Path: Orbit/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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AC: ACData/ACTConstants Orbit: OrbitCoord/BarycenterEarthMoon Orbit: OrbitCoord/ECIToEarthMoonRot Orbit: OrbitCoord/TransformEMBRToECI Orbit: OrbitData/EarthMoonSystemConstants Orbit: ThreeBody/CRTBPRHS SC: BasicOrbit/RVFromKepler SC: Ephem/MoonV1 SC: SCData/sCTConstants Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: General/CellToMat Common: General/DeBlankLT Common: General/DeleteCell Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/Plot3D Common: Graphics/PltStyle Common: Graphics/TimeLabl Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Common: Time/DTSToDTA Common: Time/Date2JD Common: Time/JD2000 Math: Linear/Cross Math: Linear/Mag Math: Linear/Unit Math: Trigonometry/CosD Math: Trigonometry/SinD
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