Method and device for an optimal management of the energy of an aircraft. The device (1) includes means (5) for determining, in an iterative manner, according to a predicted energy state and according to a management strategy, optimal commands of means (S1,S2, S3, S4, S5, S6) for controlling the energy of the aircraft, which allow the aircraft to reach a given point of a trajectory in a given operational state.
PROCEDE ET DISPOSITIF DE GESTION OPTIMISEE DE L'ENERGIE D'UN AERONEF
2016-03-11
Patent
Elektronische Ressource
Französisch
Procédé et dispositif de gestion optimisée de la trajectoire verticale d'un aéronef
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