Stefan R. asked 2 months ago
Hi André,
there seems to be a bug when using a control parameter, such as wing / elevator tilt or control surface deflection, with the normal stability analysis (T7).
Only the control parameter = 0 gets calculated. Sometimes it isn’t even possible to edit the control parameter table, disabling/enabling a range of CPs or the table gets reset to zero after the analysis.
Cheers,
Stefan
Additional comment:
Neither works in version 7.23 on macOS or 7.25 on linux.
Hi Stefan,
At some point I had to remove the feature because of excessive code complexity which I just couldn’t manage anymore. I plan on restoring it, likely in the next version, but it requires some deep code refactoring first. I just so happens that I wanted to contact you on that very matter. I’ll send you a message.
André
Alright!
As for now one can simply work around it by duplicating the aircraft and changing the specific parameter.