arenstorf_ode, a MATLAB code which sets up an ordinary differential equation (ODE) which defines a stable periodic orbit of a spacecraft around the Earth and the Moon.
Although the orbit should be periodic, and repeats after a time interval of a little more than 17 units, most ODE solvers will have difficulty coming close to periodicity.
The computer code and data files described and made available on this web page are distributed under the GNU LGPL license.
arenstorf_ode is available in a MATLAB version and an Octave version and a Python version.
matlab_ode, MATLAB codes which set up various ordinary differential equations (ODE).