PlotEMTraj:

Path: Orbit/Visualization

% Plot a trajectory in the Earth-Moon system

   Type PlotEMTraj for a demo

   Since version 11.
--------------------------------------------------------------------------
   Form:
   p = PlotEMTraj( r, frame, jD )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   r         (3,:)   Trajectory data 
   frame      (:)    Coordinate frame. May be one of the following:
                       'EMBRND'    Earth-Moon Barycenter Rotating Non-Dim.
                       'EMBR'      Earth-moon Barycenter Rotating
                       'ECI'       Earth-centered Inertial
                       'MCI'       Moon-centered Inertial
                       'MCR'       Moon-centered Rotating

   jD        (1,1)   Julian date time vector

   -------
   Outputs
   -------
   None

--------------------------------------------------------------------------

Children:

AC: ACData/ACTConstants
Orbit: OrbitCoord/BarycenterEarthMoon
Orbit: OrbitCoord/ECIToEarthMoonRot
Orbit: OrbitCoord/TransformEMBRToECI
Orbit: OrbitData/EarthMoonSystemConstants
Orbit: ThreeBody/CRTBPRHS
SC: BasicOrbit/RVFromKepler
SC: Ephem/MoonV1
SC: SCData/sCTConstants
Common: CommonData/Constants
Common: CommonData/SwooshWatermark
Common: CommonData/xSplashSmall
Common: Database/Constant
Common: General/CellToMat
Common: General/DeBlankLT
Common: General/DeleteCell
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: Time/DTSToDTA
Common: Time/Date2JD
Common: Time/JD2000
Math: Linear/Cross
Math: Linear/Mag
Math: Linear/Unit
Math: Trigonometry/CosD
Math: Trigonometry/SinD

Back to the Orbit Module page