Originally Posted by Owain
Yes, thanks for that link and graph. I see that for quite a time the elevator was moving downwards and the AOA dropping even though the sidestick was being held fully back.
I read the alpha graph to indicate that the aircraft quickly approached its 22 degree pitch limit and the down elevator bunt maneuver was to keep it from overshooting. The time ticks are relatively large 20 second increments.
Much more maneuvering g available in the example than at Habsheim.
I'm wondering whether these systems calculate limiting pitch angle based on excess thrust available at the instant? I'll have to read the report more carefully.
A33Zab, thank you for your post, which, although not directly relating to AI products, is still highly relevant.