One-Centimeter Orbit Determination for Jason-1: New GPS-Based Strategies

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Absolute phase center corrections of satellite and receiver antennas (2005, methodology): “This is also clearly demonstrated in Figure 3 of Haines et al. (2004).”
Generation of a consistent absolute phase-center correction model for GPS receiver and satellite antennas (2007, methodology): “…same time, the Jet Propulsion Laboratory (JPL) succeeded in deriving PCV maps from post-fit tracking data residuals of the antennas on-board the Jason-1 and GRACE (Gravity Recovery and Climate Experiment) satellites for both the carrier-phase and code pseudorange data types (Haines et al., 2004).”
GGM02 – An improved Earth gravity field model from GRACE (2005, background): “2003) and in reducing geographically correlated errors and their effects on satellite geodesy (Willis 2004; Haines et al. 2004).”
Precision Orbit Determination Standards for the Jason Series of Altimeter Missions (2010, methodology): “Over the past 10 years, significant effort by various groups has been committed toward the 1-cm radial accuracy challenge (Luthcke et al. 2003; Haines et al. 2004).”