GPS single-frequency orbit determination for low Earth orbiting satellites

被引:43
|
作者
Bock, H. [1 ]
Jaeggi, A. [1 ]
Dach, R. [1 ]
Schaer, S. [2 ]
Beutler, G. [1 ]
机构
[1] Univ Bern, Astron Inst, CH-3012 Bern, Switzerland
[2] Cwisstopo, Fed Off Topog, CH-3084 Wabern, Switzerland
关键词
GPS; Single-frequency; Low Earth Orbiters; Precise orbit determination; Ionosphere modeling;
D O I
10.1016/j.asr.2008.12.003
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The determination of high-precision orbits for Low Earth Orbiting (LEO) satellites (e.g., CHAMP, GRACE, MetOp-A) is based oil dual-frequency tracking data from on-board GPS (Global Positioning System) receivers. The two frequencies allow it to eliminate the first order ionosphere effects. Data screening and precise orbit determination (POD) procedures are optimized under the assumption of the availability of two frequencies. If only single-frequency data is available, the algorithms have to be modified to consider the ionospheric effect. We develop and study different approaches for POD with single-frequency data. Reduced-dynamic as well as kinematic POD techniques using pseudorange and carrier phase GPS data are considered. One week of data in the year 2007 is used to assess the potential of single-frequency POD in different environments by comparing the results with dual-frequency POD for LEOs orbiting the Earth in different heights. Data from the two GRACE and the MetOp-A satellites is processed for this purpose. Moreover, the impact of different data sampling rates oil single-frequency POD is considered. For this period with low solar activity a 3D orbit accuracy of I dill could be reached for one of the GRACE satellites. It could be shown that it is necessary to have a high data sampling of 10s or more available when the impact of the ionosphere is high due to low altitude of the satellite or high solar activity. Our study helps to define requirements for GNSS (Global Navigation Satellite System) receivers and POD algorithms for future LEO missions for which only moderate orbit accuracy of about one to few decimeter is needed. (C) 2008 COSPAR. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:783 / 791
页数:9
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