The present invention relates to a method of precision guidance to the approaching and landing aircraft such as helicopters, aircraft and the like, which comprises at least the step of using a GPS position data transmitted by the aircraft to identify the alignment/misalignment of the aircraft with respect to the desired path and a step of receive a signal indicative of the alignment/misalignment of the aircraft with respect to the path; further object of the invention is also a system for the implementation of said method.
Precision guidance method and system for aircraft approaching and landing
Präzisionsführungsverfahren und System für Flugzeugstart und -landung
Procédé et système de guidage de précision pour approche et atterrissage d'aéronef
2015-07-15
Patent
Electronic Resource
English
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