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Orbits

This is a simple test program that solves the two body problem ODE system

It was created to test how a library from the MESA stellar evolution code can be used in another different program. It uses a Runge-Kutta method that can be found in the num library of the MESA src code

To run this code, first cd into src/mechanics and compile the code with ./mk. Once the code is compiled, run ./orbit and that's it. It needs MESA installed, which means that you need to set the $MESA_DIR env variable

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