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