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Compression of ephemerides by discrete Chebyshev approximationsThe use of Chebyshev series in representing the ephemerides of satellites and planets in terms of truncated polynomial series is discussed. Emphasis is placed on a FORTRAN package which was developed for fitting satellite orbits. The features desired in any approximation are: (1) the ability to compress a satellite emphemeris; (2) the ability to represent a satellite ephemeris over several orbits; (3) guaranteed accuracy to within prescribed tolerance over the time interval of consideration; and (4) fast processing. These features are imposed with an eye towards adapting the approximation for use on microprocessor applications in which storage is limited and real time processing is required.
Document ID
19790005951
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Pickard, H. M.
(Naval Research Lab. Washington, DC, United States)
Deprit, A.
(Cincinnati Univ. Washington, DC, United States)
Poplarchek, W.
(Naval Research Lab.)
Date Acquired
August 10, 2013
Publication Date
May 1, 1978
Publication Information
Publication: NASA. Goddard Space Flight Center Flight Mechanics(Estimation Theory Symp.
Subject Category
Astrodynamics
Accession Number
79N14122
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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