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
2016-11-24
Patent
Elektronische Ressource
Englisch
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