作者: C. A. Wagner
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摘要: The linear perturbations of the radius a satellite orbit due to geopotential are derived. From these, estimates made radial error just errors from current models employing only conventional satellite-tracking data. show that about an order magnitude improvement in will be necessary utilize full accuracy independent altimeter measurements. used (1) substantial low-degree is possible indirect use Seasat altimetry at track crossovers, and (2) separation “permanent” sea topography geoid may direct heights along track.