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.
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Form:
area = CrossSection( g, bodyAngle, viewV, plot )
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Inputs
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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
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Outputs
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area (1) Cross-sectional area of spacecraft
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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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