Performance Analysis of BDS Satellite Orbits during Eclipse Periods: Results of Satellite Laser Ranging Validation

  • PENG Hanbing ,
  • YANG Yuanxi ,
  • WANG Gang ,
  • HE Haibo
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  • 1. Institute of Geographical Spatial Information, Information Engineering University, Zhengzhou 450001, China;
    2. State Key Laboratory of Geo-information Engineering, Xi'an 710054, China;
    3. Beijing Satellite Navigation Center, Beijing 100094, China

Received date: 2015-12-22

  Revised date: 2016-03-31

  Online published: 2016-06-29

Supported by

The National Natural Science Foundation of China(Nos.41020144004A;41374019;41474015);The National High-tech Research and Development Program of China(863 Program)(No. 2013AA122501)

Abstract

The performance of BeiDou satellite orbits during eclipse periods is an important part of the performance analysis of BeiDou Navigation Satellite System (BDS). Accuracy evaluation of satellite orbits in ephemeris of BDS during eclipse periods can provide support for the service performance assessment. It also helps to find possible deficiencies in the orbit modeling during eclipse periods, which may further contribute to the improvements of functional models for precise orbit determination. The effects of eclipse periods on the orbits of the three types of satellites of BDS are analyzed with the satellite laser ranging (SLR) observations ranging from January 2014 to July 2015. At the same time, the orbit radial accuracy of BDS broadcast and precise ephemeris are validated. The results show that, obvious orbit accuracy decrease can be observed in both broadcast and precise ephemeris for IGSO/MEO satellites during eclipse periods (especially the yaw-maneuver periods). And orbit radial errors of IGSO/MEO satellites in broadcast ephemeris reach 1.5~2.0 m, and exceed 10.0 cm for that in precise ephemeris. Performance decrease of the GEO satellite orbit during eclipse arcs can hardly be revealed by the orbit radial residual series. During non-eclipse periods, radial accuracy of IGSO/MEO and GEO satellite orbits in broadcast ephemeris are better than 0.5 m and 0.9 m respectively. The radial accuracy of IGSO/MEO satellite orbits in precise ephemeris are better than 10.0 cm and that of the GEO satellite is about 50.0 cm with a systematic bias of 40.0 cm around.

Cite this article

PENG Hanbing , YANG Yuanxi , WANG Gang , HE Haibo . Performance Analysis of BDS Satellite Orbits during Eclipse Periods: Results of Satellite Laser Ranging Validation[J]. Acta Geodaetica et Cartographica Sinica, 2016 , 45(6) : 639 -645 . DOI: 10.11947/j.AGCS.2016.20150637

References

[1] 杨元喜, 李金龙, 王爱兵, 等. 北斗区域卫星导航系统基本导航定位性能初步评估[J]. 中国科学:地球科学, 2014, 44(1):72-81. YANG Yuanxi, LI Jinlong, WANG Aibing, et al. Preliminary Assessment of the Navigation and Positioning Performance of BeiDou Regional Navigation Satellite System[J]. Science China Earth Sciences, 2014, 57(1):144-152.
[2] MONTENBRUCK O,STEIGENBERGER P,KHACHIKYAN R, et al. IGS-MGEX:Preparing the Ground for Multi-constellation GNSS Science[J]. Inside GNSS, 2014, 9(1):42-49.
[3] BAR-SEVER Y E. A New Model for GPS Yaw Attitude[J]. Journal of Geodesy, 1996, 70(11):714-723.
[4] DAI Xiaolei,GE Maorong,LOU Yidong,et al. Estimating the Yaw-attitude of BDS IGSO and MEO Satellites[J]. Journal of Geodesy, 2015, 89(10):1005-1018.
[5] 郭靖. 姿态、光压和函数模型对导航卫星精密定轨影响的研究[D]. 武汉:武汉大学, 2014. GUO Jing. The Impacts of Attitude, Solar Radiation and Function Model on Precise Orbit Determination for GNSS Satellites[D]. Wuhan:Wuhan University, 2014.
[6] GUO Jing, ZHAO Qile, GENG Tao, et al. Precise Orbit Determination for COMPASS IGSO Satellites during Yaw Maneuvers[C]//Proceedings of China Satellite Navigation Conference (CSNC). Berlin:Springer, 2013:41-53.
[7] MONTENBRUCK O, SCHMID R, MERCIER F, et al. GNSS Satellite Geometry and Attitude Models[J]. Advances in Space Research, 2015, 56(6):1015-1029.
[8] KOUBA J. A Simplified Yaw-attitude Model for Eclipsing GPS Satellites[J]. GPS Solutions, 2009, 13(1):1-12.
[9] DILSSNER F, SPRINGER T, GIENGER G, et al. The GLONASS-M Satellite Yaw-attitude Model[J]. Advances in Space Research, 2011, 47(1):160-171.
[10] 杨元喜, 景一帆, 曾安敏. 自适应参数估计与内外部精度的关系[J]. 测绘学报, 2014, 43(5):441-445. DOI:10.13485/j.cnki.11-2089.2014.0077. YANG Yuanxi, JING Yifan, ZENG Anmin. Adaptive Parameter Estimation and Inner and External Precision[J]. Acta Geodaetica et Cartographica Sinica, 2014, 43(5):441-445. DOI:10.13485/j.cnki.11-2089.2014.0077.
[11] 秦显平, 杨元喜, 焦文海, 等. 利用SLR和伪距资料确定导航卫星钟差[J]. 测绘学报, 2004, 33(3):205-209. QIN Xianping, YANG Yuanxi, JIAO Wenhai, et al. Determination of Navigation Satellite Clock Bias Using SLR and Pseudorange Data[J]. Acta Geodaetica et Cartographica Sinica, 2004, 33(3):205-209.
[12] 秦显平, 杨元喜, 王刚, 等. SLR资料精密测定GLONASS卫星轨道[J]. 武汉大学学报(信息科学版), 2003, 28(4):440-443. QIN Xianping, YANG Yuanxi, WANG Gang, et al. GLONASS Orbit Determination by Using SLR Data[J]. Geomatics and Information Science of Wuhan University, 2003, 28(4):440-443.
[13] PAVLIS E C, BEARD R L. The Laser Retroreflector Experiment on GPS-35 and 36[M]//BEUTLER G, MELBOURNEW G, HEING W, et al. GPS Trends in Precise Terrestrial, Airborne, and Spaceborne Applications. Berlin:Springer, 1996:154-158.
[14] APPLEBY G, OTSUBO T. Comparison of SLR Measurements and Orbits with GLONASS and GPS Microwave Orbits[C]//Proceedings of the 12th International Workshop on Laser Ranging.Matera:NASA, 2000:13-17.
[15] SOS'NICA K, THALLER D, DACH R, et al. Satellite Laser Ranging to GPS and GLONASS[J]. Journal of Geodesy, 2015, 89(7):725-743.
[16] URSCHL C, GURTNER W, HUGENTOBLER U, et al. Validation of GNSS Orbits Using SLR Observations[J]. Advances in Space Research, 2005, 36(3):412-417.
[17] MONTENBRUCK O,STEIGENBERGER P,KIRCHNER G. GNSS Satellite Orbit Validation Using Satellite Laser Ranging[C]//Proceedings of the 18th International Workshop on Laser Ranging.Fujiyoshida:NASA,2013.
[18] MONTENBRUCK O, STEIGENBERGER P. The BeiDou Navigation Message[J]. Journal of Global Positioning Systems, 2013, 12(1):1-12.
[19] MONTENBRUCK O,STEIGENBERGER P,HAUSCHILD A. Broadcast versus Precise Ephemerides:A Multi-GNSS Perspective[J]. GPS Solutions, 2015, 19(2):321-333.
[20] STEIGENBERGER P, HUGENTOBLER U, HAUSCHILD A, et al. Orbit and Clock Analysis of Compass GEO and IGSO Satellites[J]. Journal of Geodesy, 2013, 87(6):515-525.
[21] LOU Yidong, LIU Yang,SHI Chuang, et al. Precise Orbit Determination of BeiDou Constellation Based on BETS and MGEX Network[J]. Scientific Reports, 2014, 4:4692.
[22] ZHAO Qile, GUO Jing, LI Min, et al. Initial Results of Precise Orbit and Clock Determination for COMPASS Navigation Satellite System[J]. Journal of Geodesy, 2013, 87(5):475-486.
[23] LOU Yidong, LIU Yang, SHI Chuang, et al. Precise Orbit Determination of BeiDou Constellation:Method Comparison[J]. GPS Solutions, 2016, 20(2):259-268.
[24] PEARLMAN M R, DEGNAN J J, BOSWORTH J M. The International Laser Ranging Service[J]. Advances in Space Research, 2002, 30(2):135-143.
[25] DENG Zhiguo, GE Maorong, UHLEMANN M, et al. Precise Orbit Determination of BeiDou Satellites at GFZ[C]//EGU General Assembly Conference Abstracts. Vienna:EGU, 2014.
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