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.


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    Title :

    AIRCRAFT PILOT DISPLAY SYSTEM AND METHOD OF USE


    Additional title:

    FLUGZEUGPILOTANZEIGESYSTEM UND VERFAHREN ZUR VERWENDUNG
    SYSTÈME D'AFFICHAGE DE PILOTE D'AVION ET PROCÉDÉ D'UTILISATION


    Contributors:

    Publication date :

    2021-05-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS



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