Fly by wire aircraft
Hello again everybody, I am curently studying aerospace engineering at college, I have 2 fly by wire questions that although are general aircraft questions, I think particular relate to the A320. I was hoping an experianced A320 engineer could give me some guidance;
Q1) In a full time fly by wire equipped aircraft, pitch and roll servo jack position is achieved utilising:-
a) Linear variable differential transducers, thus ensuring full interchangeable components
b) Rotary variable differential transducers for roll and linear variable transducers for pitch
c) Rotary variable differential transducers for pitch and linear variable transducers for roll
Q2) In a full time fly by wire aircraft, Autopilot signals from the flight management guidance computer are :-
a) Used to control the flight control surfaces via the autopilot electrical actuator
b) Integrated into the electrical flight control system via the two electrical flight control computers
c) Fed directly to each flight control surface servojack not being utilised by the electrical flight control computers
Thankyou for your help.