LunarOrbitInsertionDemo:

% 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.

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 See also OrbitLoweringManeuvers, RHSLunarOrbit, VInfRPToRV, 
 PlotLunarOrbit, RPRA2AE, TimeOfFlightHyperbola, Period, SunV1, Constant, 
 Plot2D, TimeLabl, Date2JD, RK4
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Children:

Common: Database/Constant
Common: Graphics/Plot2D
Common: Graphics/TimeLabl
Common: Time/Date2JD
LunarCube: Simulation/OrbitLoweringManeuvers
LunarCube: Simulation/RHSLunarOrbit
LunarCube: Simulation/VInfRPToRV
Math: Integration/RK4
Missions: LunarMission/PlotLunarOrbit
Orbit: OrbitCoord/RPRA2AE
Orbit: OrbitMechanics/TimeOfFlightHyperbola
SC: BasicOrbit/Period
SC: Ephem/SunV1