A2Perige:

Path: Orbit/OrbitCoord

% Computes the perigee radius from a.

   Since version 1.
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   Form:
   rP = A2Perige( a, e )
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   ------
   Inputs
   ------
   a                     Semi major axis
   e                     Eccentricity

   -------
   Outputs
   -------
   rP                    Perigee radius

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   References: Bate, R. R., Fundamentals of Astrodynamics. pp. 20-40.
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Children:

Common: Graphics/Mesh2
Math: Linear/DupVect

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