Also, as someone might, and might not have said, if a plane does an aileron roll, the AoA will change unless the roll axis is exactly parallel to the angle of incidence of the wind. I don't think you can guarantee that. For example, in an Extra, before you do an aileron roll, you point the nose up a bit. I expect that the nose is up a bit during the whole aileron roll. That means that when inverted the wings will be providing negative lift (lift against gravity) and when the aircraft is on a knife edge, the AoA could be zero. That would mean that at 45% the AoA would have decreased a little.
Also, a particular pilot in a particular aircraft, might adjust the elevators as they complete the roll.
So, there is every reason to believe that the wing will be producing less lift during the roll. Your answer assumes that the AoA is the same at 45° bank as at 0° bank, which is wrong.