FBW pitch/thrust compensation
I am wondering how Boeing and Airbus software compensates for pitch/thrust coupling?
Does it simply monitor inertial rates and apply pitch control/trim to null them/adjust to the demanded input?
Is there also some form of commanded/actual N1 or similar input to allow the system to anticipate high compensation requirements such as go arounds &c in the same way as config trim changes are handled?
If anyone has any good in depth links to discussions of particularly the Boing but also the Airbus FBW software implementation I would be v interested in reading them.