Path: Orbit/Visualization
% Displays spacecraft and moon in a trajectory about the Earth in real time.
This function uses persistent variables.
Type TwoObjectTrajectoryViewer for a demo.
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Form:
TwoObjectTrajectoryViewer( 'initialize', n, s, gP, gM )
TwoObjectTrajectoryViewer( 'update', r1, r2, k, t )
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Inputs
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action (1,:) 'initialize', 'update'
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Outputs
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None
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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: BasicOrbit/Period SC: Ephem/MoonV1 SC: SCMat/EarthMR SC: SCMat/Moon SC: Visualization/PlotPlanet Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/DeBlankLT Common: General/MatToCell Common: General/Watermark Common: Graphics/Axis3D Common: Graphics/Mesh2 Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/TimeLabl Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Common: Time/DTSToDTA Common: Time/Date2JD Common: Time/SecToString Math: Linear/DupVect Math: Linear/Mag Math: Linear/Unit Math: Trigonometry/CosD Math: Trigonometry/SinD
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