Path: Orbit/OrbitControl

% Use Lambert with optimization of start and transfer time
   Uses fmins/fminsearch. This routine checks both direct and retrograde 
   orbit types. 

   See also FLambert and LambertTOF.
   [dV, tOptimal, el, p] = LambertOpt( r1, v1, r2, v2, dT, mu, tol )

   r1            (3,1)   Initial position vector
   v1            (3,1)   Initial velocity
   r2            (3,1)   Target position vector at current time
   v2            (3,1)   Target velocity
   dT            (1,2)   Ideal and maximum time to reach target
   mu            (1,1)   Gravitational parameter
   tol           (1,1)   Tolerance

   dV            (3,1)    Delta-V to apply at start time
   tOptimal      (1,2)    Optimal start and transfer time
   el            (1,:)    Elements of the trajectory
   p             (1,1)    The parameter for the orbit



Orbit: OrbitMechanics/LambertTOF
SC: BasicOrbit/E2M
SC: BasicOrbit/Nu2E
SC: BasicOrbit/Nu2M
SC: BasicOrbit/RV2El
Common: CommonData/SwooshWatermark
Common: General/CellToMat
Common: General/IsVersionAfter
Common: General/MatToCell
Common: General/StringToTokens
Common: General/Watermark
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle
Math: Integration/RK45
Math: Linear/Cross
Math: Linear/DupVect
Math: Linear/Mag
Math: Linear/Unit

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