Simulation study of a low-low satellite-to-satellite tracking mission

By Jeongrae Kim, Byron D. Tapley. 2000

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GGM02 – An improved Earth gravity field model from GRACE (2005, methodology): “The KBR data and background model errors are expected to cause drifts in measurement residuals on time scales longer than the orbital period, and the estimated biases are designed to accommodate this (Kim, 2000; Kim and Tapley 2002).”
The JPL lunar gravity field to spherical harmonic degree 660 from the GRAIL Primary Mission (2013, methodology): “After aligning the LGRS clocks and finding the precise LGRS Ka carrier frequency, determined by the USO frequency measurements, the dual one-way phase measurements (integrated frequency) is formed at a given coordinate time t as [Kruizinga et al., 2012; Kim 2000]”