Nose Landing Gear Assembly Steering Feedback System

An aircraft, the aircraft comprising:

• a nose landing gear assembly;
• and
• a nose landing gear assembly steering feedback system, the nose landing gear assembly steering feedback system comprising:
• a static indicator;
• a rotating sensor;
• a nose wheel steering control unit, the static indicator and the rotating sensor communicatively coupled to the nose wheel steering control unit, wherein the nose wheel steering control unit is configured to:
• responsive to receiving a first input signal from the static indicator and a second input signal from the rotating sensor, determine at least one of a relative angular position, a steering direction, or a towing angle;
• and
• provide an indication of at least one of the relative angular position, the steering direction, or the towing angle to at least one of a pilot, air traffic control, or a ground crew.