Path: Orbit/Visualization
% Plot an orbit track in the Earth/Moon Rotating System.
The input vectors are in the ECI frame. Has a built-in demo for an orbit
with an apogee of 400,000 km, a perigee of 7000 km, and a duration of 5 days.
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Forms:
EarthMoonRotFrame( r, jD, scale, lagrange, lunarCone )
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Inputs
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r (3,:) ECI position vectors (km) or
(1,6) elements
jD (:) Julian dates
scale (1,2) Planet scale (optional, default is [1 1])
lagrange (1,1) If entered draw lagrange points
lunarCone (1,3) [lat, lon, angle]
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Outputs
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none
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AC: ACData/ACTConstants AerospaceUtils: Coord/LatLonToR Orbit: OrbitCoord/RPRA2AE Orbit: OrbitCoord/SLR Orbit: OrbitMechanics/RVOrbGen SC: BasicOrbit/CP2I SC: BasicOrbit/E2M SC: BasicOrbit/E2Nu SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/Nu2E SC: BasicOrbit/Nu2M SC: Ephem/LagrangePointsL1ToL5 SC: Ephem/MoonEl SC: Ephem/MoonV1 SC: SCData/sCTConstants Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: ComponentModels/Box Common: ComponentModels/Cone Common: ComponentModels/Frustrum Common: Database/Constant Common: General/CellToMat Common: General/DeBlankLT Common: General/DeleteCell Common: General/MatToCell Common: General/Watermark Common: Graphics/Axis3D Common: Graphics/DrawVertices Common: Graphics/Ellipsd Common: Graphics/Map Common: Graphics/Mesh2 Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/TimeLabl Common: Graphics/TitleS Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Common: Quaternion/QForm Common: Quaternion/QTForm Common: Quaternion/U2Q Common: Time/DTSToDTA Common: Time/Date2JD Common: Time/JD2000 Common: Time/JD2T Math: Geometry/Perpendicular Math: Linear/Cross Math: Linear/Dot Math: Linear/DupVect Math: Linear/Mag Math: Linear/Unit Math: Trigonometry/CosD Math: Trigonometry/SinD
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