Patent ID: 11869374
Assignee: AIRBUS OPERATIONS S.L.
Field: Control (Instruments)
Classification: CPC G  Y | IPC G

Claim 1:
2. The method according to claim 1, wherein said set of computation steps comprises at least the following series of steps, implemented iteratively:
a first step comprising determining, on each iteration, as a function at least of said set of predetermined rules, a plurality of states from a state selected on a preceding iteration, a selected state used in a first iteration corresponding to a state of the aircraft at said final position, said selected states being saved;
a second step comprising attributing a cost to each of the states determined in said first step; and
a third step comprising selecting, from among the states determined in said first step, a state which exhibits a lowest cost, the state thus selected being used in a first step of a next iteration, the state selected in a last iteration being used to determine the optimal flight trajectory of the aircraft.