I think you are asking about the following which is a very simple case describing what I think you are talking about;
Bolt on the wings at an incidence of 4 degrees.
Bolt on the horizontal stabilizer at an angle of incidence of 2 degrees.
Aircraft flying along level (wing 4deg angle of attack and tail 2 deg angle of attack) and gets disturbed, nose up slightly.
Momentum carries the aircraft along original path thus increasing angle of attack on both the wing and the tail.
Say direction of the relative airflow changes by 2 degrees.
Thus angle of attack of the wing increases from 4 to 6 degrees - a 50% increase.
Angle of attack on tail increases from 2 to 4 degrees..........a doubling of the angle of attack.
That increase in angle of attack of the horizontal stabilizer increases lift and thus the tail rises to restore the original situation.
Is that what you are after?
Regards,
DFC