So...Capt Tullamraine, if you could comment, what would be the problems a pilot would face flying a "conventional" aircraft with a near zero pitch force gradient? If that was the situation for a particular C of G, mach range, for example. And for simplicity, assuming of course no auto trim, no mach trim etc.
Seems to work ok for airbus pilots.
What if the 737 auto trimmed for zero stick force?