The precision orbit determination of challenging minisatellite payload(CHAMP) satellite was done based on position and navigation data analyst(PANDA) software which is developed in Wuhan University, using the onboard ...The precision orbit determination of challenging minisatellite payload(CHAMP) satellite was done based on position and navigation data analyst(PANDA) software which is developed in Wuhan University, using the onboard GPS data of year 2002 from day 126 to 131. The orbit accuracy was assessed by analyzing the difference from GFZ post-processed science orbits (PSO), the GPS carrier and pseudo-range data residuals and the satellite laser ranging (SLR) residuals.展开更多
The earth gravity field model CDS01S of degree and order 36 has been recovered from the post processed Science Orbits and on-board accelerometer data of GFZ’s CHAMP satellite. The model resolves the geoid with an acc...The earth gravity field model CDS01S of degree and order 36 has been recovered from the post processed Science Orbits and on-board accelerometer data of GFZ’s CHAMP satellite. The model resolves the geoid with an accuracy of better than 4 cm at a resolution of 700 km half-wavelength. By using the degree difference variances of geopotential coefficients to compare the model CDS01S with EIGEN3P, EIGEN1S and EGM96, the result indicates that the coefficients of CDS01S are most close to those of EIGEN3P. The result of the comparison between the accuracies of geopotential coefficients in the above models, indicates that the accuracy of coefficients in CDS01S is higher than that in EGM96.The geoid undulations of CDS01S and GGM01C up to 30 degrees are calculated and the standard deviation is 4.7 cm between them.展开更多
A medium earth orbit （MEO） tracking and data relay satellite system （TDRSS） constellation scheme for China is proposed. This system consists of MEO satellite constellation, inter-satellite links （ISLs） and terre...A medium earth orbit （MEO） tracking and data relay satellite system （TDRSS） constellation scheme for China is proposed. This system consists of MEO satellite constellation, inter-satellite links （ISLs） and terrestrial gateway station, which can provide continuous bidirectional data transmission links between low altitude spacecrafls and the terrestrial gateway station in China. Theoretical analysis and simulation results indicate that the proposed constellation can cover the global low altitude space sphere and earth surface of China continuously, and has a preferable practical perspective.展开更多
低轨卫星导航定位是新一代卫星导航技术发展的重要方向,使用低轨卫星提供高精度定位、导航与授时(positioning,navigation and timing,PNT)服务,需要能够利用下行数据对其进行精密定轨.目前低轨卫星定轨相关研究多以星载GNSS数据和星间...低轨卫星导航定位是新一代卫星导航技术发展的重要方向,使用低轨卫星提供高精度定位、导航与授时(positioning,navigation and timing,PNT)服务,需要能够利用下行数据对其进行精密定轨.目前低轨卫星定轨相关研究多以星载GNSS数据和星间链路数据为研究对象,缺少针对低地球轨道(low earth orbit,LEO)下行数据定轨能力的分析.为分析低轨卫星下行数据定轨性能,模拟仿真了轨道高度1000 km、轨道倾角48°的Walker 90/10/1低轨卫星导航星座、150个地面测站及相应轨道、钟差和观测数据.分别使用测站数为60、90、120和150的全球测站网络观测数据进行LEO卫星精密定轨,并对定轨精度和可视测站卫星位置精度衰减因子(satellite position dilution of precision,SPDOP)值进行分析.结果表明:测站数从60增加至150可使LEO卫星轨道1d均方根(root mean square,RMS)从117.5 mm提升至39.8 mm;当测站稀疏时,LEO卫星定轨精度降低迅速;增加测站可以有效改善陆地范围可视测站SPDOP和LEO卫星定轨精度,但由于测站跟踪范围有限,海洋区域可视测站SPDOP和LEO卫星定轨精度难以获得改善,需引入新的观测数据源.研究结果可为低轨导航卫星系统建设提供支持.展开更多
The satellite constellation classes, which are suitable for the medium earth orbit tracking and data relay satellite system （MEO-TDRSS） of China, are investigated. On the basis of the functionality and the traffic d...The satellite constellation classes, which are suitable for the medium earth orbit tracking and data relay satellite system （MEO-TDRSS） of China, are investigated. On the basis of the functionality and the traffic distribution characteristic of MEO-TDRSS, the coverage performance and inter-satellite link properties of four different constellation schemes are compared by simulations. Simulation results indicate that the rosette and common-track constellations, whose satellites are distributed on the celestial sphere more uniformly, are appropriate for the implementation of MEO-TDRSS of China.展开更多
China’s efforts to develop Fengyun meteorological satellites have made major strides over the past 50 years,with the polar and geostationary meteorological satellite series achieving continuously stable operation to ...China’s efforts to develop Fengyun meteorological satellites have made major strides over the past 50 years,with the polar and geostationary meteorological satellite series achieving continuously stable operation to persistently provide data and product services globally.By the end of 2021,19 Chinese self-developed Fengyun meteorological satellites have been launched successfully.Seven of them are in operation at present,the data and products are widely applied to weather analysis,numerical weather forecasting and climate prediction,as well as environment and disaster monitoring.Since the last COSPAR report,FY-4B,the first new-generation operational geostationary satellite,and FY-3E,the first early-morning orbit satellite in China’s polar-orbiting meteorological satellite family have been launched in 2021.The characteristics of the two latest satellites and the instruments onboard are addressed in this report.The status of current Fengyun Satellites,product and data service and international cooperation and supporting activities has been introduced as well.展开更多
文摘The precision orbit determination of challenging minisatellite payload(CHAMP) satellite was done based on position and navigation data analyst(PANDA) software which is developed in Wuhan University, using the onboard GPS data of year 2002 from day 126 to 131. The orbit accuracy was assessed by analyzing the difference from GFZ post-processed science orbits (PSO), the GPS carrier and pseudo-range data residuals and the satellite laser ranging (SLR) residuals.
文摘The earth gravity field model CDS01S of degree and order 36 has been recovered from the post processed Science Orbits and on-board accelerometer data of GFZ’s CHAMP satellite. The model resolves the geoid with an accuracy of better than 4 cm at a resolution of 700 km half-wavelength. By using the degree difference variances of geopotential coefficients to compare the model CDS01S with EIGEN3P, EIGEN1S and EGM96, the result indicates that the coefficients of CDS01S are most close to those of EIGEN3P. The result of the comparison between the accuracies of geopotential coefficients in the above models, indicates that the accuracy of coefficients in CDS01S is higher than that in EGM96.The geoid undulations of CDS01S and GGM01C up to 30 degrees are calculated and the standard deviation is 4.7 cm between them.
基金National Natural Science Foundation of China (No. 60372013)
文摘A medium earth orbit （MEO） tracking and data relay satellite system （TDRSS） constellation scheme for China is proposed. This system consists of MEO satellite constellation, inter-satellite links （ISLs） and terrestrial gateway station, which can provide continuous bidirectional data transmission links between low altitude spacecrafls and the terrestrial gateway station in China. Theoretical analysis and simulation results indicate that the proposed constellation can cover the global low altitude space sphere and earth surface of China continuously, and has a preferable practical perspective.
文摘低轨卫星导航定位是新一代卫星导航技术发展的重要方向,使用低轨卫星提供高精度定位、导航与授时(positioning,navigation and timing,PNT)服务,需要能够利用下行数据对其进行精密定轨.目前低轨卫星定轨相关研究多以星载GNSS数据和星间链路数据为研究对象,缺少针对低地球轨道(low earth orbit,LEO)下行数据定轨能力的分析.为分析低轨卫星下行数据定轨性能,模拟仿真了轨道高度1000 km、轨道倾角48°的Walker 90/10/1低轨卫星导航星座、150个地面测站及相应轨道、钟差和观测数据.分别使用测站数为60、90、120和150的全球测站网络观测数据进行LEO卫星精密定轨,并对定轨精度和可视测站卫星位置精度衰减因子(satellite position dilution of precision,SPDOP)值进行分析.结果表明:测站数从60增加至150可使LEO卫星轨道1d均方根(root mean square,RMS)从117.5 mm提升至39.8 mm;当测站稀疏时,LEO卫星定轨精度降低迅速;增加测站可以有效改善陆地范围可视测站SPDOP和LEO卫星定轨精度,但由于测站跟踪范围有限,海洋区域可视测站SPDOP和LEO卫星定轨精度难以获得改善,需引入新的观测数据源.研究结果可为低轨导航卫星系统建设提供支持.
基金the National Natural Science Foundation of China (60372013)
文摘The satellite constellation classes, which are suitable for the medium earth orbit tracking and data relay satellite system （MEO-TDRSS） of China, are investigated. On the basis of the functionality and the traffic distribution characteristic of MEO-TDRSS, the coverage performance and inter-satellite link properties of four different constellation schemes are compared by simulations. Simulation results indicate that the rosette and common-track constellations, whose satellites are distributed on the celestial sphere more uniformly, are appropriate for the implementation of MEO-TDRSS of China.
基金Supported by the National Key Research and Development Program of China(2018YFB0504900,2018YFB0504905)the National Project on Fengyun Meteorological Satellite Development。
文摘China’s efforts to develop Fengyun meteorological satellites have made major strides over the past 50 years,with the polar and geostationary meteorological satellite series achieving continuously stable operation to persistently provide data and product services globally.By the end of 2021,19 Chinese self-developed Fengyun meteorological satellites have been launched successfully.Seven of them are in operation at present,the data and products are widely applied to weather analysis,numerical weather forecasting and climate prediction,as well as environment and disaster monitoring.Since the last COSPAR report,FY-4B,the first new-generation operational geostationary satellite,and FY-3E,the first early-morning orbit satellite in China’s polar-orbiting meteorological satellite family have been launched in 2021.The characteristics of the two latest satellites and the instruments onboard are addressed in this report.The status of current Fengyun Satellites,product and data service and international cooperation and supporting activities has been introduced as well.
