N-body space simulator that uses the Runge-Kutta 4 numerical integration method to solve two first order differential equations derived from the second order differential equation that governs the motion of an orbiting celestial. Also has preset demos for two-body and three-body circular orbits which use parametric equations. Uses the SFML (Simp…
c-plus-plus
simulator
simulation
space
orbit
planet
gravity
numerical-methods
n-body-simulator
orbital-simulation
celestial-bodies
orbits
numerical-integration
runge-kutta
n-body
celestial
rk4
gravity-simulate
runge-kutta-methods
-
Updated
Jun 2, 2017 - C++