Method of and system for displaying an aircraft control input

A computer-implemented method for displaying an aircraft control input, the method comprising:

• in response to an aircraft control input being inputted via a first aircraft controller, receiving a raw signal from the first aircraft controller;
• converting, by a processing unit, the raw signal from the first aircraft controller into numerical values, the numerical values being reflective of an orientation and an amplitude of the aircraft control input;
• generating, by the processing unit, a first single visual indication based on the numerical values;
• and
• causing the display of the first single visual indication on a display surface, the display of the first single visual indication providing a user viewing the first single visual indication with an understanding of the orientation and the amplitude of the aircraft control input, wherein causing the display of the first single visual indication on the display surface is in response to an event relating to the operation of an aircraft, and wherein the event comprises at least one of a detection of a change in flight mode and a dual input received from the first aircraft controller and a second aircraft controller.

A computer-implemented system for displaying an aircraft control input, the system comprising:

• a non-transitory computer-readable medium;
• a processor configured to perform:
• accessing, from the non-transitory computer-readable medium, a first indication indicative of an aircraft control input, the aircraft control input being associated with an orientation and an amplitude of the aircraft control input;
• generating, by the processor, a first single visual indication based on the first indication, the first single visual indication being reflective of the orientation and the amplitude of the aircraft control input;
• and
• causing the display of the first single visual indication on a display surface, the display of the first single visual indication providing a user viewing the first single visual indication with an understanding of the orientation and the amplitude of the aircraft control input, wherein causing the display of the first single visual indication on the display surface is in response to an event relating to the operation of an aircraft, and wherein the event comprises at least one of a detection of a change in flight mode and a dual input received from a first aircraft controller and a second aircraft controller.

A computer-implemented system for displaying an aircraft control input, the system comprising:

• a non-transitory computer-readable medium;
• a processor configured to perform:
• in response to an aircraft control input being inputted via a first aircraft controller, receiving a raw signal from the first aircraft controller;
• converting, by the processor, the raw signal from the aircraft controller into numerical values, the numerical values being reflective of an orientation and an amplitude of the aircraft control input;
• generating, by the processor, a first single visual indication based on the numerical values;
• and
• causing the display of the first single visual indication on a display surface, the display of the first single visual indication providing a user viewing the first single visual indication with an understanding of the orientation and the amplitude of the aircraft control input, wherein causing the display of the first single visual indication on the display surface is in response to an event relating to the operation of an aircraft, and wherein the event comprises at least one of a detection of a change in flight mode and a dual input received from the first aircraft controller and a second aircraft controller.