[net.space] Runga-Kutta for orbits?

fred@inuxc.UUCP (06/18/83)

	Well after spending an afternoon working out the math
it seems that a 4th order Runga Kutta numeric integration is exactly
equivalent to....

	x=xo+vo*t+.5*a*t**2

for n body problem, point gravity, no drag. That explains
why Lew had reasonable results using it in college. The error
using this form will be of the order of...
	
	fifth derivative of position*(time step)**5

	
a good approximation. It also means that this method should be good 
enough to start a predictor- corrector integration instead of having
to go through the pain of starting it with R-K.

	I'm off fishing for a week.

				Fred (ABI till August)