Perform a helicocentric simulation from one circular orbit to another.

------------------------------------------------------------------------
See also LowThrustSim., Constant, UE, Planets
------------------------------------------------------------------------

%-------------------------------------------------------------------------------
%   Copyright (c) 2000 Princeton Satellite Systems, Inc. All rights reserved.
%-------------------------------------------------------------------------------

uE            = 20*1000;
thrust        = 0.4;

p             = Planets( 'rad', [3 4] );
aU            = Constant('au');
muSun         = Constant('mu sun');
aEarth        = aU*p.a(1);
aMars         = aU*p.a(2);
m0            = 127;

[dV, tDuration] = LowThrustSim( aEarth, aMars, uE, thrust, m0, muSun )


%--------------------------------------
% PSS internal file version information
%--------------------------------------

dV =
       4.7963
tDuration =
   3.1173e+06