Path: Orbit/ThreeBody
% Generate a family of planar Lyapunov orbits Specify a range of orbit amplitudes (Ax), the system (Sun-Earth/Moon or Earth-Moon), and the point (L1 or L2) Type LyapunovFamily for a demo Since version 11. -------------------------------------------------------------------------- Form: ds = LyapunovFamily( Ax, system, point ) -------------------------------------------------------------------------- ------ Inputs ------ Ax (1,:) Normalized obit amplitudes system (:) Name of system 'SEM' or 'EM' point (1,1) Point, L1 (1) or L2 (2) ------- Outputs ------- ds (.) Data structure with stored periodic trajectories -------------------------------------------------------------------------- References: Online course notes, Prof. J.D. Mireles James, Rutgers University. http://www.math.rutgers.edu/~jmireles/notes.html --------------------------------------------------------------------------
Orbit: OrbitData/EarthMoonSystemConstants Orbit: OrbitData/SEML2OrbitData Orbit: OrbitData/SunEarthMoonSystemConstants Orbit: ThreeBody/CRTBPLinearSystem Orbit: ThreeBody/HALOInit Orbit: ThreeBody/HALOState Orbit: Visualization/HALOPlot Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/Circle Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/TimeLabl
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