A system and method for determining a lateral and vertical path for aircraft guidance from a current aircraft position to a landing runway following a complete loss of engine thrust includes determining, in a processing system, a final approach segment, a deceleration segment, and a driftdown segment. Connecting, in the processing system, the driftdown segment to the deceleration segment, and the deceleration segment to the final approach segment, to form a complete lateral and vertical path from the current aircraft position to the landing runway. And rendering, on a display device, a graphical representation of the complete lateral and vertical path from the current aircraft position to the landing runway, wherein the graphical representation of the complete lateral and vertical path updates as the aircraft travels.


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    Titel :

    SYSTEM AND METHOD FOR AIRCRAFT GUIDANCE TO RUNWAY IN CASE OF COMPLETE LOSS OF ENGINE THRUST


    Weitere Titelangaben:

    SYSTEM UND VERFAHREN ZUR FLUGZEUGFÜHRUNG ZUR LANDEBAHN BEI VOLLSTÄNDIGEM TRIEBWERKSSCHUBVERLUST
    SYSTÈME ET PROCÉDÉ DE GUIDAGE VERS UNE PISTE D'ATTERRISSAGE EN CAS DE PERTE COMPLÈTE DE POUSSÉE MOTEUR


    Beteiligte:
    GLOMSKI BILL E (Autor:in) / BOUANANI ADIB (Autor:in) / SEUSS RAYMOND (Autor:in) / LAMMERS DOMINIC (Autor:in) / SLOTTER THOMAS (Autor:in)

    Erscheinungsdatum :

    06.12.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / 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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