fred@inuxc.UUCP (06/09/83)
I'm looking for some information about orbital computation methods. I'm writing a computer program for home computer systems that essentially solve the n body gravitational (n something around ten bodies) attractional problem. I would like the program to be able to plot out earth to moon orbits, show the stabilities of the L-5 points, and demonstrate the gravitational whip and braking effects of planetary fly-bys. I intend to solve the differential equations using either a Runge Kutta or predictor corrector formulation. Now to my question. How do the big boys (NASA - JPL etc) formulate this problem when they are running orbital calculations? Fred (ABI Indy)