We continue to work on various aspects of the flight model: the roll rate has been lowered by 25%, the authority of the rudder has been increased. The drag curve between mach 0 and mach 0.250 is being adjusted to favor deceleration and landings and the CL vs AOA both alpha and beta are also being adjusted too. Fixed the propeller moi according to the weight and radius of the official propeller. The toe brake pressure has been increased to be able to drop the nose but still being controllable.
There is still refinement to do but I will give you an advance.
I apologize for my abrupt flying style showed in the video, but there have been too many hours testing this weekend and my reflexes are already failing me a bit, but the basic idea is to put the plane to the limit.
