FFEccDeltaElem2Goals:

--------------------------------------------------------------------------
   Convert element differences to eccentric geometric goals. 

   Since version 7.
--------------------------------------------------------------------------
   Usage:
   g = FFEccDeltaElem2Goals( el0, dEl, type );
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   el0          (1,6)  Initial reference orbital elements
   dEl          (1,6)  Initial orbital element differences
   type          (1)   Element set type
                          - 1   [a,theta,i,q1,q2,W]  (Alfriend format)
                          - 2   [a,i,W,w,e,M]        (standard format)

   -------
   Outputs
   -------
   g             (.)   Geometric goals data structure 
   
--------------------------------------------------------------------------

Children:

FormationFlying: Transformation/FFEccDeltaElem2Hills
FormationFlying: Transformation/FFEccHills2Goals
OrbitMiniToolbox: Support/M2Nu
SC: BasicOrbit/OrbRate