Improving satellite orbit solution using double-differenced GPS carrier phase in kinematic mode
Author:
Publisher
Springer Science and Business Media LLC
Subject
Computers in Earth Sciences,Geochemistry and Petrology,Geophysics
Link
http://link.springer.com/content/pdf/10.1007/s001900100205.pdf
Cited by 8 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Kinematic Precise Orbit Determination for LEO Satellites Using Space-borne Dual-frequency GPS Measurements;Chinese Astronomy and Astrophysics;2012-07
2. Low-degree gravity change from GPS data of COSMIC and GRACE satellite missions;Journal of Geodynamics;2012-01
3. Efficient LEO Dynamic Orbit Determination with Triple Differenced GPS Carrier Phases;Journal of Navigation;2007-04-20
4. A Triple Difference Approach to Low Earth Orbiter Precision Orbit Determination;Journal of Navigation;2003-08-26
5. Satellite orbit determination using triple-differenced GPS carrier phase in pure kinematic mode;Journal of Geodesy;2003-02-01
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