This program uses the fourth order runge-kutta method to compute and plot a variety of orbits, the various options are given below. For details on the results and numerical method please read the report.
- Two Body Orbit
- Three Body Moonshot (Stationary Moon)
- 3D (Stationary Moon)
- Three Body Moonshot (Moving Moon)
- Numerical Method Comparison
(Location: School of Physics, University of Bristol)