资源三号01星及02星星载GPS天线PCO、PCV在轨估计及对精密定轨的影响

doi:10.11947/j.AGCS.2018.20170703

摘要/Abstract

摘要： 资源三号01星与02星作为我国重要的遥感立体测绘卫星，承担了地理产品生产以及国土资源调查等任务。其中，高精度的卫星轨道确定是完成卫星任务的必备条件。资源三号01星与02星都搭载国产双频GPS接收机和SLR反射器来进行精密定轨和独立定轨精度检核。在定轨过程中，星载GPS接收机天线的PCO误差和PCV误差是制约进一步提高定轨精度的重要因素。尽管卫星入轨前获取GPS接收机天线的PCO先验值，本文通过在轨估计PCO，分析了PCO各个方向上的分量估计的可行性，发现通过使用在轨PCO，SLR检核显示ZY-3 01星和ZY-3 02星轨道RMS值分别提高了0.331 mm、0.399 mm。本文利用直接法和残差法估计了两颗卫星星载GPS接收机天线的PCV模型，整体量级在[-15 mm 15 mm]。通过使用在轨估计的PCV模型（10°×10°），ZY-3 01星SLR检核结果RMS值提高了2.143 mm（直接法模型）、1.628 mm（残差法模型），重叠弧段对比在三维位置上提高了11.377 mm（直接法模型）、13.903 mm（残差法模型），ZY-3 02星SLR检核结果RMS值提高了0.727 mm（直接法模型）、0.692 mm（残差法模型），重叠弧段对比在三维位置上提高了1.736 mm（直接法模型）、1.548 mm（残差法模型）。本文进一步探讨了PCV模型分辨率（10°×10°，5°×5°，2°×2°）对精密定轨的影响，在综合考虑计算效率、存储空间、提高幅度等因素后，发现使用残差法在轨估计5°×5° PCV模型是较好的选择。

关键词: 资源三号卫星, 精密定轨, 天线相位中心偏差, 天线相位中心变化, 精度影响

Abstract: ZY-3 01 and ZY-3 02 satellites, as important remote sensing stereoscopic mapping satellites in China, undertake the tasks of production of geographic products, land resource investigation and so on. Precision orbit determination(POD) is a prerequisite for the success of ZY-3 01 and ZY-3 02 missions. Dual-frequency GPS receiver and SLR reflector manufactured by China play significant roles in POD and independent orbits checkout. Although PCO priori values were obtained before satellites launched,by PCO estimation in-flight, this paper analyses the feasibility of PCO in different directions and finds ZY-3 01 and ZY-3 02 SLR RMS checkouts are improved 0.331 mm,0.399 mm respectively. Further, this paper estimates PCV models of ZY-3 01 and ZY-3 02 spaceborne GPS antennas using direct approach and residual approach and their PCV models can reach[-15 mm 15 mm]. Through the use of PCV models(10°×10°), ZY-3 01 orbits SLR checkouts are improved 2.143 mm (direct approach), 1.628 mm (residual approach), orbit accuracy in 3D of overlapping arcs are improved 11.377 mm (direct approach),13.903 mm (residual approach), ZY-3 02 orbits SLR checkouts are improved 0.727 mm (direct approach),0.692 mm (residual approach), orbit accuracy in 3D of overlapping arcs are improved 1.736 mm (direct approach),1.548 mm(residual approach).The effect of PCV model resolution (10°×10°,5°×5°,2°×2°) on POD is further discussed in this paper. After comprehensive consideration of computational efficiency, storage space, increase amplitude and other factors, 5°×5° PCV model by residual approach is the best choice.

Key words: ZY-3 satellites, precision orbit determination, antenna phase center offset, antenna phase center variation, precision influence

中图分类号:

P228

袁俊军, 赵春梅, 吴琼宝. 资源三号01星及02星星载GPS天线PCO、PCV在轨估计及对精密定轨的影响[J]. 测绘学报, 2018, 47(5): 672-682.

YUAN Junjun, ZHAO Chunmei, WU Qiongbao. Phase Center Offset and Phase Center Variation Estimation In-flight for ZY-3 01 and ZY-3 02 Spaceborne GPS Antennas and the Influence on Precision Orbit Determination[J]. Acta Geodaetica et Cartographica Sinica, 2018, 47(5): 672-682.

参考文献

[1] 李德仁. 我国第一颗民用三线阵立体测图卫星——资源三号测绘卫星[J]. 测绘学报, 2012, 41(3):317-322. LI Deren. China's First Civilian Three-line-array Stereo Mapping Satellite:ZY-3[J]. Acta Geodaetica et Cartographica Sinica, 2012, 41(3):317-322.
[2] 唐新明, 王鸿燕, 祝小勇. 资源三号卫星测绘技术与应用[J]. 测绘学报, 2017, 46(10):1482-1491. DOI:10.11947/j.AGCS.2017.20170251. TANG Xinming, WANG Hongyan, ZHU Xiaoyong. Technology and Applications of Surveying and Mapping for ZY-3 Satellites[J]. Acta Geodaetica et Cartographica Sinica, 2017, 46(10):1482-1491. DOI:10.11947/j.AGCS.2017.20170251.
[3] 李德仁, 王密. "资源三号"卫星在轨几何定标及精度评估[J]. 航天返回与遥感, 2012, 33(3):1-6. LI Deren, WANG Mi. On-orbit Geometric Calibration and Accuracy Assessment of ZY-3[J]. Spacecraft Recovery & Remote Sensing, 2012, 33(3):1-6.
[4] 王密, 杨博, 李德仁, 等. 资源三号全国无控制整体区域网平差关键技术及应用[J]. 武汉大学学报(信息科学版), 2017, 42(4):427-433. WANG Mi, YANG Bo, LI Deren, et al. Technologies and Applications of Block Adjustment without Control for ZY-3 Images Covering China[J]. Geomatics and Information Science of Wuhan University, 2017, 42(4):427-433.
[5] 赵春梅, 唐新明. 基于星载GPS的资源三号卫星精密定轨[J]. 宇航学报, 2013, 34(9):1202-1206. ZHAO Chunmei, TANG Xinming. Precise Orbit Determination for the ZY-3 Satellite Mission Using GPS Receiver[J]. Journal of Astronautics, 2013, 34(9):1202-1206.
[6] YUNCK T P, BERTIGER W I, WU S C, et al. First Assessment of GPS-based Reduced Dynamic Orbit Determination on TOPEX/Poseidon[J]. Geophysical Research Letters, 1994, 21(7):541-544.
[7] TAPLEY B D, BETTADPUR S, WATKINS M, et al. The Gravity Recovery and Climate Experiment:Mission Overview and Early Results[J]. Geophysical Research Letters, 2004, 31(9):L09607.
[8] REIGBER C, LVHR H, SCHWINTZER P. CHAMP Mission Status[J]. Advances in Space Research, 2002, 30(2):129-134.
[9] BOCK H, JÄGGI A, ŠVEHLA D, et al. Precise Orbit Determination for the GOCE Satellite Using GPS[J]. Advances in Space Research, 2007, 39(10):1638-1647.
[10] LI Min, LI Wenwen, SHI Chuang, et al. Precise Orbit Determination of the Fengyun-3C Satellite Using Onboard GPS and BDS Observations[J]. Journal of Geodesy, 2017, 91(11):1313-1327.
[11] 郭向, 张强, 赵齐乐, 等. 基于单频星载GPS数据的低轨卫星精密定轨[J]. 中国空间科学技术, 2013, 33(2):41-46. GUO Xiang, ZHANG Qiang, ZHAO Qile, et al. Precise Orbit Determination for LEO Satellites Using Single-frequency GPS Observations[J]. Chinese Space Science and Technology, 2013, 33(2):41-46.
[12] 龚学文, 王甫红. 海洋二号A与资源三号卫星星载GPS自主轨道确定[J]. 武汉大学学报(信息科学版), 2017, 42(3):309-313. GONG Xuewen, WANG Fuhong. Autonomous Orbit Determination of HY2A and ZY3 Missions Using Space-borne GPS Measurements[J]. Geomatics and Information Science of Wuhan University, 2017, 42(3):309-313.
[13] CHOI K R. Jason-1 Precision Orbit Determination Using GPS Combined with SLR and DORIS Tracking Data[D]. Austin:The University of Texas, 2003:2917-2916.
[14] GU Defeng, LAI Yuwang, LIU Junhong, et al. Spaceborne GPS Receiver Antenna Phase Center Offset and Variation Estimation for the Shiyan 3 Satellite[J]. Chinese Journal of Aeronautics, 2016, 29(5):1335-1344.
[15] GUO Jing, ZHAO Qile, GUO Xiang, et al. Quality Assessment of Onboard GPS Receiver and Its Combination with DORIS and SLR for Haiyang 2A Precise Orbit Determination[J]. Science China Earth Sciences, 2015, 58(1):138-150.
[16] LUTHCKE S B, ZELENSKY N P, ROWLANDS D D, et al. The 1-Centimeter Orbit:Jason-1 Precision Orbit Determination Using GPS, SLR, DORIS, and Altimeter Data Special Issue:Jason-1 Calibration/Validation[J]. Marine Geodesy, 2003, 26(3-4):399-421.
[17] MONTENBRUCK O, GARCIA-FERNANDEZ M, YOON Y, et al. Antenna Phase Center Calibration for Precise Positioning of LEO Satellites[J]. GPS Solutions, 2009, 13:23.
[18] JÄGGI A, DACH R, MONTENBRUCK O, et al. Phase Center Modeling for LEO GPS Receiver Antennas and Its Impact on Precise Orbit Determination[J]. Journal of Geodesy, 2009, 83(12):1145-1162.
[19] 胡志刚, 赵齐乐, 郭靖, 等. GPS天线相位中心校正对低轨卫星精密定轨的影响研究[J]. 测绘学报, 2011, 40(S1):34-38. HU Zhigang, ZHAO Qile, GUO Jing, et al. Research on Impact of GPS Phase Center Variation on Precise Orbit Determination of Low Earth Orbit Satellite[J]. Acta Geodaetica et Cartographica Sinica, 2011, 40(S1):34-38.
[20] MAO X, VISSER P N A M, VAN DEN IJSSEL J V. Impact of GPS Antenna Phase Center and Code Residual Variation Maps on Orbit and Baseline Determination of GRACE[J]. Advances in Space Research, 2017, 59(12):2987-3002.
[21] BOCK H, JÄGGI A, MEYER U, et al. Impact of GPS Antenna Phase Center Variations on Precise Orbits of the GOCE Satellite[J]. Advances in Space Research, 2011, 47(11):1885-1893.
[22] 田英国, 郝金明. Swarm卫星天线相位中心校正及其对精密定轨的影响[J]. 测绘学报, 2016, 45(12):1406-1412, 1433. DOI:10.11947/j.AGCS.2016.20160132. TIAN Yingguo, HAO Jinming. Swarm Satellite Antenna Phase Center Correction and Its Influence on the Precision Orbit Determination[J]. Acta Geodaetica et Cartographica Sinica, 2016, 45(12):1406-1412, 1433. DOI:10.11947/j.AGCS.2016.20160132.
[23] VAN DEN IJSSEL J, ENCARNAÇÃO J, DOORNBOS E, et al. Precise Science Orbits for the Swarm Satellite Constellation[J]. Advances in Space Research, 2015, 56(6):1042-1055.
[24] HWANG C, TSENG T P, LIN T, et al. Precise Orbit Determination for the FORMOSAT-3/COSMIC Satellite Mission Using GPS[J]. Journal of Geodesy, 2009, 83(5):477-489.
[25] SCHMID R, ROTHACHER M, THALLER D, et al. Absolute Phase Center Corrections of Satellite and Receiver Antennas[J]. GPS Solutions, 2005, 9(4):283-293.
[26] 赵春梅, 程鹏飞, 益鹏举. 基于伪随机脉冲估计的简化动力学卫星定轨方法[J]. 宇航学报, 2011, 32(4):762-766. ZHAO Chunmei, CHENG Pengfei, YI Pengju. Reduced-dynamics Satellite Orbit Determination Based on Pseudo-Stochastic Pulse Estimation[J]. Journal of Astronautics, 2011, 32(4):762-766.
[27] 秦显平, 焦文海, 程芦颖, 等. 利用SLR检核CHAMP卫星轨道[J]. 武汉大学学报(信息科学版), 2005, 30(1):38-41. QIN Xianping, JIAO Wenhai, CHENG Luying, et al. Evaluation of CHAMP Satellite Orbit with SLR Measurements[J]. Geomatics and Information Science of Wuhan University, 2005, 30(1):38-41.
[28] 周辉, 李松, 杨晋陵, 等. 资源三号卫星激光角反射器阵列质心改正值的解算[C]//中国测绘学会2012年学术年会论文集. 西安:中国测绘学会, 2012. ZHOU Hui, LI Song, YANG Jinling, et al. Calculation of Centroid Correction Value of the Laser Corner Reflector Array of ZY-3[C]//Chinese Society for Geodesy Photogrammetry and Cartography 2012 Annual Conference. Xi'an:China Society of Surveying and Mapping, 2012.