Does anybody have any information on this? I would assume they’d do what they did with the Harriers and give us a dedicated control mapping input to set the rotation of the nozzles for VTOL. Really hoping they’ll do the same here so we can control the pitch of the rear prop. Really important and beneficial feature of compound helicopters like this is the ability to control the direction and amount of thrust of the rear prop to be able to hold a nose down or nose up position in a hover without drifting. Anybody have any links or anything where they discuss this?
Depends on how thrust is done.
If thrust is done automatically via air speed and stick pitch, then probably no added controls.