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Expected orbit determination performance for the TOPEX/Poseidon mission

The research that has been conducted in the Space Geodesy Branch at NASA/Goddard Space Flight Center in preparation for meeting the 13-cm radial orbit accuracy requirement for the TOPEX/Poseidon (T/P) mission is described. New developments in modeling the Earth's gravitational field and modelin...

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Bibliographic Details
Published in:IEEE transactions on geoscience and remote sensing 1993-03, Vol.31 (2), p.333-354
Main Authors: Nerem, R.S., Putney, B.H., Marshall, J.A., Lerch, F.J., Pavlis, E.C., Klosko, S.M., Luthcke, S.B., Patel, G.B., Williamson, R.G., Zelensky, N.P.
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Language:English
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Summary:The research that has been conducted in the Space Geodesy Branch at NASA/Goddard Space Flight Center in preparation for meeting the 13-cm radial orbit accuracy requirement for the TOPEX/Poseidon (T/P) mission is described. New developments in modeling the Earth's gravitational field and modeling the complex nonconservative forces acting on T/P are highlighted. The T/P error budget is reviewed, and a prelaunch assessment of the predicted orbit determination accuracies is summarized.< >
ISSN:0196-2892
1558-0644
DOI:10.1109/36.214910