Constrained GPS Precise Orbit Determination for Low Earth Orbiters

被引:0
|
作者
Mander, Amandeep [1 ]
Bisnath, Sunil [2 ]
机构
[1] York Univ, Dept Phys & Astron, Toronto, ON M3J 2R7, Canada
[2] York Univ, Dept Earth & Space Sci & Engn, Toronto, ON M3J 2R7, Canada
来源
PROCEEDINGS OF THE 23RD INTERNATIONAL TECHNICAL MEETING OF THE SATELLITE DIVISION OF THE INSTITUTE OF NAVIGATION (ION GNSS 2010) | 2010年
基金
加拿大自然科学与工程研究理事会;
关键词
SATELLITES;
D O I
暂无
中图分类号
TP7 [遥感技术];
学科分类号
081102 ; 0816 ; 081602 ; 083002 ; 1404 ;
摘要
The degradations in accuracy of GPS precise orbit determination solutions for Low Earth Orbiters (LEOs) are analyzed under various constraints in this study. The constrained solutions are compared against a reference solution that is determined by post-processing dual-frequency data from the CHAllenging Mini-Satellite Payload (CHAMP). The constraints explored in this study are real-time processing requirements, availability of only single-frequency data, limited power onboard the LEO and limited CPU onboard the LEO. For the post-processing case, the longer the time that the receiver collects data, the more accurate the solution. This is not the case for real-time processing. In the case of post-processing, switching from single-frequency to dual-frequency data improves the orbit accuracy quite significantly in contrast to real-time processing. In the case of a limited CPU for real-time processing, altering the complexity of the dynamic models does not affect the accuracy with much significance.
引用
收藏
页码:2789 / 2796
页数:8
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