alt Hacker News> Note, too, that a larger lifting body needs to bank less to execute the same turn as a craft with more loading.
This is not really helpful for passenger comfort. For a turn to be comfortable, you want the turn to be such that the effective force the passengers feel has no sideways (relative to the passengers) component, and the required roll angle is only a function of the velocity and turning radius. The aircraft design is irrelevant.
The Wikipedia article is mediocre: https://en.wikipedia.org/wiki/Coordinated_flight
Coördination stops lateral passenger movement. It does nothing for up and down. (Coördination is also about more than comfort. It keeps the flow attached to the wing. If your passengers are slipping, so is your wing.) In a roll, with a tubular fuselage, everyone—pilot and passengers—feel about the same vertical Gs. OP’s point is in a flying wing, the folks on the tips will lift up or drop down relative to the pilot and thus experience extra Gs.
My response is (a) this can be controlled in avionics and training, i.e. don’t do that, and (b) now that I think about it, vertical Gs aren’t as sickening as lateral ones.
Specify a maximum roll rate in training and normal-law software and this problem is solved