Path: Interplanetary/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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Interplanetary: LowEnergyManeuver/LETGuess Interplanetary: LowEnergyManeuver/PropagateCRTBP Interplanetary: LowEnergyManeuver/PropagateCRTBPToPeriapse Common: Database/Constant Common: Graphics/NewFig Common: Graphics/XLabelS Common: Graphics/YLabelS Math: Linear/Mag Math: Linear/Unit
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