LEOToSunEarthL2Design:

Path: Orbit/ThreeBody

% Design a low thrust transfer from Earth orbit to Sun/Earth-Moon L2 point 
 Simulate in the CRTBP system. Apply a continuous thrust starting from a
 circular Earth orbit at a specified altitude, creating a spiral arc that
 eventually escapes Earth orbit and heads toward the L2 point. Later apply
 a short insertion thrust arc to put the spacecraft into a stable HALO
 orbit about L2. Loads SEML2OrbitData.mat

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  See also L2OrbitPlots, L2OrbitCost, L2OrbitConstraints, FCRTBPRHS
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   Copyright (c) 2012 Princeton Satellite Systems, Inc.
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   Since version 11.
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