姿态模式切换期间QZSS卫星轨道及其钟差产品特性分析

doi:10.11947/j.AGCS.2016.20150386

测绘学报 ›› 2016, Vol. 45 ›› Issue (3): 274-281.doi: 10.11947/j.AGCS.2016.20150386

姿态模式切换期间QZSS卫星轨道及其钟差产品特性分析

周佩元, 杜兰, 方善传, 路余, 张中凯, 李夫鹏

信息工程大学导航与空天目标工程学院, 河南郑州 450001

收稿日期:2015-07-21 修回日期:2015-11-03 出版日期:2016-03-20 发布日期:2016-03-25
通讯作者: 杜兰,E-mail:lan.du09@gmail.com E-mail:lan.du09@gmail.com
作者简介:周佩元(1991-),男,硕士生,研究方向为轨道力学与卫星导航。
基金资助:
国家自然科学基金(41174025;41174026;41174027)

Analysis of Characteristics of QZSS Satellite Orbit and Clock Products during Yaw Attitude Model Switching

ZHOU Peiyuan, DU Lan, FANG Shanchuan, LU Yu, ZHANG Zhongkai, LI Fupeng

School of Navigation and Aerospace Engineering, Information Engineering University, Zhengzhou 450001, China

Received:2015-07-21 Revised:2015-11-03 Online:2016-03-20 Published:2016-03-25
Supported by:
The National Natural Science Foundation of China(Nos.41174025;41174026;41174027)

摘要/Abstract

摘要： 导航卫星姿态控制模式切换对精密定轨解算得到的轨道和钟差均有较大影响。本文首先从理论上分析了卫星偏航姿态及其对精密定轨的影响,然后分别以卫星激光测距检核和钟差多项式拟合的方法对IGS MGEX分析中心的QZSS卫星轨道和钟差产品精度进行评价,最后以谱分析方法和改进阿伦方差揭示了卫星钟差的周期特性。基于2014年全年的QZSS卫星轨道和钟差产品的研究表明,一年内有两次长约20 d的地影季,太阳角呈现半年周期的波动;QZSS卫星在低太阳角时有零偏保护,其卫星轨道和钟差精度都与太阳角有显著相关性;卫星钟差具有与轨道周期相近的周期项,且周期项振幅与太阳角的大小也具有相关性,表明现有的定轨策略存在不足。考虑到QZSS与目前北斗星座中IGSO和MEO卫星姿态控制模式的相似性,该结论对于研究我国BDS姿态切换期间的精密定轨有一定参考价值。

关键词: 准天顶星系统, 姿态误差, 精密定轨, 地影季, 卫星激光测距

Abstract: Yaw attitude model switching of navigation satellites have great impact on its orbit and clock products derived from precise orbit determination. Firstly, the yaw attitude and solar radiation model of QZSS is given briefly. Then, using QZSS precise orbit and clock products provided by IGS MGEX analysis center, precision of orbit and clock is analyzed by satellite laser ranging residuals and polynomial fit residuals respectively. Finally, spectral analysis and modified Allan variance is carried out on clock products to reveal its periodic variations. Research on QZSS satellite orbit and clock products of 2014 shows that there are two eclipse seasons of 20 days and the beta angle is fluctuating with a period of half-year. And there is significant correlation between the precision of orbit and clock products and beta angle. Moreover, the satellite clock offset has periodic variations similar to orbit periods and its amplitude is changing with the beta angle which indicates problems of current orbit determination strategies. In view of similarities between QZSS and BeiDou IGSO and MEO satellites in yaw attitude model, the conclusion is beneficial to improve BeiDou precise orbit determination.

Key words: quasi-zenith satellite system(QZSS), yaw attitude error, precise orbit determination, eclipse seasons, satellite laser ranging(SLR)

中图分类号:

P228

周佩元, 杜兰, 方善传, 路余, 张中凯, 李夫鹏. 姿态模式切换期间QZSS卫星轨道及其钟差产品特性分析[J]. 测绘学报, 2016, 45(3): 274-281.

ZHOU Peiyuan, DU Lan, FANG Shanchuan, LU Yu, ZHANG Zhongkai, LI Fupeng. Analysis of Characteristics of QZSS Satellite Orbit and Clock Products during Yaw Attitude Model Switching[J]. Acta Geodaetica et Cartographica Sinica, 2016, 45(3): 274-281.

参考文献

[1] KISHIMOTO M, HASE H, MATSUMOTO A, et al. QZSS System Design and Its Performance[C]//Proceedings of the 2007 National Technical Meeting of the Institute of Navigation. San Diego, California:NTM, 2007:405-410.
[2] SAWAMURA T, TAKAHASHI T, MORIGUCHI T, et al. Performance of QZSS(Quasi-zenith Satellite System) & L-band Navigation Payload[C]//Proceedings of the 2012 International Technical Meeting of the Institute of Navigation. Newport Beach, CA:[s.n.], 2012:1228-1254.
[3] 孙宏伟, 李玉莉, 袁海波. 日本准天顶卫星系统概要[J]. 武汉大学学报(信息科学版), 2010, 35(8):1004-1007. SUN Hongwei, LI Yuli, YUAN Haibo. Outline of the Quasi-zenith Satellite System of Japan[J]. Geomatics and Information Science of Wuhan University, 2010, 35(8):1004-1007.
[4] 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.
[5] GUO Jing, ZHAO Qile, GENG Tao, et al. Precise Orbit Determination for COMPASS IGSO Satellites during Yaw Maneuvers[C]//China Satellite Navigation Conference(CSNC) 2013 Proceedings. Berlin:Springer, 2013:41-53.
[6] HAUSCHILD A, STEIGENBERGER P, RODRIGUEZ-SOLANO C. Signal, Orbit and Attitude Analysis of Japan's First QZSS Satellite Michibiki[J]. GPS Solutions, 2012, 16(1):127-133.
[7] HAUSCHILD A, STEIGENBERGER P, RODRIGUEZ-SOLANO C. QZS-1 Yaw Attitude Estimation Based on Measurements from the CONGO Network[J]. Navigation, 2012, 59(3):237-248.
[8] 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.
[9] 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.
[10] BAR-SEVER Y E. A New Model for GPS Yaw Attitude[J]. Journal of Geodesy, 1996, 70(11):714-723.
[11] KOUBA J. A Simplified Yaw-attitude Model for Eclipsing GPS Satellites[J]. GPS Solutions, 2009, 13(1):1-12.
[12] 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.
[13] 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.
[14] 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.
[15] 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 Satellite[J]. Acta Geodaetica et Cartographica Sinica, 2014, 43(4):353-359. DOI:10.13485/j.cnki.11-2089.2014.0053.
[16] ARNOLD D, MEINDL M, BEUTLER G, et al. CODE's New Solar Radiation Pressure Model for GNSS Orbit Determination[J]. Journal of Geodesy, 2015, 89(8):775-791.
[17] PEARLMAN M R, DEGNAN J J, BOSWORTH J M. The International Laser Ranging Service[J]. Advances in Space Research, 2002, 30(2):135-143.
[18] 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.
[19] SENIOR K L, RAY J R, BEARD R L. Characterization of Periodic Variations in the GPS Satellite Clocks[J]. GPS Solutions, 2008, 12(3):211-225.
[20] 郭海荣. 导航卫星原子钟时频特性分析理论与方法研究[D]. 郑州:信息工程大学, 2006. GUO Hairong. Study on the Analysis Theories and Algorithms of the Time and Frequency Characterization for Atomic Clocks of Navigation Satellites[D]. Zhengzhou:The PLA Information Engineering University, 2006.
[21] 黄观文, 张勤, 许国昌, 等. 基于频谱分析的IGS精密星历卫星钟差精度分析研究[J]. 武汉大学学报(信息科学版), 2008, 33(5):496-499. HUANG Guanwen, ZHANG Qin, XU Guochang, et al. IGS Precise Satellite Clock Model Fitting and Its Precision by Using Spectral Analysis Method[J]. Geomatics and Information Science of Wuhan University, 2008, 33(5):496-499.
[22] 赵群河, 王小亚, 何冰, 等. 卫星激光反射器质心改正的概率模型[J]. 测绘学报, 2015, 44(4):370-376. DOI:10.11947/j.AGCS.2015.20130338. ZHAO Qunhe,WANG Xiaoya,HE Bing, et al. Probability Model of Center-of-mass Calibration of Satellites' Retro-reflectors Used for Laser Ranging[J]. Acta Geodaetica et Cartographica Sinica, 2015, 44(4):370-376. DOI:10.11947/j.AGCS.2015.20130338.
[23] RILEY W J. User Manual:Stable32 Frequency Stability Analysis Version 1.5.0[M].Beaufort, SC:Hamilton Technical Services, 2007.

姿态模式切换期间QZSS卫星轨道及其钟差产品特性分析

Analysis of Characteristics of QZSS Satellite Orbit and Clock Products during Yaw Attitude Model Switching

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