Abstract: A method and system for configuring functionalities of an aircraft cockpit. The configuration system includes at least one processing unit to acquire profiles, to determine at least one combination of functionalities corresponding to the acquired profiles, based on a mapping table, and to activate at least the determined combination of functionalities. The configuration system makes it possible to adapt the functionalities of the cockpit of the aircraft to the profiles.

Abstract: A method and system for configuring functionalities of an aircraft cockpit. The configuration system includes at least one processing unit to acquire profiles, to determine at least one combination of functionalities corresponding to the acquired profiles, based on a mapping table, and to activate at least the determined combination of functionalities. The configuration system makes it possible to adapt the functionalities of the cockpit of the aircraft to the profiles.

Abstract: A system (1) including an identification unit (2) for identifying at least one actuation element to be actuated to implement a current control from a check-list, a signaling unit (3) for visually highlighting the identified actuation element, a detection unit (4) for detecting a position of a hand of a pilot, a checking unit (5) for checking whether the detected position of the hand of the pilot is consistent with the position of the identified and highlighted actuation element for the actuation thereof, an alert unit (6) for alerting the pilot to a risk of incorrect actuation, in case of absence of consistency between the detected position of the hand of the pilot and the position of the actuation element, and a recovery unit (15) for identifying, in case of incorrect actuation, at least one suggest correct actuation element.

Abstract: A system (1) including an identification unit (2) for identifying at least one actuation element to be actuated to implement a current control from a check-list, a signaling unit (3) for visually highlighting the identified actuation element, a detection unit (4) for detecting a position of a hand of a pilot, a checking unit (5) for checking whether the detected position of the hand of the pilot is consistent with the position of the identified and highlighted actuation element for the actuation thereof, an alert unit (6) for alerting the pilot to a risk of incorrect actuation, in case of absence of consistency between the detected position of the hand of the pilot and the position of the actuation element, and a recovery unit (15) for identifying, in case of incorrect actuation, at least one suggest correct actuation element.