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: AeroData/SimpleSC AerospaceUtils: CAD/BHinge AerospaceUtils: Visualization/DrawSCPlanPlugIn
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