On simulation of precise orbit determination of HY-2 with centimeter precision based on satellite-borne GPS technique

Author:

Guo Jin-Yun,Qin Jian,Kong Qiao-Li,Li Guo-Wei

Publisher

Springer Science and Business Media LLC

Subject

Geophysics

Reference34 articles.

1. Bertiger, W. I., Bar-Sever, T. E., Christensen, E. J., et al., 1994, GPS precise tracking of TOPEX/Poseidon: results and implications: Journal of Geophysical Research, 99, 24449–24464.

2. Bock, H., 2003, Efficient methods for determining precise orbits of low earth orbiters using the global positioning system: PhD Thesis, Astronomical Institute, University of Berne, Berne.

3. Guo, J. Y., Hwang, C. W., Hu, J. G., and Li, J. C., 2006a, Determination of CHAMP orbit from onboard GPS double-difference phase data with dynamic method: Geomatics and Information Science of Wuhan University, 31(3), 213–217.

4. Guo, J. L., Zhao, Q. L., and Guo, D. Y., 2006b, Reducing the influence of gravity model error on precise orbit determination of low earth orbit satellites: Geomatics and Information Science of Wuhan University, 31(3), 293–296.

5. Guo, J. Y., Hwang, C. W., Tseng, Z. P., Chang, X. T., and Han, Y. B., 2008, Research of geometry orbit determination of COSMIC satellite based on satelliteborne GPS zero-difference data: Progress in Natural Science, 18(1), 75–80.

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