Satellite Shadow Modeling and Algorithm of Satellite Shadow Parameters for GNSS

  • DU Lan ,
  • ZHOU Peiyuan ,
  • FANG Shanchuan ,
  • LIU Zejun ,
  • GUO Rui
Expand
  • 1. College of Navigation & Aerospace Engineering, Information Engineering University, Zhengzhou 450001, China;
    2. Beijing Global Information Application and Development Center, Beijing 100094, China

Received date: 2016-03-01

  Revised date: 2016-09-02

  Online published: 2016-12-03

Supported by

The National Natural Science Foundation of China (Nos. 41174025, 41174026, 41204022, 41374042)

Abstract

The satellite shadow parameters can be numerically calculated with high accuracy from the positions of the sun, the earth and the specific satellite. Unfortunately, it is difficult for the numerical calculation to give a general profile of the variations and distributions of these parameters for some certain types of orbital spacecraft. A satellite shadow model was presented based on the spatial view at the altitude of the satellite and the correlative geometry amongst the sun, the earth and the satellite. Firstly, the size and location of the satellite shadow were determined by the semi-major axis of the satellite orbit and the annual motion of the apparent sun, respectively. Secondly, the computing formulae of the satellite shadow parameters were derived, together with the correction formulae for the long-term prediction of the parameters due to oblateness perturbation, etc. Examinations on the three types of orbits for the BeiDou navigation constellation show that the proposed satellite shadow model and its shadow parameters computing formulae can provide a prompt profile of the eclipse parameters for the medium-high altitude circular orbit satellites.

Cite this article

DU Lan , ZHOU Peiyuan , FANG Shanchuan , LIU Zejun , GUO Rui . Satellite Shadow Modeling and Algorithm of Satellite Shadow Parameters for GNSS[J]. Acta Geodaetica et Cartographica Sinica, 2016 , 45(11) : 1270 -1277 . DOI: 10.11947/j.AGCS.2016.20160063

References

[1] 毛悦, 宋小勇, 贾小林, 等. 北斗导航卫星地影状态分析[J]. 测绘学报, 2014, 43(4): 353-359. DOI: 10.13485/j.cnki.11-2089.2014.0053. MAO Yue, SONG Xiaoyong, JIA Xiaolin, et al. Earth Eclipse Status Analysis of BeiDou Navigation Satellites[J]. Acta Geodaetica et Cartographica Sinica, 2014, 43(4): 353-359. DOI: 10.13485/j.cnki.11-2089.2014.0053.
[2] HUBAUX C, LEMAITRE A, DELSATE N, et al. Symplectic Integration of Space Debris Motion Considering Several Earth's Shadowing Models[J]. Advances in Space Research, 2012, 49(10): 1472-1486.
[3] 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.
[4] GUO Jing, ZHAO Qile, GENG Tao, et al. Precise Orbit Determination for COMPASS IGSO Satellites during Yaw Maneuvers[M]//SUN Jiadong, JIAO Wenhai, WU Haitao, et al. China Satellite Navigation Conference (CSNC) 2013 Proceedings. Berlin Heidelberg: Springer, 2013: 41-53.
[5] 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.
[6] 毛悦, 宋小勇, 王维, 等. IGSO姿态控制模式切换期间定轨策略研究[J]. 武汉大学学报(信息科学版), 2014, 39(11): 1352-1356. MAO Yue, SONG Xiaoyong, WANG Wei, et al. IGSO Satellite Orbit Determining Strategy Analysis with the Yaw-steering and Orbit Normal Attitude Control Mode Switching[J]. Geomatics and Information Science of Wuhan University, 2014, 39(11): 1352-1356.
[7] 陈刘成. 地影模型对导航卫星轨道数值积分的影响及改进[J]. 武汉大学学报(信息科学版), 2007, 32(5): 450-453. CHEN Liucheng. How Navigation Satellite Orbit Numerical Integration Affected by Shadow Model and Its Correcting Methods[J]. Geomatics and Information Science of Wuhan University, 2007, 32(5): 450-453.
[8] 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.
[9] STEIGENBERGER P, HAUSCHILD A, MONTENBRUCK O, et al. Orbit and Clock Determination of QZS-1 Based on the CONGO Network[J]. Navigation, 2013, 60(1): 31-40.
[10] 彭汉兵, 杨元喜, 王刚, 等. 星蚀期北斗卫星轨道性能分析——SLR检核结果[J]. 测绘学报, 2016, 45(6): 639-645. DOI: 10.11947/j.AGCS.2016.20150637. PENG Hanbing, YANG Yuanxi, WANG Gang, et al. 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.
[11] 郑军, 陈宏, 李于衡. GEO卫星能源分系统状态切换时间精确预报算法[J]. 上海航天, 2011, 28(5): 30-33. ZHENG Jun, CHEN Hong, LI Yuheng. Algorithm Analysis on Energy System State Switch Time Accurate Prediction in GEO Satellite Eclipse[J]. Aerospace Shanghai, 2011, 28(5): 30-33.
[12] LONGO C R O, RICKMAN S L. Method for the Calculation of Spacecraft Umbra and Penumbra Shadow Terminator Points[R]. NASA Technical Paper 3547, 1995.
[13] MONTENBRUCK O, GILL E. Satellite Orbits: Models, Methods and Applications[M]. Berlin Heidelberg: Springer-Verlag, 2000.
[14] BROUWER D, CLEMENCE G M. Methods of Celestial Mechanics[M]. London: Academic Press, 1961.
[15] HUBAUX C, LIBERT A S, DELSATE N, et al. Influence of Earth's Shadowing Effects on Space Debris Stability[J]. Advances in Space Research, 2013, 51(1): 25-38.
[16] 苏宜. 天文学新概论[M]. 4版. 北京: 科学出版社, 2009. SU Yi. A Brief Introduction of Astronomy[M]. 4th ed. Beijing: Science Press, 2009.
[17] 郑军, 鲍明涛, 王鑫, 等. 升交点赤经与轨道倾角对地球同步卫星地影的影响[J]. 上海航天, 2005, 22(3): 34-36, 60. ZHENG Jun, BAO Mingtao, WANG Xin, et al. Affection of Longitude Ascending Node and Orbit Inclination on the Eclipse for Geosynchronous Satellite[J]. Aerospace Shanghai, 2005, 22(3): 34-36, 60.
[18] BAR-SEVER Y E. A New Model for GPS Yaw Attitude[J]. Journal of Geodesy, 1996, 70(11): 714-723.
[19] KOUBA J. A Simplified Yaw-attitude Model for Eclipsing GPS Satellites[J]. GPS Solutions, 2009, 13(1): 1-12.
[20] MULLINS L D. Calculating Satellite Umbra/Penumbra Entry and Exit Positions and Times[J]. Journal of the Astronautical Sciences, 1991, 39: 411-422.
[21] 张世杰, 曹喜滨. 卫星进/出地影位置和时间的计算算法[J]. 上海航天, 2001, 18(6): 9-22. ZHANG Shijie, CAO Xibin. Calculating Method of Satellite Entry and Exit Positions and Times through Umbra/Penumbra[J]. Aerospace Shanghai, 2001, 18(6): 9-22.
Outlines

/