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Preliminary Lunar Swingby Calculations
SPECS Dynamics and Control Preliminary Lunar Swingby Calculations
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Preliminary Lunar Swingby Calculations
SPECS Dynamics and Control Preliminary Lunar Swingby Calculations -Get and from other STK trajectory to L2 -Assume from swingby entirely co-planar -So must place Moon in plane of S/C orbit, where is within the SOI of the Moon. -Using departure conditions from Moon SOI, work backwards to find the hyperbolic orbit and entrance conditions into Moon SOI. -Reference these Moon SOI entrance conditions back to Earth to find the geocentric orbit.
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