Path: Orbit/Visualization
% Plot an orbit track in the Earth/Moon System.
The plots 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.
See also MoonV1, MoonEl.
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Forms:
EarthMoon( r, jD, scale, rMoon )
EarthMoon( elements, jD, scale, rMoon )
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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])
rMoon (3,:) Moon position
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Outputs
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none
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Orbit: OrbitCoord/RPRA2AE SC: BasicOrbit/RVFromKepler SC: Ephem/MoonEl SC: Ephem/MoonV1 SC: SCMat/EarthMR SC: SCMat/Moon Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/DeBlankLT Common: General/MatToCell Common: General/Watermark Common: Graphics/Axis3D 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 Common: Time/JD2T Math: Linear/Mag Math: Linear/Unit Math: Trigonometry/CosD Math: Trigonometry/SinD
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