深空探测器精密定轨与重力场解算系统(WUDOGS)及其应用分析

doi:10.11947/j.AGCS.2017.20160525

测绘学报 ›› 2017, Vol. 46 ›› Issue (3): 288-296.doi: 10.11947/j.AGCS.2017.20160525

深空探测器精密定轨与重力场解算系统(WUDOGS)及其应用分析

叶茂¹, 李斐^1,2, 鄢建国¹, 郝卫峰², 杨轩¹, 金炜桐¹, 曲春凯²

1. 武汉大学测绘遥感信息工程国家重点实验室, 湖北武汉 430079;
2. 武汉大学中国南极测绘研究中心, 湖北武汉 430079

收稿日期:2016-11-14 修回日期:2017-01-04 出版日期:2017-03-20 发布日期:2017-04-11
通讯作者: 李斐 E-mail:fli@whu.edu.cn
作者简介:叶茂(1989-),男,博士后,研究方向为行星探测器精密定轨,重力场及软件解算系统。E-mail:mye@whu.edu.cn
基金资助:
国家自然科学基金（41374024；41604004；41174019）；湖北省自然科学基金重点项目创新群体类项目（2015CFA011）；中国博士后科学基金（2016M602360）

Wuhan University Deep-space Orbit Determination and Gravity Recovery System(WUDOGS) and Its Application Analysis

YE Mao¹, LI Fei^1,2, YAN Jianguo¹, HAO Weifeng², YANG Xuan¹, JIN Weitong¹, QU Chunkai²

1. State Key Laboratory of Information Engineering in Surveying, Mapping and Remote Sensing, Wuhan University, Wuhan 430079, China;
2. Chinese Antarctic Center of Surveying and Mapping, Wuhan University, Wuhan 430079, China

Received:2016-11-14 Revised:2017-01-04 Online:2017-03-20 Published:2017-04-11
Supported by:
The National Natural Science Foundation of China(Nos. 41374024;41604004;41174019),The Hubei Province Natural Science Foundation Innovation Group Project(No. 2015CFA011);The China Postdoctoral Science Foundation(No. 2016M602360)

摘要/Abstract

摘要： WUDOGS是武汉大学自主研发的深空探测器精密定轨与重力场解算软件系统。该软件目前已经具备月球、火星探测器的高精度定轨能力。本文首先简要介绍了WUDOGS设计思路及其主要功能，然后重点介绍了WUDOGS与国际上领先水平的行星探测器精密定轨软件系统GEODYN-Ⅱ的交叉验证测试过程。结果表明：对于探测器的轨道预报，WUDOGS与GEODYN-Ⅱ的1个月位置差异小于0.3mm，2d位置差值小于5×10^-3mm；双程测距、双程测速的理论计算值和GEODYN-Ⅱ的差值分别在0.06mm、0.002mm/s的水平；对月球探测器“嫦娥一号”的精密定轨显示WUDOGS和GEODYN-Ⅱ符合在2cm水平，对火星探测器MEX的精密定轨显示WUDOGS和欧空局精密轨道符合在25m水平。该软件目前的研发情况及其与国外研究水平的对比表明WUDOGS具有良好的应用前景，对满足我国后续深空探测发展的需求以及深空探测器精密定轨软件的研发具有重要意义。

关键词: 深空探测, 精密定轨, 行星重力场, WUDOGS

Abstract: WUDOGS(Wuhan University deep-space orbit determination and gravity recovery system) is a software system designed for deep spacecraft precise orbit determination and planetary gravity recovery, developed independently at Wuhan University. WUDOGS now has the function for Lunar and Mars spacecraft precision orbit determination. Its design pattern and main function are briefly introduced. The cross verification test(CVT) between WUDOGS and state of the art planetary precise orbit determination software GEODYN-Ⅱ are elaborated. The results show that:①for orbit propagation, with all the same forces and other configuration, the predicted orbit difference in R,T,N directions are less than 0.3 mm for one month arc, 5×10^-3 mm for 2 days arc, compared with GEODYN-Ⅱ;②the difference RMS of computed values of observables for two-way range and two-way range rate is at levels of 0.06 mm and 0.002 mm/s respectively;③for Chinese Chang'E-1 POD, the reconstructed orbit difference between WUDOGS and GEODYN-Ⅱ is at 2 cm level, for ESA MEX POD, the reconstructed orbit difference between WUDOGS and ESA is at 25 m level. Current developing situation of WUDOGS and comparison with international research level show that WUDOGS has a good application prospect, which will be important for meeting the demand of Chinese future planetary exploration and the development of deep space spacecraft POD software.

Key words: deep-space exploration, precise orbit prediction, planet gravity field, WUDOGS

中图分类号:

P228

叶茂, 李斐, 鄢建国, 郝卫峰, 杨轩, 金炜桐, 曲春凯. 深空探测器精密定轨与重力场解算系统(WUDOGS)及其应用分析[J]. 测绘学报, 2017, 46(3): 288-296.

YE Mao, LI Fei, YAN Jianguo, HAO Weifeng, YANG Xuan, JIN Weitong, QU Chunkai. Wuhan University Deep-space Orbit Determination and Gravity Recovery System(WUDOGS) and Its Application Analysis[J]. Acta Geodaetica et Cartographica Sinica, 2017, 46(3): 288-296.

参考文献

[1] 中国科学院月球与深空探测总体部. 月球与深空探测[M]. 广州:广东科技出版, 2014. Department of Lunar and Deep Space Exploration, CAS. Lunar and Deep Space Exploration[M]. Guangzhou:Guangdong Science and Technology Press, 2014.
[2] 欧阳自远, 李春来. 绕月探测工程科学目标专题研究[M]. 北京:科学出版社, 2015. OUYANG Ziyuan, LI Chunlai. Monographic Study on Scientific Objectives of Lunar Explorer Project[M]. Beijing:Science Press, 2015.
[3] 欧阳自远, 李春来. 绕月探测工程月球科学与探测技术研究[M]. 北京:科学出版社, 2015. OUYANG Ziyuan, LI Chunlai. Research on Lunar Science and Exploration Technology in Lunar Explorer Project[M]. Beijing:Science Press, 2015.
[4] 赵齐乐. GPS导航星座及低轨卫星的精密定轨理论和软件研究[D]. 武汉:武汉大学, 2004. ZHAO Qile. Research on Precise Orbit Determination Theory and Software of GPS Navigation Constellation and LEO Satellite[D]. Wuhan:Wuhan University, 2004.
[5] 魏子卿, 阮仁桂, 贾小林, 等. 卫星定位定轨系统SPODS:理论与测试[J]. 测绘学报, 2014, 43(1):1-4. DOI:10.13485/j.cnki.11-2089.2014.0001. WEI Ziqing, RUAN Rengui, JIA Xiaolin, et al. Satellite Positioning and Orbit Determination System SPODS:Theory and Test[J]. Acta Geodaetica et Cartographica Sinica, 2014, 43(1):1-4. DOI:10.13485/j.cnki.11-2089.2014.0001.
[6] 胡松杰, 唐歌实. 北京中心深空探测器精密定轨与分析软件系统[J]. 飞行器测控学报, 2010, 29(5):69-74. HU Songjie, TANG Geshi. BACC Orbit Determination and Analysis Software for Deep-space Explorers[J]. Journal of Spacecraft TT & C Technology, 2010, 29(5):69-74.
[7] MOYER T D. Mathematical Formulation of the Double Precision Orbit Determination Program (DPODP)[R]. JPL-TR 32-1527. Pasadena, CA:Jet Propulsion Lab, 1971.
[8] MOYER T D. Formulation for Observed and Computed Values of Deep Space Network Data Types for Navigation[M]. Hoboken:John Wiley & Sons, 2003.
[9] EVANS S, TABER W, DRAIN T, et al. Monte:The Next Generation of Mission Design & Navigation Software[C]//Proceedings of the 6th International Conference on Astrodynamics Tools and Techniques (ICATT). Darmstadt, Germany:[s.n.], 2016.
[10] PAVLIS D E, WIMERT J, MCCARTHY J J. GEODYN Ⅱ System Description[R]. Greenbelt, MD:SGT Inc, 2013:1-5.
[11] MEYER U, CHARLOT P, BIANCALE R. GINS:A New Multi-technique Software for VLBI Analysis[C]//International VLBI Service for Geodesy and Astrometry 2000 General Meeting Proceedings.[S.l.]:NASA, 2000(1):324-328.
[12] BUDNIK F, MACKENZIE R. Orbit Determination Software at ESOC Flight Dynamics[C]//MORE Relativity Meeting. Rome, Italy:[s.n.], 2009.
[13] MACKENZIE R, BUDNIK F. Orbit Determination Software Design at ESOC[C]//MORE Relativity Meeting. Rome, Italy:[s.n.], 2009.
[14] ANDERT T P. Masses of Small Bodies:Mass Estimation of Small Solar System Bodies Using Radio Science Data from Close Flybys[D]. Köln:Universität zu Köln, 2010.
[15] ANDERT T P, ROSENBLATT P, PÄTZOLD M, et al. Precise Mass Determination and the Nature of Phobos[J]. Geophysical Research Letters, 2010, 37(9):L09202.
[16] CICALÒ S, SCHETTINO G, DI RUZZA S, et al. The BepiColombo MORE Gravimetry and Rotation Experiments with the Orbit14 Software[J]. Monthly Notices of the Royal Astronomical Society, 2016, 457(2):1507-1521.
[17] TOMMEI G, MILANI A, VOKROUHLICKY D. Light-time Computations for the BepiColombo Radio Science Experiment[J]. Celestial Mechanics and Dynamical Astronomy, 2010, 107(1-2):285-298.
[18] BERTONE S, ARNOLD D, JÄGGI A, et al. GRAIL Gravity Field Determination Using the Celestial Mechanics Approach-status Report[C]//AGU Fall Meeting Abstracts.[S.l.]:AGU, 2014.
[19] ARNOLD D, BERTONE S, JÄGGI A, et al. GRAIL Gravity Field Determination Using the Celestial Mechanics Approach[J]. Icarus, 2015, 261:182-192.
[20] 曹建峰, 刘磊, 刘勇, 等. 嫦娥二号再拓展试验测定轨精度研究[J]. 飞行器测控学报, 2012, 31(4):84-89. CAO Jianfeng, LIU Lei, LIU Yong, et al. Orbit Determination Analysis for CE-2 Second Extended Mission[J]. Journal of Spacecraft TT & C Technology, 2012, 31(4):84-89.
[21] 曹建峰, 张宇, 胡松杰, 等. 嫦娥三号着陆器精确定位与精度分析[J]. 武汉大学学报(信息科学版), 2016, 41(2):274-278. CAO Jianfeng, ZHANG Yu, HU Songjie, et al. An Analysis of Precise Positioning and Accuracy of the CE-3 Lunar Lander Soft Landing[J]. Geomatics and Information Science of Wuhan University, 2016, 41(2):274-278.
[22] 黄勇, 胡小工, 曹建峰, 等. 上海天文台火星卫星定轨软件系统[J]. 飞行器测控学报, 2009, 28(6):83-89. HUANG Yong, HU Xiaogong, CAO Jianfeng, et al. The Mars Satellite Orbit Determination Software at Shanghai Astronomical Observatory[J]. Journal of Spacecraft TT & C Technology, 2009, 28(6):83-89.
[23] 黄勇, 昌胜骐, 李培佳, 等. "嫦娥三号"月球探测器的轨道确定和月面定位[J]. 科学通报, 2014, 59(23):2268-2277. HUANG Yong, CHANG Shengqi, LI Peijia, et al. Orbit Determination of Chang'E-3 and Positioning of the Lander and the Rover[J]. Chinese Science Bulletin, 2014, 59(23):2268-2277.
[24] 李培佳. 我国月球探测工程中的定轨和定位[D]. 上海:中国科学院上海天文台,2013. LI Peijia. Researches on the Orbit Determination and Positioning of the Chinese Lunar Exploration Program[D]. Shanghai:Shanghai Astronomical Observatory,Chinese Academy of Sciences,2013.
[25] 李斐, 鄢建国. 月球重力场的确定及构建我国自主月球重力场模型的方案研究[J]. 武汉大学学报(信息科学版), 2007, 32(1):6-10. LI Fei, YAN Jianguo. Principle and Method of Lunar Gravity Field Determination and Project on Self-determinational Lunar Gravity Field[J]. Geomatics and Information Science of Wuhan University, 2007, 32(1):6-10.
[26] 李斐, 郝卫峰, 鄢建国, 等. 空间跟踪技术的发展对月球重力场模型的改进[J]. 地球物理学报, 2016, 59(4):1249-1259. LI Fei, HAO Weifeng, YAN Jianguo, et al. Advancement of Lunar Gravity Model due to the Development of Space Tracking Techniques[J]. Chinese Journal of Geophysics, 2016, 59(4):1249-1259.
[27] 鄢建国, 李斐, 平劲松, 等. 利用LP多普勒数据解算月球重力场模型的分析[J]. 测绘学报, 2009, 38(1):6-11. YAN Jianguo, LI Fei, PING Jinsong, et al. Lunar Gravity Field Recovery Based on LP Doppler Data[J]. Acta Geodaetica et Cartographica Sinica, 2009, 38(1):6-11.
[28] 鄢建国, 李斐, 平劲松. 基于MGS测图段部分弧段的精密定轨及火星重力场模型解算[J]. 测绘学报, 2010, 39(5):484-490. YAN Jianguo, LI Fei, PING Jinsong. Precision Orbit Determination of MGS Mapping Phase Arcs and Martian Gravity Field Model Solution[J]. Acta Geodaetica et Cartographica Sinica, 2010, 39(5):484-490.
[29] 叶茂. 月球探测器精密定轨软件研制与四程中继跟踪测量模式研究[J]. 测绘学报, 2016, 45(9):1132. DOI:10.11947/j.AGCS.2016.20160339. YE Mao. Development of Lunar Spacecraft Precision Orbit Determination Software System and Research on a Four-way Relay Tracking Measurement Mode[J]. Acta Geodaetica et Cartographica Sinica, 2016, 45(9):1132. DOI:10.11947/j.AGCS.2016.20160339.
[30] LI Fei, YE Mao, YAN Jianguo, et al. A Simulation of the Four-way Lunar Lander-orbiter Tracking Mode for the Chang'E-5 Mission[J]. Advances in Space Research, 2016, 57(11):2376-2384.
[31] YE Mao, YAN Jianguo, LI Fei, et al. Preliminary Results of LUGREAS and Its CVT with GEODYN-Ⅱ[C]//International Symposium on Lunar and Planetary Science. Wuhan:ISLPS, 2016.
[32] BUDNIK F, MORLEY T A, MACKENZIE R A. ESOC's System for Interplanetary Orbit Determination:Implementation and Operational Experience[C]//Proceedings of the 18th International Symposium on Space Flight Dynamics. Munich, Germany:[s.n.], 2004, 548:387.
[33] 叶茂, 肖驰, 李斐, 等. 三种关于引力位及其一、二阶导数计算方法的比较与分析研究[J]. 地球物理学进展, 2015, 30(6):2581-2588. YE Mao, XIAO Chi, LI Fei, et al. Analysis and Comparison of Three Different Calculational Methods for Gravitational Potential and Its Derivatives[J]. Progress in Geophysics, 2015, 30(6):2581-2588.
[34] LEMOINE F G, GOOSSENS S, SABAKA T J, et al. High-degree Gravity Models from GRAIL Primary Mission Data[J]. Journal of Geophysical Research:Planets, 2013, 118(8):1676-1698.
[35] 叶茂, 李斐, 鄢建国, 等. GRAIL月球重力场模型定轨性能分析[J]. 武汉大学学报(信息科学版), 2016, 41(1):93-99. YE Mao, LI Fei, YAN Jianguo, et al. Orbit Determination Ability Analysis of the GRAIL Gravity Model[J]. Geomatics and Information Science of Wuhan University, 2016, 41(1):93-99.
[36] ROSENBLATT P, LAINEY V, LE MAISTRE S, et al. Accurate Mars Express Orbits to Improve the Determination of the Mass and Ephemeris of the Martian Moons[J]. Planetary and Space Science, 2008, 56(7):1043-1053.

深空探测器精密定轨与重力场解算系统(WUDOGS)及其应用分析

Wuhan University Deep-space Orbit Determination and Gravity Recovery System(WUDOGS) and Its Application Analysis

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