OptimalSMADemo:

% Computes optimal semi-major axis  and eccentricity control.
 Four values of eccentricity are analyzed, [0 0.1 0.4 0.8]

   Since version 7.
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  Reference: Colin R. McInnes, "Solar Sailing: Technology, Dynamics and
        Mission Applications", Springer Praxis, London, 1999, pp. 136-148. 
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  See also Plot2D
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   Copyright (c) 2005 Princeton Satellite Systems, Inc.
   All rights reserved.
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Children:

Common: Graphics/Plot2D