SubOrbTrajAnalysis:

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   Analyze the trajectories for around-the-Earth sub-orbital launches.

   Generates multiple sub-orbital trajectories that connect the given
   coordinate sets. Creates plots to analyze the relationship
   between time of flight, initial velocity, initial flight path angle,
   maximum altitude.

   Simplifications made for this analysis:
     + Desired velocity is applied instantaneously -- no launch dynamics.
     + The rotation of the Earth is ignored
     + Atmospheric forces are ignored

   Since version 1.0
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   Form:
   d = SubOrbTrajAnalysis( lla0, llaF, tFDes, dragIsOn )
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   Inputs
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   lla0            (3,1)    Initial latitude, longitude, altitude
   llaF            (3,1)    Final
   tFDes           (1,:)    Desired time of flight
   dragIsOn        (1,1)    Optional, default is 0 (off)

   -------
   Outputs
   -------
   d                (.)   Data structure of output

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Children:

Common: Graphics/Circle
Common: Graphics/NewFig
LaunchVehicle: SubOrbital/SubOrbDistance
LaunchVehicle: SubOrbital/SubOrbLambert
LaunchVehicle: Utilities/LaunchConstants
Math: Integration/RK4TI
Math: Linear/Mag