Thales

Chris Deseure

Laurent Flotte

Guillaume Urbanski

Yannick Le Roux

Gilles Francois

François Michel

Sylvain Lissajoux

Fabien Guilley

Denis Bonnet

Xavier Chazottes

Didier Gautheron

Patrick Serrot

Sébastien Boussiron

This electronic configuration assist device of a flight of an aircraft includes:

Electronic device and method for assisting in the configuration of an aircraft flight, related computer program

Methods and systems for assisting the piloting of an aircraft are provided. The system includes at least one avionics type system and at least one non-avionics type system. The method includes steps involving receiving avionics type data associated with a flying context of the aircraft; forwarding the avionics type data to a non-avionics type system or computer; determining, in the non-avionics computer, one or more adjustment recommendations for equipment based on the received flying context and/or on predetermined data; displaying one or more recommendations. Various developments are described, in particular the conditions for requesting and/or computing recommendations (e.g. ongoing adjustment of the avionics, similar previous configuration, etc.), the selection and the categorization of recommendations, the handling of adjustment data for the avionics, etc. Software aspects are described.

Management of an aircraft

The invention relates to a method for controlling the restitution of alert(s) and/or of system(s) reconfiguration procedure(s), including the surveillance of device(s) of a vehicle and the determination of alert(s) and/or of associated reconfiguration procedure(s) to be restituted for the crew, the vehicle operating according to a mission carried out by using at least one operational capacity,

Method for controlling the restitution of alert(s) and/or system(s) reconfiguration procedure(s), related computer program product and control system

A method for processing an error when performing a predetermined avionics procedure, related computer program and detection and alert system is disclosed. In one aspect, the method is carried out automatically by the detection and alert system of an aircraft, the method including monitoring the operation of one or several avionics device(s) of the aircraft, the monitoring based on the tracking of a sequence representative of the predetermined avionics procedure being carried out. The method further includes: detecting a break of the sequence due to an incorrect command and/or skipping of at least one expected command according to the predetermined avionics procedure being performed, and retrieving at least one piece of information representative of the break in the sequence.

Method for processing an error when performing a predetermined avionics procedure, related computer program and detection and alert system

This decision aid method includes the following steps:

Method and system for pilot decision aid for the aircraft piloting and associated computer program product

A method and a device for configuring an alerts management system for an aircraft comprises: generating a list of a plurality of alerts and of resolution procedures for an aircraft; for each alert, defining: distinctive characteristics of the alert; logic for detecting the alert; at least one procedure for resolving the alert; and, for each alert, defining recording in a dedicated alerts file the set of information defined for said alert, the alerts file having a structure and a format of data that are predefined for the alerts and the procedures; determining existing links between the dedicated alerts files; and in response to the determining step, updating the content of the dedicated alerts files according to the links identified.

Method and device for configuring an alerts management system for an aircraft

A method to develop a system for management of warnings and electronic procedures for an aircraft, comprising a database of parameters relating to the warnings and to logic and procedures, the aircraft comprising ATA equipment, comprises definition and calculation of maturity criteria for development of the system, which comprises, in order: A) verification of warnings in the database with respect to predefined lists of warnings and calculation of a maturity criterion, B) if the criterion of A&#x3e;predetermined threshold, verification of the coherence of the logic for the warnings then definition and calculation of a maturity criterion, C) if the criterion of B&#x3e;predetermined threshold, verification of the existence of the procedures and, for each warning, analysis of its logic with respect to its procedure, then definition and calculation of a maturity criterion, the system being fully set up when the latter criterion&#x3e;predetermined threshold.

Growing community of inventors

Toulouse, France

Chris Deseure