No CONF, I have a conception of the logic at engineering level. If you want to think of it as a physical analogy, picture a metal sheet in a G-clamp. The Normal Law protections are the G-clamp and prevent the flight surfaces from exceeding a certain position. The closer to the airframe limits the aircraft gets, the tighter the G-clamp is wound, but the protections do not directly order the flight surfaces not to exceed a given position.
Take the G-clamp away and there is no restriction.
Last edited by DozyWannabe; 10th August 2012 at 21:55.