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Path: Orbit/LowEnergyManeuver
% Compute a periodic orbit for a LET transfer. The orbit has nearest periapsis
at r1.
Since version 9.
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Form:
[d] = LETGuess( p1, mu, family );
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Inputs
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mu (1) Gravity ratio of the CRTBP
p1 (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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Common: Database/Constant Orbit: LowEnergyManeuver/CRTBPJacobiConstant Orbit: LowEnergyManeuver/PeriodicOrbitFromGuess Orbit: LowEnergyManeuver/V0FromJacobiConstant Orbit: ThreeBody/PropagateCRTBP
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