Signal-In-Space Precision Analysis for IGSO and MEO Satellites of BDS Considering the Age of Data
Abstract The paper analyzes the characteristics of AODE in broadcast ephemeris for different orbit of BDS from 2013 to 2015. According to the AODE distribution of IGSO and MEO, the signal-in-space accuracy based on different AODE is analyzed in the paper. The results show: AODE of satellites is in period and is consistent with the orbit. For IGSO satellites, the average AODE is about 1.7 hours, reaching to a maximum of 7 hours. Considering orbit alone, the URE of different AODE varies 0.5 m at the worst. For MEO satellites, the average AODE is about 11 hours, and the maximum reachedis two days. Considering orbit alone, the URE of different AODE varies 0.9 m for the worst. During 2013 to 2015,the average URE of IGSO satellites are 0.81 m, 0.84 m and 1.11 m; for MEO satellites they are 0.84 m, 0.82 m and 1.04 m.
Key words :
BDS
navigation message
AODE
signal-in-space precision
Cite this article:
LIU Yuxi,JIA Xiaolin. Signal-In-Space Precision Analysis for IGSO and MEO Satellites of BDS Considering the Age of Data[J]. jgg, 2018, 38(4): 390-393.
LIU Yuxi,JIA Xiaolin. Signal-In-Space Precision Analysis for IGSO and MEO Satellites of BDS Considering the Age of Data[J]. jgg, 2018, 38(4): 390-393.
URL:
http://www.jgg09.com/EN/ OR http://www.jgg09.com/EN/Y2018/V38/I4/390
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ZHAO Hui,JIN Shuanggen,LUO Peng. Applicability of Different Solar Radiation Pressure Models for Beidou IGSO and MEO Satellites Orbit Determination [J]. jgg, 2022, 42(1): 9-14.
[2]
E Shenglong,ZHOU Gang,LONG Hai,LUO Yingting,XU Hailin,RAO Zhangquan,ZHOU Yongyan. Performance Evaluation of BDS Global Positioning Service and Zenith Tropospheric Delay Estimation [J]. jgg, 2021, 41(8): 789-794.
[3]
DING Yitao,GUO Meijun. Accuracy Analysis of Beidou Ionosphere Model [J]. jgg, 2021, 41(2): 131-139.
[4]
JIANG Yi,LIU Chen,LUO Fangyuan,ZHAO Huakai. Analysis of Anti-Disturbance Capability of Ionospheric Correction for BDS [J]. jgg, 2020, 40(9): 892-897.
[5]
Lü Weicai,GAO Jingxiang,YAN Chao,XU Wei,HUANG Hui,YANG Haisheng. Research on Cycle Slip Detection Algorithm for Beidou Triple-Frequency Carrier Pseudorange Combination [J]. jgg, 2020, 40(2): 117-122.
[6]
HE Maihang,SUN Fuping,XIAO Kai,ZHANG Lundong,ZHU Xinhui. Model and Verification of Beidou Triple-Frequency IF-PPP Based on Space Geometric Principle [J]. jgg, 2020, 40(12): 1290-1293.
[7]
YIN Hengyi,GUO Chunxi,HUI Zhe,ZHAO Hong,WANG Wei,CHENG Xiawei. Precision Analysis of Precipitable Water Vapor in Different BDS Ephemeris [J]. jgg, 2020, 40(11): 1182-1187.
[8]
XU Yangyin,YANG Yuanxi,ZENG Anmin,MA Yueyuan. Accuracy Assessment of Signal in Space of BDS-3 Global System [J]. jgg, 2020, 40(10): 1000-1006.
[9]
WANG Xingxing,TU Rui,HONG Ju,LIU Chongjin,LIU Jinhai. BDS Velocity Estimation and Performance Analysis Based on Time-Difference Model [J]. jgg, 2019, 39(1): 7-12.
[10]
WU Renpan,LIU Wanke,WU Fengbo,LI Jianlong. Analysis of TTFF and Accuracy of BDS Medium-Long Baseline Kinematic Relative Positioning [J]. jgg, 2018, 38(7): 668-672.
[11]
PENG Hanbing,YANG Yuanxi,WANG Gang,LI Yu. Effect Analysis of GPS/BDS Combined Orbit Determination on Beidou Satellite Orbits [J]. jgg, 2018, 38(12): 1262-1267.
[12]
CHANG Zhiqiao,HU Xiaogong,HUANG Hua,HU Guangming,LI Xiaojie,TANG Chengpan,DONG Enqiang. The Broadcast Ephemeris Fitting Algorithm Combining No Singularity Orbital Elements with Coordinate Rotation and Its Performance Evaluation= [J]. jgg, 2017, 37(7): 732-736.
[13]
LIU Yuxi,JIA Xiaolin,RUAN Rengui. Beidou IGSO Satellite Orbit Determination Precision Analysis Based on New Attitude Control Mode [J]. jgg, 2017, 37(6): 614-617.
[14]
LI Xin,ZENG Qi,GUAN Shoukui. Methods of Beidou Pseudorange Multipath Deviation Correction [J]. jgg, 2016, 36(8): 727-731.
[15]
LIU Weiping,HAO Jinming,WEI Wei,et al. Comparison of Two Methods of Precise Orbit Determination of Beidou Satellites [J]. jgg, 2016, 36(3): 211-215.