> Q. How are actuators controlled?
> A. For the aerosurface actuators, each of the four computers sends out an independent command on an independent bus. With no failures, the commands should be identical. The voting is done at the actuator using a hydraulic voting mechanism, called a force-fight voter. In it, there are four hydraulic ports called secondary ports, each commanded by one of the four GPCs. The secondary ports go into the primary ports, which are heavy-duty actuators that connect to what's called a "summing bar," which is no more than a massive steel rod. If there are three good computers and one bad one, the three good commands physically out-muscle the fourth. This limits the control authority a little bit--we don't get the total force we'd like to get, but there's still enough power to control the vehicle. If you have a large enough pressure differential for a large enough time, the port is hydraulically bypassed, which relieves the pressure in that one port. The remaining three ports then regain their full authority.
The whole article is worth a read: http://klabs.org/DEI/Processor/shuttle/shuttle_primary_compu...