It has been a while, but as I remember it, as the stall is approached, the elevator feel shift centre position moves and its hydraulic pressure increases. This is combined with the speed trim system trimming (aircraft) nose down. The combination is meant to emulate the old fashioned "stick pusher" on older aircraft with hydraulic controls.
My guess is that the speed trim is inhibited as the stick shaker is activated (perhaps as an assumption a trim system malfunction is the reason for the high AOA), but if AOA is further increased to the point that the stall is imminent, the speed trim is reactivated to trim nose down.
Last edited by Whippersnapper; 24th October 2010 at 20:22.