N2A:

Path: Orbit/OrbitMechanics

% Computes the semi-major axis given the mean orbit rate.
   Has a built-in demo with a plot.

   Since version 1.
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   Form:
   a = N2A( n, mu )
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   ------
   Inputs
   ------
   n                     Mean orbit rate
   mu                    Gravitational constant (default is Earth)

   -------
   Outputs
   -------
   a                     Semi-major axis

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   References:   Bates, R.B. Fundamentals of Astrodynamics, pp. 185-187.
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Children:

Common: Graphics/Plot2D

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