Path: AerospaceUtils/CAD

% Determine cross-sectional area from CAD model. 
 This routine assumes that the first body is the core and the next n bodies, if
 any, are rotated by the corresponding body angle.

 Type CrossSection for demo.
   area = CrossSection( g, bodyAngle, viewV, plot )

   g                 (:)  CAD model struct
   bodyAngle       (n,1)  Body angles, if applicable*
   viewV           (3,1)  Vector viewpoint, nominally [1;0;0] *
   plot              (1)  Plot flag*
                             * Optional
   area              (1)  Cross-sectional area of spacecraft



AerospaceUtils: CAD/BHinge
AerospaceUtils: CAD/Dim
AerospaceUtils: CAD/DrawSCPlanPlugIn
AerospaceUtils: CAD/DrawSpacecraftPatches
SC: Ephem/Eclipse
SC: Ephem/SunV1
SC: SCModels/SCForImaging
SC: SCModels/SimpleSat
SC: SCModels/TwoArraySC
Common: CommonData/SwooshWatermark
Common: General/CellToMat
Common: General/CloseFigure
Common: General/DeBlankLT
Common: General/IsValidField
Common: General/IsVersionAfter
Common: General/MatToCell
Common: General/StringToTokens
Common: General/Watermark
Common: Graphics/NPlot
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle
Common: Graphics/XLabelS
Common: Graphics/YLabelS
Common: Graphics/ZLabelS
Common: Quaternion/AU2Q
Common: Quaternion/Q2Mat
Common: Time/DTSToDTA
Common: Time/Date2JD
Common: Time/JD2000
Math: Linear/Dot
Math: Linear/DupVect
Math: Linear/Mag
Math: Linear/Unit
Math: Trigonometry/CosD
Math: Trigonometry/SinD

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