Path: Orbit/LowEnergyManeuver
% Calculate a low energy transfer in a CRTBP.
The transfer is from a circular orbit of radius r1 to a circular orbit
of radius r2.
Type LowEnergyTransferInCRTBP for a demo between two circular orbits.
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Form:
LET = LowEnergyTransferInCRTBP( r1,r2,mu,orientation );
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Inputs
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r1 (1,1) Initial circular orbit radius
r2 (1,1) Final circular orbit radius
mu (1,1) Gravity ratio of the CRTBP
orientation (1,1) orientation of the maneuver
- ' '
- 'p'
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Outputs
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LET (.) Data structure with information about the orbit
.mu
.JacobiConstant
.initialState
.period
.tF
.dV1
.family
.dV2
.theta2
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AC: ACData/ACTConstants Orbit: LowEnergyManeuver/CRTBPJacobiConstant Orbit: LowEnergyManeuver/CheckForOptimizationToolbox Orbit: LowEnergyManeuver/LETGuess Orbit: LowEnergyManeuver/PeriodicOrbitFromGuess Orbit: LowEnergyManeuver/PropagateCRTBP Orbit: LowEnergyManeuver/PropagateCRTBPToPeriapse Orbit: LowEnergyManeuver/RHSCRTBP Orbit: LowEnergyManeuver/V0FromJacobiConstant Orbit: LowEnergyManeuverData/f16Ref Orbit: LowEnergyManeuverData/f16pRef Orbit: LowEnergyManeuverData/f26pRef SC: SCData/sCTConstants Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: General/CellToMat Common: General/DeBlankLT Common: General/DeleteCell Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/XLabelS Common: Graphics/YLabelS Math: Linear/Mag Math: Linear/Unit
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