EarthSpiralDemo:

Path: Orbit/Demos/ThreeBody

% Simulates a spiral out from LEO.
  The trajectory as plotted as well as the orbital elements in the 
  heliocentric frame. The final orbital elements at the end of the 
  spiral out are printed to the command window. This demo demonstrates 
  several coordinate transformation

   Since version 10.
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  See also Constant, CRTBPRHS, El2RV, RV2El, TransformECIToSEMR,
  SEMRToSEMI, FCRTBPRHS, LowThrustCRTBP_StopFcn, Plot2D, PlotSEMTraj
  ------------------------------------------------------------------------
%
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	 Copyright (c) 2012 Princeton Satellite Systems, Inc. All rights reserved.
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Children:

Common: Database/Constant
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Time/Date2JD
Math: Linear/Mag
Math: Linear/Unit
Orbit: OrbitCoord/SEMRToSEMI
Orbit: OrbitCoord/TransformECIToSEMR
Orbit: ThreeBody/CRTBPRHS
Orbit: ThreeBody/FCRTBPRHS
Orbit: ThreeBody/LowThrustCRTBP_StopFcn
Orbit: Visualization/PlotSEMTraj
OrbitMiniToolbox: Support/El2RV
SC: BasicOrbit/RV2El

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