Path: Interplanetary/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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Interplanetary: LowEnergyManeuver/CRTBPJacobiConstant Interplanetary: LowEnergyManeuver/PeriodicOrbitFromGuess Interplanetary: LowEnergyManeuver/PropagateCRTBP Interplanetary: LowEnergyManeuver/V0FromJacobiConstant Common: Database/Constant
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