Path: Orbit/OrbitManeuver

% Helps design patched conic trajectories.
   [vInf, b, el, r0] = PatchedConicPlanner( planet, r, v, t, muC, pPF )

   planet (1,:) Planet data structure
                .mu    (1,1) Gravitational parameter
                .r     (1,1) Planet radius
                .name  (1,:) Planet name
   r      (3,:) Spacecraft position
   v      (3,:) Spacecraft velocity
   t      (1,:) Corresponding time vector
   muC    (1,1) Gravitational constant for the central body
   pPF    (1,1) Patch point fraction of sphere of influence

   vInf   (1,1) Velocity at infinity for the planet centric hyperbola
   b      (1,1) Impact parameter
   el     (1,6) Hyperbola elements
   r0     (1,1) Periapsis



Common: Database/Constant
Common: Graphics/Map
Common: Graphics/NewFig
Common: Graphics/TitleS
Common: Graphics/XLabelS
Common: Graphics/YLabelS
Common: Graphics/ZLabelS
Common: Quaternion/Mat2Q
Common: Quaternion/QForm
Math: Linear/Cross
Math: Linear/Dot
Math: Linear/Mag
Math: Linear/Unit
Orbit: OrbitCoord/RPRA2AE
Orbit: OrbitMechanics/RVOrbGen
Orbit: OrbitMechanics/SphOI
SC: BasicOrbit/Period
SC: BasicOrbit/RV2El

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