OrbMnvrCircularize:

Path: Orbit/OrbitManeuver

% Computes the delta-V for a 2-burn transfer to a circular orbit at rF. 
   The delta-Vs are at

     a. the initial orbit
     b. the final orbit

   Since version 9.
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   Form:
   [deltaV, tOF, transfer] = OrbMnvrCircularize( rI, vI, gammaI, rF, mu )
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   ------
   Inputs
   ------
   rI          (1,1)  Initial radius
   vI          (1,1)  Initial velocity
   gammaI      (1,1)  Initial flight path angle   (rad)
   rF          (1,1)  Final radius
   mu          (1,1)  Gravitational parameter

   -------
   Outputs
   -------
   deltaV      (1,1)  Delta-V data structure. 
                      .total (1,1)	Total required delta-V
                      .a     (1,1) Delta-V at point a
                      .b     (1,1) Delta-V at point b
   tOF         (1,1)  Time of flight

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Children:

Math: Linear/Mag
Orbit: OrbitCoord/RV2AE
SC: BasicOrbit/Nu2M
SC: BasicOrbit/VOrbit

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