>>1670629Learn your dynamic modes, scrub.
https://ocw.mit.edu/courses/aeronautics-and-astronautics/16-333-aircraft-stability-and-control-fall-2004/lecture-notes/lecture_6.pdfElevator input drives steady-state AOA, after short-period oscillations are dampened. The relationship is affected by CG/static margin, and flaps or throttle can affect trim state somewhat as well, but for a given configuration there is a direct and linear relationship between elevator input and steady-state AOA.
