Just read the "official" report. I'm no expert on that case, but it doesn't say anywhere that :
flight controls refused to follow the order limiting the attitude between 13 and 14 deg and the AoA between 14 and 15 deg when that one should have gone to 17.5 deg (Alpha Max) with a full back stick demand ?
Rather, the report states that:" had the elevator control been brought to full aft
sooner or faster, an aoa greater that 15 degrees could have been reached before impact" It then goes on to say that "however, without a sooner application of go-around thrust, such a maneuver would not have prevented impact with the trees"
Looking at the timeline, engines were at idle, even when at 32 feet above the ground and 122 kts (6 secs before impact), with TOGA selected four secs before impact and with not enough time to accelerate to full power.
At one sec before impact, the sidestick is now at full aft with N1 at 67% and 112 kts.