Path: SC/BasicOrbit
% Propagate an ECI state into the future with point mass orbit. Uses FOrbCart. -------------------------------------------------------------------------- Form: x = OrbitProp( x0, jD, time ) -------------------------------------------------------------------------- ------ Inputs ------ x0 (6,1) Initial state [km; km/s] time (1,:) Time vector [sec] ------- Outputs ------- x (6,:) Time history of ECI states [km; km/s] -------------------------------------------------------------------------- See also: FOrbCart --------------------------------------------------------------------------
SC: BasicOrbit/El2RV SC: BasicOrbit/FOrbCart SC: BasicOrbit/Period Common: Graphics/Plot3D Math: Integration/RK4
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