Journals
Publish with us
Publishing partnerships
About us
Blog
Abstract and Applied Analysis
Journal overview
For authors
For reviewers
For editors
Table of Contents
Special Issues
Abstract and Applied Analysis
/
2014
/
Article
/
Tab 3
/
Research Article
A Note on the Use of Generalized Sundman Anomalies in the Numerical Integration of the Elliptical Orbital Motion
Table 3
Number of steps to get a precision of
Km.
rk4
2287352
1562132
969798
662225
601888
595921
rk8
73994
41764
21428
13302
16091
12091