Path: Orbit/LowEnergyManeuver
% Compute a periodic orbit for a LET transfer.
The orbit has nearest periapsis at r1. Loads a mat-file for the specified
family which must be in the paty.
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Form:
[d] = LETGuess( p1, mu, family );
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Inputs
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mu (1,1) Gravity ratio of the CRTBP
p1 (1,1) Nearest periapse radius
family (1,:) Family name from Markellos catalog
- 'f16'
- 'f16p'
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Outputs
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d (:) Data structure with inforamation about the orbit
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AC: ACData/ACTConstants Orbit: LowEnergyManeuver/CRTBPJacobiConstant Orbit: LowEnergyManeuver/CheckForOptimizationToolbox Orbit: LowEnergyManeuver/PeriodicOrbitFromGuess Orbit: LowEnergyManeuver/PropagateCRTBP Orbit: LowEnergyManeuver/RHSCRTBP Orbit: LowEnergyManeuver/V0FromJacobiConstant Orbit: LowEnergyManeuverData/f16Ref Orbit: LowEnergyManeuverData/f16pRef SC: SCData/sCTConstants Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: General/CellToMat Common: General/DeleteCell Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle
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