ONSLunarMissionDesign:

Path: OpticalNavigation/Core

%  Lunar mission planning
 Compute transfer delta-Vs and simulate a lunar landing starting from 
 low Earth orbit. The entire spacecraft lands, there is no portion left in
 lunar orbit. The steps are:

 # Set the elements and date so that transfer orbit and lunar orbit match. 
 # Compute the insertion delta-v
 # Circularize the lunar orbit
 # Do a Hohmann descent to the powered landing altitude
 # Do a powered landing using BilinearTangent
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