In one example, a method to guide and navigate the aircraft during a complete engine failure is disclosed. Nearby airport data is obtained based on aircraft current location upon detecting the complete aircraft engine failure. Minimum and maximum glide distances of the aircraft are computed based on the current aircraft state parameters and environmental parameters. Candidate reachable airports are determined using the obtained nearby airport data for safe landing based on the computed minimum and maximum glide distances. A glide path for each candidate reachable airport is determined. The aircraft is navigated and guided to a selected one of the candidate reachable airports using an associated glide path.
NAVIGATING AND GUIDING AN AIRCRAFT TO A REACHABLE AIRPORT DURING COMPLETE ENGINE FAILURE
2017-06-08
Patent
Elektronische Ressource
Englisch
IPC: | G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS |
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