FFEccFrenet2Goals:

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   Compute geometric goals given Frenet frame state and orbit info

   Since version 7.
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   Form:
   [g,D] = FFEccFrenet2Goals( e, nu, xF, n );
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   Inputs
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   e                (1)   Eccentricity
   nu               (1)   True anomaly [rad]
   xF              (6,1)  Frenet frame state at nu (time-domain)
   n                (1)   Mean orbit rate [rad/s] (optional)
                           * uses time-derivatives if provided
                           * uses nu-derivatives if NOT provided

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   Outputs
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   g                (.)   Data structure of geometric goals

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	  Copyright (c) 2007 Princeton Satellite Systems, Inc. 
   All rights reserved.
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Children:

FormationFlying: Transformation/FFEccHills2Goals
FormationFlying: Transformation/Frenet2Hills