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Present status and future trends in near-Earth satellite orbit determinationThe major components of an orbit determination system and the evolution of the elements making up each component are reviewed. Typical accuracies presently achievable in the orbit determination process, the factors limiting the accuracies, and improvements in the dynamic models used in the process are summarized. Models are developed for orbit determination programs which include: (1) time varying area for solar radiation pressure; (2) a time varying model for albedo radiation pressure; (3) Earth tides which account for the distortions in the Earth's body due to Sun and Moon attraction; and (4) ocean tides which affect satellite altimeter data.
Document ID
19820006279
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Fuchs, A. J.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 10, 2013
Publication Date
August 1, 1981
Publication Information
Publication: ESA Spacecraft Flight Dyn.
Subject Category
Astrodynamics
Accession Number
82N14152
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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