ECIToRLP:

Path: Orbit/OrbitCoord

% Transform from ECI to Rotating Libration Point Coordinates
 Generates the transformation matrix from ECI to Rotating Libration Point
 Coordinates. Neglects perturbations due to other bodies.
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   Form:
   c = ECIToRLP( xS )
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   ------
   Inputs
   ------
   xS          (6,1)  [r;v] of the secondary

   -------
   Outputs
   -------
   c           (6,6)  Transformation from ECI To RLP

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Children:

SC: Ephem/MoonV1
SC: Ephem/MoonV2
Common: Time/DTSToDTA
Common: Time/Date2JD
Common: Time/JD2000
Math: Linear/Cross
Math: Linear/Mag
Math: Linear/Unit
Math: Trigonometry/CosD
Math: Trigonometry/SinD

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