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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
Goddard Space Flight Center
Document Type
Conference Paper
Authors
H M Pickard
(Naval Research Lab. Washington, DC, United States)
A Deprit
(Cincinnati Univ. Washington, DC, United States)
W Poplarchek
(Naval Research Lab.)
Date Acquired
August 10, 2013
Publication Date
October 1, 1977
Publication Information
Publication: Flight Mechanics/Estimation Theory Symposium
Publisher: National Aeronautics and Space Administration
Subject Category
Astrodynamics
Report/Patent Number
NASA-CP-2050
NASA/CP-19790005950
Meeting Information
Meeting: Flight Mechanics/Estimation Theory Symposium
Location: Greenbelt, MD
Country: US
Start Date: October 1, 1977
Accession Number
79N14122
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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