Long-term planetary integration with individual time steps
Prasenjit Saha, Scott Tremaine
Abstract
We describe an algorithm for long-term planetary orbit integrations, including the dominant post-Newtonian effects, that employs individual timesteps for each planet. The algorithm is symplectic and exhibits short-term errors that are O(εΩ2τ2) where τ is the timestep, Ω is a typical orbital frequency, and ε1 is a typical planetary mass in solar units. By a special starting procedure long-term errors over an integration interval T can be reduced to O(ε2Ω3τ2T). A sample 0.8 Myr integration of the nine planets illustrates that Pluto can have a timestep more than 100 times Mercury's, without dominating the positional error. Our algorithm is applicable to other N-body systems.
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