Florida Institute of Technology C++ Programming Project
Description
You are to solve these equations using the 4th-order Runge-Kutta scheme. You must write a computer program that
accepts as input the aphelion (farthest) distance the planet is from the sun in astronomical units (AU), the eccentricity
of the orbit, 0 1 ? ?e , and how many orbits are to be calculated. With the help of the equations on the next page, your
code will solve the four ODEs above, resulting in data to allow you to plot the position of the orbiting body (starting
at the aphelion) as a function of time as it orbits counterclockwise about the sun. Your code should continue until a
user-specified number of orbital periods (i.e. complete orbits) have been calculated
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