[justsid]

It litereally means two completely different architectures, on two physically disconnected computers. Here is a diagram: https://i.imgur.com/Tj0GKbQ.png

Also visible in the diagram is that each side has its own watchdog, both connected to each other. The way this whole thing work is fail safe, so if one computer fails the backup can jump in, and if that fails too the flight controls will either retract or stop in their current position depending on what makes the most sense. It’s also mirrored, so for example if spoiler 2 on the right wing fails and is retracted, spoiler 2 on the left wing will also retract.

Here is a description about the flight controls and how pilot input gets passed through to the control surfaces: http://www.smartcockpit.com/docs/A320-Flight_Controls.pdf

And here is a general overview about the architecture: http://www.skybrary.aero/bookshelf/books/2313.pdf

[i336_]

Oh, wow, that's amazing. Now I understand why avionics are so expensive - verifying the correctness of such a system sounds like a lot of "fun," or at least a lot of time.

(I wonder if there are any systems built on multiple architectures where each unit is itself a redundant system with CPUs in lockstep.....)

Am I to intuit from this diagram that the watchdog watches all the components - power, I/O, memory, and CPU? That's very impressive. Or does it watch a central bus/backplane everything is connected to?

Also, how does either side decide/figure out the other side has failed? Simply deciding that the other half is wrong if it doesn't match this half's output could fail catastrophically if one of the sides reaches this conclusion after entering an invalid state (ie, it's the other side that is correct, and this side is wrong).

I'm also mildly curious as to why the I/O on one side has two connections to the actuators, while the other has only one.