Path: Orbit/LowEnergyManeuver
% Compute a periodic orbit for a LET transfer. The orbit has nearest periapsis at r1. Loads the corresponding mat-files to the selected family: f16, f17, f18, f19, f20, and f26. Type IteratePeriodicOrbit for a demo. -------------------------------------------------------------------------- Form: d = IteratePeriodicOrbit( p1, mu, family ) -------------------------------------------------------------------------- ------ Inputs ------ mu (1,1) Gravity ratio of the CRTBP p1 (1,1) Nearest periapse radius family (1,:) Family name from Markellos catalog e.g. 'f16','f16p' ------- Outputs ------- d (:) Data structure with information about the orbit --------------------------------------------------------------------------
Toolboxes: SourceCode/f20pData Toolboxes: SourceCode/f20pRef Orbit: LowEnergyManeuver/CRTBPJacobiConstant Orbit: LowEnergyManeuver/PeriodicOrbitFromGuess Orbit: LowEnergyManeuver/PropagateCRTBP Orbit: LowEnergyManeuverData/f16Data Orbit: LowEnergyManeuverData/f16Ref Orbit: LowEnergyManeuverData/f16pData Orbit: LowEnergyManeuverData/f16pRef Orbit: LowEnergyManeuverData/f17Data Orbit: LowEnergyManeuverData/f17Ref Orbit: LowEnergyManeuverData/f17pData Orbit: LowEnergyManeuverData/f17pRef Orbit: LowEnergyManeuverData/f18Data Orbit: LowEnergyManeuverData/f18Ref Orbit: LowEnergyManeuverData/f18pData Orbit: LowEnergyManeuverData/f18pRef Orbit: LowEnergyManeuverData/f19Data Orbit: LowEnergyManeuverData/f19Ref Orbit: LowEnergyManeuverData/f19pData Orbit: LowEnergyManeuverData/f19pRef Orbit: LowEnergyManeuverData/f20Data Orbit: LowEnergyManeuverData/f20Ref Orbit: LowEnergyManeuverData/f26Data Orbit: LowEnergyManeuverData/f26Ref Orbit: LowEnergyManeuverData/f26pData Orbit: LowEnergyManeuverData/f26pRef Common: Database/Constant
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