A system may include a processor installed in an aircraft. The processor may be configured to: obtain (702) runway friction coefficient data and runway surface condition data for a runway; obtain (704) braking coefficient data and braking action index data; obtain (706) equivalent runway condition data and runway length data for the runway; obtain (708) aircraft speed data of the aircraft and aircraft configuration data; based at least on the runway friction coefficient data (710), the runway surface condition data, the braking coefficient data, the braking action index data, the equivalent runway condition data, the aircraft speed data, and the aircraft configuration data, determine a rejected takeoff (RTO) initiating point (RIP) and a start automated RTO sequence point; and cause (712) an automated RTO sequence to be performed if the start automated RTO sequence point is reached without the automated RTO sequence being manually overridden.


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    Title :

    REJECTED TAKEOFF AIRCRAFT SYSTEM AND METHOD


    Additional title:

    SYSTEM UND VERFAHREN FÜR FLUGZEUGSTARTABBRUCH
    SYSTÈME ET PROCÉDÉ D'AÉRONEF À DÉCOLLAGE REJETÉ


    Contributors:

    Publication date :

    2022-06-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS



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