Method and avionics computer for adjusting anchor point of final leg with respect to landing entry point for non-precision approach

The invention relates to a method for adjusting an anchor point of a final leg with respect to a landing entry point for non-precision approach and an avionics computer. The avionics computer includes a processing unit configured to: compare a distance between a first position and a second position,...

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Bibliographic Details
Main Authors ESSOUCY MARIE-HELENE, FOURCADE DOMINIQUE, VALIPPE OLIVIER
Format Patent
LanguageChinese
English
Published 17.05.2024
Subjects
PHYSICS
SIGNALLING
TRAFFIC CONTROL SYSTEMS
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