A method for processing data generated by an event management device determining mission adaptation suggestions from current or future mission data sources, the method comprising the following steps of: receiving at least one suggestion comprising an item of information and a datum related to its construction; generating a notification for each received suggestion; storing the notification in a notifications memory. The method further comprises at least one iteration of the following steps: applying a classification operation to the notification; applying processing to the notification as a function of the classification operation, the processing comprising a step of rendering the notification on a Human-Machine interface in response to a display condition, the rendering using a display form and display dynamics.
BOARD OF TRUSTEES OF MICHIGAN STATE UNIVERSITY (USA)
INRIA INSTITUT NATIONAL DE RECHERCHE EN INFORMATIQUE ET EN AUTOMATIQUE (France)
Inventeur(s)
Anghelone, David
Faure, Philippe
Chen, Cunjian
Ross, Arun
Dantcheva, Antitza
Abrégé
Provided is a cross-spectral face recognition learning method based on a set of associated face images, a thermal image and a visual image, of a plurality of persons. The thermal image is coded in two different ways. A style encoder provides a style code of the thermal image. An identity encoder provides an identity code of the thermal image. The visual image is coded in a similar way with a style encoder providing a style code and with an identity encoder providing an identity code. The two face images of the same person share in the identity features a common part in the respective identity codes, noted as common identity code, whereas the style codes for the two images comprise features only relevant two the specific style, i.e. either thermal or visual, of the image. Other embodiments disclosed.
H04N 23/11 - Caméras ou modules de caméras comprenant des capteurs d'images électroniquesLeur commande pour générer des signaux d'image à partir de différentes longueurs d'onde pour générer des signaux d'image à partir de longueurs d'onde de lumière visible et infrarouge
H04N 23/23 - Caméras ou modules de caméras comprenant des capteurs d'images électroniquesLeur commande pour générer des signaux d'image uniquement à partir d'un rayonnement infrarouge à partir du rayonnement infrarouge thermique
BOARD OF TRUSTEES OF MICHIGAN STATE UNIVERSITY (USA)
INRIA (France)
Inventeur(s)
Anghelone, David
Faure, Philippe
Chen, Cunjian
Dantcheva, Antitza
Strizhkova, Valeriya
Abrégé
Provided is a thermal face and landmark detection method for providing a ground truth reference database, capturing a thermal image comprising at least one face, detecting a face in the thermal image, cropping the thermal image creating a cropped face thermal image, applying a Gaussian filters method to the cropped face thermal image creating an improved cropped face thermal image and applying a landmark detector to the improved cropped face thermal image creating an landmarked cropped face thermal image. Other embodiments disclosed.
An optical window including on its surface two electrodes connected to a voltage generator in which at least one of the electrodes is a doped diamond electrode, the diamond being doped with an element that makes the diamond conductive.
H01B 1/06 - Conducteurs ou corps conducteurs caractérisés par les matériaux conducteurs utilisésEmploi de matériaux spécifiés comme conducteurs composés principalement d'autres substances non métalliques
G01P 5/26 - Mesure de la vitesse des fluides, p. ex. d'un courant atmosphériqueMesure de la vitesse de corps, p. ex. navires, aéronefs, par rapport à des fluides en mesurant l'influence directe du courant de fluide sur les propriétés d'une onde optique de détection
5.
METHOD FOR MANAGING ACCESS BY A THREAD TO A SLAVE DEVICE
The present disclosure relates to a data processing system comprising a bus interconnect structure, a slave device coupled to the bus interconnect structure, a slave protection unit coupled to the bus interconnect structure, a plurality of master devices coupled to the bus interconnect structure, each master device of said plurality of master devices having a master identifier, wherein a master device is configured to run concurrently different threads, and, when a thread run by said master device requests access to said slave device, for issuing on the bus interconnect structure an access request comprising its master identifier and a thread identifier assigned to said thread.
A sight for a shooting system, including a transparent screen able to display an image, and a catadioptric optical device able to collimate an incident light beam coming from the image displayed on the transparent screen into a sighting window superimposed on the direct view of a scene.
An airborne measurement system borne by an aircraft, and comprising a plurality of conventional navigational-aid sensors generating data referred to as conventional data, at least one SPAD camera comprising a single-photon avalanche diode matrix-array detector and generating SPAD data comprising a first image and a second image of a scene to be observed, the system comprising a processing unit connected to the conventional sensors and to the at least one SPAD camera, the processing unit being adapted to: choose, in accordance with a predetermined criterion and on the basis of the conventional data and/or of the SPAD data, a use of the conventional data which is referred to as the conventional mode, or a use of the SPAD data, and possibly comprising conventional data, which is referred to as the SPAD mode, and for the conventional mode, generate measurement information referred to as conventional information on the basis of conventional data, for the SPAD mode: determine, on the basis of the first image and of the second image, an error band for the measurement of the horizontal position of the aircraft, called the protection radius, generate measurement information referred to as reinforced information on the basis of at least SPAD data.
G01C 21/00 - NavigationInstruments de navigation non prévus dans les groupes
G06T 7/521 - Récupération de la profondeur ou de la forme à partir de la télémétrie laser, p. ex. par interférométrieRécupération de la profondeur ou de la forme à partir de la projection de lumière structurée
G06T 7/55 - Récupération de la profondeur ou de la forme à partir de plusieurs images
8.
ACCELEROMETER-TYPE BIAS CORRECTION ULTRACOLD ATOM SENSOR
An accelerometer-type interferometric ultracold atom inertial sensor including an atom chip including at least one set of a first and a second elementary sensor; an atom generation device; a generator for generating a uniform magnetic field; a power supply device; with the arrangement of the group of one or more conductive elements of each sensor and the sequence being further configured so that the trajectories associated with the first elementary sensor and the trajectories associated with the second elementary sensor are parallel to each other, are of the same length, are covered simultaneously and so that the departure direction of the first clouds, from the first and the second elementary sensor respectively, are opposite; the sensor further comprising a detection system.
G01C 19/64 - Gyromètres utilisant l'effet Sagnac, c.-à-d. des décalages induits par rotation de faisceaux électromagnétiques dans des directions opposées
9.
COLD-ATOM SENSOR OF GYROMETER TYPE WITH BIAS CORRECTED
An interferometric inertial ultracold-atom sensor of gyrometer type, including an atom chip comprising at least one set of a first and second elementary sensor, a power-supplying device, the magnetic-field generator and the power-supplying device being configured to apply the magnetic field, the DC currents and the microwave signals in a predetermined sequence, the arrangement of the group of one or more conductive elements of each sensor and the sequence further being configured so that the path associated with the first elementary sensor and the path associated with the second elementary sensor are identical and traced simultaneously and in inverse directions by the clouds of ultracold atoms associated with a given internal state, the sensor further comprising a detecting system.
G01C 19/64 - Gyromètres utilisant l'effet Sagnac, c.-à-d. des décalages induits par rotation de faisceaux électromagnétiques dans des directions opposées
10.
Platform for execution of avionic applications, and associated method and computer program
A platform for executing avionics applications including a shared memory space, a plurality of avionics partitions and an IOTC server for access to shared resources. The shared memory space is configured to perform any data sharing between a producer partition and a predetermined group of N data consuming partitions exclusively via a data sharing structure allocated in the shared memory space. The data sharing structure includes at least two saving addresses which may be used by the data producing partition for writing two different data.
The present invention relates to a method for manufacturing a system in package having several layers, including for each current layer realization of a dielectric substrate by an additive manufacturing technique, deposition of an adhesive in receiving zones, deposition of electronic components in the corresponding receiving zones, deposition of interconnection elements between the electronic components, creation of at least one interconnection with an adjacent layer, encapsulation of the current layer with filler material, the filler material forming an outer surface, and preparation of the outer surface for receiving the next layer.
H01L 23/538 - Dispositions pour conduire le courant électrique à l'intérieur du dispositif pendant son fonctionnement, d'un composant à un autre la structure d'interconnexion entre une pluralité de puces semi-conductrices se trouvant au-dessus ou à l'intérieur de substrats isolants
H01L 21/02 - Fabrication ou traitement des dispositifs à semi-conducteurs ou de leurs parties constitutives
H01L 23/00 - Détails de dispositifs à semi-conducteurs ou d'autres dispositifs à l'état solide
H01L 23/29 - Encapsulations, p. ex. couches d’encapsulation, revêtements caractérisées par le matériau
H01L 23/36 - Emploi de matériaux spécifiés ou mise en forme, en vue de faciliter le refroidissement ou le chauffage, p. ex. dissipateurs de chaleur
H01L 25/10 - Ensembles consistant en une pluralité de dispositifs à semi-conducteurs ou d'autres dispositifs à l'état solide les dispositifs étant tous d'un type prévu dans une seule des sous-classes , , , , ou , p. ex. ensembles de diodes redresseuses les dispositifs ayant des conteneurs séparés
12.
ELECTRONIC DISPLAY DEVICE OF EMISSIVE PIXEL SCREEN TYPE, FOR AN AIRCRAFT COCKPIT
A screen based on emissive pixels for an aircraft cockpit, including a flat substrate bearing a plurality of electroluminescent diodes in the same emission spectrum and wherein each pixel is made up of at least one compact group of several of the electroluminescent diodes. In a pixel of the screen, the electroluminescent diodes of one of the groups are covered with a layer forming a cover common to the electroluminescent diodes of the group and relaying a diffuse light, with or without photoluminescence, in response to the emission of light by the electroluminescent diodes of the group.
H01L 25/075 - Ensembles consistant en une pluralité de dispositifs à semi-conducteurs ou d'autres dispositifs à l'état solide les dispositifs étant tous d'un type prévu dans une seule des sous-classes , , , , ou , p. ex. ensembles de diodes redresseuses les dispositifs n'ayant pas de conteneurs séparés les dispositifs étant d'un type prévu dans le groupe
H01L 33/32 - Matériaux de la région électroluminescente contenant uniquement des éléments du groupe III et du groupe V de la classification périodique contenant de l'azote
H01L 33/50 - DISPOSITIFS À SEMI-CONDUCTEURS NON COUVERTS PAR LA CLASSE - Détails caractérisés par les éléments du boîtier des corps semi-conducteurs Éléments de conversion de la longueur d'onde
A display system in an aircraft cockpit, including a plurality of display surfaces, a processing module configured to host applications capable of generating images to be displayed on one or more display surfaces, a graphic generation module configured to generate a composite graphic flow including images from one or more applications and intended to be displayed on different display surfaces, wherein each display surface is configured to receive the composite graphic flow and to extract images for display on that display surface.
A satellite platform includes an array of N antennas (Ai, i=1 to 6) and a beamformer, each antenna comprising the satellite casing and a respective metal strand (i=1 to 6) extending in the plane of the Earth face of the satellite, such that if N>2, the axis of the nth strand on the Earth face of the satellite is obtained by rotation of +2π/N, n=2 to N, of the axis of the (n-1)th strand; the beamformer calculates, as a function of a target directivity and polarization to be implemented by the antenna array, an attenuation and a phase-shift selectively for each antenna and applies, to the electrical signal intended for each antenna, the attenuation and phase-shift calculated for the antenna and delivers the duly adapted signal to the antenna to the associated connector.
H01Q 21/26 - Antennes tourniquet ou similaires comportant des dispositions de trois éléments ou plus allongés disposés radialement et symétriquement dans un plan horizontal par rapport à un centre commun
H01Q 1/28 - Adaptation pour l'utilisation dans ou sur les avions, les missiles, les satellites ou les ballons
H01Q 3/34 - Dispositifs pour changer ou faire varier l'orientation ou la forme du diagramme de directivité des ondes rayonnées par une antenne ou un système d'antenne faisant varier la phase relative ou l’amplitude relative et l’énergie d’excitation entre plusieurs éléments rayonnants actifsDispositifs pour changer ou faire varier l'orientation ou la forme du diagramme de directivité des ondes rayonnées par une antenne ou un système d'antenne faisant varier la distribution de l’énergie à travers une ouverture rayonnante faisant varier la phase par des moyens électriques
H01Q 21/24 - Combinaisons d'unités d'antennes polarisées dans des directions différentes pour émettre ou recevoir des ondes polarisées circulairement ou elliptiquement ou des ondes polarisées linéairement dans n'importe quelle direction
15.
Aircraft piloting assistance method, and associated electronic piloting assistance device and assistance system
A method for assisting the piloting of an aircraft, including acquiring an aircraft piloting model and a reward function including a piloting constraint, and application, to the piloting model, of a reinforcement learning algorithm to obtain state variables and piloting commands. The method also includes formation of data group(s) from the state variables and the commands. For the or each group, the method includes assignment of at least one aircraft state to the state variables and at least one piloting action to the commands, to generate a piloting rule including the state(s) and piloting action(s). The method also includes transmission of at least one piloting rule to a display device for display to a pilot of the aircraft.
An interaction system in the cockpit of an aircraft for controlling at least one avionics system with setting values, including a setting medium configured to generate a setting signal corresponding to a setting value selected by an operator following a first action, and a validation signal corresponding to a validation of the selected setting value following a second action, a display module configured to display the selected setting value and to generate a feedback signal including a graphic signature of the displayed setting value, and a processing module configured to receive each feedback signal and each validation signal, to detect each modification in the setting value and to verify that each detected modification corresponds to a validation signal.
A display device including elementary components for composing an image. Each component is made up of a compact assembly of light-emitting diodes, one group of diodes comprising a red diode and one or more other diodes which together have an emission spectrum comprising, during nominal operation, less red than that of the red diode, the group carrying out with the other elementary components a colour display for an operator to the naked eye. The assembly further comprises an additional diode which has, during nominal operation, with respect to the red diode, a wavelength that is less close to red, and with respect to the common spectrum a supplementary emission spectrum, for a colour display compatible with the use by an operator and in the vicinity of the display device of a night-vision tool sensitive to the near-infrared.
G09G 3/32 - Dispositions ou circuits de commande présentant un intérêt uniquement pour l'affichage utilisant des moyens de visualisation autres que les tubes à rayons cathodiques pour la présentation d'un ensemble de plusieurs caractères, p. ex. d'une page, en composant l'ensemble par combinaison d'éléments individuels disposés en matrice utilisant des sources lumineuses commandées utilisant des panneaux électroluminescents semi-conducteurs, p. ex. utilisant des diodes électroluminescentes [LED]
H01L 25/075 - Ensembles consistant en une pluralité de dispositifs à semi-conducteurs ou d'autres dispositifs à l'état solide les dispositifs étant tous d'un type prévu dans une seule des sous-classes , , , , ou , p. ex. ensembles de diodes redresseuses les dispositifs n'ayant pas de conteneurs séparés les dispositifs étant d'un type prévu dans le groupe
H01L 33/50 - DISPOSITIFS À SEMI-CONDUCTEURS NON COUVERTS PAR LA CLASSE - Détails caractérisés par les éléments du boîtier des corps semi-conducteurs Éléments de conversion de la longueur d'onde
H04N 5/33 - Transformation des rayonnements infrarouges
A digital radio altimeter validation system, provided with an input/output RF interface and characterized by an incompressible latency τ, configured to receive a linear chirp (FMCW) signal s(t) with linearly frequency-modulated continuous-wave f(t)=αt+β and with quadratic phase s(t)=e2jπ(αt2/2+βt+γ), that can also be written in complex form in cartesian coordinates I(t)+jQ(t), t representing the time, and configured to retransmit it according to a configurable delay and deliver to the radio altimeter a signal I′(t)+jQ′(t) that is exactly frequency-compensated for the latency τ by a linear extrapolation of its phase by calculation of difference between the current phase and the digitally delayed phase of the value to be compensated τ.
A method for assisting the guidance of a surface vessel intended to tow an underwater device, the method includes a) discretizing the geographical sector around the surface vessel into a plurality of zones, with each zone being classified according to a degree of accessibility from among a set of degrees of accessibility; b) computing a set of candidate trajectories of the surface vessel in the geographical sector, with each candidate trajectory corresponding to a different gyration rate from the current position of the surface vessel; c) classifying each candidate trajectory as a function of the degree of accessibility of the zone of the geographical sector traversed by the possible trajectory, and as a function of the feasibility of one or more predefined actions on the candidate trajectory; d) generating a display of the zones and of the candidate trajectories on a human-machine interface, as a function of their classification and/or a transmission of instructions relating to the actions.
B63B 49/00 - Aménagements relatifs aux instruments nautiques ou d'aide à la navigation
B63B 21/66 - Équipements spécialement adaptés au remorquage sous l'eau des objets ou des navires, p. ex. carénages hydrodynamiques pour câbles de remorquage
B63G 8/00 - Navires submersibles, p. ex. sous-marins
B63G 8/39 - Disposition des instruments de veille sonique, p. ex. basse fréquence, sonar
A system for maneuvering a marine craft, the system being intended to be placed at the edge of a ship, the system comprising a ramp positioned on the ship, the ramp comprising a first end, a carriage designed to move along the ramp, a fender body connected to the carriage and designed to press against the ramp, the fender body being able to rotate with respect to the carriage. The system comprising at least one fender arm comprising a second device for attachment to the marine craft, the fender arm being able to rotate through a limited angular range with respect to the fender body.
B63B 27/14 - Aménagement des équipements de bord pour l'embarquement ou le débarquement des cargaisons ou des passagers des rampes, coupées ou échelles extérieures
B63B 27/08 - Aménagement des équipements de bord pour l'embarquement ou le débarquement des cargaisons ou des passagers des treuils
B63B 27/16 - Aménagement des équipements de bord pour l'embarquement ou le débarquement des cargaisons ou des passagers des ascenseurs ou appareils de levage
21.
METHOD TO STORE DATA PERSISTENTLY BY A SOFTWARE PAYLOAD
A method to store data persistently by a payload of an owner, the method including establishing a secure channel between the owner and the software payload itself when running into a hardware-based trusted executed environment, HW TEE, at the instance of a cloud service provider; generating, by the owner, a payload identifier using information shared from the payload during the establishment of the secure channel; generating, by the owner, a key initiator and persistently storing at the owner side the key initiator associated to the payload identifier; sending, by the owner, the payload identifier and the key initiator to the payload; using the key initiator, by the payload, to encrypt data; and persistently storing, by the payload, the encrypted data and the payload identifier.
G06F 21/53 - Contrôle des utilisateurs, des programmes ou des dispositifs de préservation de l’intégrité des plates-formes, p. ex. des processeurs, des micrologiciels ou des systèmes d’exploitation au stade de l’exécution du programme, p. ex. intégrité de la pile, débordement de tampon ou prévention d'effacement involontaire de données par exécution dans un environnement restreint, p. ex. "boîte à sable" ou machine virtuelle sécurisée
A flight management system of an aircraft includes a first non-critical or open world module for creating an enhanced enriched flight plan, the first module being configured to create the enhanced enriched flight plan iteratively by the following steps: initialisation of pseudo-constraints; and iterative enhancement of the choice of pseudo-constraints, until an objective of enhancement or of absence of enhancement with respect to the last best choice of pseudo-constraints is reached, based on at least one optimisation criterion and on at least one parameter representative of the environment of the flight of the aircraft; the second critical or flight management avionics module certified to calculate a path, comprising at least one critical computer and/or at least one critical piece of software for calculating and delivering as output a secured path, based on the enhanced enriched flight plan supplied by the first module.
Method to establish a secure channel between the party of a software payload and the software payload itself when running into a hardware-based trusted execution environment, HW TEE, at the instance of a cloud service provider, including sending, by the party, a nonce to the software payload; generating, by the software payload, a payload key pair: public key and private key; mixing, by the software payload, the payload public key with the nonce; computing, by the HW TEE, an attestation using this nonce mixed with the payload public key; sending, by the software payload, the attestation, and the payload public key to the party; verifying, by the party, the attestation using the sent nonce mixed with the received payload public key; generating, by the software payload and the party, a session key; and establishing a secure channel between the party and the software payload running into the HW TEE.
H04L 9/14 - Dispositions pour les communications secrètes ou protégéesProtocoles réseaux de sécurité utilisant plusieurs clés ou algorithmes
H04L 9/32 - Dispositions pour les communications secrètes ou protégéesProtocoles réseaux de sécurité comprenant des moyens pour vérifier l'identité ou l'autorisation d'un utilisateur du système
An ultracold-atom sensor includes an atom chip (ACh) comprising a first and a second waveguide (CPWX1, CPWX2) that are suitable for propagating microwave waves and DC currents, at least a first conductive wire and a second conductive wire (WId, WId1) the respective projections of which are secant at a point defining a first crossing point (C1), an atom generation device (ACG), a power supply device (PSD) comprising at least one microwave generator (GMW) and at least one DC current generator (GDC), the power supply device being configured to apply, to the first and second waveguides and to spatially separate the two traps, the microwave signals in order to initiate the spatial separation, and then the CMW electric currents instead of the microwave signals in order to maintain the spatial separation.
G01P 15/08 - Mesure de l'accélérationMesure de la décélérationMesure des chocs, c.-à-d. d'une variation brusque de l'accélération en ayant recours aux forces d'inertie avec conversion en valeurs électriques ou magnétiques
G01C 19/56 - Dispositifs sensibles à la rotation utilisant des masses vibrantes, p. ex. capteurs vibratoires de vitesse angulaire basés sur les forces de Coriolis
25.
Obstacle detection method implemented by an aircraft embedded system and associated obstacle detection system
The present invention relates to an obstacle detection method implemented by an obstacle detection system on-board an aircraft, the aircraft including at least one on-board camera having an associated field of view configured to acquire full-field digital images. The method comprises the steps of:
(a)—reception (50) of at least one full-field digital image captured by said at least one on-board camera,
b)—determination (54) of a spatial position of a zone of interest of predetermined size in said full-field digital image, and extraction (56) of said zone of interest from said full-field digital image,
c)—implementation of an obstacle detection module (58) on said extracted zone of interest, implementing a neural network previously trained to detect and classify obstacles in images having said predetermined size, each obstacle detected being located in said zone of interest.
G06V 20/17 - Scènes terrestres transmises par des avions ou des drones
G06V 10/25 - Détermination d’une région d’intérêt [ROI] ou d’un volume d’intérêt [VOI]
G06V 10/764 - Dispositions pour la reconnaissance ou la compréhension d’images ou de vidéos utilisant la reconnaissance de formes ou l’apprentissage automatique utilisant la classification, p. ex. des objets vidéo
G06V 10/82 - Dispositions pour la reconnaissance ou la compréhension d’images ou de vidéos utilisant la reconnaissance de formes ou l’apprentissage automatique utilisant les réseaux neuronaux
26.
SPACE SYSTEM AND METHOD FOR WIRELESS COMMUNICATION BY TRANSMITTING RADIOFREQUENCY AND OPTICAL SIGNALS ON A RETURN CHANNEL
A communication satellite configured to transmit an optical signal, through an optical transmission channel, in response to the reception of at least one modulated and encoded radiofrequency signal. The satellite comprises: a unit for applying soft demodulation to the at least one received radiofrequency signal, and providing N intermediate demodulated data frames B1-n, each frame B1-n comprising a set of digitized soft values; a unit for applying an error correction code to the frames B1-n, and providing N encoded intermediate demodulated data frames B2-n; a unit for interleaving the N frames B2-n, and providing M interleaved data frames I2-m; and a unit for applying, to each frame I2-m, an optical carrier modulation so as to form the optical signal.
H04B 10/118 - Dispositions spécifiques à la transmission en espace libre, c.-à-d. dans l’air ou le vide spécialement adaptées aux communications par satellite
An avionics communication gateway including a module for acquiring at least one data message, each message being according to a communication protocol and including a header and a payload including a plurality of successive fields, a module for filtering each acquired message, validating the message if it complies with a set of filter criteria, and blocking it otherwise, and a module for transmitting, to a corresponding recipient, each validated message. The filter module includes a unit for generating a main table for each message, representing a tree of the fields of the payload of the message according to a set of levels related to the communication protocol, and a unit for calculating, for each message, a dictionary table and at least one auxiliary table from among first, second and third auxiliary tables, the filter module using the at least one auxiliary table for filtering the message.
An iris diaphragm having an optical axis, includes a fixed ring, a mobile ring designed to rotate about the optical axis with respect to the fixed ring and comprising a plurality n of guidance guideways, a plurality of n blades defining an elliptical diaphragm aperture having a major axis (a) and a minor axis (b), each blade being able to pivot with respect to the fixed ring about a respective axis and comprising a respective mobile pin able to move in one of the respective guidance guideways by bearing along the respective guidance guideway, a control ring designed to rotate about the optical axis with respect to the fixed ring and comprising a control guideway wherein one of the mobile pins, referred to as control pin, is able to move by bearing along the control guideway, a shape of each guidance guideway on which the respective mobile pin bears being designed so that a rotation of the control ring about the optical axis gives rise, via the control pin, to a rotation of the mobile ring and a movement of the mobile pins in the guidance guideways so as to modify an area of the elliptical aperture without modifying an orientation of the major axis and of the minor axis and without modifying a ratio of the major axis to the minor axis.
The present invention relates to a method for estimating an environmental footprint of a flight of an aircraft. The method is implemented by a decentralized electronic estimating system including at least a first entity, a second entity and a third entity, the second entity being distinct from the first entity and the third entity. The method includes receipt, by the second entity, from the first entity, at least one datum relative to the aircraft or its environment during the flight. The method also includes association, by the second entity, of a measurement uncertainty with each datum received by the second entity. The method further includes estimation, by the third entity, of an environmental indicator representative of the environmental footprint, on the basis of at least one datum and of the uncertainty associated with the at least one datum.
Centre national de la recherche scientifique (France)
Inventeur(s)
Debuisschert, Thierry
Mayer, Ludovic
Tallaire, Alexandre
Achard, Jocelyn
Brinza, Ovidiu
Abrégé
A method for manufacturing a device including a diamond crystal, the method including making available a substrate, growing a crystalline diamond layer on the substrate, the layer having a crystal lattice, the layer including at least a first set of XV centers in the crystal lattice, each XV center having a quantification axis, a main direction being defined for the first set, the quantification axes of the XV centers of the first set being parallel to the main direction, the normal direction being distinct from the main direction of the first set, removing a first part of the diamond layer in order to reveal a first face perpendicular to the main direction of the first set, and removing of a second part of the diamond layer in order to reveal a second face perpendicular to the first face.
A method for generating a secure secret key, includes the following steps: A. receiving, in a communication station referred to as the transmitting station, a first secret key by way of a quantum encryption channel via satellite, the first secret key also being transmitted to at least one other communication station by way of the quantum encryption channel; B. generating, in the transmitting station, a second secret key using a trusted random number generator; C. generating an encrypted secret key using the first secret key and the second secret key by the one-time pad method; D. transmitting the encrypted secret key from the transmitting station to the one or more other communication stations.
An iris diaphragm having an optical axis, includes a fixed ring, a plurality of [Formula (I)] blades defining a diaphragm aperture of predetermined shape, the blades being able to move in a plane perpendicular to the optical axis with respect to the fixed ring, each blade comprising a control pin, a control ring designed to rotate about the optical axis with respect to the fixed ring and comprising m control guideways, each control pin being able to move along a respective one of the control guideways by bearing along the respective control guideway, a rotation of the control ring about the optical axis giving rise, via the movement of the control pins in the control guideways, to the movement of the blades with respect to the fixed ring so as to modify the area of the aperture while maintaining the predetermined aperture shape, without causing a rotation of the predetermined shape with respect to the fixed ring.
An optical signal generation device for quantum key exchange, includes a photon source generating at least one pulse stream, an ADC transducer converting the photons of a pulse stream into a random binary string, a quantum state modulator putting the photons of the pulses into a number and quantum state defined by a control word in order to generate the optical signal from one of the pulse streams, digital computing means: generating at least one random sequence having a given probability distribution and rate, based on the random binary string, generating the control word in accordance with the key exchange protocol based on said at least one random sequence. A payload for a satellite, comprising such an optical signal generation device is also provided.
H04B 10/118 - Dispositions spécifiques à la transmission en espace libre, c.-à-d. dans l’air ou le vide spécialement adaptées aux communications par satellite
34.
METHOD FOR CONSTRUCTING AND AUTOMATICALLY CONTROLLING A SPEED PROFILE COMPRISING AT OR AT OR ABOVE SPEED RESTRICTIONS
A method for managing speed constraints of a flight plan of an aircraft, the method includes the following steps: identifying a current flight phase, determining CAS speed profile, the speed profile establishing a behavior of the aircraft with respect to a speed setpoint, determining a Mach speed profile, the Mach speed profile establishing a behavior of the aircraft with respect to a Mach setpoint, the Mach setpoint being a speed setpoint transcribed into an equivalent Mach number, determining a Cross-Over altitude, the Cross-Over altitude being an altitude of transition from an automatic control of the aircraft according to the CAS speed profile to an automatic control according to the Mach speed profile, determining an end-of-applicability criterion of the speed profile and of the Mach speed profile.
A detection system includes a phased array antenna having unitary radiating elements, the system being suitable for, in each cycle, successively directing, by way of the successive application of a first and a second determined phase law to the electrical signals for supplying power to the array antenna, the antenna radiation towards a first target area (Z1), then a second target area (Z2), which is separate from the first target area (Z1), and determining an image of each target area (Z1) on the basis of the echoes received from each of the first and second target areas.
G01S 13/90 - Radar ou systèmes analogues, spécialement adaptés pour des applications spécifiques pour la cartographie ou la représentation utilisant des techniques d'antenne synthétique
36.
Electronic avionics system with additional configuration file
Avionics system includes a bootstrap package including system partitions, and a primary configuration table, of a first type with hardware resource configuration values, a boot automaton launching the bootstrap package, at least one secondary configuration table of a second type with configuration values usable by a set of partitions, tertiary system configuration tables for the set of partitions, of a third type with configuration values used by a respective partition, application partitions, each including an avionics application and a tertiary configuration table, of the third type and containing configuration values of resources used by the respective application partition. The boot automaton checks whether an additional configuration file is present, and launches the additional configuration file including at least one configuration table of the first, second or third type, same being used instead of a table of the same type among the primary, secondary, tertiary system and tertiary application tables.
A computer platform on board an aircraft, that executes a set of application partitions, hosts an operating system and includes: resources; a boot package including a kernel, at least one resource driver, a set of system partitions and at least one resource configuration table, each system partition including at least one operating system service; and a boot controller able to be executed first, following power-up of the platform and configured to launch the boot package. The boot controller verifies whether an additional configuration file is present in the storage memory, and launches, before the boot package, the additional configuration file including at least one resource configuration table, then used instead of a respective table of the same type from among the at least one table of the boot package.
Commissariat à l'énergie atomique et aux énergies alternatives (France)
THALES (France)
Centre national de la recherche scientifique (France)
UNIVERSITE GRENOBLE ALPES (France)
Inventeur(s)
Grezes, Cécile
Vila, Laurent
Attane, Jean-Philippe
Bibes, Manuel
Abrégé
An electronic system includes an electronic device having a stack of layers, the stack including a first electrode, a subassembly with electrically controllable remanent states, a two-dimensional electron gas, a magnetic subassembly comprising at least one magnetic layer, and a second electrode having two first contacts and a second contact. The system also includes a writing device writing remanent states by applying an electric field between the two electrodes, and a Hall-effect reading device reading the remanent state by applying a current between the two first contacts and by measuring the voltage between the second contact and a reference potential.
G11C 11/16 - Mémoires numériques caractérisées par l'utilisation d'éléments d'emmagasinage électriques ou magnétiques particuliersÉléments d'emmagasinage correspondants utilisant des éléments magnétiques utilisant des éléments dans lesquels l'effet d'emmagasinage est basé sur l'effet de spin
A device for protecting an electronic equipment item, configured to limit the electric current between an electric power generator and an electronic equipment item consuming electric power. The device includes a control circuit connected to a power circuit, the power circuit including power semiconductors, the power circuit being able to be connected in series between the electric power generator and the electronic equipment item. The control circuit includes event detection modules, a current setpoint variation module, and a control module for controlling the power semiconductors, configured to supply a control signal for limiting the electric current in the power circuit as a function of the current limitation setpoint signal.
Commissariat à l'énergie atomique et aux énergies alternatives (France)
THALES (France)
Centre national de la recherche scientifique (France)
UNIVERSITE GRENOBLE ALPES (France)
Inventeur(s)
Attane, Jean-Philippe
Vila, Laurent
Bibes, Manuel
Abrégé
The present invention relates to an electronic device comprising:
a first electrode comprising a contact,
a ferroelectric subassembly having a ferroelectric polarization,
a spin polarization subassembly which spin-polarizes an incident current and comprises a layer of ferromagnetic or ferrimagnetic material,
an interfacing subassembly which is arranged between the two subassemblies and converts the spin current into a charge current, the ferroelectric subassembly and the interfacing subassembly having a contact, and
a second electrode which comprises two contacts and delimits the polarization subassembly,
the contact of the first electrode changing the state of polarization by applying a potential difference between this contact and another contact.
H10N 50/20 - Dispositifs à courant commandé à polarisation de spin
G11C 11/16 - Mémoires numériques caractérisées par l'utilisation d'éléments d'emmagasinage électriques ou magnétiques particuliersÉléments d'emmagasinage correspondants utilisant des éléments magnétiques utilisant des éléments dans lesquels l'effet d'emmagasinage est basé sur l'effet de spin
H01L 29/66 - Types de dispositifs semi-conducteurs
A method for checking an estimated location of a mobile machine receiving geopositioning signals from satellites, k=1 to s; a database storing the geographical coordinates of virtual beacons and the heading of the path segment on which the virtual beacon is located; a location indicating a virtual beacon, estimated to be on the same path segment as the machine, wherein for k=1 to s: the delay, ΔτSk(t,B1), is computed between the geopositioning signal received from and the theoretical geopositioning signal; values hdg and RxB1 are estimated that respect:
A method for checking an estimated location of a mobile machine receiving geopositioning signals from satellites, k=1 to s; a database storing the geographical coordinates of virtual beacons and the heading of the path segment on which the virtual beacon is located; a location indicating a virtual beacon, estimated to be on the same path segment as the machine, wherein for k=1 to s: the delay, ΔτSk(t,B1), is computed between the geopositioning signal received from and the theoretical geopositioning signal; values hdg and RxB1 are estimated that respect:
Δ
τ
S
1
(
t
,
B
1
)
=
1
c
(
cos
(
el
1
)
)
-
1
cos
(
az
1
′
)
RxB
1
+
ε
1
⋮
Δ
τ
S
s
(
t
,
B
1
)
=
1
c
(
cos
(
el
s
)
)
-
1
cos
(
az
s
′
)
RxB
1
+
ε
s
A method for checking an estimated location of a mobile machine receiving geopositioning signals from satellites, k=1 to s; a database storing the geographical coordinates of virtual beacons and the heading of the path segment on which the virtual beacon is located; a location indicating a virtual beacon, estimated to be on the same path segment as the machine, wherein for k=1 to s: the delay, ΔτSk(t,B1), is computed between the geopositioning signal received from and the theoretical geopositioning signal; values hdg and RxB1 are estimated that respect:
Δ
τ
S
1
(
t
,
B
1
)
=
1
c
(
cos
(
el
1
)
)
-
1
cos
(
az
1
′
)
RxB
1
+
ε
1
⋮
Δ
τ
S
s
(
t
,
B
1
)
=
1
c
(
cos
(
el
s
)
)
-
1
cos
(
az
s
′
)
RxB
1
+
ε
s
the location being identified as unreliable depending on comparison of the estimated hdg with the stored value of the heading of the path segment of the beacon.
G01S 19/07 - Éléments coopérantsInteraction ou communication entre les différents éléments coopérants ou entre les éléments coopérants et les récepteurs fournissant des données pour corriger les données de positionnement mesurées, p. ex. DGPS [GPS différentiel] ou corrections ionosphériques
G01S 19/10 - Éléments coopérantsInteraction ou communication entre les différents éléments coopérants ou entre les éléments coopérants et les récepteurs fournissant des signaux de positionnement supplémentaires dédiés
42.
Neural network digital signature encoding method, device and corresponding computer program
A method for encoding a digital signature of a neural network, implemented by an electronic device, the neural network being stored within a data structure including blocks of parameters. The method includes, for a current block of parameters including at least M parameters representing real numbers: an operation of acquiring a signature binary image from the digital signature including a set of bits extracted from parameters of the current block of parameters, and an operation of combining the signature binary image with a reference binary image delivering a coded binary image.
A method of digitally watermarking a neural network, implemented by an electronic device, the neural network being stored within a data structure including blocks of parameters. The method includes, for a current parameter block consisting of at least N parameters representing real numbers, obtaining a message including N bits, at least N iterations of a parameter modification operation within the current block, including obtaining a current parameter, from among the at least N parameters of the current parameter block, and updating the value of a predetermined index bit of the current parameter as a function of a bit in the message.
A method for learning a prediction algorithm, the learning being implemented by a machine learning technique, the method including reception of a current set of learning data, reception of an invariance property of the prediction of the algorithm with respect to the inputs according to an initial symmetry group endowed with an initial probability law, determination of a subgroup of the initial group endowed with a subgroup probability law and intended to apply transformations to the current set, according to an optimization technique using the current set, the initial group and the initial law under an optimization constraint deduced from predetermined constraints, generation of data using the determined subgroup, the law of the subgroup and the whole current set, and implementation of a learning of the algorithm using the generated data.
CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
GLOPHOTONICS (France)
Inventeur(s)
Benabid, Abdelfatah
Debord, Benoît
Beaudou, Benoît
Feugnet, Gilles
Morbieu, Bertrand
Abrégé
A device for coupling optical fibers, includes a first coupling-inhibited hollow-core optical fiber comprising a first microstructured cladding comprising a plurality of first confining tubular features distributed in a ring and encircling, at least partially, a first core so as to confine at least radiation at a wavelength λop to the first core, a second coupling-inhibited hollow-core optical fiber comprising a second microstructured cladding comprising a plurality of second confining tubular features distributed in a ring and encircling, at least partially, a second core so as to confine the light radiation to the second core, a coupling element arranged between the first and second cores, the coupling element comprising at least one coupling tubular feature comprised at least partially in the first microstructured cladding and/or the second microstructured cladding and having a wall thickness tcp called the coupling thickness and a material index ncp called the coupling index, an arrangement of the coupling element, the coupling thickness tcp and the coupling index ncp being configured so as to create a leakage channel at the wavelength λop allowing the radiation guided by the first optical fiber to be coupled to the second optical fiber and/or the radiation guided by the second optical fiber to be coupled to the first optical fiber.
G02B 6/28 - Moyens de couplage optique ayant des bus de données, c.-à-d. plusieurs guides d'ondes interconnectés et assurant un système bidirectionnel par nature en mélangeant et divisant les signaux
Electronic portion of a CRPA antenna of an anti-jamming device for a GNSS receiver and associated anti-jamming device and method for processing signals
An electronic portion of a CRPA antenna of an anti-jamming device for a GNSS receiver, including M elementary signal inputs, for each input, a bandpass filter bank which is configured to break down each elementary signal received by this input at a frequency Fe, into P sub-bands to obtain P sub-sampled signals at a frequency Fe/P, a calculational component which is configured to apply in parallel anti-jamming processing at the frequency Fe/P to the sub-sampled signals, to obtain a cleaned sub-sampled signal, and a summation component which is configured to receive all the cleaned sub-sampled signals and to form, from these sub-sampled signals a resulting corresponding cleaned signal at the frequency Fe.
COMMISSARIAT A L'ENERGIE ATOMIQUE ET AUX ENERGIES ALTERNATIVES (France)
Inventeur(s)
Delga, Alexandre
Espiau De Lamaestre, Roch
Abrégé
An optoelectronic device includes at least one pixel comprising: a plurality of optical resonators, each optical resonator comprising a photodetecting structure confined between a first reflective metal layer and a second metal layer; and a connection microstructure that is arranged on a support made of dielectric material and is configured to electrically interconnect the second metal layers of the optical resonators belonging to the same pixel; and a readout integrated circuit arranged on a substrate and assembled with the pixel; the readout circuit comprising a buried readout electrode associated with the pixel and a metal or dielectric outer layer. The assembly comprising at least the first metal layer and the outer layer of the readout integrated circuit is called a planar assembly structure. The second metal layers of the resonators of a pixel are connected to the associated readout electrode by way of a metal via connected to the connection microstructure and passing through the support.
A flight management system for an aircraft, includes a critical first avionics module for trajectory calculation, i.e. a module the integrity level and availability level of which are specified by regulatory standards in force, delivering as output a safe trajectory, based on a flight plan; a second module for trajectory calculation that is less critical than the critical first module, i.e. a module the integrity level and availability level of which are lower than those of the first module, delivering as output an improved trajectory that is less safe than the trajectory delivered by the critical first avionics module, based on a flight plan; a critical avionics module for trajectory verification, configured to validate or invalidate the safety of the less safe improved trajectory; and a critical avionics module for decision-making configured to select a trajectory from the safe trajectory and the less safe trajectory.
40 - Traitement de matériaux; recyclage, purification de l'air et traitement de l'eau
41 - Éducation, divertissements, activités sportives et culturelles
42 - Services scientifiques, technologiques et industriels, recherche et conception
Produits et services
(1) Services de télécommunications; services de télécommunications par fibres optiques; services de fourniture d'accès à internet pour des utilisateurs [fournisseurs de services]; fourniture d'accès et de location d'accès à une base de données informatique; transmission de communications cryptées; fourniture et location d'installations et d'équipement de télécommunication, tous les services précités étant dans les domaines de la défense, de l'aérospatiale, de l'aéronautique, de la sécurité, du transport terrestre, aérien et naval, de la banque et de la finance.
(2) Impression, et développement photographique et cinématographique.
(3) Formation; édition, tous les services précités étant dans les domaines de la défense, de l'aérospatiale, de l'aéronautique, de la sécurité, du transport terrestre, aérien et naval, de la banque de la finance et de l'informatique.
(4) Services scientifiques, technologiques et de recherches; services d'analyses industrielles, de recherches industrielles et de dessin industriel; services de contrôle de qualité et d'authentification; conception et développement d'ordinateurs et de logiciels; conseil en intelligence artificielle; recherche dans le domaine de l'intelligence artificielle; plates-formes pour intelligence artificielle en tant que logiciel-service [SaaS]; fourniture de programmes informatiques d'intelligence artificielle sur des réseaux de données; services des technologies de l'information; services scientifiques et technologiques; tests, authentification et contrôle de la qualité; services de stockage électronique de données électroniques, service de conception, développement, mise à jour, installation, et maintenance de bases de données; services d'assistance technique en matière de matériel informatique et de logiciels; services de cryptage, décryptage et authentification d'informations, de messages et de données; surveillance de systèmes informatiques pour la détection d'accès non autorisés ou d'atteintes à la protection de données; consultation en matière de sécurité informatique; analyse de la menace sur la sécurité informatique pour la protection des données; installation de logiciel de contrôle d'accès en tant que service (ACaaS); hébergement de données; hébergement de blogues; plateforme informatique en tant que service [PaaS]; développement de plateformes informatiques, tous les services précités étant dans les domaines de la défense, de l'aérospatiale, de l'aéronautique, de la sécurité, du transport terrestre, aérien et naval, de la banque et de la finance et de l'informatique.
40 - Traitement de matériaux; recyclage, purification de l'air et traitement de l'eau
41 - Éducation, divertissements, activités sportives et culturelles
42 - Services scientifiques, technologiques et industriels, recherche et conception
Produits et services
Telecommunication services; fiber optic telecommunication services; providing user access to the Internet [service providers]; provision of access and rental of access time to a computer database; transmission of encrypted communications; provision and rental of telecommunication facilities and equipment, all the aforementioned services in the fields of defense, aerospace, aeronautics, security, land, air and naval transportation, banking and finance. Printing, and photographic and cinematographic development. Training; editing, all the aforementioned services in the fields of defense, aerospace, aeronautics, security, land, air and naval transportation, banking, finance and computing. Scientific, technological and research services; industrial analysis, industrial research and industrial design services; quality control and authentication services; design and development of computers and software; advice with respect to artificial intelligence; research in the field of artificial intelligence; platforms for artificial intelligence as SaaS [Software as a Service]; providing artificial-intelligence computer programs on data networks; information technology services; scientific and technological services; quality control, authentication and testing; electronic storage of electronic data, design, development, updating, installation, and maintenance of databases; technical support services with respect to computer hardware and software; encryption, decryption and authentication services for information, messages and data; monitoring of computer systems for the detection of unauthorized access or data protection breaches; consultation with respect to computer security; analyzing computer security threats for data protection; installing access control as a service (ACaaS) software; data hosting; hosting weblogs [blogs]; computer Platform as a Service [PaaS]; developing computer platforms, all the aforementioned services being in the fields of defense, aerospace, aeronautics, security, land, air and naval transportation, banking and finance and computing.
51.
METHOD FOR AUTOMATICALLY GENERATING A SEQUENCE OF NMAX INSTRUCTIONS IN ASSEMBLY LANGUAGE, THE SEQUENCE BEING EXECUTABLE ERROR-FREE BY A MULTI-CORE PROCESSOR
A method for automatically generating a sequence of Nmax instructions in assembly language, the sequence being executable error-free by a multi-core processor, the method comprising steps of: initializing registers of the processor, then selecting a first instruction of the predetermined sequence, optionally at random; and selecting an N+1th instruction among an instruction to read from a memory connected to the cores of the processor by a memory bus, an instruction to write to said memory, and a local instruction using only the registers of the processors, according to rules and to priorities between the rules, the rules using respective differences between statistical-metric values of statistical metrics of a memory access pattern of the sequence of N previous instructions having statistical-metric values, and setpoint values.
An aerodynamic measurement probe intended to measure a local angle of attack of an airflow circulating along the fuselage of an aircraft, the support comprising a circular cover with a central opening which is passed through by the mobile shaft, the outer surface of the cover comprising a frustoconical face exhibiting symmetry of revolution about the longitudinal axis, the cover comprising polyether ether ketone reinforced with glass or carbon fibers, with a thermal conductivity of less than 3 W.m−1·K−1 and being provided with metallic inserts at its fastenings, at least one metallic electrical continuity insert being configured to establish an electrical connection between the inner part of the probe and an interface of the metallic insert disposed under the lower periphery of that part of the metallic insert which is furthest away from the shaft.
This angle-of-attack sensor, in particular for an aircraft, of the type including a sensor body (11) on which a wind vane (12) is mounted movable in rotation by a flow, is characterized in that the wind vane (12) includes at least one deflector (13, 14) extending from the leading edge of this wind vane over at least part of the intrados and/or extrados thereof.
COMMISSARIAT A L'ENERGIE ATOMIQUE ET AUX ENERGIES ALTERNATIVES (France)
Inventeur(s)
Quinchard, Grégory
Mismer, Colin
Abrégé
A method for fabricating a device includes the following steps: fabricating at least one first microstructure and one second microstructure on the substrate, fabricating a connection microstructure making it possible to electrically connect at least the first microstructure to the second microstructure by fabricating a support made of dielectric material by solidifying, by means of a lithography method, a part of a deposited resin layer and by depositing a first metallic layer on at least a part of the support comprising at least a part linking the first microstructure and the second microstructure.
H01L 31/02 - Dispositifs à semi-conducteurs sensibles aux rayons infrarouges, à la lumière, au rayonnement électromagnétique d'ondes plus courtes, ou au rayonnement corpusculaire, et spécialement adaptés, soit comme convertisseurs de l'énergie dudit rayonnement e; Procédés ou appareils spécialement adaptés à la fabrication ou au traitement de ces dispositifs ou de leurs parties constitutives; Leurs détails - Détails
H01L 31/18 - Procédés ou appareils spécialement adaptés à la fabrication ou au traitement de ces dispositifs ou de leurs parties constitutives
55.
METHOD FOR COMMUNICATION BETWEEN AN AIR TRAFFIC CONTROL SYSTEM AND A COMMUNICATION MODULE
A method for communication between an air traffic control system and a communication module, the communication method includes a step of determining environmental optimization time slots based on the air traffic absorption capacities of the various flight information regions, the environmental optimization time slots at least partially covering one or more flight information regions, each environmental optimization time slot having an associated efficiency level; a step of negotiation, between the pilot via the communication module and the air traffic control system, to negotiate changes to the flight plan on the basis of the environmental optimization time slots and the environmental optimization levels of the environmental optimization time slots.
Centre national de la recherche scientifique (France)
UNIVERSITE PARIS-SACLAY (France)
Inventeur(s)
Grollier, Julie
Martin, Erwann
Querlioz, Damien
Petrisor, Teodora
Abrégé
A neuromorphic circuit implementing a spiking neural network and including bidirectional synapses made by a set of memristors arranged in an array, neurons firing spikes at a variable rate and connected to neurons via a synapse, and a neural network training module including, for at least one bidirectional synapse, an estimation unit obtaining an estimation of the time derivative of the spike rate of each neuron, an interconnection having at least two positions between the synapse and each neuron, and a controller sending a control signal to the interconnection after a spike, the signal changing the position of the interconnection, so as to connect the estimation unit and the synapse.
G06N 3/063 - Réalisation physique, c.-à-d. mise en œuvre matérielle de réseaux neuronaux, de neurones ou de parties de neurone utilisant des moyens électroniques
57.
METHOD AND DEVICE FOR PERFORMING PREDICTIVE ANALYSIS OF THE BEHAVIOUR OF AN OPERATOR INTERACTING WITH A COMPLEX SYSTEM
A device and a method implemented by computer, allowing the behavior and the actions of an operator interacting with a complex system to be predicted, based on the observation of his/her behavior in real time and on the instantiation of models of human behavior which are constructed by learning from past data collected for a plurality of operators, the models of human behavior having been learnt by the application of artificial intelligence techniques to cognitive models and to procedural models taking into account parameters of human factors of influence.
A pressure measurement probe for an aircraft, includes a pressure sensor board comprising an electronic board equipped with a pressure sensor provided with an air inlet, the electronic board further comprising at least four fixing points distributed on a circle at regular angular intervals and configured to allow the sensor board to be fixed in the pressure measurement probe in such a way as to have, when the aircraft is on the ground, a pressure sensor air inlet that is directed downward and an angular offset less than or equal to 45° between the axis of the air inlet of the pressure sensor and the vertical, irrespective of the position of the probe on the aircraft.
G01P 5/14 - Mesure de la vitesse des fluides, p. ex. d'un courant atmosphériqueMesure de la vitesse de corps, p. ex. navires, aéronefs, par rapport à des fluides en mesurant les différences de pression dans le fluide
B64D 45/00 - Indicateurs ou dispositifs de protection d'aéronefs, non prévus ailleurs
59.
Methods for the compression and decompression of a digital terrain model file; associated compressed and decompressed files and associated computer program product
Method for compressing a digital terrain model file including a tile including a matrix of cells, each cell including an elevation value for a geographical point of the terrain, by representing the tile in the form of an initial tree having a plurality of depth levels, each terminal node of the initial tree representing a zone of the tile corresponding to a single cell, pruning the initial tree so as to obtain a pruned tree, encoding the elevation value associated with each of the terminal nodes of the pruned tree to obtain a differential elevation value starting from a reference elevation, and serializing the pruned tree resulting from the encoding to obtain a compressed file indicating the reference elevation, followed by a plurality of sequences, each sequence including a header and a load, indicative of a depth level and a differential elevation value of a terminal node, respectively.
An aeronautical probe that presents a generally profiled shape, is provided with a fixing base and has undulations on at least part of its leading edge.
G01P 5/14 - Mesure de la vitesse des fluides, p. ex. d'un courant atmosphériqueMesure de la vitesse de corps, p. ex. navires, aéronefs, par rapport à des fluides en mesurant les différences de pression dans le fluide
A probe for measuring static or parietal pressure includes a pressure sensor module, a mounting plate equipped with air inlets which is intended to be mounted on the skin of an aircraft, and a shut-off means equipped with shut-off fingers which are configured to plug the air inlets of the mounting plate, and an actuator, controlled by a control module, configured to move the shut-off means in a translational movement so as to plug or unplug the air inlets of the mounting plate by the shut-off fingers.
B64D 43/02 - Aménagements ou adaptations des instruments pour indiquer la vitesse des aéronefs ou les conditions de décrochage
G01L 19/00 - Détails ou accessoires des appareils pour la mesure de la pression permanente ou quasi permanente d'un milieu fluent dans la mesure où ces détails ou accessoires ne sont pas particuliers à des types particuliers de manomètres
G01L 19/06 - Moyens pour empêcher la surcharge ou l'influence délétère du milieu à mesurer sur le dispositif de mesure ou vice versa
62.
Antenna system comprising an antenna and a passive device for angular deflection of a main radiation lobe of the antenna.
An antenna system includes an antenna and a passive device for angular deflection of a main radiation lobe of the antenna, characterized in that the device consists of a lens, said lens having a constant thickness and having a progressive relative permittivity between an inner edge of the lens located on the side of the geometric center of the antenna and an outer edge of the lens located on the side of a periphery of the antenna, the profile of the relative permittivity as a function of distance to the geometrical center of the antenna being adapted such that the lens deflects the main radiation lobe of the antenna by a predefined deflection angle over at least a portion of an operating frequency band of the antenna.
An aerodynamic measurement probe intended to measure a local angle of attack of an air stream flowing along the fuselage of an aircraft, includes a support and a shaft that is able to rotate about a longitudinal axis with respect to the support, the support and the shaft being configured to form between them a gap, passing around an annular tab at the end of the shaft in the support, making it possible to maintain a functional clearance to allow one end of the shaft to pivot freely in the support, and communicating with an impurity discharge circuit, the gap comprising an inner annular groove about the axis of rotation, made in the support, and opening out away from the axis directly onto the end part of the annular tab, the profile of the inner groove being rounded.
COMMISSARIAT A L’ENERGIE ATOMIQUE ET AUX ENERGIES ALTERNATIVES (France)
Inventeur(s)
Demiguel, Stéphane
Reverchon, Jean-Luc
Benfante, Marco
Abrégé
A method for fabricating an optoelectronic component includes at least one photodiode, the steps of the method making it possible to move the electric carrier collection field to the layer least sensitive to radiation, thus reducing the influence of irradiation on the dark current.
Method and apparatus for monitoring - with contention mitigation - avionics application(s) running on a platform with multi-core processor, related electronic avionics system and computer program
A method for monitoring avionics software application(s) executed by an avionics platform, on-board an aircraft, including a multi-core processor and hosting an operating system, is implemented by an electronic monitoring device and includes, for each software application running, a monitoring phase including acquisition at least one characteristic variable value representative of a use of the platform, each acquired value being associated with the respective software application, comparison of each acquired value with a respective threshold corresponding to the characteristic variable, and stopping the execution of the respective software application if at least one acquired value is higher than the respective threshold.
A rat-race balun includes a transmission line loop and 4 input-output ports P1, P2, P3, P4 connected to the transmission line loop, the respective transmission line section between the adjacent ports P1 and P4 is of electrical length 2θ2, of impedance Z3 and is a line section loaded by a capacitor of capacitance C2; where θ2<135 and the following equalities are satisfied:
A rat-race balun includes a transmission line loop and 4 input-output ports P1, P2, P3, P4 connected to the transmission line loop, the respective transmission line section between the adjacent ports P1 and P4 is of electrical length 2θ2, of impedance Z3 and is a line section loaded by a capacitor of capacitance C2; where θ2<135 and the following equalities are satisfied:
C
2
=
-
2
tan
(
θ
2
)
ω
Z
P
1
P
4
tan
(
2
θ
2
)
and
Z
3
=
-
Z
P
1
P
4
tan
(
θ
2
)
w being equal to 2πf, with f the operating frequency, and ZP1P4 being the impedance of the unloaded transmission line section of physical length 3λ/4 equivalent to the loaded line section.
A reception chain allowing the reception of IFF and ADS-B signals while rejecting at least one intermediate frequency band, includes a reception antenna, an analog part with: a two-band filtering device passing around the frequency bands of the IFF and ADS-B signals while rejecting the intermediate frequency band, a low-noise amplifier, a mixer configured to transpose the IFF and ADS-B signals to lower frequencies, an analog-digital converter, a digital part configured to duplicate the digitized signal, and to process the duplicated signals respectively on a first, IFF, path and a second, ADS-B, path each comprising a filtering device, a frequency transposition device, and signal processing means.
H04B 1/10 - Dispositifs associés au récepteur pour limiter ou supprimer le bruit et les interférences
H04B 1/00 - Détails des systèmes de transmission, non couverts par l'un des groupes Détails des systèmes de transmission non caractérisés par le milieu utilisé pour la transmission
68.
Rat-race balun and associated method for reducing the footprint of a rat-race balun
A rat-race balun includes a transmission line loop and 4 input-output ports P1, P2, P3, P4 connected to the transmission line loop, the balun being designed to receive a first signal on the port P1, and to divide the first signal into a second signal that is delivered to the port P2 and a third signal that is delivered to the port P4, the second signal and the third signal being in phase opposition with one another, the balun wherein the balun is kidney-shaped and the ports P2, P4 each comprise at least a first section connected to the transmission line, the first section of the port P2 being parallel to the first section of the port P4.
H01P 5/10 - Dispositifs de couplage du type guide d'ondes destinés au couplage de lignes ou de dispositifs de différentes sortes destinés au couplage de lignes ou de dispositifs équilibrés avec des lignes ou des dispositifs déséquilibrés
69.
ACCELERATION-MEASURING SENSOR ASSEMBLY COMPRISING AN ACCELEROMETER SUBASSEMBLY WITH THREE MEASUREMENT AXES, AND A SEISMIC MASS MOVING IN A STRAIGHT LINE ALONG A PRINCIPAL AXIS A, WHICH ASSEMBLY IS MOUNTED IN A HOUSING AND CONFIGURED TO DETERMINE AN ACCELERATION ALONG A MEASUREMENT AXIS Y
An acceleration-measuring sensor assembly includes an accelerometer subassembly with three measurement axes, mounted in a housing equipped with securing elements, and configured to determine an acceleration along a principal axis A, the assembly comprising: a single-axis principal accelerometer with a seismic mass moving in a straight line along a principal axis A, measuring acceleration along the principal axis A which is misaligned with respect to a reference axis Y by at most 50 mrad, a secondary accelerometer having at least two measurement axes and measuring respectively along two axes X and Z which with the reference axis Y form a direct orthonormal trihedron (O, X, Y, Z), the measurement precision of the two-axis accelerometer along each of its axes being at least ten times inferior to the measurement precision of the single-axis accelerometer, and an electronic processing unit configured to calculate a compensated acceleration S.
G01P 15/18 - Mesure de l'accélérationMesure de la décélérationMesure des chocs, c.-à-d. d'une variation brusque de l'accélération dans plusieurs dimensions
G01P 15/08 - Mesure de l'accélérationMesure de la décélérationMesure des chocs, c.-à-d. d'une variation brusque de l'accélération en ayant recours aux forces d'inertie avec conversion en valeurs électriques ou magnétiques
INSTITUT NATIONAL DES SCIENCES APPLIQUEES DE RENNES (France)
UNIVERSITE DE RENNES (France)
CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
CENTRALESUPELEC (France)
NANTES UNIVERSITE (France)
Inventeur(s)
Cailleux, Aymeric
Hogommat-Chabrot, Laure
Fourn, Erwan
Abrégé
A dual-band analogue filter that is passing for IFF signals and ADS-B signals in a first and a second frequency band, and to reject signals received outside these bands, implemented using multi-planar technology, and comprising, in succession: a layer comprising an input port and an output port, a layer comprising a ground plane having openings facing the input port and the output port, a layer comprising N band-pass resonators, a layer comprising N band-stop resonators, arranged such that: the band-pass resonators are connected in pairs by coupling, the first and the last band-pass resonator are connected to the input port and the output port by electromagnetic coupling, each band-pass resonator is connected to a band-stop resonator by electromagnetic coupling.
H04B 1/00 - Détails des systèmes de transmission, non couverts par l'un des groupes Détails des systèmes de transmission non caractérisés par le milieu utilisé pour la transmission
A device for securing a file system of a remote stand-alone system using an operating system associated with the file system having a double partition for A/B updates, the remote stand-alone system being updated by atomic update, and further including a secure boot tool, the device for securing being configured for signing the file system relying on an asymmetric two-key cryptography including a public key and a private key, the public key being integrated into the kernel of the operating system, and the lifetime of the private key being limited, the two public and private keys being regenerated by the device for securing each time a new atomic update of the remote stand-alone system is produced.
G06F 21/57 - Certification ou préservation de plates-formes informatiques fiables, p. ex. démarrages ou arrêts sécurisés, suivis de version, contrôles de logiciel système, mises à jour sécurisées ou évaluation de vulnérabilité
G06F 21/62 - Protection de l’accès à des données via une plate-forme, p. ex. par clés ou règles de contrôle de l’accès
72.
Onboard edge computation device, associated electronic system and method for executing software applications
An edge computation device on board an aircraft is configured for communicating with one or a plurality of onboard electronic devices having certified operation, and with at least one remote computation system. Same includes local computational resources, and is configured for implementing a management module for a plurality of software applications suitable for providing at least one control parameter and/or receiving at least one datum from at least one onboard electronic device, a module for activating the execution of at least one of the stored software applications, a management module for an execution stack, configured for determining, for each software application to be executed, an allocation of local computation resources and, where appropriate, for executing locally a first part of the application, and for requesting remote execution, by means of the remote computation system, of a second part of the application to be executed.
Disclosed is an avionics device for assisting in the control of at least one automated system of an aircraft, the device being able to connect, via a network, to the at least one automated system and to a plurality of distinct sources of the automated system. The device is configured for: collecting avionics data supplied by the plurality of sources and supplied by the at least one automated system; classifying and analyzing the collected data as a function of each predetermined property to be restored to the at least one automated system; and determining, from the classified and analyzed data and from a current state of the aircraft, whether an avionics setpoint, manually entered into the device, can be attained by the at least one automated system.
B64D 45/00 - Indicateurs ou dispositifs de protection d'aéronefs, non prévus ailleurs
G01C 23/00 - Instruments combinés indiquant plus d’une valeur de navigation, p. ex. pour l’aviationDispositifs de mesure combinés pour mesurer plusieurs variables du mouvement, p. ex. la distance, la vitesse ou l’accélération
74.
supervision device configured for communicating with an edge computation device onboard an aircraft and an associated electronic system for executing software applications
A supervision device configured for communicating with a computation device onboard an aircraft, wherein the onboard edge device is configured for executing software applications related with one or a plurality of onboard electronic devices with certified operation, the supervision device comprising a human-machine interface and being configured for receiving, from the edge computation device, observability signals comprising data relating to local computing resources of the onboard edge computation device and information relating to the execution of at least one of the software applications, the supervision device including at least one computing processor configured for computing a state of operation of the edge computation device and a state of execution of the at least one software application from the received observability signals and for displaying the state of operation and the state of execution on the human-machine interface.
G05B 19/4155 - Commande numérique [CN], c.-à-d. machines fonctionnant automatiquement, en particulier machines-outils, p. ex. dans un milieu de fabrication industriel, afin d'effectuer un positionnement, un mouvement ou des actions coordonnées au moyen de données d'un programme sous forme numérique caractérisée par le déroulement du programme, c.-à-d. le déroulement d'un programme de pièce ou le déroulement d'une fonction machine, p. ex. choix d'un programme
75.
WIDE-ANGLE IMPEDANCE-MATCHING DEVICE FOR RADIATING-ELEMENT ARRAY ANTENNA AND METHOD OF DESIGNING SUCH A DEVICE
CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
NANTES UNIVERSITE (France)
INSA DE RENNES (France)
CENTRALESUPELEC (France)
Inventeur(s)
Gillard, Raphael
Garcia Vigueras, Maria
Bermudez-Martin, Diego
Legay, Hervé
Abrégé
A wide-angle impedance-matching device for a radiating-element array antenna includes a transmission screen having a first surface intended to be positioned facing the radiating-element array parallel to the radiating aperture of the antenna and being configured to match the impedance of the antenna for an H-plane scan, and a set of metal pins placed orthogonally, on at least one surface of the transmission screen, at the intersection of at least some of the respective anti-symmetry planes of the electric field radiated by the antenna for an H-plane scan, for two linear polarizations in two orthogonal directions, the set of metal pins being configured to match the impedance of the antenna for an E-plane scan.
H01Q 1/50 - Association structurale d'antennes avec commutateurs de terre, dispositions de descente d'antennes ou parafoudres
H01Q 5/335 - Éléments rayonnants individuels ou couplés, chaque élément étant alimenté d’une façon non précisée utilisant des circuits ou des composants dont la réponse dépend de la fréquence, p. ex. des circuits bouchon ou des condensateurs au point d’alimentation, p. ex. aux fins d’adaptation d’impédance
76.
WIDE-ANGLE IMPEDANCE-MATCHING DEVICE FOR RADIATING-ELEMENT ARRAY ANTENNA AND METHOD OF DESIGNING SUCH A DEVICE
CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
NANTES UNIVERSITE (France)
INSA DE RENNES (France)
CENTRALESUPELEC (France)
UNIVERSITE DE RENNES (France)
Inventeur(s)
Gillard, Raphael
Garcia Vigueras, Maria
Bermudez-Martin, Diego
Legay, Herve
Abrégé
Wide-angle impedance-matching device (102) for a radiating-element array antenna, comprising: - a transmission screen (103) having a first surface intended to be positioned facing the radiating-element array parallel to the radiating aperture of the antenna and being configured to match the impedance of the antenna for an H-plane scan, - and a set of metal pins (104) placed orthogonally, on at least one surface of the transmission screen (103), at the intersection of at least some of the respective anti-symmetry planes of the electric field radiated by the antenna for an H-plane scan, for two linear polarizations in two orthogonal directions, said set of metal pins (104) being configured to match the impedance of the antenna for an E-plane scan.
The present invention relates to a method for determining detection thresholds of a CFAR detection system of a sensor observing an environment, the CFAR detection system being provided with an estimator adapted to determine an estimate of parameters related to noise affecting the sensor depending on parameters related to the environment, the method comprising the steps of:
estimation of parameters related to noises, in order to obtain a parameter vector,
computation of first detection thresholds so that, for all possible configurations of the parameter vector, the CFAR detection system operates at a predefined false alarm probability,
characterization of estimation errors of the estimator, and
correction of each first detection threshold in order to obtain second detection thresholds, the step of correcting taking into account the error parameters.
The invention concerns a system for receiving by a gNB a location information sent by a GNSS chipset comprised in a mobile equipment, the location information being part of a signalling message as part of an initial access procedure, before network dedicated signaling ciphering setup procedure occurs, the GNSS chipset returning to the mobile equipment the location information concealed by a crypto scheme that does not need any diversification from one chipset to another, the concealed location information being de-concealed by a deciphering server at the level of the gNB by a reversed crypto scheme that does not need any diversification from one chipset to another for sending the location information in clear to a dedicated 5G core network, the dedicated 5G core network being the one able to handle a communication with the mobile equipment.
A method for managing a head-mounted display having a predetermined field of view and a predetermined axis of sight and configured to display a plurality of graphic messages, the method comprising the following steps implemented when the head-mounted display is being worn by a user in a predetermined environment comprising a plurality of information interfaces:
A1. determining a first datum (D1) relating to a position and orientation of a head of the user with respect to the environment based on information relating to a spatial arrangement of the environment;
B. modifying a brightness of the head-mounted display and/or adjusting the graphic messages, depending on a dataset containing the first datum and containing information relating to the interfaces.
G09G 3/00 - Dispositions ou circuits de commande présentant un intérêt uniquement pour l'affichage utilisant des moyens de visualisation autres que les tubes à rayons cathodiques
B64D 43/00 - Aménagements ou adaptations des instruments
G06F 3/01 - Dispositions d'entrée ou dispositions d'entrée et de sortie combinées pour l'interaction entre l'utilisateur et le calculateur
80.
End-to-end integrity check of a communication stream
A method of integrity control, an allocation of virtual identifier, to each stream, only known to each transmitter or receiver, located at one end of the stream, a transmission by a transmitter at the end of a stream, of a message including the payload, the value of a counter of transmitted messages, and a transmission aggregate determined from the virtual identifier known to the transmitter, the value, the payload, the reception by a receiver, at the other end of the stream, of the message, and determination of a reception aggregate from the virtual identifier known to the receiver, the value received, the payload received, the end-to-end integrity check by comparing transmission and reception aggregates.
A method for measuring the performance of a CFAR detection system of a sensor in observing an environment, the CFAR detection system being provided with an estimator suitable for determining an estimate of parameters related to noise affecting the sensor depending on parameters related to the environment, the measurement method including estimating noise-related parameters, obtaining detection thresholds for the CFAR detection system, characterizing estimation errors of the estimator of the CFAR detection system, determining each detection threshold likely to be actually used by the CFAR system due to estimation errors, and calculating the performance of the CFAR detection system on the basis of the detection thresholds determined.
A method of protecting an incoming stream, the incoming stream including at least one incoming elementary video stream, the incoming elementary video stream including a succession of incoming video packets, the method characterized by the disassembling of the incoming stream for separating a current packet; the encryption of the current packet with a session key, the building of a confidentiality metadata packet including a time stamp field corresponding to a time stamp of the current packet and a confidentiality field containing the session key, the encryption of the confidentiality data packet with an encryption key, and the assembling of an outgoing stream including an outgoing elementary stream grouping together the encrypted current packets and an elementary confidentiality metadata stream including the encrypted confidentiality metadata packets.
A method for controlling the pointing of an antenna situated on a platform in the direction of a communications device emitting a reference signal, includes the following steps: S1) apply a first mode of pointing of the antenna using almanac data for the platform and for the communications device so as to obtain an initial position of pointing in azimuth and in elevation of the boresight of the antenna; S2) apply a second mode of pointing of the antenna, comprising at least one scan of the antenna around the initial position so as to point the antenna in a direction that maximizes a received power of the reference signal; S3) apply a third mode of pointing of the antenna wherein at least one triangulation manoeuvre is implemented for pointing the antenna based on the maximum power.
H01Q 3/34 - Dispositifs pour changer ou faire varier l'orientation ou la forme du diagramme de directivité des ondes rayonnées par une antenne ou un système d'antenne faisant varier la phase relative ou l’amplitude relative et l’énergie d’excitation entre plusieurs éléments rayonnants actifsDispositifs pour changer ou faire varier l'orientation ou la forme du diagramme de directivité des ondes rayonnées par une antenne ou un système d'antenne faisant varier la distribution de l’énergie à travers une ouverture rayonnante faisant varier la phase par des moyens électriques
H01Q 3/26 - Dispositifs pour changer ou faire varier l'orientation ou la forme du diagramme de directivité des ondes rayonnées par une antenne ou un système d'antenne faisant varier la phase relative ou l’amplitude relative et l’énergie d’excitation entre plusieurs éléments rayonnants actifsDispositifs pour changer ou faire varier l'orientation ou la forme du diagramme de directivité des ondes rayonnées par une antenne ou un système d'antenne faisant varier la distribution de l’énergie à travers une ouverture rayonnante
84.
TARGET CHARACTERISATION METHOD FOR A DETECTION DEVICE OF MULTI-PANEL RADAR OR SONAR TYPE WITH ELECTRONIC SCANNING
The invention relates to a target characterisation method for a detection device of multi-panel radar or sonar type with electronic scanning, comprising the steps of:
generating a plurality of pulses on a plurality of antenna panels (PE1, PE2, PE3) of the detection device according to a temporal and angular interleaving pattern, so as to perform a scan over all of the relative bearing domain of the detection device;
generating a plurality of detection maps, by the acquisition of a plurality of observations combined with one another by coherent or non-coherent integration of the echoes corresponding to the plurality of pulses, each detection map being obtained in a given direction (EL1, EL2, EL3) corresponding to the width of the main lobe of the antenna panel;
combining the detection maps so as to detect a presence of a target in the relative bearing domain of the detection device.
G01S 7/295 - Moyens pour transformer des coordonnées ou pour évaluer des données, p. ex. en utilisant des calculateurs
G01S 7/41 - Détails des systèmes correspondant aux groupes , , de systèmes selon le groupe utilisant l'analyse du signal d'écho pour la caractérisation de la cibleSignature de cibleSurface équivalente de cible
G01S 7/53 - Moyens pour transformer les coordonnées ou pour évaluer les données, p. ex. utilisant des calculateurs
G01S 7/539 - Détails des systèmes correspondant aux groupes , , de systèmes selon le groupe utilisant l'analyse du signal d'écho pour la caractérisation de la cibleSignature de cibleSurface équivalente de cible
G01S 13/42 - Mesure simultanée de la distance et d'autres coordonnées
G01S 13/89 - Radar ou systèmes analogues, spécialement adaptés pour des applications spécifiques pour la cartographie ou la représentation
G01S 15/42 - Mesure simultanée de la distance et d'autres coordonnées
G01S 15/89 - Systèmes sonar, spécialement adaptés à des applications spécifiques pour la cartographie ou la représentation
85.
METHOD FOR CONTROLLING AT LEAST ONE DRONE AND ASSOCIATED CONTROLLER
Procédé de contrôle d'au moins un drone (12) comprenant au moins un capteur d'images (22) configuré pour observer un motif d'observation (24), le procédé de contrôle comprenant une phase d'exploitation, comprenant des étapes de : - obtention d'une carte d'observation pour une région (16) comprenant une pluralité de zones géographiques, la carte d'observation définissant une partie des zones géographiques de la région (16) comme des zones à observer ; - réception d'une carte d'éclairage, comprenant, pour chaque zone à observer, un état d'observation par le drone (12) ; - réception d'une information de drone relative à une position du drone (12) et/ou une orientation du capteur d'images (22) ; - détermination d'au moins une commande pour le drone (12) par au moins un réseau de neurones.
86.
Method of and system for explainability for link prediction in knowledge graph
There is provided a method and a system for evaluating a relevance score of a given subset of nodes in a knowledge graph (KG) for purpose of link prediction. An ontology used to generate the KG is obtained and clustered to obtain a set of ontology clusters. A set of vectors having been generated by using an embedding model on the KG is obtained and clustered to obtain a set of vector clusters. Training subgraphs are generated based on the set of ontology clusters and the set of vector clusters by removing subsets of nodes from the KG. Respective prediction models are trained on each training subgraph and ranked based on their link predictions. The relevance score of each removed subset of nodes is determined based on the ranked models. A given subset of nodes is provided as a potential explanation based on the relevance score.
Ce procédé de protection d'un flux entrant (10), le flux entrant comportant au moins un flux élémentaire vidéo entrant (11), le flux élémentaire vidéo entrant comportant une succession de paquets vidéo entrants (12), est caractérisé par : le désassemblage (32) du flux entrant pour séparer un paquet courant ; le cryptage du paquet courant avec une clé de session (TEK) ; la construction (35) d'un paquet de métadonnées de confidentialité comportant un champ d'étiquette temporelle correspondant à une étiquette temporelle du paquet courant et un champ de confidentialité reprenant la clé de session ; le chiffrage du paquet de données de confidentialité avec une clé de chiffrage (KEK) ; l'assemblage (36) d'un flux sortant (20) comportant un flux élémentaire sortant regroupant les paquets courants cryptés (22) et d'un flux élémentaire de métadonnées de confidentialité comportant les paquets de métadonnées de confidentialité chiffrés (26).
An antenna system including at least one elementary antenna, a metallic plane provided around the elementary antenna, and a decoupling device arranged on the metallic plane, the decoupling device being of the three-dimensional electromagnetic absorption structure type constituted of a plurality of cells arranged in an array, each cell includes, stacked according to a direction normal to the metal plane, a base surmounted by a raised wall, the antenna system being characterized in that the raised wall is shaped so as to form a recessed pattern for trapping electromagnetic waves.
A method for processing a data stream from an uncertified video source, the data stream being intended to be displayed at least partially on a display screen of a cockpit of an aircraft, the display screen having predetermined dimensions and a predetermined resolution. The processing method comprises a calibration mode comprising a step wherein a window of interest is selected on the display screen of the cockpit by the pilot. The processing method further comprises a step wherein a portion of the data stream corresponding to the selected window of interest is displayed on the display screen.
G06F 3/04886 - Techniques d’interaction fondées sur les interfaces utilisateur graphiques [GUI] utilisant des caractéristiques spécifiques fournies par le périphérique d’entrée, p. ex. des fonctions commandées par la rotation d’une souris à deux capteurs, ou par la nature du périphérique d’entrée, p. ex. des gestes en fonction de la pression exercée enregistrée par une tablette numérique utilisant un écran tactile ou une tablette numérique, p. ex. entrée de commandes par des tracés gestuels par partition en zones à commande indépendante de la surface d’affichage de l’écran tactile ou de la tablette numérique, p. ex. claviers virtuels ou menus
B64D 43/00 - Aménagements ou adaptations des instruments
G06F 3/041 - Numériseurs, p. ex. pour des écrans ou des pavés tactiles, caractérisés par les moyens de transduction
G06F 3/04842 - Sélection des objets affichés ou des éléments de texte affichés
G06F 3/04845 - Techniques d’interaction fondées sur les interfaces utilisateur graphiques [GUI] pour la commande de fonctions ou d’opérations spécifiques, p. ex. sélection ou transformation d’un objet, d’une image ou d’un élément de texte affiché, détermination d’une valeur de paramètre ou sélection d’une plage de valeurs pour la transformation d’images, p. ex. glissement, rotation, agrandissement ou changement de couleur
G06F 3/14 - Sortie numérique vers un dispositif de visualisation
90.
Method for sharing data between aeronautical equipment, related data sharing electronic system and computer program
A method sharing data between aeronautical equipment items. At least one equipment item is included in an aircraft carrying out a flight mission. The method includes obtaining a set of data coming from said equipment item. The method further includes adding of the set of data to a common group including data common to all aeronautical equipment items. The method incudes filtering the data of the common group in order to determine at least one first relevant datum for successfully completing the flight mission. The method incudes transmitting, to at least one other equipment item, of only the at least first relevant datum to be used for a display to a respective user, or for a computation, of a command of the aircraft.
A method allowing an aircraft to follow a lateral path with a determined safety level. The method consists in determining a 3D corridor around a predicted path of the aircraft, based on at least one computed safety distance. If the safety corridor conflicts with at least one obstacle in a terrain and obstacle database, the vertical flight profile of the aircraft is modified in order to increase the altitude of the aircraft, to avoid obstacles while keeping lateral path constant.
G06V 10/80 - Fusion, c.-à-d. combinaison des données de diverses sources au niveau du capteur, du prétraitement, de l’extraction des caractéristiques ou de la classification
The invention relates to a method for allocating time-frequency telecommunication resources in a telecommunication system (10) comprising a satellite (11), user terminals UE (20_1, 20_2), the satellite simultaneously rendering multiple telecommunication beams (B_1, B_2) that are each associated with a separate user terminal UE (20_1, 20_2) and dynamically re-centering each beam on the associated UE; said method comprising: - given a set (80) of grids each representing at least a portion of the Earth's surface and each comprising a plurality of areas, the distance between any two areas of a grid being above a determined non-zero threshold associated with the grid, the time-frequency resources are allocated relative to a time T by applying at least the following rule: a time- frequency resource associated with the grid may be allocated to each of 2 UEs (20_1, 20_2) only if the positions of said 2 UEs are in separate areas of the grid.
A method for allocating time-frequency telecommunication resources in a telecommunication system includes a satellite, user terminals UE (20_1, 20_2), the satellite simultaneously rendering multiple telecommunication beams (B_1, B_2) that are each associated with a separate user terminal UE (20_1, 20_2) and dynamically re-centering each beam on the associated UE; the method comprising: given a set of grids each representing at least a portion of the Earth's surface and each comprising a plurality of areas, the distance between any two areas of a grid being above a determined non-zero threshold associated with the grid, the time-frequency resources are allocated relative to a time T by applying at least the following rule: a time-frequency resource associated with the grid may be allocated to each of 2 UEs (20_1, 20_2) only if the positions of the 2 UEs are in separate areas of the grid.
H04B 7/06 - Systèmes de diversitéSystèmes à plusieurs antennes, c.-à-d. émission ou réception utilisant plusieurs antennes utilisant plusieurs antennes indépendantes espacées à la station d'émission
94.
SYSTEM AND METHOD FOR MANAGING THE OPERATION OF A TRAVELLING WAVE TUBE AMPLIFIER
A satellite system includes a radio frequency signal amplifier device comprising a control and supply module and a plurality of travelling wave tubes. The module is configured to apply to at least one of the tubes an anode voltage operating value, generating a cathode current in response. The module is moreover configured to measure at least one sum of the cathode currents that is associated with the plurality of tubes, the at least one measurement of the sum of the cathode currents being implemented on the basis of a single measuring circuit, and to determine at least one corrected anode voltage operating value, associated with the at least one of the tubes, on the basis of the at least one measurement of the sum of the cathode currents.
H03F 1/06 - Modifications des amplificateurs pour augmenter leur rendement, p. ex. étages classe A à pente glissante, utilisation d'une oscillation auxiliaire dans les amplificateurs à tubes à décharge pour augmenter le rendement de l'amplification des ondes modulées de fréquence radio-électriqueModifications des amplificateurs pour augmenter leur rendement, p. ex. étages classe A à pente glissante, utilisation d'une oscillation auxiliaire dans les amplificateurs à tubes à décharge pour augmenter le rendement des amplificateurs fonctionnant aussi en modulateurs
H03F 3/189 - Amplificateurs à haute fréquence, p. ex. amplificateurs radiofréquence
95.
METHOD FOR REMOTELY CONTROLLING THE FLIGHT OF AN AIRCRAFT, AND ASSOCIATED COMMUNICATION MODULE
A method for remotely controlling the flight of an aircraft following a first flight plan, the aircraft includes a communication module connected to a flight management centre of the aircraft, the communication module being suitable for allowing a communication between a terrestrial communication station and the aircraft, the method comprising the following steps:
determining, in the terrestrial communication station, an incapacity of the pilot or pilots of the aircraft,
using the communication module, receiving a first signal that has been coded using a predetermined code and transmitted by the terrestrial communication station, and then decoding the first signal using the predetermined code, which has previously been stored in the communication module,
after the first signal has been decoded, sending, using the communication module, a command to the flight management centre prompting a second flight plan to be followed by the aircraft.
A scope observing a scene, the scope includes a first optical sub-assembly, called the afocal module, and a second optical sub-assembly, called the display module, the afocal module comprising: a removable and switchable linear polarizer, a first polarization-splitting element, an afocal optical system the first polarization-splitting element the display module comprising: a half-wave plate, called the distribution plate, a display, an optical objective configured to collimate the display light; a second polarization-splitting element arranged after the distribution half-wave plate.
G02B 23/04 - Télescopes ou lunettes d'approche, p. ex. jumellesPériscopesInstruments pour voir à l'intérieur de corps creuxViseursPointage optique ou appareils de visée comprenant des prismes ou des miroirs afin de partager ou de combiner des faisceaux lumineux, p. ex. munis d'oculaires pour plus d'un observateur
F41G 1/30 - Appareils de visée à réflexion spécialement adaptés aux armes à feu individuelles ou aux pièces d'artillerie
F41G 1/38 - Appareils de visée télescopiques spécialement adaptés aux armes à feu individuelles ou aux pièces d'artillerieLeurs supports ou leurs montures
G02B 5/122 - Réflecteurs reflex du type en sommet de cube, en trièdre ou en réflecteur triple
G02B 27/28 - Systèmes ou appareils optiques non prévus dans aucun des groupes , pour polariser
G02F 1/139 - Dispositifs ou dispositions pour la commande de l'intensité, de la couleur, de la phase, de la polarisation ou de la direction de la lumière arrivant d'une source lumineuse indépendante, p. ex. commutation, ouverture de porte ou modulationOptique non linéaire pour la commande de l'intensité, de la phase, de la polarisation ou de la couleur basés sur des cristaux liquides, p. ex. cellules d'affichage individuelles à cristaux liquides caractérisés par l'effet électro-optique ou magnéto-optique, p. ex. transition de phase induite par un champ, effet d'orientation, interaction entre milieu récepteur et matière additive ou diffusion dynamique basés sur des effets d'orientation où les cristaux liquides restent transparents
97.
SYSTEM AND METHOD FOR MANAGING THE OPERATION OF A TRAVELLING WAVE TUBE AMPLIFIER
The proposal is a satellite system (10) comprising a radio frequency signal amplifier device (100) comprising a control and supply module (1040) and a plurality of travelling wave tubes (1020-n). The module (1040) is configured to apply to at least one of said tubes an anode voltage operating value, generating a cathode current in response. The module (1040) is moreover configured to measure at least one sum of the cathode currents that is associated with said plurality of tubes, said at least one measurement of the sum of the cathode currents being implemented on the basis of a single measuring circuit (1044), and to determine at least one corrected anode voltage operating value, associated with said at least one of said tubes, on the basis of said at least one measurement of the sum of the cathode currents.
H03F 3/58 - Amplificateurs utilisant l'effet de temps de transit dans des tubes ou des dispositifs à semi-conducteurs utilisant des tubes à ondes progressives
H03F 3/189 - Amplificateurs à haute fréquence, p. ex. amplificateurs radiofréquence
H03F 3/20 - Amplificateurs de puissance, p. ex. amplificateurs de classe B, amplificateur de classe C
A method for controlling an unmanned aircraft includes determining a maximum flying altitude for a ground position of the aircraft, the method comprising: for each point from a plurality of ground points situated within a perimeter around the ground position of the aircraft, referred to as “surrounding points”, determining one or more intersections between firstly a circle, the centre of which is the point and the radius of which is the maximum authorized ground distance at this point, referred to as the “determination circle”, and secondly a vertical related to the ground position of the aircraft, the circle being contained in a vertical plane comprising the vertical related to the ground position of the aircraft; and for all of the intersections thus obtained, selecting the greatest altitude as the maximum flying altitude.
CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
INSA DE RENNES (France)
NANTES UNIVERSITE (France)
CENTRALESUPELEC (France)
Inventeur(s)
Legay, Hervé
Stoumpos, Charalampos
Fraysse, Jean-Philippe
Abrégé
A device for controlling radiofrequency beams comprising a set of cells. Each cell comprises a support frame and an excitation element, and emits and/or receives beams in an invariant manner according to the direction of propagation of the beam. The frame is inscribed within a generally tubular shape, oriented along the axis Z of a reference frame, having a cross section of perimeter P, and comprises an entrance, an exit and a number N of slots between the exit and a position Zo located between the entrance and the exit. Each slot has a variable width along Z. The slot width has a minimum value at the position Zo, and a maximum value at the exit that is determined on the basis of the perimeter P and the number N.
H01Q 13/08 - Terminaisons rayonnantes de lignes de transmission micro-ondes à deux conducteurs, p. ex. lignes coaxiales ou lignes micro-rayées
H04B 7/06 - Systèmes de diversitéSystèmes à plusieurs antennes, c.-à-d. émission ou réception utilisant plusieurs antennes utilisant plusieurs antennes indépendantes espacées à la station d'émission
An unmanned aircraft includes three parallel beams extending in at least one longitudinal direction X from a rear side to a front side of the aircraft, the central beam forming a main fuselage containing a powertrain, with a propeller of diameter D configured to be driven by the powertrain being attached to a front end of the central beam, each side beam being at a distance L/2 from the central beam and each side beam supporting a radar at a front end of the beam.
B64U 20/87 - Montage des dispositifs d’imagerie, p. ex. montage des suspensions à cardan
B64U 20/70 - Caractéristiques de construction du corps du véhicule aérien sans pilote
B64U 50/20 - Transmission de puissance mécanique à des rotors ou des hélices
G01S 13/933 - Radar ou systèmes analogues, spécialement adaptés pour des applications spécifiques pour prévenir les collisions d'aéronefs ou d'engins spatiaux