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The TiGL Geometry Library to process aircraft geometries in pre-design.

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The install instruction for TiGL in Python for the latest version (3.2.3) found [here](https://dlr-sc.github.io/tigl/doc/3.2.3/tigl_installation.html) still request an installation of Python 3.6, which has been EOL since the beginning of the...

As discussed previously with @joergbrech, currently only STEP files are supported for inclusion as generic geometry components, whereas, according to the [CPACS docs](https://www.cpacs.de/documentation/CPACS_3_4_0_Docs/html/fc38f77f-bb60-7599-4cbf-1abdf520e8ba.htm), STL and IGES should also be supported....

I just realized, that the number of Iso Lines in U-Direction does not change anymore. The code has not changed for a while, so I suppose it is a bug...

bug

## Description Fixes #883. This PR updates the CPACS schema file to 3.3. Apart from some syntactic changes (e.g. renamed xml nodes for kinks) and some small bug fixes the...

With the update to CPACS 3.3 in #907, we should implement the possibility to set a stringerFramePosition via a SectionElementUid, see also https://github.com/DLR-SL/CPACS/issues/680.

Currently, TiGL only support pointList and 2D CST profiles for wings and pointList profiles for fuselages. With the update to CPACS 3.3 in #907, we should implement parametric fuselage profiles...

With the Update to CPACS 3.3 in https://github.com/DLR-SC/tigl/pull/907, we should implement the geometry of landing gears. See also https://github.com/DLR-SL/CPACS/issues/632.

According to the [CPACS documentation](https://www.cpacs.de/documentation/CPACS_3_4_0_Docs/html/fda3a776-8768-8029-bd55-47efdbe97c80.htm) the hingeLineRotation of a control surface path is defined to be mathematically positive around the vector pointing from the inner hinge point to the outer...

Steps to reproduce: - Open a CPACS configuration - Show the wing flaps and keep the dialog for manipulating the deflection open, - Modify the CPACS file to that the...