Hostname: page-component-76fb5796d-vfjqv Total loading time: 0 Render date: 2024-04-26T06:04:34.711Z Has data issue: false hasContentIssue false
  • English
  • Français

Long-term integration error of KS regularized orbital motion

Published online by Cambridge University Press:  26 May 2016

Hideyoshi Arakida  and
Toshio Fukushima
Hideyoshi Arakida
Affiliation:
Graduate University for Advanced Studies, 2-21-1, Osawa, MItaka, Tokyo, 181-8588 JAPAN
Toshio Fukushima
Affiliation:
National Astronomical Observatory of Japan, 2-21-1, Osawa, MItaka, Tokyo, 181-8588 JAPAN

Abstract

Core share and HTML view are not available for this content. However, as you have access to this content, a full PDF is available via the ‘Save PDF’ action button.

We show the effectiveness of the KS regularization and the method of variation of parameter for integrating of the perturbed two body problems.

Type
Posters
Information
Symposium - International Astronomical Union , Volume 208: Astrophysical Supercomputing using Particle Simulations , 2003 , pp. 375 - 376
Copyright
Copyright © Astronomical Society of the Pacific 2003 

References

Arakida, H., & Fukushima, T., 2000, AJ, 120, 3333 CrossRefGoogle Scholar
Arakida, H., & Fukushima, T., 2001, AJ, 121, 1764 CrossRefGoogle Scholar
Stiefel, E., Rössler, Waldvogel, J., & Burdet, C. A., 1967, Method of Regularization for computing Orbits in Celestial Mechanics, NASA Constructor Report NASA CR-769 Google Scholar
Stiefel, E.L., & Sheifele, G., 1971, Linear and Regular Celestial Mechanics, Springer CrossRefGoogle Scholar