A yaw feedback system for use by an aircraft is provided. The yaw feedback system includes a processor, a runway centerline indicator, and a yaw feedback indicator. The processor is configured to determine a yaw difference between a current track of the aircraft and a runway centerline. The runway centerline indicator is configured to virtually extend a runway visual range (RVR) for a pilot of the aircraft. The yaw feedback indicator is coupled to the processor and configured to prompt the pilot for a yaw input to compensate for the yaw difference.
AIRCRAFT PILOT DISPLAY SYSTEM AND METHOD OF USE
FLUGZEUGPILOTANZEIGESYSTEM UND VERFAHREN ZUR VERWENDUNG
SYSTÈME D'AFFICHAGE DE PILOTE D'AVION ET PROCÉDÉ D'UTILISATION
05.05.2021
Patent
Elektronische Ressource
Englisch
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