Precise orbit determination for Jason-1 satellite using on-board GPS data with cm-level accuracy

Science China Press., Co. Ltd. - Tập 54 - Trang 196-202 - 2009
DongJu Peng1,2, Bin Wu1
1Shanghai Astronomical Observatory, Chinese Academy of Sciences, Shanghai, China
2Graduate University of Chinese Academy of Sciences, Beijing, China

Tóm tắt

The joint US/French Jason-1 satellite altimeter mission, launched from the Vandenberg Air Force Base on December 7, 2001, continues the time series of centimeter-level ocean topography observations as the follow-on to the highly successful T/P radar altimeter satellite. Orbit error especially the radial orbit error is a major component in the overall budget of all altimeter satellite missions, in order to continue the T/P standard of observations. Jason-1 has a radial orbit error budget requirement of 2.5 cm. In this work, two cycles (December 19, 2002 to January 7, 2003) of the Jason-1 on-board GPS data were processed using the zero-difference (ZD) dynamic precise orbit determination (POD) technique. The resulting Jason-1 orbit accuracy was assessed by comparison with the precise orbit ephemeris (POE) produced by JPL, orbit overlaps and SLR residuals. These evaluations indicate that the RMS radial accuracy is in the range of 1–2 cm.

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