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Aviation Australia Module 11f 11.5.2.1 Avionic Systems Auto Flight
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what is this
power assisted actuator

what is this
power operated actuator
what are the 2 types of hydraulic flight control actuator
power assisted and power operated

what system is this
fly by wire
what are damping systems used for in auto flight
correct for non pilot attitude change

what is this
artificial feel
what is single channel auto pilot
control about roll only
what is multi axis audio pilot
controll about pitch,yaw,roll

what system are these components a part of
auto flight
what are the 2 loops in an autopilot channel
inner and out
what does the inner loop of an autopilot channel do
compares actual and desired attitudes
what does the outer loop of an autopilot channel do
external sensors

what is this
autopilot servo loops
what are the 4 autopilot elements
sensing, command, computer, output
what is fail passive autoland
dual AP- aircraft returns to stable condition if one fails
what is fail operational in autoland
triple AP- autoland continues if one fails

what is this
auto flight/ flight director mode select panel

what is this
flight controller

what is this
control wheel steering transducer

what is this
autopilot trim indicator

what does this button do
autopilot disengage

what is this
attitude director indicator

what is this
flight mode annunciator
what are the 3 main types of servomotor
electropneumatic, electromechanical, electrohydraulic

what is this
electropneumatic servo
what are the 2 types of electromechanical servomotor
intermittent dc motor, continuous dc motor

what is this
intermittent dc servomotor

what is this
continuous dc servomotor

what is this
AC servomotor

what is this
electrohydraulic actuator

what is this
electrohydraulic actuator for autopilot

what is this showing
need for torque limiting
what is another term for torque limiting
gain scheduling

what is this system
autopilot interlock

what mode is this autopilot in
manual

what is this showing
speed select and autothrottle engage

what is 1 indicating
autothrottle disconnect

what is 2 indicating
TOGA switch

what is this system
flight management system/ FMS
what are 3 elements of an FMS
FMC, CDU, data bus