QuadPlane Transition Airbraking

Hi all,

Currently trying to better understand and setup the transition air-braking behavior. In all VTOL and wingborne modes, I would like to have pitch limits of, say, +/-25 degrees. However, I would like the transition air-braking to NOT take the vehicle to such pitch attitudes, and be limited to, say, +/-15 degrees for air-braking only. Is there a way to do this?

I’ve played with the brake delay, brake accel, and transition time delay between 0 pitch angle and max pitch angle…but no luck.

Any thoughts?