Homework Statement
Run a numerical analysis on elliptical orbits using the standard Runka-Kutta method. I already have the equations from Euler-Lagrange method in cartesian x,y-coordinates.
d2x/dt2 = -K x (x2 + y2 )-3/2
d2y/dt2 = -K y (x2 + y2 )-3/2
Homework Equations
I find it a little to...
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