Path: LunarMissions/Visualization
% Plot a trajectory in the Earth-Moon system
Type PlotEMTraj for a demo
Since version 11.
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Form:
p = PlotEMTraj( r, frame, jD )
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Inputs
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r (3,:) Trajectory data
frame (:) Coordinate frame. May be one of the following:
'EMBRND' Earth-Moon Barycenter Rotating Non-Dim.
'EMBR' Earth-moon Barycenter Rotating
'ECI' Earth-centered Inertial
'MCI' Moon-centered Inertial
'MCR' Moon-centered Rotating
jD (1,1) Julian date time vector
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Outputs
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None
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Interplanetary: ThreeBody/CRTBPRHS LunarMissions: LunarData/EarthMoonSystemConstants Orbit: OrbitCoord/TransformEMBRToECI SC: Ephem/MoonV1 Common: Time/Date2JD
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