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公开(公告)号：US11762837B2
公开(公告)日：2023-09-19
申请号：US17845943
申请日：2022-06-21
Applicant: THALES
Inventor： Thierry Ganille , François Leullier , Patrice Colzato
CPC classification number: G06F16/2358 , G06F16/252
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.
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公开(公告)号：US12217330B2
公开(公告)日：2025-02-04
申请号：US17774807
申请日：2020-11-03
Applicant: THALES
Inventor： Thierry Ganille , Guillaume Pabia , Christian Nouvel
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.
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公开(公告)号：US11789927B2
公开(公告)日：2023-10-17
申请号：US16935960
申请日：2020-07-22
Applicant: THALES
Inventor： Thierry Ganille , Pierre-Yves Dumas , Philippe Gaultier
CPC classification number: G06F16/2365 , B64D45/04 , G01S19/15 , G06F16/29
Abstract: The invention relates to a method for validating at least one position stored in a database of an aircraft comprising a satellite positioning system, the database containing at least one radionavigation beacon position, a runway threshold position, and a displaced runway threshold position on a runway, on which the aircraft is intended to land, the validation of said at least one position comprising a consistency check between at least:
a signal received by the aircraft from a radionavigation beacon associated with said at least one position, and
the position of the aircraft provided by the satellite positioning system, and
the value of the position stored in the database.-
公开(公告)号：US20210150923A1
公开(公告)日：2021-05-20
申请号：US16952975
申请日：2020-11-19
Applicant: THALES
Inventor： Thomas RIPOCHE , Thierry Ganille , Pierre-Yves Dumas
Abstract: Electronic device for estimating a position of an air traffic element intended to be carried on board an aircraft, and comprising a module for acquiring a measured position of the air traffic element and complementary measured navigation information of the air traffic element; and a module for calculating an estimated position of the air traffic element.
The calculation module is configured to calculate the estimated position of the air traffic element as a function of the measured position and of the complementary measured navigation information acquired for the air traffic element.
The complementary measured navigation information is preferably a measured position of the complementary air traffic element, or a set of at least two measured positions of the complementary air traffic element, or even a measured speed of the air traffic element.-
公开(公告)号：US20210026836A1
公开(公告)日：2021-01-28
申请号：US16935960
申请日：2020-07-22
Applicant: THALES
Inventor： Thierry Ganille , Pierre-Yves Dumas , Philippe Gaultier
Abstract: The invention relates to a method for validating at least one position stored in a database of an aircraft comprising a satellite positioning system, the database containing at least one radionavigation beacon position, a runway threshold position, and a displaced runway threshold position on a runway, on which the aircraft is intended to land, the validation of said at least one position comprising a consistency check between at least: a signal received by the aircraft from a radionavigation beacon associated with said at least one position, and the position of the aircraft provided by the satellite positioning system, and the value of the position stored in the database.
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Patent Agency Ranking
公开(公告)号：US11651302B2
公开(公告)日：2023-05-16
申请号：US17027629
申请日：2020-09-21
Applicant: THALES
Inventor： Thierry Ganille , Guillaume Pabia
CPC classification number: G06Q10/04 , G05D1/0088 , G05D1/101 , G06F18/214 , G06F18/217 , G06F30/27 , G06N3/04 , G06N20/00
Abstract: A computer-implemented method for generating synthetic training data for an artificial-intelligence machine, the method includes at least steps of: defining parameters for at least one approach scenario of an aircraft approaching a runway; using the parameters of the at least one scenario in a flight simulator to generate simulated flight data, the flight simulator being configured to simulate the aircraft in the phase of approach toward the runway and to simulate an associated automatic pilot; using the simulated flight data to generate a plurality of ground-truth images, the ground-truth images corresponding to various visibility conditions; and generating, from each ground-truth image, a plurality of simulated sensor images.
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公开(公告)号：US11629976B2
公开(公告)日：2023-04-18
申请号：US16706484
申请日：2019-12-06
Applicant: THALES
Inventor： Thierry Ganille , Florent Mennechet , Xavier Servantie
Abstract: A method for guidance and for assisting in following a trajectory for velocity-vector piloting of an aircraft includes a step of calculating, at all times, lateral and vertical offsets of the current position of the aircraft from a target trajectory, estimated by a flight management system, and then a joining heading and a joining gradient for the aircraft to join the trajectory depending on these offsets; and a following fourth step of displaying, in head-up or head-down form, a consistent guidance symbol centered on the calculated joining heading and the calculated joining gradient for joining the trajectory, on a piloting screen showing a velocity vector. The fourth step may display, in addition to the guidance symbol, one or more items of information anticipating the next trajectory break.
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公开(公告)号：US11237573B2
公开(公告)日：2022-02-01
申请号：US16430127
申请日：2019-06-03
Applicant: THALES
Inventor： Thierry Ganille , Emmanuel Monvoisin , Alexandre Fine , Pierre Mariani , Hélène Misson
Abstract: The invention relates to a method for securing the operation of a synthetic viewing system of an aircraft. This method comprises the steps of determining at least one control object in the field of view of the synthetic vision system and determining at least one control point belonging to each control object and verifying the consistency of the display of the synthetic vision system. The verification step comprises the sub-steps of recovering a first position corresponding to the displayed position of each control point on the corresponding outline on the display of the synthetic vision system, determining a second position of each control point on the display of the synthetic vision system and comparing the first and second positions.
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公开(公告)号：US10802276B2
公开(公告)日：2020-10-13
申请号：US16140131
申请日：2018-09-24
Applicant: Thales
Inventor： Pierre-Yves Dumas , Thierry Ganille , Bruno Aymeric
Abstract: The invention relates to a display system included in a device for traveling a path between at least two distinct points and for using at least one heading datum, wherein the display system comprises at least: an image sensor configured to acquire environmental images during the path traveled by the device; an image processing module capable of determining the drift of the device in real time; a module for determining information that is representative of the route taken by the device, a module for real-time determination of the true heading followed by the device from the information that is representative of the route and the drift of the device, a module for returning to the user information that is representative of the true heading.
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10.发明授权公开(公告)号：US10249094B2
公开(公告)日：2019-04-02
申请号：US15469555
申请日：2017-03-26
Applicant: THALES
Inventor： Thierry Ganille , Bruno Aymeric , Johanna Lux
IPC: G06T19/00 , G01S17/89 , G02B27/01 , G06T15/20 , H04N7/18 , G01C23/00 , G06K9/00 , G08G5/00 , G08G5/02 , G01S7/24 , G01S13/89 , G01S13/91 , G01S13/94 , B64D45/08 , H04N5/33
Abstract: A method of synthetic representation of elements of interest in a viewing system for aircraft, the viewing system comprises location sensors, a cartographic database and a database of elements of interest, an image sensor, a unit for processing images and a unit for generating three-dimensional digital images representative of the terrain overflown and a viewing device, wherein, when the terrain overflown comprises an element of interest, the method of synthetic representation comprises: a first step of searching for and detecting the element of interest in each image of a sequence of images, and; a second step of generating three-dimensional digital images representative of the terrain overflown, the element of interest represented according to a first representation if it has not been detected in any of the images of the sequence of images and according to a second representation if it is detected.
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