OrbitDeltaV:

Path: Missions/Comsat

% Updates orbital elements based on an impulsive delta-V
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   Form:
   el = OrbitDeltaV( el, dV, mu )
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   ------
   Inputs
   ------
   el              (1,6)  Keplerian Elements [a,i,W,w,e,M] (angles in rad)
   dV              (3,1)  Vector delta-V
   mu              (1,1)  Gravitational constant

   -------
   Outputs
   -------
   el              (1,6)  Keplerian Elements [a,i,W,w,e,M] (angles in rad)

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Children:

SC: BasicOrbit/El2RV
SC: BasicOrbit/RV2El

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