NonKeplerSunSim:

% Simulate a non-Keplerian sail orbit in a cylindrical sun-centered frame.
  The sail enables a displaced orbit above the ecliptic plane.

  Initially the sail elevation angle is fixed, resulting in an unstable
  orbit. Then, the sail pitch angle is fixed instead, resulting in a stable
  oscillation.

   Since version 7.
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   Reference: Colin R. McInnes, "Solar Sailing: Technology, Dynamics and Mission
              Applications", Springer Praxis, London, 1999, Fig. 5.7 p. 186 and 
              Fig. 5.9 on p. 191.
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  See also Constant, InformDlg, Plot2D, Plot3D, NonKeplerianSun, 
  FRotatingSun
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%
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    Copyright (c) 2007 Princeton Satellite Systems, Inc.
    All rights reserved.
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Children:

Common: Database/Constant
Common: Graphics/InformDlg
Common: Graphics/Plot2D
Common: Graphics/Plot3D
Sail: Analysis/NonKeplerianSun
Sail: OrbitDynamics/FRotatingSun