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On the geographical correlation of orbit errorThe orbit accuracies needed to support the global crustal dynamics project and recent satellite altimeter missions have placed unique demands on the data analysis and orbit analysis systems. These demands include accurate and well distributed observations, improved computational techniques and substantial enhancements in the force models which represent the satellite's motion. For example, the satellite altimeter mission (TOPEX), whose objectives will be: (1) to measure the time variable ocean surface topography, and (2) to demonstrate the ability to map the general ocean circulation, requires that the radial component of the satellite's orbit be known with an rms accuracy of 13 cm for the three year mission lifetime. The primary force model uncertainty which limits the contemporary orbit computation accuracy is the inaccuracy in the values assigned to the spherical harmonic coefficients used to model the Earth's gravity field.
Document ID
19860003413
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tapley, B. D.
(Texas Univ. Austin, TX, United States)
Rosborough, G. W.
(Texas Univ. Austin, TX, United States)
Date Acquired
August 12, 2013
Publication Date
October 1, 1985
Publication Information
Publication: NASA, Washington Geopotential Res. Mission (GRM)
Subject Category
Astrodynamics
Accession Number
86N12881
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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