Patent ID: 11955013
Assignee: THALES
Field: Control (Instruments)
Classification: CPC G | IPC G

Claim 15:
16. A non-transitory computer-readable medium comprising a computer program comprising software instructions which, when executed by a computer, implement a method comprising:
acquisition of a flight modality, previously selected by a user from a set of predefined flight modalities, the set of predefined flight modalities including a minimum distance flown modality, a modality for arriving at destination as soon as possible, a minimum turbulence modality, a route modality with a best network connectivity, and a modality for a minimum quantity of fuel consumed;
determination of a group of avionics functional component(s) according to the acquired flight modality, each functional component presenting an elementary score for each predefined flight modality, an overall score being calculated for each possible group of components from the elementary score or scores of the components of the said group for the acquired modality, the determined group being the one having a best overall score among the calculated overall scores,
each avionics functional component being selected from the group consisting of: a takeoff condition component, a landing condition component, a taxi management component, a passenger management component, a crew management component, a flight management component, an aircraft status component, and a takeoff procedure component; and
display of information relating to each component of the determined group of avionics functional component(s),
generation, via the determined group of avionics functional component(s), at least one change command relating to a flight phase of the aircraft, and
transmission of each generated change command to at least one corresponding avionics system, so that the generated change command is taken into account by the avionics system.