Path: LunarMissions/LunarMission
% Lunar Orbit Insertion Demo Simulate a spacecraft in a hyperbolic lunar orbit entering lunar orbit and doing a circularization burn. This script can be modifed for any starting hyperbolic orbit. RHSLunarOrbit has just the lunar gravity. It models point mass motion in the gravity field. This script uses OrbitLoweringManeuvers to schedule and implement the orbit change maneuvers. See also OrbitLoweringManeuvers, RHSLunarOrbit, VInfRPToRV, PlotLunarOrbit, RPRA2AE, TimeOfFlightHyperbola, Period, SunV1, Constant, Plot2D, TimeLabl, Date2JD, RK4 ------------------------------------------------------------------------- % -------------------------------------------------------------------------- Copyright (c) 2016 Princeton Satellite Systems, Inc. All rights reserved. -------------------------------------------------------------------------- Since 2016.1 --------------------------------------------------------------------------