How are exactly calculated the root and tip chord of both the horizontal and vertical stabilizers?
Seeing that no root chord is set in the config file, I understand the algorithm is different than the one given for the wing in the Flight Model Physics section of the SDK.
However, when using real dimensions, the shape is wrongly interpreted and give as a result two triangles opposed by a common point, as can be seen in the screenshot below:
In red, the leading edge, in yellow, the trailing edge.
The same happens with the VStab (same colour coding):
Could we get better control on the shape of these surfaces?
It could in the form of specifying their taper ratio for example, using hstab_taper_ratio and vstab_taper_ratio parameters, and specifying their root chords.
At least, could the above behaviour get fixed so that we have the proper shape of the stabilizers?