A method and system for managing automatic guidance of an aircraft during a complete engine failure. Said system includes means for monitoring engines so as to be able to detect a complete failure of the engines; means for detecting whether the aircraft is in flight; means for detecting whether the aircraft is in a different guidance mode from a guidance mode configured to make the aircraft descend with a reduced engine thrust and a fixed speed; and control means for automatically bringing guidance means of the aircraft into a guidance configuration compatible with the situation associated with the complete failure of the engines.
PROCEDE ET DISPOSITIF DE GESTION AUTOMATIQUE DU GUIDAGE D'UN AERONEF LORS D'UN ARRET COMPLET DES MOTEURS.
2015-12-11
Patent
Elektronische Ressource
Französisch
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