Path: Orbit/ThreeBody
% Compute and plot a family of stable HALO orbits in the given system
Type HALOFamily for a demo.
Since version 11.
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Form:
ds = HALOFamily( Ax, Az, system, point );
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Inputs
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Ax (1,n) Amplitudes of oscillation in the x direction (AU)
Az (1,n) Amplitudes of oscillation in the z direction (AU)
system (:) String name of system: 'SEM' or 'EM'
point (1,1) Which libration point: L1 (1) or L2 (2)
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Outputs
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ds (.) Data structure array with system constants and fields:
.point
.x0
.x0f
.tf
.x0Hist
.t
.xSTM
.x
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References:
Online course notes, Prof. J.D. Mireles James, Rutgers University.
http://www.math.rutgers.edu/~jmireles/notes.html
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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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