TransformECIToEMBR:

Path: Orbit/OrbitCoord

% Transform ECI pos. and vel. to Earth Moon barycenter rotating frame.
   
   The EMBR coordinate frame is +x pointing at the earth along
   the earth-moon line. +z normal to the earth moon plane
   and +y completing the set. Uses MoonV1. Computes the plane
   by looking at the moon vector at jD(k) and then 1 day later.

   Type

   TransformECIToEMBR

   for a demo

   Since version 10.
--------------------------------------------------------------------------
   Form:
   [rEMBR,vEMBR,m] = TransformECIToEMBR( jD, rECI, vECI )
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   ------
   Inputs
   ------
   rECI          (6,:)       Position vector in ECI frame
   vECI          (6,:)       Velocity vector in ECI frame
   jD            (1,:)       Julian date (days)
   -------
   Outputs
   -------
   rEMBR         (6,:)       Position vector in EMBR frame          
   vEMBR         (6,:)       Velocity vector in EMBR frame          
   m              {:}        Rotation matrix

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Children:

Common: Database/Constant
Common: Graphics/Plot3D
Common: Time/JD2000
Orbit: OrbitCoord/ECIToEarthMoonRot

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