实时产品,对为期一周的重力场恢复和气候实验(gravity recovery and climate experiment,GRACE)C卫星的GPS双频实测数据模拟在轨实时精密定轨处理。实验结果表明,在考虑极区改正数接收中断的情况下,所提实时精密定轨方法可以达到7.04 cm的位置精度以及0.20 mm/s的速度精度,所提方法具有可行性和有效性。