HeliopauseWithLaserSimulation:

% Planar heliopause mission simulation.
   Can use either a built-in specular sail force disturbance function or the 
   full sail disturbance function. Uses the FlatSail CAD model.
   The sail characteristic acceleration is about 4.6e-6 km/s2.

   This simulation has a simple laser model. When the spacecraft is
   past earth orbit it adds the power from the laser model along the 
   velocity vector. This is added to the sun acceleration. The laser model
   only works with the specular model. The logic works by turning on the 
   laser after the spacecraft has flown by the sun.

   Functions demonstrated:
       RHSHelio2DOrbit
       HeliopauseSailAngle
       FlatPlate

   Since version 10.
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  See also Constant, Plot2D, TimeLabl, JD2000, HeliopauseSailAngle
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%
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	Copyright (c) 2005,2006 Princeton Satellite Systems, Inc. 
   All rights reserved.
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Children:

Common: Database/Constant
Common: Graphics/Plot2D
Common: Graphics/TimeLabl
Common: Time/JD2000
Sail: Guidance/HeliopauseSailAngle