A method for determining a degree of danger of an aircraft is provided. The method includes steps of: (a) obtaining a first past trajectory of the radiosonde from a time t-m to the time t to thereby allow a radiosonde position obtaining part to predict each of first predicted position candidates of the radiosonde at respective times up to the time t+k or thereby obtain each of the first predicted position candidates of the radiosonde at respective times up to the time t+k from a separate radiosonde information predicting subject, and obtaining a second past trajectory of the aircraft from a time t-n to the time t to thereby allow an aircraft position obtaining part to predict each of second predicted position candidates of the aircraft at respective times up to the time t+k or thereby obtain each of the second predicted position candidates of the aircraft at respective times up to the time t+k from a separate aircraft information predicting subject; and (b) the server (i) comparing each of the first predicted position candidates of the radiosonde at respective times up to the time t+k and each of the second predicted position candidates of the aircraft at respective times up to the time t+k, and (ii) if a specific first predicted position at a specific time is included within a first threshold range, determining or supporting another device to determine the specific second predicted position of the aircraft at the specific time to be dangerous.
METHOD FOR DETERMINING DEGREE OF DANGER OF AIRCRAFT AND SERVER USING THE SAME
VERFAHREN ZUR BESTIMMUNG DES GEFÄHRDUNGSGRADES VON FLUGZEUGEN UND SERVER DAMIT
PROCÉDÉ POUR DÉTERMINER LE DEGRÉ DE DANGER D'AÉRONEF ET SERVEUR L'UTILISANT
2023-11-15
Patent
Electronic Resource
English
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