Precision orbit determination for TOPEX/POSEIDON
作者： B. D. Tapley , J. C. Ries , G. W. Davis , R. J. Eanes , B. E. Schutz
DOI: 10.1029/94JC01645
关键词:
摘要: The TOPEX/POSEIDON mission objective requires that the radial position of the spacecraft be determined with an accuracy better than 13 cm RMS (root mean square). This stringent …
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