Review of the LEO Orbit Determination Using GNSS and Application Prospect in TT&C

被引:0
作者
Wang, Chong [1 ,2 ]
Zhu, Jun [1 ,2 ]
Fang, Yanan [1 ,2 ]
Li, Jie [1 ,2 ]
机构
[1] State Key Lab Astronaut Dynam, Xian 710043, Peoples R China
[2] Xian Satellite Control Ctr, Xian 710043, Peoples R China
来源
CHINA SATELLITE NAVIGATION CONFERENCE PROCEEDINGS, CSNC 2022, VOL I | 2022年 / 908卷
关键词
Onboard GNSS; international GNSS Monitoring and Assessment System (iGMAS); Ultra-rapid products; Orbit determination; TT&C; GPS; JASON-1; GOCE;
D O I
10.1007/978-981-19-2588-7_16
中图分类号
TN [电子技术、通信技术];
学科分类号
0809 ;
摘要
For a LEO satellite with an onboard GNSS receiver, the TT&C equipment on the ground can receive dual-frequency GNSS observation data with an arc length of about 12 h of the satellite within about 10 min of the visible arc. At the same time, the international GNSS Monitoring and Assessment System (iGMAS) of China can provide Ultra-rapid orbit and clock offset products of the BDS, GPS, GLONASS and Galileo satellites, and high-precision Earth Orientation Parameters (EOP) in this data arc. Therefore, using these Ultra-rapid products and the dual-frequency GNSS data, we can achieve the precise orbit determination and complete the orbit prediction. Based on this technology, it is possible to reduce the number of laps of satellite tracking by ground equipment, and to achieve precision orbit determination; at the same time, the orbit determination software can realize automatic and autonomous operation.
引用
收藏
页码:169 / 177
页数:9
相关论文
共 30 条
[1]   GPS PRECISE TRACKING OF TOPEX/POSEIDON - RESULTS AND IMPLICATIONS [J].
BERTIGER, WI ;
BARSEVER, YE ;
CHRISTENSEN, EJ ;
DAVIS, ES ;
GUINN, JR ;
HAINES, BJ ;
IBANEZMEIER, RW ;
JEE, JR ;
LICHTEN, SM ;
MELBOURNE, WG ;
MUELLERSCHOEN, RJ ;
MUNSON, TN ;
VIGUE, Y ;
WU, SC ;
YUNCK, TP ;
SCHUTZ, BE ;
ABUSALI, PAM ;
RIM, HJ ;
WATKINS, MM ;
WILLIS, P .
JOURNAL OF GEOPHYSICAL RESEARCH-OCEANS, 1994, 99 (C12) :24449-24464
[2]   Sub-Centimeter Precision Orbit Determination with GPS for Ocean Altimetry [J].
Bertiger, Willy ;
Desai, Shailen D. ;
Dorsey, Angie ;
Haines, Bruce J. ;
Harvey, Nate ;
Kuang, Da ;
Sibthorpe, Ant ;
Weiss, Jan P. .
MARINE GEODESY, 2010, 33 :363-378
[3]   Precise orbit determination for the GOCE satellite using GPS [J].
Bock, H. ;
Jaeggi, A. ;
Svehla, D. ;
Beutler, G. ;
Hugentobler, U. ;
Visser, P. .
ADVANCES IN SPACE RESEARCH, 2007, 39 (10) :1638-1647
[4]   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
[5]  
[郭恒洋 Guo Hengyang], 2021, [全球定位系统, Gnss World of China], V46, P24
[6]  
Guo Jing, 2013, Geomatics and Information Science of Wuhan University, V38, P52
[7]  
Haines B., 2003, Navigation. Journal of the Institute of Navigation, V50, P171
[8]   One-Centimeter Orbit Determination for Jason-1: New GPS-Based Strategies [J].
Haines, Bruce ;
Bar-Sever, Yoaz ;
Bertiger, Willy ;
Desai, Shailen ;
Willis, Pascal .
MARINE GEODESY, 2004, 27 (1-2) :299-318
[9]   Precise orbit determination for GRACE using undifferenced or doubly differenced GPS data [J].
Jaeggi, A. ;
Hugentobler, U. ;
Bock, H. ;
Beutler, G. .
ADVANCES IN SPACE RESEARCH, 2007, 39 (10) :1612-1619
[10]   Precise orbit determination for GRACE [J].
Kang, Z ;
Nagel, P ;
Pastor, R .
INTEGRATED SPACE GEODETIC SYSTEMS AND SATELLITE DYNAMICS, 2003, 31 (08) :1875-1881