Hi, I see it this way:
The aircraft type fly-by-ware, in the cockpit there should be 2 emergence switches placed in standby instruments area (horizon-indicator,speed indicator-altitude indicator, also their systems must be totally separate from the other system, also add and mounting 4 ° pitot tube and 4°static port)
In the unusual emergency phase of putting on 1 switch must be activated on the system of flight controls direct with protection dumping elevator and rudder, but at the same time it must overraide all computer law: the normal law, alternate law , direct law, etc..
On news airplanes fly-by-ware, in the unusual emergency, last action must be only the pilots and not the law of computer. The computers works very goodin normal operations, but they’re stupid when in terrible Cb.
I'm Sorry, I Not well writing English language.