How do rate gyros and other sensors send information to the flight control computer in an F-16? 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.
The F-16 uses a MIL-STD-1553 data bus and was the first aircraft to do so.

References: 


https://www.testandmeasurementtips.com/making-measurements-mil-std-1553-connections/
https://www.aim-online.com/wp-content/uploads/2019/01/aim-ovw1553-u.pdf