SPECS 2004 Dynamics and Control

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SPECS 2004 Dynamics and Control
Preliminary Lunar Swingby Calculations
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SPECS 2004 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.