That was a very long answer to a complicated question, but in a nutshell, you will get 2.5 g up until you get to the 30 degree pitch protection. Pitch protection will override the g-command (side stick demand). Also believe I misspoke slightly about rate of change vs g-load. In normal law, the airbus will ALWAYS pitch faster (due to increased g-demand) with a greater side stick deflection, *regardless of airspeed*, until another protection (in this case g-protection) intervenes. This is a function of the ELAC2 computer, and is not the conventional aerodynamics I explained in paragraph 2 of my previous post.