Numerically integrated ephemerides of the solar system and the Moon require very accurate integrations of systems of second order ordinary differential equations. We present a new family of 8-9 pairs and assess the performance of two new 8-9 pairs on the equations used to create the ephemeris DE102. Part of this work is the introduction of these equations as a test problem for integrators of initial value ordinary differential equations. |
Keywords
numerically integrated ephemerides, explicit Runge-Kutta pairs, efficient
Math Review Classification
Primary 65L06
Last Updated
December 9, 1999
Length
9 pages
Availability
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