When the aircraft flies at a high angle of attack the vortices leaving the tips of the canards will pass on the upper side of the wing, where they help keep the air flow attached to the wing, even if the canards are mounted in the plane of the wing. It is then also possible to deflect wing flaps somewhat further. Increasing the angle at which the air detaches from the wing and the increased flap deflection both increase the lift, allow the aircraft to fly at lower speed.
Okay, but how much lift does that create compared to a more classical high canard-low wing configuration? What are the pros and cons of same level as wing canard configuration, compared to the classical one?