Flyby:

Path: Orbit/OrbitMechanics

% Calculates orbital elements and perigee radius for a planetary flyby.

   Since version 2.
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   Form:
   [el, rP] = Flyby( vA, vD, vP, muP )
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   ------
   Inputs
   ------
   vA 		      (3,1)   Approach velocity of the spacecraft
   vD 		      (3,1)   Departure velocity of the spacecraft
   vP 		      (3,1)   Velocity of the planet
   muP         (1,1)   Gravitational parameter of the encountered planet

   -------
   Outputs
   -------
   el 		      (:)     Elements in the planet frame
                       el.a, el.i, el.w, el.W, el.e, el.M
   rP 		      (1,1)   Radius of perigee
             
--------------------------------------------------------------------------

Children:

Orbit: OrbitCoord/SLR
Orbit: OrbitMechanics/RVOrbGen
SC: BasicOrbit/CP2I
SC: BasicOrbit/E2M
SC: BasicOrbit/E2Nu
SC: BasicOrbit/M2E
SC: BasicOrbit/M2EApp
SC: BasicOrbit/M2EEl
SC: BasicOrbit/M2EHy
SC: BasicOrbit/Nu2E
SC: BasicOrbit/Nu2M
Common: CommonData/SwooshWatermark
Common: General/CellToMat
Common: General/DeBlankLT
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/Axis3D
Common: Graphics/Mesh2
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle
Common: Graphics/TimeLabl
Common: Graphics/XLabelS
Common: Graphics/YLabelS
Common: Graphics/ZLabelS
Math: Linear/Cross
Math: Linear/DupVect
Math: Linear/Mag

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