Which component adjusts flight control trim based on pilot inputs?

Which component adjusts flight control trim based on pilot inputs?

• A. Outer loop
• B. Inner loop
• C. Electronic stabilizer
• D. Mechanical actuator

Answer: (A)

The outer loop is responsible for making adjustments to the flight control trim based on pilot inputs. In a flight control system, the outer loop typically processes the broader aspects of aircraft control, such as altitude and heading adjustments. When a pilot makes inputs, such as adjusting the control yoke or stick to change the aircraft's attitude or flight path, the outer loop interprets these commands and adjusts the trim accordingly to maintain optimal control and stability. This means that as the pilot inputs commands, the outer loop dynamically manages the trim settings to ensure that the aircraft remains in a desired flight condition with minimal input effort from the pilot. This functionality is essential for enhancing pilot workload management, ensuring that the aircraft responds effectively to commands while maintaining stability and efficiency during flight. The inner loop, in contrast, focuses more closely on smaller, immediate adjustments required for maintaining stability and handling characteristics in response to disturbances. The electronic stabilizer might work alongside the flight control system, but it doesn't directly adjust the trim based on pilot inputs in the manner that the outer loop does. Mechanical actuators are the physical components that implement the adjustments, but they act in response to the commands processed by the outer loop rather than initiating actions based on pilot input alone.

The outer loop is responsible for making adjustments to the flight control trim based on pilot inputs. In a flight control system, the outer loop typically processes the broader aspects of aircraft control, such as altitude and heading adjustments. When a pilot makes inputs, such as adjusting the control yoke or stick to change the aircraft's attitude or flight path, the outer loop interprets these commands and adjusts the trim accordingly to maintain optimal control and stability.

This means that as the pilot inputs commands, the outer loop dynamically manages the trim settings to ensure that the aircraft remains in a desired flight condition with minimal input effort from the pilot. This functionality is essential for enhancing pilot workload management, ensuring that the aircraft responds effectively to commands while maintaining stability and efficiency during flight.

The inner loop, in contrast, focuses more closely on smaller, immediate adjustments required for maintaining stability and handling characteristics in response to disturbances. The electronic stabilizer might work alongside the flight control system, but it doesn't directly adjust the trim based on pilot inputs in the manner that the outer loop does. Mechanical actuators are the physical components that implement the adjustments, but they act in response to the commands processed by the outer loop rather than initiating actions based on pilot input alone.