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A Precision Recursive Estimate for Ephemeris Refinement (PREFER)A recursive filter/smoother orbit determination program was developed to refine the ephemerides produced by a batch orbit determination program (e.g., CELEST, GEODYN). The program PREFER can handle a variety of ground and satellite to satellite tracking types as well as satellite altimetry. It was tested on simulated data which contained significant modeling errors and the results clearly demonstrate the superiority of the program compared to batch estimation.
Document ID
19800019895
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gibbs, B.
(Business and Technological Systems, Inc. Seabrook, MD, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1980
Publication Information
Publication: NASA. Goddard Space Flight Center Flight Mech.(Estimation Theory Symp.
Subject Category
Astrodynamics
Accession Number
80N28396
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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