105 lines
4.0 KiB
XML
105 lines
4.0 KiB
XML
<?xml version="1.0" encoding="UTF-8"?>
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<GenerateModel xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:noNamespaceSchemaLocation="generateMetaModel_Module.xsd">
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<PythonExport
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Father="TopoShapePy"
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Name="TopoShapeShellPy"
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Twin="TopoShape"
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TwinPointer="TopoShape"
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Include="Mod/Part/App/TopoShape.h"
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Namespace="Part"
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FatherInclude="Mod/Part/App/TopoShapePy.h"
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FatherNamespace="Part"
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Constructor="true">
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<Documentation>
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<Author Licence="LGPL" Name="Juergen Riegel" EMail="Juergen.Riegel@web.de" />
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<UserDocu>Create a shell out of a list of faces</UserDocu>
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</Documentation>
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<Methode Name="add">
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<Documentation>
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<UserDocu>Add a face to the shell.
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add(face)
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</UserDocu>
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</Documentation>
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</Methode>
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<Methode Name="getFreeEdges" Const="true">
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<Documentation>
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<UserDocu>Get free edges as compound.
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getFreeEdges() -> compound
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</UserDocu>
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</Documentation>
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</Methode>
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<Methode Name="getBadEdges" Const="true">
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<Documentation>
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<UserDocu>Get bad edges as compound.
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getBadEdges() -> compound
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</UserDocu>
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</Documentation>
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</Methode>
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<Methode Name="makeHalfSpace" Const="true">
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<Documentation>
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<UserDocu>Make a half-space solid by this shell and a reference point.
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makeHalfSpace(point) -> Solid
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</UserDocu>
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</Documentation>
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</Methode>
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<Attribute Name="Mass" ReadOnly="true">
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<Documentation>
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<UserDocu>Returns the mass of the current system.</UserDocu>
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</Documentation>
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<Parameter Name="Mass" Type="Object"/>
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</Attribute>
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<Attribute Name="CenterOfMass" ReadOnly="true">
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<Documentation>
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<UserDocu>Returns the center of mass of the current system.
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If the gravitational field is uniform, it is the center of gravity.
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The coordinates returned for the center of mass are expressed in the
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absolute Cartesian coordinate system.</UserDocu>
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</Documentation>
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<Parameter Name="CenterOfMass" Type="Object"/>
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</Attribute>
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<Attribute Name="MatrixOfInertia" ReadOnly="true">
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<Documentation>
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<UserDocu>Returns the matrix of inertia. It is a symmetrical matrix.
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The coefficients of the matrix are the quadratic moments of
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inertia.
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| Ixx Ixy Ixz 0 |
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| Ixy Iyy Iyz 0 |
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| Ixz Iyz Izz 0 |
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| 0 0 0 1 |
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The moments of inertia are denoted by Ixx, Iyy, Izz.
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The products of inertia are denoted by Ixy, Ixz, Iyz.
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The matrix of inertia is returned in the central coordinate
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system (G, Gx, Gy, Gz) where G is the centre of mass of the
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system and Gx, Gy, Gz the directions parallel to the X(1,0,0)
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Y(0,1,0) Z(0,0,1) directions of the absolute cartesian
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coordinate system.</UserDocu>
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</Documentation>
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<Parameter Name="MatrixOfInertia" Type="Object"/>
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</Attribute>
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<Attribute Name="StaticMoments" ReadOnly="true">
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<Documentation>
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<UserDocu>Returns Ix, Iy, Iz, the static moments of inertia of the
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current system; i.e. the moments of inertia about the
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three axes of the Cartesian coordinate system.</UserDocu>
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</Documentation>
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<Parameter Name="StaticMoments" Type="Object"/>
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</Attribute>
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<Attribute Name="PrincipalProperties" ReadOnly="true">
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<Documentation>
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<UserDocu>Computes the principal properties of inertia of the current system.
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There is always a set of axes for which the products
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of inertia of a geometric system are equal to 0; i.e. the
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matrix of inertia of the system is diagonal. These axes
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are the principal axes of inertia. Their origin is
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coincident with the center of mass of the system. The
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associated moments are called the principal moments of inertia.
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This function computes the eigen values and the
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eigen vectors of the matrix of inertia of the system.</UserDocu>
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</Documentation>
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<Parameter Name="PrincipalProperties" Type="Dict"/>
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</Attribute>
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</PythonExport>
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</GenerateModel>
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