A symplectic exponentially fitted modified Runge Kutta Nyström method for the numerical integration of orbital problems

Details A symplectic exponentially fitted modified Runge Kutta Nyström method for the numerical integration of orbital problems A symplectic exponentially fitted modified Runge Kutta Nyström method for the numerical integration of orbital problems

Mar 2005

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2005newa...10..261v&link_type=abstract

New Astronomy, Volume 10, Issue 4, p. 261-269.

Astronomy and Astrophysics

Astronomy

4

02.60, 02.70.Bf, 95.10.Ce, 95.10.Eg, 95.75.Pq.

Scientific paper

A symplectic exponentially fitted modified Runge Kutta Nyström
method is derived in this paper. It is a two-stage second-order method
with FSAL-property. An application to some well known orbital problems
shows the properties of the developed method.

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