Matlab Database > Ordinary Differential Equations > Arenstorf orbits

Matlab File(s)

Title: Arenstorf orbits
Author: Bernd Flemisch
Institution: University of Stuttgart
Description: Solution of the ODE arising from the three body problem via an adaptive RK4(3) scheme.
The file arenmenu.m sets up a GUI. Different default orbits and tolerances for the Runge Kutta scheme can be selected. It is also possible to specify arbitrary initial values.
The output visualizes the calculated orbit and the chosen time steps.
Keywords: ODE, three body problem, Arenstorf orbit, Runge Kutta
File Name:
File Size: 7 KB
File Version: 2.0
Matlab Version: 6.1
Date: 2002-10-28
Downloads: 3210
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