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    METHOD AND DEVICE FOR GENERATING LEARNING DATA FOR AN ARTIFICIAL INTELLIGENCE MACHINE FOR AIRCRAFT LANDING ASSISTANCE
    1.
    发明申请
    METHOD AND DEVICE FOR GENERATING LEARNING DATA FOR AN ARTIFICIAL INTELLIGENCE MACHINE FOR AIRCRAFT LANDING ASSISTANCE 有权

    公开(公告)号：US20220406040A1

    公开(公告)日：2022-12-22

    申请号：US17774807

    申请日：2020-11-03

    Applicant: THALES

    Inventor： Thierry GANILLE ,  Guillaume PABIA ,  Christian NOUVEL

    IPC: G06V10/774 ,  G06T5/50

    Abstract: A computer-implemented method for generating labeled training data for an artificial intelligence machine is provided. The method comprises at least the steps of: defining parameters for a scenario of an aircraft approaching a runway; using the parameters of the scenario in a flight simulator to generate simulated flight data, the flight simulator being configured so as to simulate the aircraft in the approach phase and an associated autopilot; using the simulated flight data in a sensor simulator to generate simulated sensor data, the sensor simulator being configured so as to simulate a forward-facing sensor on board an aircraft and able to provide sensor data representative of information of interest of a runway, the simulated sensor data that are generated being representative of information of interest of the runway; and using the simulated flight data and the simulated sensor data to generate a ground truth, the ground truth associated with the simulated sensor data forming a pair of simulated labeled training data.

    METHOD AND APPARATUS FOR UPDATING AND SHARING AN OBSTACLE DATABASE FOR AIRCRAFT
    2.
    发明申请
    METHOD AND APPARATUS FOR UPDATING AND SHARING AN OBSTACLE DATABASE FOR AIRCRAFT 有权

    公开(公告)号：US20220414083A1

    公开(公告)日：2022-12-29

    申请号：US17845943

    申请日：2022-06-21

    Applicant: THALES

    Inventor： Thierry GANILLE ,  François LEULLIER ,  Patrice COLZATO

    IPC: G06F16/23 ,  G06F16/25

    Abstract: An apparatus and a method allowing a pilot or more generally a crew to enrich a database of user obstacles directly inside the aircraft, on the ground and even during flight. Generally, the apparatus is based on a new software component, which allows new services to be provided for the functional avionic components and for the human machine interfaces HMI of the avionics. This new software component is configured to allow: user obstacles to be created, changed, deleted at the request of components of HMIs of the avionics; user obstacles to be sent to clients of the services of this new software component, which are either other functional components of the avionics or other components of HMIs of the avionics; user obstacles to be recorded to a nonvolatile memory and restored from this nonvolatile memory.

    METHOD AND SYSTEM FOR READJUSTING, VIA AN SVS SYNTHETIC VISION SYSTEM, ON A WORN HEAD-UP DISPLAY, A SYMBOLOGY WHICH PERTAINS TO THE PILOTING OF AN AIRCRAFT AND WHICH IS CONFORMAL TO THE REAL OUTSIDE WORLD
    4.
    发明申请
    METHOD AND SYSTEM FOR READJUSTING, VIA AN SVS SYNTHETIC VISION SYSTEM, ON A WORN HEAD-UP DISPLAY, A SYMBOLOGY WHICH PERTAINS TO THE PILOTING OF AN AIRCRAFT AND WHICH IS CONFORMAL TO THE REAL OUTSIDE WORLD 审中-公开

    公开(公告)号：US20190197995A1

    公开(公告)日：2019-06-27

    申请号：US16213932

    申请日：2018-12-07

    Applicant: THALES

    Inventor： Thierry GANILLE ,  Daniel MAULET ,  Olivier LEMOINE

    IPC: G09G5/38 ,  G02B27/01 ,  G01C21/16

    Abstract: A method is provided for readjusting a worn head-up display via an SVS synthetic vision system for viewing information pertaining to the piloting of an aircraft, the information being conformal with the real outside world, comprises steps consisting in: launching the readjusting method by displaying all or some of the conformal piloting information in a readjusting state, frozen on the display with respect to head movements and free with respect to the movement of the aircraft; then carrying out a series of N measurements of relative orientations {circumflex over (K)}l of the head corresponding to targeting actions Vi that superpose the various elements of piloting information displayed in the readjusting state with corresponding landmarks of the real outside world; then conjointly determining the relative orientation M01 between the display D0 and the tracking mobile element D1 and the relative orientation M3t of the inertial device D3 with respect to the Earth on the basis of a system of dual harmonization equations using the measurements {circumflex over (K)}l.

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