A method of predicting a parameter for an aircraft includes detecting an actual approach profile of the aircraft. The actual approach profile includes an actual approach angle. The method also includes comparing, by a processor, the actual approach profile to a predetermined approach profile to determine a difference between the actual and predetermined approach profiles. The predetermined approach profile includes a predetermined approach angle. The method further includes determining, by the processor, an effective approach angle by combining the actual approach angle and the predetermined approach angle according to a factor that varies based on the difference between the actual and predetermined approach profiles. Moreover, the method includes determining, by the processor, the predicted parameter based on the effective approach angle.


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    Title :

    METHOD AND SYSTEM FOR DETERMINING EFFECTIVE APPROACH ANGLE AND PREDICTING AIRCRAFT LANDING DISTANCE


    Additional title:

    VERFAHREN UND SYSTEM ZUR BESTIMMUNG EINES EFFEKTIVEN ANFLUGWINKELS UND VORHERSAGE DER FLUGZEUGLANDESTRECKE
    PROCÉDÉ ET SYSTÈME POUR DÉTERMINER UN ANGLE D'APPROCHE EFFICACE ET PRÉDIRE LA DISTANCE D'ATTERRISSAGE D'UN AÉRONEF


    Contributors:
    HE GANG (author) / JOHNSON STEVE (author)

    Publication date :

    2021-04-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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