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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

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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