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.
METHOD AND SYSTEM FOR DETERMINING EFFECTIVE APPROACH ANGLE AND PREDICTING AIRCRAFT LANDING DISTANCE
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
2021-04-14
Patent
Elektronische Ressource
Englisch
METHOD AND SYSTEM FOR DETERMINING EFFECTIVE APPROACH ANGLE AND PREDICTING AIRCRAFT LANDING DISTANCE
Europäisches Patentamt | 2018
|Method and system for determining effective approach angle and predicting aircraft landing distance
Europäisches Patentamt | 2019
|METHOD AND SYSTEM FOR DETERMINING EFFECTIVE APPROACH ANGLE AND PREDICTING AIRCRAFT LANDING DISTANCE
Europäisches Patentamt | 2018
|