I’ve been running several SITLs to test the backtransition logic, as I have been unable to disable airbraking on my quadplane. It appears setting Q_BACKTRANS_MS to 0 should accomplish this, however I still see the commanded pitch rising to Q_ANGLE_MAX during backtransition, as opposed to staying flat and level as I would expect.
The only other parameter I have seen to affect the backtransition is Q_TRANS_DECEL, but it doesn’t seem like that would affect airbraking.
I’ve looked at the code a bit, and it appears the airbrake logic is more complicated than I originally assumed, and I’m not sure if the code currently allows the airbrake to be disabled, even though that seems to be what Q_BACKTRANS_MS was supposed to do. Would appreciate any help/advice on this.
