228 lines
9.0 KiB
XML
228 lines
9.0 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="TopoShapeFacePy"
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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>TopoShapeFace is the OpenCasCade topological face wrapper</UserDocu>
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</Documentation>
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<Methode Name="addWire">
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<Documentation>
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<UserDocu>Adds a wire to the face.
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addWire(wire)
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</UserDocu>
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</Documentation>
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</Methode>
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<Methode Name="makeOffset" Const="true">
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<Documentation>
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<UserDocu>Offset the face by a given amount.
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makeOffset(dist) -> Face
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--
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Returns Compound of Wires. Deprecated - use makeOffset2D instead.
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</UserDocu>
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</Documentation>
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</Methode>
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<Methode Name="makeEvolved" Const="true" Keyword="true">
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<Documentation>
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<UserDocu>Profile along the spine</UserDocu>
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</Documentation>
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</Methode>
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<Methode Name="getUVNodes" Const="true">
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<Documentation>
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<UserDocu>Get the list of (u,v) nodes of the tessellation
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getUVNodes() -> list
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--
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An exception is raised if the face is not triangulated.
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</UserDocu>
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</Documentation>
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</Methode>
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<Methode Name="tangentAt" Const="true">
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<Documentation>
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<UserDocu>Get the tangent in u and v isoparametric at the given point if defined
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tangentAt(u,v) -> Vector
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</UserDocu>
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</Documentation>
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</Methode>
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<Methode Name="valueAt" Const="true">
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<Documentation>
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<UserDocu>Get the point at the given parameter [0|Length] if defined
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valueAt(u,v) -> Vector
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</UserDocu>
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</Documentation>
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</Methode>
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<Methode Name="normalAt" Const="true">
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<Documentation>
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<UserDocu>Get the normal vector at the given parameter [0|Length] if defined
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normalAt(pos) -> Vector
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</UserDocu>
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</Documentation>
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</Methode>
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<Methode Name="derivative1At" Const="true">
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<Documentation>
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<UserDocu>Get the first derivative at the given parameter [0|Length] if defined
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derivative1At(u,v) -> (vectorU,vectorV)
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</UserDocu>
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</Documentation>
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</Methode>
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<Methode Name="derivative2At" Const="true">
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<Documentation>
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<UserDocu>Vector = d2At(pos) - Get the second derivative at the given parameter [0|Length] if defined
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derivative2At(u,v) -> (vectorU,vectorV)
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</UserDocu>
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</Documentation>
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</Methode>
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<Methode Name="curvatureAt" Const="true">
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<Documentation>
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<UserDocu>Get the curvature at the given parameter [0|Length] if defined
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curvatureAt(u,v) -> Float
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</UserDocu>
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</Documentation>
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</Methode>
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<Methode Name="isPartOfDomain" Const="true">
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<Documentation>
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<UserDocu>Check if a given (u,v) pair is inside the domain of a face
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isPartOfDomain(u,v) -> bool
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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 face and a reference point.
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makeHalfSpace(pos) -> Shape
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</UserDocu>
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</Documentation>
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</Methode>
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<Methode Name="validate">
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<Documentation>
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<UserDocu>Validate the face.
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validate()
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</UserDocu>
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</Documentation>
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</Methode>
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<Methode Name="countNodes" Const="true">
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<Documentation>
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<UserDocu>Returns the number of nodes of the triangulation.</UserDocu>
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</Documentation>
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</Methode>
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<Methode Name="countTriangles" Const="true">
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<Documentation>
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<UserDocu>Returns the number of triangles of the triangulation.</UserDocu>
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</Documentation>
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</Methode>
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<Methode Name="curveOnSurface" Const="true">
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<Documentation>
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<UserDocu>Returns the curve associated to the edge in the parametric space of the face.
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curveOnSurface(Edge) -> (curve, min, max) or None
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--
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If this curve exists then a tuple of curve and parameter range is returned.
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Returns None if this curve does not exist.
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</UserDocu>
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</Documentation>
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</Methode>
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<Methode Name="cutHoles">
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<Documentation>
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<UserDocu>Cut holes in the face.
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cutHoles(list_of_wires)
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</UserDocu>
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</Documentation>
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</Methode>
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<Attribute Name="Tolerance">
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<Documentation>
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<UserDocu>Set or get the tolerance of the vertex</UserDocu>
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</Documentation>
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<Parameter Name="Tolerance" Type="Float"/>
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</Attribute>
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<Attribute Name="ParameterRange" ReadOnly="true">
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<Documentation>
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<UserDocu>Returns a 4 tuple with the parameter range</UserDocu>
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</Documentation>
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<Parameter Name="ParameterRange" Type="Tuple"/>
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</Attribute>
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<Attribute Name="Surface" ReadOnly="true">
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<Documentation>
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<UserDocu>Returns the geometric surface of the face</UserDocu>
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</Documentation>
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<Parameter Name="Surface" Type="Object"/>
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</Attribute>
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<Attribute Name="Wire" ReadOnly="true">
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<Documentation>
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<UserDocu>The outer wire of this face
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deprecated -- please use OuterWire</UserDocu>
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</Documentation>
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<Parameter Name="Wire" Type="Object"/>
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</Attribute>
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<Attribute Name="OuterWire" ReadOnly="true">
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<Documentation>
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<UserDocu>The outer wire of this face</UserDocu>
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</Documentation>
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<Parameter Name="OuterWire" Type="Object"/>
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</Attribute>
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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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