Kalman-filter-based GPS clock estimation for near real-time positioning

被引:158
作者
Hauschild, Andre [1 ]
Montenbruck, Oliver [1 ]
机构
[1] Deutsch Zentrum Luft & Raumfahrt, GSOC, D-82234 Wessling, Germany
关键词
Clock estimation; Precise orbit determination; Real-time; Kalman filter;
D O I
10.1007/s10291-008-0110-3
中图分类号
TP7 [遥感技术];
学科分类号
081102 ; 0816 ; 081602 ; 083002 ; 1404 ;
摘要
In this article, an algorithm for clock offset estimation of the GPS satellites is presented. The algorithm is based on a Kalman-filter and processes undifferenced code and carrier-phase measurements of a global tracking network. The clock offset and drift of the satellite clocks are estimated along with tracking station clock offsets, tropospheric zenith path delay and carrier-phase ambiguities. The article provides a brief overview of already existing near-real-time and real-time clock products. The filter algorithm and data processing scheme is presented. Finally, the accuracy of the orbit and clock product is assessed with a precise orbit determination of the MetOp satellite and compared to results gained with other real-time products.
引用
收藏
页码:173 / 182
页数:10
相关论文
共 17 条
[1]  
Bar-Sever Y., 2003, SPACE APPL NASA GLOB
[2]  
BARSEVER Y, 2008, NASA GLOBAL DIFFEREN
[3]  
BOCK H, 2008, AEROSP SCI TEC UNPUB
[4]  
Collins P, 1996, PROCEEDINGS OF THE 52ND ANNUAL MEETING - THE INSTITUTE OF NAVIGATION, P519
[5]  
Dach R., 2007, BERNESE GPS SOFTWARE
[6]  
Hutsell S. T., 1996, 27 ANN PREC TIM TIM, P291
[7]  
*IGS, 2008, WEEKL SIN FIL
[8]  
McCarthy DD., 2004, IERS conventions (2003)
[9]   Reduced dynamic orbit determination using GPS code and carrier measurements [J].
Montenbruck, O ;
van Helleputte, T ;
Kroes, R ;
Gill, E .
AEROSPACE SCIENCE AND TECHNOLOGY, 2005, 9 (03) :261-271
[10]  
MONTENBRUCK O, 2008, TRACKING ORBIT DETER