I am not good in math and have zero education or training in aerodynamics, physics and engineering, I did not understand some of it.
Bottom line: just listen to what Brett says, and fly what Fitzgerald flies (or just copy it and change the shape of the rudder, move the canopy forward or back and then claim you designed it.)
If you go back and read Gialdini's write-up for his Olympic way back when in American Modeler, take note of his dumbbell drawings and discussion.
This probably isn't quite correctly written: think of how a tapered planform wing has progressively less area per each inch of span as it moves out towards the tips compared to a constant chord wing. In "upset" conditions it will roll less than a constant-chord wing simply because it has progressively less area. It's an area times moment arm (from the center-line of your fuselage) thing. You may have noted that, in general, constant chord wings fly pretty choppy in bad wind conditions. Years ago at Brodaks I watched Dr. Reuben fly his Pathfinder in bad air conditions. It was rolling, and hacking, and puking all over. The next flight was his son, Stevey, flying a Cardinal Evo. That thing came around the circle flying flat liike it was on rails. Same wind conditions. Staright chord versus tapered chord.