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

   [deltaV, tOF, transfer] = OrbMnvrCircularize( rI, vI, gammaI, rF, mu )

   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

   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



Orbit: OrbitCoord/RV2AE
SC: BasicOrbit/E2M
SC: BasicOrbit/Nu2E
SC: BasicOrbit/Nu2M
SC: BasicOrbit/VOrbit
Common: CommonData/SwooshWatermark
Common: General/CellToMat
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle
Math: Linear/Cross
Math: Linear/Dot
Math: Linear/DupVect
Math: Linear/Mag

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