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format TopoShapeShellPy.xml

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This commit is contained in:
flachyjoe
2021-03-22 22:25:11 +01:00
committed by wwmayer
parent 37764982bd
commit 7111e137a1
1 changed files with 42 additions and 34 deletions
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76
src/Mod/Part/App/TopoShapeShellPy.xml
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@@ -1,12 +1,12 @@
<?xml version="1.0" encoding="UTF-8"?>
<GenerateModel xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:noNamespaceSchemaLocation="generateMetaModel_Module.xsd">
<PythonExport
Father="TopoShapePy"
Name="TopoShapeShellPy"
Twin="TopoShape"
TwinPointer="TopoShape"
Include="Mod/Part/App/TopoShape.h"
Namespace="Part"
<PythonExport
Father="TopoShapePy"
Name="TopoShapeShellPy"
Twin="TopoShape"
TwinPointer="TopoShape"
Include="Mod/Part/App/TopoShape.h"
Namespace="Part"
FatherInclude="Mod/Part/App/TopoShapePy.h"
FatherNamespace="Part"
Constructor="true">
@@ -16,22 +16,30 @@
</Documentation>
<Methode Name="add">
<Documentation>
<UserDocu>Add a face to the shell.</UserDocu>
<UserDocu>Add a face to the shell.
add(face)
</UserDocu>
</Documentation>
</Methode>
<Methode Name="getFreeEdges" Const="true">
<Documentation>
<UserDocu>Get free edges as compound.</UserDocu>
<UserDocu>Get free edges as compound.
getFreeEdges() -> compound
</UserDocu>
</Documentation>
</Methode>
<Methode Name="getBadEdges" Const="true">
<Documentation>
<UserDocu>Get bad edges as compound.</UserDocu>
<UserDocu>Get bad edges as compound.
getBadEdges() -> compound
</UserDocu>
</Documentation>
</Methode>
<Methode Name="makeHalfSpace" Const="true">
<Documentation>
<UserDocu>Make a half-space solid by this shell and a reference point.</UserDocu>
<UserDocu>Make a half-space solid by this shell and a reference point.
makeHalfSpace(point) -> Solid
</UserDocu>
</Documentation>
</Methode>
<Attribute Name="Mass" ReadOnly="true">
@@ -51,43 +59,43 @@ absolute Cartesian coordinate system.</UserDocu>
</Attribute>
<Attribute Name="MatrixOfInertia" ReadOnly="true">
<Documentation>
<UserDocu>Returns the matrix of inertia. It is a symmetrical matrix.
The coefficients of the matrix are the quadratic moments of
inertia.
<UserDocu>Returns the matrix of inertia. It is a symmetrical matrix.
The coefficients of the matrix are the quadratic moments of
inertia.
| Ixx Ixy Ixz 0 |
| Ixy Iyy Iyz 0 |
| Ixz Iyz Izz 0 |
| 0 0 0 1 |
| Ixx Ixy Ixz 0 |
| Ixy Iyy Iyz 0 |
| Ixz Iyz Izz 0 |
| 0 0 0 1 |
The moments of inertia are denoted by Ixx, Iyy, Izz.
The products of inertia are denoted by Ixy, Ixz, Iyz.
The matrix of inertia is returned in the central coordinate
system (G, Gx, Gy, Gz) where G is the centre of mass of the
system and Gx, Gy, Gz the directions parallel to the X(1,0,0)
Y(0,1,0) Z(0,0,1) directions of the absolute cartesian
The moments of inertia are denoted by Ixx, Iyy, Izz.
The products of inertia are denoted by Ixy, Ixz, Iyz.
The matrix of inertia is returned in the central coordinate
system (G, Gx, Gy, Gz) where G is the centre of mass of the
system and Gx, Gy, Gz the directions parallel to the X(1,0,0)
Y(0,1,0) Z(0,0,1) directions of the absolute cartesian
coordinate system.</UserDocu>
</Documentation>
<Parameter Name="MatrixOfInertia" Type="Object"/>
</Attribute>
<Attribute Name="StaticMoments" ReadOnly="true">
<Documentation>
<UserDocu>Returns Ix, Iy, Iz, the static moments of inertia of the
current system; i.e. the moments of inertia about the
<UserDocu>Returns Ix, Iy, Iz, the static moments of inertia of the
current system; i.e. the moments of inertia about the
three axes of the Cartesian coordinate system.</UserDocu>
</Documentation>
<Parameter Name="StaticMoments" Type="Object"/>
</Attribute>
<Attribute Name="PrincipalProperties" ReadOnly="true">
<Documentation>
<UserDocu>Computes the principal properties of inertia of the current system.
There is always a set of axes for which the products
of inertia of a geometric system are equal to 0; i.e. the
matrix of inertia of the system is diagonal. These axes
are the principal axes of inertia. Their origin is
coincident with the center of mass of the system. The
associated moments are called the principal moments of inertia.
This function computes the eigen values and the
<UserDocu>Computes the principal properties of inertia of the current system.
There is always a set of axes for which the products
of inertia of a geometric system are equal to 0; i.e. the
matrix of inertia of the system is diagonal. These axes
are the principal axes of inertia. Their origin is
coincident with the center of mass of the system. The
associated moments are called the principal moments of inertia.
This function computes the eigen values and the
eigen vectors of the matrix of inertia of the system.</UserDocu>
</Documentation>
<Parameter Name="PrincipalProperties" Type="Dict"/>