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The intermediate anomalyTime transformations of the equation dt = cr to the n ds, where s is a variable called the intermediate anomaly, are known to reduce global error in the solution of gravitational systems obtained by numerical integration. Attention is given to the Sundman time transformation, and its relation to equations of Keplerian elliptical motion.
Document ID
19780048604
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Nacozy, P.
(Texas, University Austin, Tex., United States)
Date Acquired
August 9, 2013
Publication Date
November 1, 1977
Publication Information
Publication: Celestial Mechanics
Volume: 16
Subject Category
Numerical Analysis
Accession Number
78A32513
Distribution Limits
Public
Copyright
Other

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