How do rate gyros and other sensors send information to the flight control computer in an F-16? I mean is it a hardwired communication or it is done through a bus? If by bus, what is the bus called?
I have read some articles about A-Mux. Is it the bus that the gyros transmit data through? I have the same question about the actuators. How does the flight control computer send information to the actuators? By bus or hard-wired? If you have references, that will be appreciated.