Path: Orbit/Visualization
% Simulate and plot an Earth orbit to L2 point low thrust transfer.
Sequence is: spiral out / coast / reverse thrust / halo orbit
Type L2OrbitPlots for a demo which loads SEML2OrbitData.mat
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Form:
L2OrbitPlots( x, d )
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Inputs
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x (4,1) Decision variables [phase, T1, T2, dT]
- phase Initial phase angle of Earth orbit in xy plane
- T1 Time to stop spiral thrust arc
- T2 Time to start insertion thrust arc
- dT Duration of reverse thrust arc
d (.) Data structure describing spacecraft model and CRTBP
system
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Outputs
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None
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See also L2OrbitSim.
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Orbit: OrbitData/SEML2OrbitData Orbit: OrbitData/SunEarthMoonSystemConstants Orbit: OrbitManeuver/LTSpiral Orbit: ThreeBody/L2OrbitSim Common: Graphics/Circle Common: Graphics/NewFig
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