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Solar radiation force modeling for TDRS orbit determinationThe relative orbit determination accuracies resulting from several TDRS models are evaluated. These models include spherical, single-plate, and restricted two-plate models. The plate models can be adjusted in both area and reflectivity through differential correction. The restricted two-plate model has an Earth-pointing plate and a solar plate; the orientation of the solar plate is restricted to rotation about an axis perpendicular to the satellite's orbital plane.
Document ID
19820002194
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lee, T.
(Computer Sciences Corp. Silver Spring, MD, United States)
Lucas, M. J.
(Computer Sciences Corp. Silver Spring, MD, United States)
Shanklin, R. E., Jr.
(Computer Sciences Corp. Silver Spring, MD, United States)
Date Acquired
August 10, 2013
Publication Date
October 1, 1981
Publication Information
Publication: NASA. Goddard Space Flight Center Sixth Ann. Flight Mech.(Estimation Theory Symp.
Subject Category
Solar Physics
Accession Number
82N10067
Funding Number(s)
CONTRACT_GRANT: NAS5-24300
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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