Path: AerospaceUtils/Coord

% Convert roll, pitch, r and v to QECIToBody 
 The spacecraft is assumed aligned with LVLH when roll and pitch are zero.
 Roll is about the LVLH x vector and Pitch about the LVLH y vector.

 Type RollPitchToQECI for a demonstration.
  q = RollPitchToQECI( r, v, roll, pitch )

   r     	(3,:)   Position vector in the ECI frame (km)
   v     	(3,:)   Velocity vector in the ECI frame (km)
   roll   	(1,:)   Roll angle (rad)
   pitch 	(1,:)   Pitch angle (rad)

   q      	(4,:)   Quaternion ECI to Body



AerospaceUtils: Coord/QLVLH
SC: BasicOrbit/RVFromKepler
Common: CommonData/SwooshWatermark
Common: General/CellToMat
Common: General/DeBlankLT
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/Plot3D
Common: Graphics/PltStyle
Common: Graphics/TimeLabl
Common: Graphics/XLabelS
Common: Graphics/YLabelS
Common: Graphics/ZLabelS
Common: Quaternion/Mat2Q
Common: Quaternion/Q2Mat
Common: Quaternion/QPose
Math: Linear/Cross
Math: Linear/Unit

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