RVOrbGenDV:

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   Generate an orbit by propagating Keplerian elements with impulsive delta-vs.

   Since version 7.
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   Form:
   [r, v] = RVOrbGenDV( el, t, dV, dVTime )
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   ------
   Inputs
   ------
   elI        Elements vector [a,i,W,w,e,M] or structure
   t          Times from 0 to ? (sec)
   dV         Array of 3xN delta-v's to be applied (Hills frame)  [km/sec]
   dVTime     Array of 1xN times at which delta-v's are applied   [sec]

   -------
   Outputs
   -------
   r          Position vectors for times t
   v          Velocity vectors for times t
   el         Times at which r and v are calculated

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Children:

FormationFlying: Coord/GetHillsMats
Orbit: OrbitMechanics/RVOrbGen
SC: BasicOrbit/RV2El