To maintain stability and control of an aircraft

To provide guidance to the aircraft

To generate thrust for the aircraft

To control the aircraft's attitude

Ailerons

Elevators

Rudder

Flaps

To control the aircraft's roll

To control the aircraft's pitch

To control the aircraft's yaw

To control the aircraft's altitude

To control the aircraft's roll

To control the aircraft's pitch

To control the aircraft's yaw

To control the aircraft's altitude

To control the aircraft's roll

To control the aircraft's pitch

To control the aircraft's yaw

To control the aircraft's altitude

Stability refers to the aircraft's ability to return to its equilibrium state after a disturbance, while control refers to the ability to maneuver the aircraft as desired.

Stability refers to the aircraft's ability to maintain its attitude, while control refers to the ability to change its attitude.

Stability refers to the aircraft's ability to resist disturbances, while control refers to the ability to generate disturbances.

Stability refers to the aircraft's ability to fly in a straight line, while control refers to the ability to turn.

To provide information about the aircraft's state to the control system

To generate control inputs based on the desired aircraft state

To compare the actual aircraft state with the desired state and generate corrective control inputs

To stabilize the aircraft's attitude

To receive sensor data and generate control inputs

To store flight control laws and algorithms

To communicate with other aircraft systems

To monitor the health of the flight control system

To provide information about the aircraft's state to the control system

To generate control inputs based on the desired aircraft state

To compare the actual aircraft state with the desired state and generate corrective control inputs

To stabilize the aircraft's attitude

To receive control inputs from the flight control computer

To generate control forces and moments

To move the aircraft's control surfaces

To stabilize the aircraft's attitude

To generate lift and drag

To provide stability and control

To generate thrust

To control the aircraft's attitude

In an open-loop system, the control inputs are generated without feedback from the aircraft's state, while in a closed-loop system, feedback is used to adjust the control inputs.

In an open-loop system, the control inputs are generated based on a predetermined set of rules, while in a closed-loop system, the control inputs are generated based on real-time sensor data.

In an open-loop system, the control inputs are generated by a human pilot, while in a closed-loop system, the control inputs are generated by an autopilot.

In an open-loop system, the control inputs are generated by a computer, while in a closed-loop system, the control inputs are generated by a human pilot.

To adjust the aircraft's control surfaces to maintain a desired attitude without continuous pilot input

To generate control inputs to counteract disturbances

To provide stability and control to the aircraft

To move the aircraft's control surfaces

To provide inputs to the flight control system

To monitor the aircraft's state and make adjustments as needed

To communicate with air traffic control

To navigate the aircraft