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SUPPORT SITE |
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SUPPORT SITE |
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Path: Orbit/LowEnergyManeuver
% Calculate the nominal transfer time for a low energy transfer
Since version 9.
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Form:
[det,orbits] = LETPhasing(x0,desiredPhasing,moon,planet,et);
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InputsP
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x0 (1) Initial guess for a transfer time
desiredPhasing (1) Angle of the moon at the final time in the
Sun/Planet rotating coordinate system
moon (1) String name of moon
planet (1) String name of planet
et (1) Seconds after the epoch jDate at which the
transfer initiates
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Outputs
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det (1) estimated transfer time
orbits (1) number of lunar orbits during transfer
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Common: Database/Constant Orbit: OrbitCoord/J20002RotPuls SC: BasicOrbit/RV2El SC: Ephem/PlanetPositionEMBarycenter
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