NuInf:

Path: Orbit/OrbitMechanics

% Computes the asymptote angle for a hyperbola. 

 If e is < 1 it substitutes 1.

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   Form:
   psi = NuInf( e )
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   ------
   Inputs
   ------
   e                    Eccentricity

   -------
   Outputs
   -------
   psi                  Asymptote angle (rad)

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	  References: Wiesel, W. E., Spaceflight Dynamics, McGraw-Hill, 1988, 
               pp. 54.
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Children:

Common: Graphics/Plot2D

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