High-precision orbit determination for a LEO nanosatellite using BDS-3

被引:32
作者
Zhao, Xinglong [1 ,2 ,3 ]
Zhou, Shanshi [1 ,2 ]
Ci, Ying [4 ]
Hu, Xiaogong [1 ,2 ]
Cao, Jianfeng [5 ]
Chang, Zhiqiao [6 ]
Tang, Chengpan [1 ,2 ]
Guo, Danni [7 ]
Guo, Kai [7 ]
Liao, Min [8 ]
机构
[1] Chinese Acad Sci, Shanghai Astron Observ, Shanghai 200030, Peoples R China
[2] Shanghai Key Lab Space Positioning & Nav, Shanghai 200030, Peoples R China
[3] Univ Chinese Acad Sci, Beijing 100049, Peoples R China
[4] Beijing Inst Tracking & Telecommun Technol, Beijing 100094, Peoples R China
[5] Beijing Aerosp Control & Command Ctr, Beijing 100094, Peoples R China
[6] Beijing Satellite Nav Ctr, Beijing 100094, Peoples R China
[7] Xian Satellite Control Ctr, Xian 710043, Peoples R China
[8] Insight Data Technol Shenzhen Corp Ltd, Shenzhen 518000, Peoples R China
基金
中国国家自然科学基金;
关键词
LEO satellite; Nanosatellite; POD; Sub-dm-level; GPS; BDS; GPS RECEIVER; ONBOARD GPS; GRACE; CHAMP; DORIS; GOCE;
D O I
10.1007/s10291-020-01015-9
中图分类号
TP7 [遥感技术];
学科分类号
081102 ; 0816 ; 081602 ; 083002 ; 1404 ;
摘要
The Tianping-1B is a 20-kg low earth orbit nanosatellite with a commercial multi-GNSS receiver based on a microelectromechanical system. This receiver collects concurrent code and phase dual-frequency measurements from the global positioning system (GPS) and the second and third generations of the BeiDou Global Navigation Satellite System (i.e., BDS-2 and BDS-3). However, BDS-3 signals with pseudorandom noise code numbers greater than 32 cannot be received. In this study, onboard GPS and BDS measurements from Tianping-1B are collected for days 133-147 of 2019. The performance of the onboard BDS-3 measurements is analyzed, and the potential of the BDS-3-based precise orbit determination (POD) for Tianping-1B is assessed. The carrier-to-noise-density ratio of the BDS-3 is higher than that of the BDS-2 and approaches that of the GPS. The BDS-3 has a smaller code multipath error than the BDS-2 and the GPS and therefore a higher quality of code measurements. The results of the overlap comparison show a GPS-based orbit consistency below 3.5 cm in three dimensions (3D) and below 1.2 cm in the radial direction. The mean of satellite laser ranging validation residual RMS is 1.7 cm. The orbit obtained using onboard BDS measurements is assessed using the GPS-based orbit as a reference: The mean 3D root mean square (RMS) difference between the BDS-3-only-based POD and the reference orbit is 4.57 cm. Thus, a sub-dm-level orbit can be achieved using only onboard BDS-3 measurements. A POD with slightly higher precision than the BDS-3-only-based POD is obtained using both BDS-3 and BDS-2 measurements, using higher weights for the BDS-3 data than the BDS-2 data. Then, the combined BDS-3/GPS POD is performed: The RMS difference between this joint orbit and the GPS-based orbit is 1 cm in 3D. This study can be used as a reference for the development of BDS-3 based POD, which will approve in accuracy and precision upon completion of BDS-3.
引用
收藏
页数:14
相关论文
共 39 条
[1]   GOCE: precise orbit determination for the entire mission [J].
Bock, Heike ;
Jaeggi, Adrian ;
Beutler, Gerhard ;
Meyer, Ulrich .
JOURNAL OF GEODESY, 2014, 88 (11) :1047-1060
[2]  
Bowman B.R., 2008, AIAAAAS ASTRODYNAMIC, DOI [10.2514/6.2008-6438, DOI 10.2514/6.2008-6438]
[3]  
Cao J, 2017, COOPERATIVE POSITION, DOI [10.1109/CPGPS.2017.8075112, DOI 10.1109/CPGPS.2017.8075112]
[4]  
Dach R, 2020, CODE FINAL PRODUCT S, P1
[5]   GOCE: ESA's first Earth Explorer Core mission [J].
Drinkwater, MR ;
Floberghagen, R ;
Haagmans, R ;
Muzi, D ;
Popescu, A .
SPACE SCIENCE REVIEWS, 2003, 108 (1-2) :419-432
[6]   TEQC: The Multi-Purpose Toolkit for GPS/GLONASS Data [J].
Estey, Louis H. ;
Meertens, Charles M. .
GPS SOLUTIONS, 1999, 3 (01) :42-49
[7]  
Fernandez J, 2019, SENTINEL 3A VALIDATI, DOI [10.1007/1345_2019_64, DOI 10.1007/1345_2019_64]
[8]  
Flechtner F, 2010, ADV TECHNOLOGIES EAR
[9]  
Flechtner F, 2010, ADV TECHNOL EARTH SC, P41, DOI 10.1007/978-3-642-10228-8_4
[10]  
Folkner W.M., 2009, IPN Progress Report 42-178, P1