Simulated Error-free Orbits of Gravity Satellite Mission (Inertial Reference)
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Error-free position and velocity of two gravity satellites of the ChiGaM/TIANQIN2 missions simulated in the Inertial Frame of Reference FileName='ChiGaM.nc'; ncdisp(FileName) ChiGaM= ncread(FileName,'ChiGaM'); FileName='TIANQIN2.nc'; ncdisp(FileName) TIANQIN2= ncread(FileName,'TIANQIN2');
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Zenodo创建时间:
2025-10-09



