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Application and analysis of satellite orbit prediction techniquesThe numerical accuracy of a satellite orbit computation program was investigated. The effects of roundoff and truncation errors on the solution were determined. New formulations that have the mean motion based on the total energy are compared to the more classical formulations and evaluated via numerical experiments.
Document ID
19790020037
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 3, 2013
Publication Date
April 12, 1977
Subject Category
Astrodynamics
Report/Patent Number
NASA-CR-157219
JSC-12571
REPT-77-FM-19
Report Number: NASA-CR-157219
Report Number: JSC-12571
Report Number: REPT-77-FM-19
Accession Number
79N28208
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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