Path: SC/Ephem

% Computes the position and velocity of stable Lagrange points.
   Assumes thes positive x axis in the rotating frame is towards the moon 
   from the Earth.
   See also LagrangePointsL1ToL5 and MoonV1.
   [r, v, mLEToECI] = TransformLagrangePoints( p, jD )

   p              (2,:)  Points
   jD             (1,1)  Date of interest

   r              (3,1)  Position of stable point in ECI frame
   v              (3,1)  Velocity of stable point in ECI frame
   mLEToECI       (3,3)  Transformation matrix from Lunar-Earth to ECI



SC: Ephem/LagrangePointsL1ToL5
SC: Ephem/MoonV1
Common: General/DeBlankLT
Common: Graphics/Axis3D
Common: Graphics/Ellipsd
Common: Graphics/Map
Common: Graphics/NewFig
Common: Graphics/PltStyle
Common: Graphics/TitleS
Common: Graphics/XLabelS
Common: Graphics/YLabelS
Common: Graphics/ZLabelS
Common: Time/DTSToDTA
Common: Time/Date2JD
Common: Time/DateStringToJD
Math: Linear/Cross
Math: Linear/DupVect
Math: Linear/Mag
Math: Linear/Unit
Math: Trigonometry/CosD
Math: Trigonometry/SinD

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