2012-08-09 13:58:02 +06:00
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/*!
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\page inertia_page Inertia
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2014-05-05 12:16:12 +06:00
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This operation returns the axial moments of inertia for the selected geometrical object.
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\image html measures4.png
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The table displays:
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2022-04-15 20:29:38 +05:00
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- 3*3 matrix of its own moments of inertia (in cells <b>i:j</b>) and
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- the main (principal) moments of inertia <b>Ip1</b>, <b>Ip2</b> and <b>Ip3</b>
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2022-04-13 18:19:54 +05:00
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\note 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 system
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and Gx, Gy, Gz the directions parallel to the X(1,0,0), Y(0,1,0), Z(0,0,1)
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directions of the absolute cartesian coordinate system.
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\note There is always a set of axes for which the products of inertia
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of a geometric system are equal to 0. These axes are the principal
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axes of inertia. Their origin is coincident with the center of mass
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of the system. The associated moments are called the principal moments
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of inertia. The principal axes are not reported by this functionality.
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\br
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2014-05-05 12:16:12 +06:00
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2014-11-19 17:40:00 +05:00
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\note This dialog supports navigation through the selectable objects (in OCC 3D viewer only):
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- Scroll mouse wheel with pressed \em Ctrl key or press \em "S", \em "P" keys when input focus is
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in the viewer to navigate between selectable objects.
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- Press left mouse button to select an appropriate object to the dialog box.
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.
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For more details, please refer to the \em "Functionality common for OCC and VTK viewers" chapter
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of the GUI module's documentation.
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<b>TUI Command:</b> <em>geompy.Inertia(Shape),</em> where \em Shape is
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2022-04-13 18:19:54 +05:00
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a shape for which the own matrix of inertia and the main (principal) moments
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of inertia are returned.
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2012-08-09 13:58:02 +06:00
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See also a \ref tui_inertia_page "TUI example".
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2014-05-05 12:16:12 +06:00
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2012-08-09 13:58:02 +06:00
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*/
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