Sorry for poor pic, but I don't have a scanner and didn't wanna drive down to the UPS store.
The graphs at top are the "laws", or functions. lower right are stick pressures versus gee or roll rate.
I can do it better if anyone cares, but I would really like to see a similar graphic for the 'bus in any of the "modes" or "laws".
Note that in the upper middle we have the "standby gains" for when air data was deemed unreliable. So those values were applied to many functions for control surface movement and rates. I see no such concept/implementation for the Airbus. Why is that?
The left side of the page I used has much more detail, but I need to get a good PDF scan to show how all the functions are added/divided/integrated etc.
We didn't have all this in our operating manuals. I only have it as I was the Chief of Academics for the first training squadron and had to answer questions from the dweeb students, heh heh.
enjoy,
