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AssigneeAirbus France
InventorsVincent Foucart, Eric Albert, Simon Innocent
Estimating the term…
Method and system for aiding the piloting of an aircraft, during a maneuver bringing about an increase in the attitude of the aircraft. The system (1) comprises a set (2) of information sources, determining at least one current attitude of the aircraft, a first means (11) for transmitting a first value of attitude which preferably corresponds to the minimum value between, on the one hand, an optimal value of attitude at the end of the maneuver and, on the other hand, a value of attitude of protection against a rear collision, a second means (12) for determining an attitude deviation, by subtracting the first value of attitude from the current attitude, and a head-up display device (5) which is able to present, on a display screen (7), superimposed with the environment, at least one horizon line and a first means of indication which indicates said attitude deviation.
A method of aiding the piloting of an aircraft during a maneuver bringing about an increase in the attitude of the aircraft, according to which method the following steps are carried out automatically and repeatedly:
A system for aiding piloting for an aircraft, said system (1) comprising:
Dependencies are inferred from the claim text.