09 - Scientific and electric apparatus and instruments
Goods & Services
Thermal imaging cameras; thermal imaging apparatus for night
vision; thermal imaging apparatus [other than for medical
use]; target sights for artillery [telescopic]; target
sights for artillery [electronic]; target sights for
artillery [laser]; target sights for guns [telescopic];
target sights for guns [electronic]; sensors; sensors,
detectors and monitoring instruments; light sensors; air
temperature sensors; active infrared sensors; sensors for
determining position; sensors for monitoring physical
movements; sensors, detectors and monitoring instruments;
gimbals for digital cameras; Thermal imaging cameras;
thermal imaging apparatus for night vision; thermal imaging
apparatus [other than for medical use]; cameras; security
cameras; infrared gun sighting apparatus; fire control
apparatus; surveillance cameras; security surveillance
apparatus; electronic tracking apparatus and instruments;
computer software; computer hardware; software for
situational awareness and alerting; opto-electronics
software; software relating to situational awareness and
decision support; computer software and computer hardware
for recording, detecting, managing, analyzing and providing
insights into images, videos and data; computer software and
computer hardware for recording, detecting, managing,
analyzing and providing insights into images, videos and
data in video management systems, surveillance systems,
sensors; data processing software; target detection
software; image processing software; sensor data processing
software; defence and security data processing software;
computer hardware and software for providing activity event
notifications and alerts and generating activity event
reports; computer software and computer hardware for video
surveillance, data analytics, and operational intelligence;
imaging apparatus; apparatus providing night vision; devices
providing night vision; image identifier night vision
devices; digital sensors; detection apparatus; detectors;
electrical sensors; electronic surveillance apparatus;
intruder identification apparatus [other than for vehicles];
infrared sensors; infrared detectors; infrared cameras;
infrared locating apparatus; infrared detection apparatus;
infrared optical apparatus; infrared devices for aiming
weapons; infrared devices for guiding weapons; motion
detectors; network monitoring cameras namely for
surveillance; target surveillance apparatus [optical];
target surveillance apparatus [electric]; target
surveillance apparatus [electronic]; target trackers
[optical]; target seekers [optical]; target location
apparatus [optical]; threat detection software; video
surveillance cameras.
09 - Scientific and electric apparatus and instruments
Goods & Services
Thermal imaging cameras; thermal imaging apparatus for night
vision; thermal imaging apparatus [other than for medical
use]; target sights for artillery [telescopic]; target
sights for artillery [electronic]; target sights for
artillery [laser]; target sights for guns [telescopic];
target sights for guns [laser]; target sights for guns
[electronic]; sensors; sensors, detectors and monitoring
instruments; meteorological instruments; meteorological
apparatus; temperature sensors; light sensors; distance
sensors; bio-sensors; proximity sensors; vibration sensors;
position sensors; pressure sensors; laser sensors; air
temperature sensors; position determining sensors; position
detection sensors; active infra-red sensors; sensors used in
meteorology; sensors for determining velocity; sensors for
determining position; sensors for monitoring physical
movements; sensors, detectors and monitoring instruments;
gimbals for digital cameras; thermal imaging cameras;
thermal imaging apparatus for night vision; thermal imaging
apparatus [other than for medical use]; cameras; security
cameras; infrared gun sighting apparatus; sighting
telescopes for firearms; telescopes for firearms (sighting
-); laser pointers; fire control apparatus; laser range
finders; surveillance cameras; security surveillance
apparatus; navigation, guidance, tracking, targeting and map
making devices; electronic tracking apparatus and
instruments; computer software; computer hardware; software
for situational awareness and alerting; command and control
software; opto-electronics software; software relating to
situational awareness and decision support; computer
software and computer hardware for recording, detecting,
managing, analyzing and providing insights into images,
videos and data; computer software and computer hardware for
recording, detecting, managing, analyzing and providing
insights into images, videos and data in video management
systems, surveillance systems, security cameras, sensors,
security, and operations systems; military hardware control
software; data processing software; target detection
software; image processing software; sensor data processing
software; defence and security data processing software;
computer hardware and software for providing activity event
notifications and alerts and generating activity event
reports; computer software and computer hardware for video
surveillance, data analytics, and operational intelligence;
computer software for data management, analysis,
interpretation, identification, reporting, and decision
support related to recorded and non-recorded voice, video
and radio; computer software to enable situation planning,
response and analysis; computer software for data
management, analysis, interpretation, identification,
real-time analytics, decision-making, agent guidance and
process automation; imaging apparatus; apparatus providing
night vision; devices providing night vision; image
identifier night vision devices; transceiver; digital
sensors; detection apparatus; detectors; electrical sensors;
electric control panels; electronic surveillance apparatus;
intruder identification apparatus [other than for vehicles];
infrared sensors; infrared detectors; infrared cameras;
infrared locating apparatus; infrared detection apparatus;
infrared optical apparatus; infrared devices for aiming
weapons; infrared devices for guiding weapons; lasers; laser
pointers; motion detectors; network monitoring cameras
namely for surveillance; target surveillance apparatus
[optical]; target surveillance apparatus [electric]; target
surveillance apparatus [electronic]; target trackers
[optical]; target trackers [electric]; target trackers
[electronic]; target seekers [optical]; target location
apparatus [electronic]; target location apparatus
[electric]; target location apparatus [optical]; threat
detection software; video surveillance cameras.
09 - Scientific and electric apparatus and instruments
13 - Firearms; explosives
Goods & Services
Thermal imaging cameras; thermal imaging apparatus for night
vision; thermal imaging apparatus [other than for medical
use]; target sights for artillery [telescopic]; target
sights for artillery [electronic]; target sights for
artillery [laser]; target sights for guns [telescopic];
target sights for guns [laser]; target sights for guns
[electronic]; sensors; sensors, detectors and monitoring
instruments; meteorological instruments; meteorological
apparatus; temperature sensors; light sensors; distance
sensors; bio-sensors; proximity sensors; vibration sensors;
position sensors; pressure sensors; laser sensors; air
temperature sensors; position determining sensors; position
detection sensors; active infrared sensors; sensors used in
meteorology; sensors for determining velocity; sensors for
determining position; sensors for monitoring physical
movements; sensors, detectors and monitoring instruments;
gimbals for digital cameras; thermal imaging cameras;
thermal imaging apparatus for night vision; thermal imaging
apparatus [other than for medical use]; cameras; security
cameras; infrared gun sighting apparatus; sighting
telescopes for firearms; telescopes for firearms (sighting
-); laser pointers; fire control apparatus; laser range
finders; surveillance cameras; security surveillance
apparatus; navigation, guidance, tracking, targeting and map
making devices; electronic tracking apparatus and
instruments; computer software; computer hardware; software
for situational awareness and alerting; command and control
software; opto-electronics software; software relating to
situational awareness and decision support; computer
software and computer hardware for recording, detecting,
managing, analyzing and providing insights into images,
videos and data; computer software and computer hardware for
recording, detecting, managing, analyzing and providing
insights into images, videos and data in video management
systems, surveillance systems, security cameras, sensors,
security, and operations systems; military hardware control
software; data processing software; target detection
software; image processing software; sensor data processing
software; defence and security data processing software;
computer hardware and software for providing activity event
notifications and alerts and generating activity event
reports; computer software and computer hardware for video
surveillance, data analytics, and operational intelligence;
computer software for data management, analysis,
interpretation, identification, reporting, and decision
support related to recorded and nonrecorded voice, video and
radio; computer software to enable situation planning,
response and analysis; computer software for data
management, analysis, interpretation, identification,
realtime analytics, decision-making, agent guidance and
process automation; imaging apparatus; apparatus providing
night vision; devices providing night vision; image
identifier night vision devices; transceiver; digital
sensors; detection apparatus; detectors; electrical sensors;
electric control panels; electronic surveillance apparatus;
intruder identification apparatus [other than for vehicles];
infrared sensors; infrared detectors; infrared cameras;
infrared locating apparatus; infrared detection apparatus;
infrared optical apparatus; infrared devices for aiming
weapons; infrared devices for guiding weapons; lasers; laser
pointers; motion detectors; network monitoring cameras
namely for surveillance; target surveillance apparatus
[optical]; target surveillance apparatus [electric]; target
surveillance apparatus [electronic]; target trackers
[optical]; target trackers [electric]; target trackers
[electronic]; target seekers [optical]; target location
apparatus [electronic]; target location apparatus
[electric]; target location apparatus [optical]; threat
detection software; video surveillance cameras. Grenade launcher.
5.
HYBRID POWER CONTROL ALGORITHM FOR RADIO FREQUENCY TERMINALS
An aircraft satellite communication terminal includes a modem to receive data packets from an aircraft on-board network, encode the data packets, and convert the encoded data packets to intermediate frequency signaling. The terminal includes an upconverter circuit that receives the intermediate frequency signaling and upconverts to satellite carrier frequency signaling. The terminal includes a satellite antenna aperture configured to receive the satellite carrier frequency signaling and transmit the satellite carrier frequency signaling for receipt by a satellite. The terminal includes power measurement circuits configured to measure power at inputs and/or outputs of the terminal components. The terminal includes a power controller configured to control power of the intermediate frequency signaling provided through the output interface of the modem and/or to control power of the satellite carrier frequency signaling provided through the output interface of the upconverter circuit, based on the power measurements by the measurement circuits.
An electronic processing device designed to be onboard an aircraft and including a first reception module that is configured to receive an encrypted message, a second reception module that is configured to receive an associated decrypted message, the decrypted message being calculated by means of a decryption algorithm applied to the encrypted message by a decryption device, external to the processing device, and wherein it further includes a verification module that is configured to verify the behavior of the decryption device by means of a comparison between the encrypted message and the associated decrypted message according to a set of comparison criteria.
H04L 9/32 - Arrangements for secret or secure communicationsNetwork security protocols including means for verifying the identity or authority of a user of the system
7.
Method for detecting an interfering signal in a GNSS receiver and associated detection device
A method for detecting an interfering signal in a GNSS receiver, including calculating k groups of isolated correlators over an integration interval, each group of isolated correlators being composed of the same number and same types of correlators as a tracking group of correlators, the correlators of each group of isolated correlators being ahead of or behind the corresponding correlators of the tracking group, determining a plurality of consecutive phase shifts between the punctual correlators of the groups of isolated correlators, estimating a mean phase shift between the correlators inside the groups of isolated correlators, and detecting an interfering signal by applying a likelihood criterion.
A method of operating a target detection radar following a first mode of operation and at least one second mode of operation, the first mode of operation being a synthetic aperture radar imaging mode and each second mode of operation being different from the first mode of operation, the method including the implementation of several recurrences of a signal emission/reception operation, wherein, for each N, the Nth recurrence of the operation including the following sub-operations: generation of a sequence of consecutive pulses, each pulse of the sequence being associated with a respective mode of operation, emission of the pulses in different frequency bands, and reception of the pulse echoes in a common time window, during the sub-operation of emission, at least one of the pulses, called the out of phase pulse, being emitted with a random phase associated with the number N.
A method for operating a target-detection radar following a first radar mode and a second radar mode corresponding to Doppler modes, the method including the implementation of several recurrences of a signal emission/reception operation, each N-th recurrence of the operation including the following sub-operations: generation of two consecutive pulses associated with different radar modes and different emission directions, emission of the pulses in different frequency bands, and reception in a common time window of the echoes of the pulses.
G01S 7/02 - Details of systems according to groups , , of systems according to group
G01S 13/524 - Discriminating between fixed and moving objects or between objects moving at different speeds using transmissions of interrupted pulse modulated waves based upon the phase or frequency shift resulting from movement of objects, with reference to the transmitted signals, e.g. coherent MTi
G01S 13/53 - Discriminating between fixed and moving objects or between objects moving at different speeds using transmissions of interrupted pulse modulated waves based upon the phase or frequency shift resulting from movement of objects, with reference to the transmitted signals, e.g. coherent MTi performing filtering on a single spectral line and associated with one or more range gates with a phase detector or a frequency mixer to extract the Doppler information, e.g. pulse Doppler radar
G01S 13/58 - Velocity or trajectory determination systemsSense-of-movement determination systems
THALES ALENIA SPACE ITALIA S.P.A. CON UNICO SOCIO (Italy)
Inventor
Ferrero, Mauro
Abstract
The present invention concerns a Contamination Ground Support Equipment - CGSE - (1) designed to be installed in proximity of contamination sensitive surfaces and/or items of a spacecraft such as a satellite for contamination control during ground operations on said spacecraft, wherein said CGSE (1) comprises: a case (100); a real¬ time particle fall out detector (101) arranged inside the case (100) for real-time particulate fall out monitoring; a molecular contamination sensor (102) for real-time molecular fall out monitoring arranged on a side of the case (100); inner and outer PFO witness plates (103); inner and outer MOC witness sensors (104); an inlet and an outlet fluidic interface (105, 106) for purging provisions, arranged on opposite sides of the case (100), and wherein the CGSE (1) is equipped with a baffle (109, 112, 113) arranged on a central portion of the top surface of the case (100) on top of the real-time particle fall out detector (101).
G01N 15/0227 - Investigating particle size or size distribution by optical means using imagingInvestigating particle size or size distribution by optical means using holography
G01N 15/06 - Investigating concentration of particle suspensions
G01N 15/00 - Investigating characteristics of particlesInvestigating permeability, pore-volume or surface-area of porous materials
G01N 1/22 - Devices for withdrawing samples in the gaseous state
A navigation and positioning device including an inertial measurement unit, a receiver for receiving GNSS satellite positioning measurements, a closed-loop primary Kalman filter configured to compute navigation data corrections by hybridizing satellite data and non-satellite data, as well as a bank of N closed-loop secondary Kalman filters, each configured to compute navigation data corrections based solely on the non-satellite positioning data delivered at least by the inertial measurement unit, each secondary Kalman filter of index i, where 1≤i≤N, being able to reconfigure itself to the primary Kalman filter at a time (i−1)T from the start of navigation of the vehicle, and then periodically at a period N×T, T being a predetermined duration.
G01S 19/49 - Determining position by combining or switching between position solutions derived from the satellite radio beacon positioning system and position solutions derived from a further system whereby the further system is an inertial position system, e.g. loosely-coupled
G01S 19/39 - Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
12.
Method for assembling a housing, and associated assembly system and housing
A method for assembling a housing including an electronic board, a solder fillet and a cap, the method including at least the following operations of positioning the electronic board inside a closed enclosure, positioning a solder preform and the cap, the solder preform being interposed between the electronic board and the cap along a stacking direction, injecting a sealing gas until a first pressure of the sealing gas is reached, increasing a temperature to heat the solder preform, the electronic board, the solder preform and the cap being free to move, when the solder preform has reached a first temperature threshold, additionally injecting sealing gas until a second pressure is reached, and decreasing the temperature inside the enclosure.
A cylindrical coaxial combiner includes an inner conductor of rectangular section; an outer cover of rectangular section; a cavity between the inner conductor and the outer cover; two outer conductors disposed at the ends of the outer cover, provided with a coaxial connector at their outer end; power amplifying electronic circuit boards connected electrically to the inner conductor; at least one solid-state amplifier, per power amplifying electronic circuit board; and a cooling circuit comprising at least one through portion configured to make a heat-transfer fluid circulate, to inside the inner conductor of the coaxial combiner, disposed in contact with the rear part of a power amplifying electronic circuit board on which at least one solid-state amplifier is disposed.
A navigation and positioning device including at least an inertial measurement unit, a GNSS measurement receiver, a unit for modeling the displacement(s) of the vehicle, a main Kalman filter calculating navigation data corrections by data hybridization, and at the output of the main Kalman filter at least two distinct Kalman sub-filters including a first Kalman sub-filter calculating navigation data corrections by hybridization of data provided by the inertial measurement unit and by the receiver of GNSS satellite positioning measurements, and a second Kalman sub-filter calculating navigation data corrections by hybridization of data provided by the inertial measurement unit and by the unit for modeling displacement(s) of the vehicle.
G01S 19/47 - Determining position by combining measurements of signals from the satellite radio beacon positioning system with a supplementary measurement the supplementary measurement being an inertial measurement, e.g. tightly coupled inertial
G01S 19/39 - Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
G01S 19/40 - Correcting position, velocity or attitude
15.
Space module designed to be deployed in space to form a space platform and associated space platform
A space module designed to be deployed in space to form a space platform, the space module being formed of a predetermined number of elements all having the same flat shape in an extension plane of the corresponding element, each element being of a predetermined type, with at least one element forming a payload.
B64G 1/22 - Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
16.
Electronic system and method for assisting a civil aircraft operator in decision making with the elaboration of aeronautical indicator(s), related civil aircraft and computer program
An electronic decision-making assistance system for an operator of a civil aircraft, including an electronic display device for displaying information, an electronic production device for producing aeronautical indicators, including an acquisition module for acquiring at least one aeronautical information message including a header and a useful part, the useful part including several data fields, including a free-format text field called free field, a calculation module for calculating a plurality of aeronautical indicators for each aeronautical information message by applying an artificial intelligence (AI) algorithm to the message, the AI algorithm receiving the free field as input and delivering the indicators as output, the indicators being distinct from the data contained in the message, and a display module for displaying a readout of the aeronautical indicators.
The present invention relates to a method for transmitting dynamic coverage availability information between a core network, comprising an access and mobility management function and collaborative with an access network having dynamic coverage, and a user equipment able to connect to the access network, the method comprising the following steps, for the access and mobility management function:
receiving a set of points characterizing anticipated positions of the user equipment,
retrieving dynamic coverage availability information for at least one point belonging to the anticipated positions of the user equipment,
sending to the user equipment a signaling message, in the Non-Access Stratum NAS layer, comprising the retrieved dynamic coverage availability information.
09 - Scientific and electric apparatus and instruments
Goods & Services
Thermal imaging cameras; thermal imaging apparatus for night vision; thermal imaging apparatus [other than for medical use]; target sights for artillery [telescopic]; target sights for artillery [electronic]; target sights for artillery [laser]; target sights for guns [telescopic]; target sights for guns [electronic]; sensors; sensors, detectors and monitoring instruments; light sensors; air temperature sensors; active infrared sensors; sensors for determining position; sensors for monitoring physical movements; gimbals for digital cameras; cameras; security cameras; infrared gun sighting apparatus; fire control apparatus; surveillance cameras; security surveillance apparatus; electronic tracking apparatus and instruments; computer software; computer hardware; software for situational awareness and alerting; opto-electronics software; software relating to situational awareness and decision support; computer software and computer hardware for recording, detecting, managing, analyzing and providing insights into images, videos and data; computer software and computer hardware for recording, detecting, managing, analyzing and providing insights into images, videos and data in video management systems, surveillance systems, sensors; data processing software; target detection software; image processing software; sensor data processing software; defence and security data processing software; computer hardware and software for providing activity event notifications and alerts and generating activity event reports; computer software and computer hardware for video surveillance, data analytics, and operational intelligence; imaging apparatus; apparatus providing night vision; devices providing night vision; image identifier night vision devices; digital sensors; detection apparatus; detectors; electrical sensors; electronic surveillance apparatus; intruder identification apparatus [other than for vehicles]; infrared sensors; infrared detectors; infrared cameras; infrared locating apparatus; infrared detection apparatus; infrared optical apparatus; infrared devices for aiming weapons; infrared devices for guiding weapons; motion detectors; network monitoring cameras namely for surveillance; target surveillance apparatus [optical]; target surveillance apparatus [electric]; target surveillance apparatus [electronic]; target trackers [optical]; target seekers [optical]; target location apparatus [optical]; threat detection software; video surveillance cameras.
A method of facilitating the landing of a civil aircraft on a potential landing zone divided into sub-zones. The method includes a step of producing a digital surface model of the potential landing zone using topographic terrain data. In a placement step, the digital surface model is positioned and/or orientated in space to obtain a placed digital surface model. In a calculation step, an overall risk level is calculated for each sub-zone on the basis of the placed digital surface model and characteristics of the sub-zone including topography, accessibility, loss of visibility, and presence of living beings. A reporting step comprises generating an information signal dependent on the overall risk levels, and/or transmitting a control signal dependent on the overall risk levels.
09 - Scientific and electric apparatus and instruments
13 - Firearms; explosives
Goods & Services
(1) Thermal imaging cameras; thermal imaging apparatus for night vision; thermal imaging apparatus [other than for medical use]; target sights for artillery [telescopic]; target sights for artillery [electronic]; target sights for artillery [laser]; target sights for guns [telescopic]; target sights for guns [laser]; target sights for guns [electronic]; sensors; sensors, detectors and monitoring instruments; meteorological instruments; meteorological apparatus; temperature sensors; light sensors; distance sensors; bio-sensors; proximity sensors; vibration sensors; position sensors; pressure sensors; laser sensors; air temperature sensors; position determining sensors; position detection sensors; active infrared sensors; sensors used in meteorology; sensors for determining velocity; sensors for determining position; sensors for monitoring physical movements; sensors, detectors and monitoring instruments; gimbals for digital cameras; thermal imaging cameras; thermal imaging apparatus for night vision; thermal imaging apparatus [other than for medical use]; cameras; security cameras; infrared gun sighting apparatus; sighting telescopes for firearms; telescopes for firearms (sighting -); laser pointers; fire control apparatus; laser range finders; surveillance cameras; security surveillance apparatus; navigation, guidance, tracking, targeting and map making devices; electronic tracking apparatus and instruments; computer software; computer hardware; software for situational awareness and alerting; command and control software; opto-electronics software; software relating to situational awareness and decision support; computer software and computer hardware for recording, detecting, managing, analyzing and providing insights into images, videos and data; computer software and computer hardware for recording, detecting, managing, analyzing and providing insights into images, videos and data in video management systems, surveillance systems, security cameras, sensors, security, and operations systems; military hardware control software; data processing software; target detection software; image processing software; sensor data processing software; defence and security data processing software; computer hardware and software for providing activity event notifications and alerts and generating activity event reports; computer software and computer hardware for video surveillance, data analytics, and operational intelligence; computer software for data management, analysis, interpretation, identification, reporting, and decision support related to recorded and nonrecorded voice, video and radio; computer software to enable situation planning, response and analysis; computer software for data management, analysis, interpretation, identification, realtime analytics, decision-making, agent guidance and process automation; imaging apparatus; apparatus providing night vision; devices providing night vision; image identifier night vision devices; transceiver; digital sensors; detection apparatus; detectors; electrical sensors; electric control panels; electronic surveillance apparatus; intruder identification apparatus [other than for vehicles]; infrared sensors; infrared detectors; infrared cameras; infrared locating apparatus; infrared detection apparatus; infrared optical apparatus; infrared devices for aiming weapons; infrared devices for guiding weapons; lasers; laser pointers; motion detectors; network monitoring cameras namely for surveillance; target surveillance apparatus [optical]; target surveillance apparatus [electric]; target surveillance apparatus [electronic]; target trackers [optical]; target trackers [electric]; target trackers [electronic]; target seekers [optical]; target location apparatus [electronic]; target location apparatus [electric]; target location apparatus [optical]; threat detection software; video surveillance cameras.
(2) Grenade launcher.
09 - Scientific and electric apparatus and instruments
Goods & Services
(1) Thermal imaging cameras; thermal imaging apparatus for night vision; thermal imaging apparatus [other than for medical use]; target sights for artillery [telescopic]; target sights for artillery [electronic]; target sights for artillery [laser]; target sights for guns [telescopic]; target sights for guns [laser]; target sights for guns [electronic]; sensors; sensors, detectors and monitoring instruments; meteorological instruments; meteorological apparatus; temperature sensors; light sensors; distance sensors; bio-sensors; proximity sensors; vibration sensors; position sensors; pressure sensors; laser sensors; air temperature sensors; position determining sensors; position detection sensors; active infra-red sensors; sensors used in meteorology; sensors for determining velocity; sensors for determining position; sensors for monitoring physical movements; sensors, detectors and monitoring instruments; gimbals for digital cameras; thermal imaging cameras; thermal imaging apparatus for night vision; thermal imaging apparatus [other than for medical use]; cameras; security cameras; infrared gun sighting apparatus; sighting telescopes for firearms; telescopes for firearms (sighting -); laser pointers; fire control apparatus; laser range finders; surveillance cameras; security surveillance apparatus; navigation, guidance, tracking, targeting and map making devices; electronic tracking apparatus and instruments; computer software; computer hardware; software for situational awareness and alerting; command and control software; opto-electronics software; software relating to situational awareness and decision support; computer software and computer hardware for recording, detecting, managing, analyzing and providing insights into images, videos and data; computer software and computer hardware for recording, detecting, managing, analyzing and providing insights into images, videos and data in video management systems, surveillance systems, security cameras, sensors, security, and operations systems; military hardware control software; data processing software; target detection software; image processing software; sensor data processing software; defence and security data processing software; computer hardware and software for providing activity event notifications and alerts and generating activity event reports; computer software and computer hardware for video surveillance, data analytics, and operational intelligence; computer software for data management, analysis, interpretation, identification, reporting, and decision support related to recorded and non-recorded voice, video and radio; computer software to enable situation planning, response and analysis; computer software for data management, analysis, interpretation, identification, real-time analytics, decision-making, agent guidance and process automation; imaging apparatus; apparatus providing night vision; devices providing night vision; image identifier night vision devices; transceiver; digital sensors; detection apparatus; detectors; electrical sensors; electric control panels; electronic surveillance apparatus; intruder identification apparatus [other than for vehicles]; infrared sensors; infrared detectors; infrared cameras; infrared locating apparatus; infrared detection apparatus; infrared optical apparatus; infrared devices for aiming weapons; infrared devices for guiding weapons; lasers; laser pointers; motion detectors; network monitoring cameras namely for surveillance; target surveillance apparatus [optical]; target surveillance apparatus [electric]; target surveillance apparatus [electronic]; target trackers [optical]; target trackers [electric]; target trackers [electronic]; target seekers [optical]; target location apparatus [electronic]; target location apparatus [electric]; target location apparatus [optical]; threat detection software; video surveillance cameras.
09 - Scientific and electric apparatus and instruments
13 - Firearms; explosives
Goods & Services
Thermal imaging cameras; thermal imaging apparatus for night vision; thermal imaging apparatus [other than for medical use]; target sights for artillery [telescopic]; target sights for artillery [electronic]; target sights for artillery [laser]; target sights for guns [telescopic]; target sights for guns [laser]; target sights for guns [electronic]; sensors; sensors, detectors and monitoring instruments; meteorological instruments; meteorological apparatus; temperature sensors; light sensors; distance sensors; bio-sensors; proximity sensors; vibration sensors; position sensors; pressure sensors; laser sensors; air temperature sensors; position determining sensors; position detection sensors; active infrared sensors; sensors used in meteorology; sensors for determining velocity; sensors for determining position; sensors for monitoring physical movements; sensors, detectors and monitoring instruments; gimbals for digital cameras; thermal imaging cameras; thermal imaging apparatus for night vision; thermal imaging apparatus [other than for medical use]; cameras; security cameras; infrared gun sighting apparatus; sighting telescopes for firearms; telescopes for firearms (sighting -); laser pointers; fire control apparatus; laser range finders; surveillance cameras; security surveillance apparatus; navigation, guidance, tracking, targeting and map making devices; electronic tracking apparatus and instruments; computer software; computer hardware; software for situational awareness and alerting; command and control software; opto-electronics software; software relating to situational awareness and decision support; computer software and computer hardware for recording, detecting, managing, analyzing and providing insights into images, videos and data; computer software and computer hardware for recording, detecting, managing, analyzing and providing insights into images, videos and data in video management systems, surveillance systems, security cameras, sensors, security, and operations systems; military hardware control software; data processing software; target detection software; image processing software; sensor data processing software; defence and security data processing software; computer hardware and software for providing activity event notifications and alerts and generating activity event reports; computer software and computer hardware for video surveillance, data analytics, and operational intelligence; computer software for data management, analysis, interpretation, identification, reporting, and decision support related to recorded and nonrecorded voice, video and radio; computer software to enable situation planning, response and analysis; computer software for data management, analysis, interpretation, identification, realtime analytics, decision-making, agent guidance and process automation; imaging apparatus; apparatus providing night vision; devices providing night vision; image identifier night vision devices; transceiver; digital sensors; detection apparatus; detectors; electrical sensors; electric control panels; electronic surveillance apparatus; intruder identification apparatus [other than for vehicles]; infrared sensors; infrared detectors; infrared cameras; infrared locating apparatus; infrared detection apparatus; infrared optical apparatus; infrared devices for aiming weapons; infrared devices for guiding weapons; lasers; laser pointers; motion detectors; network monitoring cameras namely for surveillance; target surveillance apparatus [optical]; target surveillance apparatus [electric]; target surveillance apparatus [electronic]; target trackers [optical]; target trackers [electric]; target trackers [electronic]; target seekers [optical]; target location apparatus [electronic]; target location apparatus [electric]; target location apparatus [optical]; threat detection software; video surveillance cameras. Grenade launcher.
09 - Scientific and electric apparatus and instruments
Goods & Services
Thermal imaging cameras; thermal imaging apparatus for night vision; thermal imaging apparatus [other than for medical use]; target sights for artillery [telescopic]; target sights for artillery [electronic]; target sights for artillery [laser]; target sights for guns [telescopic]; target sights for guns [laser]; target sights for guns [electronic]; sensors; sensors, detectors and monitoring instruments; meteorological instruments; meteorological apparatus; temperature sensors; light sensors; distance sensors; bio-sensors; proximity sensors; vibration sensors; position sensors; pressure sensors; laser sensors; air temperature sensors; position determining sensors; position detection sensors; active infra-red sensors; sensors used in meteorology; sensors for determining velocity; sensors for determining position; sensors for monitoring physical movements; sensors, detectors and monitoring instruments; gimbals for digital cameras; thermal imaging cameras; thermal imaging apparatus for night vision; thermal imaging apparatus [other than for medical use]; cameras; security cameras; infrared gun sighting apparatus; sighting telescopes for firearms; telescopes for firearms (sighting -); laser pointers; fire control apparatus; laser range finders; surveillance cameras; security surveillance apparatus; navigation, guidance, tracking, targeting and map making devices; electronic tracking apparatus and instruments; computer software; computer hardware; software for situational awareness and alerting; command and control software; opto-electronics software; software relating to situational awareness and decision support; computer software and computer hardware for recording, detecting, managing, analyzing and providing insights into images, videos and data; computer software and computer hardware for recording, detecting, managing, analyzing and providing insights into images, videos and data in video management systems, surveillance systems, security cameras, sensors, security, and operations systems; military hardware control software; data processing software; target detection software; image processing software; sensor data processing software; defence and security data processing software; computer hardware and software for providing activity event notifications and alerts and generating activity event reports; computer software and computer hardware for video surveillance, data analytics, and operational intelligence; computer software for data management, analysis, interpretation, identification, reporting, and decision support related to recorded and non-recorded voice, video and radio; computer software to enable situation planning, response and analysis; computer software for data management, analysis, interpretation, identification, real-time analytics, decision-making, agent guidance and process automation; imaging apparatus; apparatus providing night vision; devices providing night vision; image identifier night vision devices; transceiver; digital sensors; detection apparatus; detectors; electrical sensors; electric control panels; electronic surveillance apparatus; intruder identification apparatus [other than for vehicles]; infrared sensors; infrared detectors; infrared cameras; infrared locating apparatus; infrared detection apparatus; infrared optical apparatus; infrared devices for aiming weapons; infrared devices for guiding weapons; lasers; laser pointers; motion detectors; network monitoring cameras namely for surveillance; target surveillance apparatus [optical]; target surveillance apparatus [electric]; target surveillance apparatus [electronic]; target trackers [optical]; target trackers [electric]; target trackers [electronic]; target seekers [optical]; target location apparatus [electronic]; target location apparatus [electric]; target location apparatus [optical]; threat detection software; video surveillance cameras.
Provided is a coverage management network function integrated in a fifth-generation network core configured to operate in collaboration with a satellite system having dynamic coverage, the network core collaborating with an access network (RAN), said coverage management network function responding to the requirements defined for a service-based architecture for a network function, this coverage management network function being further configured to collect coverage information by the satellite system, to process this coverage information according to at least one geographical area defined by another network function of the core network, also satisfying the requirements defined for a service-based architecture, in order to generate access network availability information in real time and provide it to this other network function of the core network. Other embodiments are disclosed.
A protective device for protecting a protruding aerial part of an anemobarometric sensor includes a sheath to protect the protruding part, a gripping handle including a bar that can be grasped between the thumb and the other fingers, and at least one locking element for locking the protective device on the body of the anemobarometric sensor, the protective device not covering up attachment holes intended for attaching the body of the sensor to an aircraft.
A method for locating an aircraft with respect to a landing pad including reflective elements, the method including reception of a reflected signal including a plurality of measurement points presenting a characteristic magnitude, filtering of the plurality of measurement points according to a criterion, determination of a set of filtered measurement points respecting a condition of number and/or relative positioning of the measurement points, selection of a set among the determined sets by minimizing a position offset between the real measurement points and the expected measurement points, and localization of the aircraft based on the positions of the measurement points of the selected set.
The invention relates to an electronic device for generating an obstacle database for an aircraft, comprising an acquisition module for an initial obstacle database, the initial obstacle database including elevation and position data for several obstacles, a creation module for at least one global obstacle volume at least partially encompassing a plurality of obstacles and including an envelope with an upper surface of area greater than a predefined minimum area, the upper surface having a constant elevation value and being, at least at one point, distant from the ground by at least a predefined minimum height, and a generation module for a modified obstacle database from the acquired initial obstacle database, the modified obstacle database including the at least one created global obstacle volume.
An ultracold atom measuring system, the measuring system including an assembly of ultracold atom inertial sensors, each sensor of the assembly being an interferometric sensor configured to measure a physical magnitude by implementing an interferometry sequence, a processing unit configured, for at least one sub-assembly of sensors, to apply a respective interferometry sequence to each sensor of a sub-assembly of sensors, the implementation of the respective interferometry sequences by the at least one sub-assembly of sensors causing the sensors of the sub-assembly to measure the same physical magnitude following a travel trajectory when displaced varying, from one sensor of the sub-assembly to another sensor of the sub-assembly, by at least one trajectory-related parameter.
G01P 15/08 - Measuring accelerationMeasuring decelerationMeasuring shock, i.e. sudden change of acceleration by making use of inertia forces with conversion into electric or magnetic values
G01C 19/64 - Gyrometers using the Sagnac effect, i.e. rotation-induced shifts between counter-rotating electromagnetic beams
G21K 1/00 - Arrangements for handling particles or ionising radiation, e.g. focusing or moderating
30.
Method for simultaneous localization and mapping; associated system and computer program
A method carried out by an on-board calculator on a vehicle, including acquiring a set of points at the current time, delivered by a Doppler radar system of the vehicle, acquiring the attitude of the vehicle at the current time, delivered by a vehicle inertial navigation system, orienting the set of points at the current time with respect to a land reference frame taking into account the attitude at the current time, processing the radial speeds of the points to calculate an estimated speed of the vehicle at the current time, calculating a position of the vehicle at the current time from the estimated speed at the current time, and executing a simultaneous localization and mapping algorithm based on the position of the vehicle at the current time over a plurality of successive times.
G05D 1/246 - Arrangements for determining position or orientation using environment maps, e.g. simultaneous localisation and mapping [SLAM]
G01S 13/28 - Systems for measuring distance only using transmission of interrupted, pulse modulated waves wherein the transmitted pulses use a frequency- or phase-modulated carrier wave with time compression of received pulses
G01S 13/53 - Discriminating between fixed and moving objects or between objects moving at different speeds using transmissions of interrupted pulse modulated waves based upon the phase or frequency shift resulting from movement of objects, with reference to the transmitted signals, e.g. coherent MTi performing filtering on a single spectral line and associated with one or more range gates with a phase detector or a frequency mixer to extract the Doppler information, e.g. pulse Doppler radar
G01S 13/89 - Radar or analogous systems, specially adapted for specific applications for mapping or imaging
An underwater device intended to be towed by a surface ship, the surface ship being capable of including a handling system for stowing and deploying the underwater device. The handling system includes a tow cable and an attachment cable. The underwater device includes a flexible elongate body and a towed body, the towed body being capable of being arranged between the tow cable and the flexible elongate body. The underwater device also includes an intermediate element capable of being arranged between the towed body and the flexible elongate body. The intermediate element is connected to the towed body by a first connection. The intermediate element is connected to the flexible elongate body by a second connection, the first connection being an articulated mechanical connection. The intermediate element is a cable of low stiffness. The underwater device includes a recovery cord.
A display apparatus is provided. The display apparatus includes a waveguide and a collimating optics that are positioned at a first side of the display apparatus and coupled to each other. The display apparatus includes an image source and a collimating optics module arranged at a second side of the display apparatus. The second side of the display apparatus is different from the first side of the display apparatus. The display apparatus includes a coherent fiber bundle (CFB) that is positioned between and coupled to (i) the waveguide and the collimating optics and (ii) the image source and the collimating optics module.
A seat entertainment system includes a display unit, a handheld controller, and an entertainment system controller. The handheld controller includes an input interface with a grid of touch sensitive elements spaced apart on the input interface, and an interchangeable user input pad which overlays and covers the grid of touch sensitive elements and has indicia indicating locations of user selectable functions. The entertainment system controller includes a set of operational functions and a mapping of the operations functions to corresponding different user touch locations in the grid of touch sensitive elements. The entertainment system controller is operative to: receive signaling from the handheld controller indicating where a user has touch selected the interchangeable user input pad; identify one of the operational functions corresponding to the user touch location based on the mapping; and perform the operational function to control an operation of the seat entertainment system.
A ground-based in-flight entertainment (IFE) security correlation system performs operations to receive heartbeat notifications periodically communicated from an aircraft-based IFE security observability system while in-flight. The operations further generate a security alert notification responsive to detecting failure to receive a heartbeat notification from the aircraft-based IFE security observability system within a threshold time of last receipt of a heartbeat notification. Related aircraft-based IFE security observability systems are disclosed.
G08G 5/21 - Arrangements for acquiring, generating, sharing or displaying traffic information located onboard the aircraft
G08G 5/26 - Transmission of traffic-related information between aircraft and ground stations
G08G 5/55 - Navigation or guidance aids for a single aircraft
H04L 67/12 - Protocols specially adapted for proprietary or special-purpose networking environments, e.g. medical networks, sensor networks, networks in vehicles or remote metering networks
A power divider/combiner component of the coaxial guide type, characterized in that it is fabricated using “substrate integrated waveguide” technology, in a multilayer integrated circuit board, which includes a stack of a plurality of conductive layers separated from each other by insulating layers.
A ground-based in-flight entertainment (IFE) security correlation system performs operations to receive heartbeat notifications periodically communicated from an aircraft-based IFE security observability system while in-flight. The operations further generate a security alert notification responsive to detecting failure to receive a heartbeat notification from the aircraft-based IFE security observability system within a threshold time of last receipt of a heartbeat notification. Related aircraft-based IFE security observability systems are disclosed.
A spectrometer including a slit suitable for receiving a light beam, a detector, a diffraction grating with at least one curvature, a collimating lens capable of sending the light beam from the slit onto the diffraction grating so as to obtain a plurality of diffracted beams, a deflecting mirror capable of reflecting the plurality of diffracted beams, and a focusing lens capable of receiving the plurality of reflected diffracted beams and focusing them on the detector, at least one optic, referred to as an optimized optic, from among the collimating lens, deflecting mirror, and focusing lens, so as to improve the image quality of the image generated by the detector from the plurality of diffracted beams.
09 - Scientific and electric apparatus and instruments
12 - Land, air and water vehicles; parts of land vehicles
13 - Firearms; explosives
Goods & Services
Missile guidance systems; missile aiming systems; missile
warning systems; missile trackers; missile launch control
apparatus; apparatus for the automatic control of missiles;
apparatus for the remote control of missiles; apparatus for
signalling missiles; sensors for tracking missiles in
flight; flight path controls for missiles; optical apparatus
for use in guiding missiles; weapons control apparatus;
weapons control installations; apparatus for the guidance of
weapon systems; electric control apparatus for military
weapons; electronic control apparatus for military weapons;
optical apparatus for use in aiming weapons; military
electronic apparatus; signal analysis apparatus for use in
weapon control systems; apparatus for the automatic control
of vehicles, armoured vehicles and combat vehicles;
apparatus for the control and remote control of missiles,
vehicles, armoured vehicles and combat vehicles; electric
control apparatus for motor land vehicles, armoured
vehicles, combat vehicles and missiles; electronic control
apparatus, electric control apparatus and remote control
apparatus for missiles, vehicles, armoured vehicles, combat
vehicles, missile systems, weapon systems, naval strike
missile systems, combat systems, coastal defence systems and
defence systems; signalling apparatus for vehicles, armoured
vehicles and combat vehicles and missiles; signalling
apparatus and instruments for missiles, vehicles, armoured
vehicles, combat vehicles, missile systems, weapon systems,
naval strike missile systems, combat systems, coastal
defence systems and defence systems; sensors, detectors and
monitoring instruments for missiles, vehicles, armoured
vehicles, combat vehicles, missile systems, weapon systems,
naval strike missile systems, combat systems, coastal
defence systems and defence systems; apparatus and
instruments that transmits, receives and processes
information relating to missile systems, weapon systems,
naval strike missile systems, combat systems, coastal
defence systems and defence systems; electronic apparatus
and instruments for measuring, navigation, communication,
signalling, control, supervision and data management of
missiles, vehicles, armoured vehicles, combat vehicles and
weapons; installations for monitoring component functions of
vehicles, armoured vehicles and combat vehicles and
missiles; remote controls for operating vehicles (other than
toy vehicles); strategic telecommunication apparatus for
land vehicles, armoured vehicles and combat vehicles;
electrical communications apparatus adapted for use on
vehicles, armoured vehicles and combat vehicles; apparatus
for remote control of automatically guided vehicles,
armoured vehicles and combat vehicles; control modules for
vehicles and vehicle systems (on-board computers) including
armoured vehicles and combat vehicles; apparatus for the
remote control of industrial operations; apparatus for use
in remote control (other than remote controls for toys);
flight path controls for projectiles; optical apparatus for
use in guiding projectiles; sensors for tracking projectiles
in flight; apparatus for the control of unmanned flying
objects; apparatus for the directional guidance of unmanned
flying objects; electronic control installations and
communications installations for tactical defence, missile
systems, weapons systems, naval strike missile systems,
combat systems, coastal defence systems and defence systems;
electronic apparatus for jamming weapons systems; encoded
programs for weapon systems computers; encryption apparatus
for use in weapons guidance systems; scientific, research,
navigation, surveying, photographic, cinematographic,
audiovisual, optical, weighing, measuring, signalling,
detecting, testing, inspecting, life-saving and teaching
apparatus and instruments relating to missile systems,
weapon systems, naval strike missile systems, combat
systems, coastal defence systems and defence systems;
electrical and electronic control systems, apparatus,
components, instruments and equipment; computers; firmware;
computer hardware, apparatus, networks and systems;
telecommunications and communications software, hardware,
apparatus, equipment, networks, installations and systems;
military communications software, hardware, apparatus,
equipment; telecommunications and communications networks,
installations and systems; radar apparatus; target tracking
apparatus; target surveillance apparatus; target recognition
apparatus; data communications apparatus, hardware,
installations and software (downloadable); data processing
apparatus, equipment, programmes and systems; computer
software, application software, downloadable software and
downloadable software applications (apps) including those
used to implement, integrate, access, connect, control,
coordinate, monitor, operate, navigate, guide, deploy,
supervise and manage missile systems, weapon systems, naval
strike missile systems, combat systems, coastal defence
systems and defence systems; software for the integration of
missile systems with naval platforms and utility vehicles;
software (downloadable), apparatus, networks and systems for
monitoring, tracking, reporting, collecting, storing,
organising and analysing data and information relating to
missile systems, weapon systems, naval strike missile
systems, combat systems, coastal defence systems and defence
systems; software for the navigation and remote control of
missiles, vehicles, armoured vehicles, combat vehicles and
weapons systems; software for the diagnostic testing of
missile systems, weapon systems, naval strike missile
systems, combat systems, coastal defence systems and defence
systems; software for simulation and training for missile
systems, weapon systems, naval strike missile systems,
combat systems, coastal defence systems and defence systems;
security and encryption software for missile systems
communication; apparatus and equipment for capturing,
displaying, processing, storing and transmitting data;
information storage apparatus and devices (electric or
electronic); electronic apparatus for recording,
transmission, reproduction, reception, processing,
retrieval, analysis, display and printing of sound, images
and/or data; data carriers (blank); global positioning
system (GPS) tracking and location devices; navigation,
guidance, tracking, targeting and mapping devices; machine
readable data carrying apparatus; databases; computer
databases; computer, data and local area networks; digital
electronic devices, wireless devices and internet-capable
devices; electronic publications (downloadable); electronic
and recorded multimedia publications; computer based
training apparatus; education, interactive and simulation
software; training apparatus, software and simulators;
teaching and instructional apparatus; instructional and
teaching apparatus and instruments; training aids (apparatus
for teaching people); training guides in the form of a
computer program; training manuals in electronic format;
training materials (apparatus); downloadable and electronic
materials and resources including books, electronic books,
audio books, booklets, charts, maps, magazines, newsletters,
guides, catalogues, articles and periodicals; geographical
and road maps, electronic; charts, electronic; downloadable
video files, image files and audio files; electronic control
stations (apparatus) as centres of operation for missile
systems, weapon systems, naval strike missile systems,
combat systems, coastal defence systems and defence systems;
all associated parts, accessories and fittings for the
aforesaid goods in this class. Military vehicles; vehicles adapted for military purposes;
vehicles adapted for missiles; vehicles adapted for use with
weapons; vehicles adapted for combat; vehicles adapted for
naval strike missile systems; vehicles adapted for combat
systems; vehicles adapted for coastal defence systems;
vehicles adapted for defence systems; land vehicles for
military use; combat vehicles; military vehicles for
transport; armoured vehicles; armoured land vehicles; armour
protected land vehicles; wheeled military vehicles; vehicles
adapted for operation by remote control; remote control
vehicles (other than toys); remote controlled vehicles;
remotely operated vehicles; remote controlled flying
vehicles; operator-controlled vehicles; trucks being motor
land vehicles; tank (tanker) trucks; utility vehicles;
unmanned vehicles; unmanned vehicles, equipped with airborne
apparatus for causing aircraft to change course; military
aircraft; military drones; security systems for vehicles
(other than locks); electrical security apparatus for
vehicles, other than electric locks; electronic security
apparatus for vehicles, other than electric locks; all
associated parts, accessories and fittings for the aforesaid
goods in this class. Vehicles equipped with weapon systems; vehicles equipped
with missiles; vehicles equipped with naval strike missile
systems; vehicles equipped with combat systems; vehicles
equipped with coastal defence systems; vehicles equipped
with defence systems; armoured combat vehicles; motorized
military vehicles equipped with weapon systems; motorized
military vehicles equipped with weapon launchers; missiles;
naval strike missiles; guided missiles; guided projectiles;
guided rockets; guided weapons; projectiles (weapons);
firearms; ammunition; explosives; infantry weapons;
conventional air delivered weapons; tanks (weapons);
ammunition for tanks (weapons); weapon apparatus; weapon
installations; weapon systems; weapons for launching
missiles; weapons for launching projectiles; weapon carriage
apparatus for installation on land vehicles; weapon carriage
apparatus for installation on military vehicles; weapon
carriage apparatus for installation on military craft;
weapon release apparatus for installation on land vehicles;
weapon release apparatus for installation on military craft;
weapon carriage and release apparatus and equipment;
projecting apparatus for missiles, projectiles and weapons;
releasing apparatus for missiles, projectiles and weapons;
motorized apparatus for launching weapons; fastening point
systems for missiles, projectiles and weapons; weapon
mounts; armaments; armaments installations; apparatus for
launching weapons; armament systems for armoured vehicles;
apparatus for firing weapons; apparatus for use in the
firing of missiles; launchers for projectiles; defence
apparatus (weapons); defence installations (weapons); decoy
apparatus (weapon); decoy installations (weapon); unmanned
remote-controlled powered aircraft for use as targets for
military use; targets for military use; containers
specifically adapted for storing and launching weapons;
missile launching systems; tactical guided missile
apparatus; tactical guided missile installations; all
associated parts, accessories and fittings for the aforesaid
goods in this class.
39.
Evaluation method of the level of fatigue of an operator and associated evaluation system
A method of evaluation of the level of fatigue of an operator implemented by a transportable evaluation device, the method including identification of the operator, acquisition or determination of contextual data relating to the context in which the evaluation is implemented, acquisition of physiological data of the operator, analysis of all the data acquired or determined for determining the level of fatigue of the operator, and communication of the determined level of fatigue.
G16H 50/30 - ICT specially adapted for medical diagnosis, medical simulation or medical data miningICT specially adapted for detecting, monitoring or modelling epidemics or pandemics for calculating health indicesICT specially adapted for medical diagnosis, medical simulation or medical data miningICT specially adapted for detecting, monitoring or modelling epidemics or pandemics for individual health risk assessment
A61B 5/00 - Measuring for diagnostic purposes Identification of persons
A61B 5/16 - Devices for psychotechnicsTesting reaction times
A61B 5/18 - Devices for psychotechnicsTesting reaction times for vehicle drivers
40.
Determining method of a statistic fatigue level relative to a population of operators and associated determining system
A method for determining a statistical fatigue level, including acquiring a plurality of operator assessment data determined from operator physiological data, acquiring a plurality of general context data, acquiring a plurality of particular context data, pre-processing all the data acquired, acquiring a time range for determining the level of statistical fatigue and acquiring a filter criterion, the filter criterion being based on the general context data and/or the particular context data, and determining, from the pre-processed data set, a statistical fatigue level according to the filter criterion acquired over the acquired time range.
A method for evaluating the fatigue level of an operator during a mission, the method including the following phases implemented by one or more portable evaluation devices: an initial collection phase implemented before the mission and including an operation of acquiring personal and physiological data of the operator, and a final collection phase implemented after the mission and including an operation of acquiring data related to the mission, the method further including an analysis phase including an operation of analyzing all the collected data and an operation of determining the operator's fatigue level before and/or after their mission through this analysis.
A61B 5/16 - Devices for psychotechnicsTesting reaction times
A61B 5/00 - Measuring for diagnostic purposes Identification of persons
A61B 5/18 - Devices for psychotechnicsTesting reaction times for vehicle drivers
G16H 10/20 - ICT specially adapted for the handling or processing of patient-related medical or healthcare data for electronic clinical trials or questionnaires
G16H 40/67 - ICT specially adapted for the management or administration of healthcare resources or facilitiesICT specially adapted for the management or operation of medical equipment or devices for the operation of medical equipment or devices for remote operation
42.
Method for determining an objective fatigue level of an operator performing a mission, associated determination system and method for estimating and determining such a fatigue level
A method for determining an objective level of fatigue of an operator performing a mission, the method including acquisition of a first estimation of fatigue from a biomathematics model of prediction of fatigue from plurality of mission data related to the mission, acquisition of a second estimation of fatigue from a physiological model of prediction of fatigue from physiological data of the operator, and determination of an objective level of fatigue by merging the two estimations of fatigue.
G16H 40/63 - ICT specially adapted for the management or administration of healthcare resources or facilitiesICT specially adapted for the management or operation of medical equipment or devices for the operation of medical equipment or devices for local operation
43.
Characterizing Method of Aeronautic Routes and Associated Characterizing System
A method for characterizing aeronautic routes, each aeronautic route featuring a sequence of flights performed by the same operator, the method including acquisition of a plurality of evaluation data relative to a population of operators, the evaluation data being determined from operator physiological data, preprocessing of the evaluation data, acquisition of a plurality of specific context data relative to the specific evaluation context of the operators, extraction from the specific context data, of data on flights performed by the operators and identification of a plurality of corresponding aeronautic routes, and for each identified aeronautic route, determination of a fatigue indicator based on the evaluation data of the operators having performed this route.
Various embodiments of the present disclosure are directed to an IFE system including at least one network interface, at least one processor connected to communicate through the at least one network interface, and at least one memory storing instructions executable by the at least one processor to perform operations. The operations include obtaining an aircraft geographic location and heading. The operations also include selecting a set of AOEs from an AOEs database that satisfy a relevance rule to what is viewable by a passenger through a window of an aircraft. The operations also include communicating with a display device to display an indication of the AOEs in the selected set which are viewable by the passenger.
The present invention relates to a gyroscopic measurement method by means of a sensor (10) comprising a housing (12) and a vibrating element (15) able to vibrate relative to the housing (12) simultaneously according to a direction (x) of a pilot mode and a direction (y) of a detection mode, comprising the control (110) of a first and a second vibration amplitude of the vibrating element (15) according to the directions of the pilot mode and detection mode respectively to a predetermined pilot amplitude (xmax) and detection amplitude (ymax), and the determination (120) of an instantaneous angular speed (Ωmes) of the housing (12).
The present invention relates to a gyroscopic measurement method by means of a sensor (10) comprising a housing (12) and a vibrating element (15) able to vibrate relative to the housing (12) simultaneously according to a direction (x) of a pilot mode and a direction (y) of a detection mode, comprising the control (110) of a first and a second vibration amplitude of the vibrating element (15) according to the directions of the pilot mode and detection mode respectively to a predetermined pilot amplitude (xmax) and detection amplitude (ymax), and the determination (120) of an instantaneous angular speed (Ωmes) of the housing (12).
A predetermined bias (ξ(t)) is introduced into a measurement of an angular position (θ) of the direction (x) of the pilot mode used to determine a biased force (Fass,bias) to be exerted on the vibrating element (15) for the control of the first and/or second vibration amplitude, to cause controlled rotation of the direction (x) of the pilot mode in the plane of vibration (XY).
The present invention relates to a method (400) of gyroscopic measurement by means of a sensor (10) comprising a housing (12) and a vibrating element (15) apt to vibrate relative to the housing (12) comprising supplying a first servo module (20) with a first force (Fx) to be exerted along the direction of the pilot mode (x) on the vibrating element (15), and a pilot amplitude (xmax) for servoing the vibrations along the direction of the pilot mode (x); the simultaneous use of the first force (Fx) and of the servoing of the vibrating element (15) along the direction (x) of the pilot mode; the supply to a second servo module (25) of a second force (Fy) to be exerted in phase quadrature with the first force along the direction of the detection mode (y), and a non-zero vibration servo amplitude (ymax) along the direction (y) of the detection mode; the simultaneous use of the second force (Fy) and of the servoing along the direction (y) of the detection mode; and the determination of an instantaneous angular speed (Ω(t)) of the housing in an inertial frame of reference.
The present invention relates to a sensor (10) comprising a housing (12) and a vibrating element (15) apt to vibrate relative to the housing (12), comprising:
an initialization (410), to provide a pilot amplitude (xmax), a detection amplitude (ymax), an adjustment command (Tth) of predetermined spectral signature, and a calibration angular speed (Ωcal);
a calibration (420), comprising the servoing to the pilot amplitude and to the detection amplitude of the vibrations of the vibrating element (15) along the direction (x) of the pilot mode and the direction (y) of the detection mode, and simultaneously the exertion of a first stable force (Fy,phase,suppapp) configured not to disturb the measurement of the sensor (10) from the adjustment command (Tth), as well as the application of a second force (Fy,quadapp) determined on the basis of the spectral signature of the adjustment command so as to cause a rotation of the direction of the pilot mode, an instantaneous angular speed (Ω(t)) of the housing (12) being imposed as equal to the calibration angular speed (Ωcal), and the determination of a reference angular speed (Ωref);
an acquisition (430), analogous to the calibration but with a free instantaneous angular speed (Ω(t)); a determination (440) of a measured instantaneous angular speed (Ωmes(t)).
The present invention relates to a finite impulse response filtering method, including acquisition of a digital signal corresponding to an analog signal converted by an analog/digital converter, application of a digital processing to the digital signal in order to transform the signal into a sum of a time-variable part and a time-constant part, removal of the variable part of the transformed digital signal so as to obtain a constant digital signal, by applying a sequence of a plurality of sinusoidal band-stop filters, digital processing of the constant digital signal so as to obtain an amplitude of the signal, and transmission of the amplitude to an application software.
A computer-implemented method comprising: receiving, at a first point in time, a first data set from a user and upon receipt of the first data set: performing feature extraction on the first data set to obtain a first feature vector, generating a first integer vector representation of the first feature vector, generating, using the first integer vector representation and a master key, a user-specific key, and sending, to a remote server, a user ID together with the user-specific key.
H04L 9/32 - Arrangements for secret or secure communicationsNetwork security protocols including means for verifying the identity or authority of a user of the system
A method for detecting an anomaly in an electronic system in operation, in particular a cyberattack, the electronic system including processors that are each composed of hardware blocks, the processor being capable of executing an application with the application interacting with the hardware blocks. The detection method includes at least measuring, when the electronic system is in operation, at least one parameter representative of the interactions of the application with one of the hardware blocks, comparing each measurement with an associated reference dataset to detect potential inconsistencies between the measurement and the reference dataset, the reference dataset being representative of the operation of the electronic system when no anomalies are present, and sending an alert according to an alert criterion relating to the one or more detected inconsistencies.
G06F 21/55 - Detecting local intrusion or implementing counter-measures
54.
METHOD AND SYSTEM FOR REAL-TIME PERFORMANCE EVALUATION OF AN AIR TRAFFIC SURVEILLANCE SYSTEM, AS WELL AS A REAL-TIME MANAGEMENT METHOD FOR SAID SURVEILLANCE SYSTEM
A method and a system are described for the real-time evaluation of the performance of a cooperative air traffic surveillance system, designed to monitor the presence and movements of mobiles (A, C) within a surveillance region (CV), wherein a plurality of receiving stations (R1-R3; R) is configured to receive respective identification signals from mobiles, wherein the surveillance region (CV) includes at least one operational service volume (SV) and is divided into monitoring cells. A plurality of identification signals associated with a respective mobile (A; C) present in the surveillance region (CV) over a predetermined time interval forms a track or report of the mobile. A plurality of surveillance system performance metrics obtainable from the identification signals is selected, and the values of the selected performance metrics are calculated for at least each monitoring cell that at least partially covers an operational service volume (SV) and for each monitoring cell where at least one selected metric has values below a predetermined minimum value, an overall performance level or system state within the cell is determined according to a predefined correlation matrix among the selected evaluation metrics.
G01S 5/02 - Position-fixing by co-ordinating two or more direction or position-line determinationsPosition-fixing by co-ordinating two or more distance determinations using radio waves
G08G 5/22 - Arrangements for acquiring, generating, sharing or displaying traffic information located on the ground
G08G 5/72 - Arrangements for monitoring traffic-related situations or conditions for monitoring traffic
55.
QUICK CONNECT/DISCONNECT CONNECTION UNIT WITH DUST BARRIER FOR FLUIDIC LINES
THALES ALENIA SPACE ITALIA S.P.A. CON UNICO SOCIO (Italy)
Inventor
Ferroni, Stefano
Abstract
A connection unit (1) comprising at least a first and a second connector (2, 3) connectable to respective circuit branches of a fluidic line and provided with respective first sealing elements (20, 80) configured to assume a closed position wherein they block flow through the respective connector (2, 3) and an open position wherein they allow flow through the respective connector (2, 3), respective second sealing elements (11, 90) suitable for cooperating with each other to establish a fluidic connection between said connectors (2, 3), a pre-coupling device (38, 84) configured to define a mechanical pre-coupling condition of said connectors (2, 3) in which the respective first sealing elements (20, 80) are held in the closed position, and a locking device (63) configured to define a connection condition of the connectors (2, 3) wherein the first sealing elements (20, 80) are in the open position and the respective second sealing elements (11, 90) are sealingly coupled together; the connection unit (1) comprises a sealing system (96) active in the condition of mechanical pre-coupling and connection between the connectors (2, 3) and configured to protect the first sealing elements (20, 80) and the second sealing elements (11, 90) from the entry of external agents.
F16L 37/113 - Couplings of the quick-acting type in which the connection between abutting or axially-overlapping ends is maintained by locking members using a rotary external sleeve or ring on one part the male part having lugs on its periphery penetrating into the corresponding slots provided in the female part
F16L 37/34 - Couplings of the quick-acting type with fluid cut-off means with fluid cut-off means in each of two pipe-end fittings at least one of two lift valves being opened automatically when the coupling is applied at least one of the lift valves being of the sleeve type, i.e. a sleeve being telescoped over an inner cylindrical wall
F16L 37/36 - Couplings of the quick-acting type with fluid cut-off means with fluid cut-off means in each of two pipe-end fittings with two lift valves being actuated to initiate the flow through the coupling after the two coupling parts are locked against withdrawal
56.
QUICK CONNECT/DISCONNECT CONNECTION UNIT FOR FLUIDIC LINES
THALES ALENIA SPACE ITALIA S.P.A. CON UNICO SOCIO (Italy)
Inventor
Ferroni, Stefano
Abstract
A connection unit comprising at least a first and a second connector (2, 3) connectable to respective circuit branches of a fluidic line and provided with respective first sealing elements (20, 80) configured to assume a closed position wherein they block flow through the respective connector (2, 3) and an open position wherein they allow flow through the respective connector (2, 3), respective second sealing elements (11, 90) adapted to cooperate with each other to establish a fluidic connection between said connectors (2, 3), a pre-coupling device (38, 84) configured to define a mechanical pre-coupling condition of said connectors (2, 3) in which the respective first sealing elements (20, 80) are held in the closed position, and a locking device (63) configured to define a connection condition of the connectors (2, 3) wherein the first sealing elements (20, 80) are in the open position and the respective second sealing elements (11, 90) are sealingly coupled together, the unit comprises a control element (47) movable between a first rest position and a second position and a snap-action drive mechanism (95, 50, 62, 18) comprising elastic means (95) configured to accumulate elastic energy during at least a first portion of the stroke of the control element (47) between the first and second positions, the snap-action drive mechanism (95, 50, 62, 18) being activatable at least indirectly by the control element (47) at the end of its stroke to bring the connectors (2, 3) from the connection position to the pre-coupling position under the thrust of said elastic means (95).
F16L 37/113 - Couplings of the quick-acting type in which the connection between abutting or axially-overlapping ends is maintained by locking members using a rotary external sleeve or ring on one part the male part having lugs on its periphery penetrating into the corresponding slots provided in the female part
F16L 37/34 - Couplings of the quick-acting type with fluid cut-off means with fluid cut-off means in each of two pipe-end fittings at least one of two lift valves being opened automatically when the coupling is applied at least one of the lift valves being of the sleeve type, i.e. a sleeve being telescoped over an inner cylindrical wall
F16L 37/36 - Couplings of the quick-acting type with fluid cut-off means with fluid cut-off means in each of two pipe-end fittings with two lift valves being actuated to initiate the flow through the coupling after the two coupling parts are locked against withdrawal
The invention relates to measuring equipment, comprising a heating device, and intended to be arranged externally, at the skin of a vehicle which can move in a hostile climate environment with icing climate conditions, said equipment corresponding to a body consisting of a mast supporting a tube closed at one of the ends thereof, the heating device being intended to be housed within said tube and comprising at least one heating wire coiled inside the body of said tube, according to a bridged coiling defined by the presence of a bridge (P), the bridge corresponding to a portion of heating wire overlapping, along the axis of said tube, a predetermined number of turns of the end of said coiling located near the open end (12) of said tube, the overlapping turns being evenly spaced at a predetermined pitch associated with the overlapping zone.
A transportable system of evaluation of a level of fatigue of at least one operator. The system includes a case, a camera configured to acquire images of the face of an operator, a sensor configured to measure a heart rate of the operator, a calculator, and a human-machine interaction device. The calculator is configured to receive the images acquired from the camera and the measurement of the heart rate from the sensor, and configured to process the images and the measurement to calculate a level of fatigue of the operator. The human-machine interaction device is configured to transmit an alert if the calculated level of fatigue is greater than a predefined threshold. The calculator and the human-machine interaction device are at least partially integrated into the case. The camera and the sensor are integrated or apt to be stowed in the case.
G08B 25/01 - Alarm systems in which the location of the alarm condition is signalled to a central station, e.g. fire or police telegraphic systems characterised by the transmission medium
59.
Improved multi-port elementary antenna and associated active electronically scanned array antenna
Centre national de la recherche scientifique (France)
INSTITUT POLYTECHNIQUE DE BORDEAUX (France)
Inventor
Ghiotto, Anthony
Le Gall, Timothée
Varault, Stefan
Louis, Bruno
Abstract
The elementary antenna includes a radiating element, provided with N excitation zones, and a transmit and receive module, including, for each integer i between 1 and N, an i-th chain connected, via an i-th feed line to the i-th excitation zone, the i-th chain including an i-th amplifier. The elementary antenna includes, in the i-th chain, an i-th robustness phase shifter on a first side of the i-th amplifier, between the i-th amplifier and the radiating element, and an i-th compensation phase shifter on a second side of the i-th amplifier, opposite the first side. The sum of phases brought in by the i-th robustness phase shifter and compensation phase shifter is constant whatever the chain considered, and the phase brought in by the i-th robustness phase shifter is strictly different from the phase brought in by the other robustness phase shifters of the other chains of the elementary antenna.
H01Q 3/30 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the relative phase or relative amplitude of energisation between two or more active radiating elementsArrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system varying the distribution of energy across a radiating aperture varying the phase
A method for establishing a communication of the IP multimedia subsystem in local routing mode where user data are routed directly at one or more interconnected satellites, without passing through the ground, between two UE terminals connected to a regenerative satellite of a communication network comprising a satellite constellation. A session control function of the IMS core network interrogates a server linked to the satellite constellation with the information relating to the satellite access networks of the two terminals. The server is able to determine, by verification of an inter-satellite link between the regenerative satellites corresponding to the information relating to the satellite access networks of the two terminals, whether local routing of the user plane without passing through the ground is available to directly connect the two terminals are connected by link.
A method for maintaining a secure channel between a client and a server through a wireless network, a secret being shared between the client and the server. the method including while the client is in sleep mode and data must be transmitted from the client to the server, wake-up of the client and initiating, by the client, a procedure for restoring the secure channel by transmitting to the server a change of state wake-up message, protected by using the secret, and while the client is in sleep mode and that data must be transmitted from the server to the client, wake-up of the client by the server by means of the transmission of a paging message and launching by the client, the restoring procedure of the secure channel by transmitting to the server, a change of state wake-up message using the secret.
The present invention relates to a method for enriching a structured database intended to assist a pilot of an aircraft in decision-making. The method comprises the following steps:
obtaining an initial structured database, called the initial structured base, comprising a plurality of objects,
determination of at least two indicators from the group of indicators consisting of: a frequency indicator, an interconnection indicator, a relevance indicator, and a precision indicator,
comparison of each determined indicator with at least one respective threshold,
if the result of the comparison is negative, sending an enrichment command of the initial structured database to form an enriched structured database, called enriched structured base, comprising a larger number of objects than the initial structured base.
A docking station for storing a handset. A storage tray has a first recessed area for storing the handset and a second recessed area for a passenger to grip a top surface of the stored handset. The docking station includes a second latch extended into the second recessed area to engage an indent in the bottom surface of the handset. The docking station includes a first latch extended into the second recessed area to engage an indent located in the front surface of the handset. Depression of a release actuator retracts the first latch to release the top surface of the handset. The release actuator extends through an opening in the first recessed area, which has a length sufficient to allow a finger to actuate the release actuator and grip the top surface of the remote control handset while the remote control handset is stored in the storage tray.
An input/output control system for at least one avionics application including at least two computing platforms implemented using similar hardware and software resources, each platform including a primary stage configured to acquire analogue signals, an intermediate stage configured to digitally process digital signals, a final stage configured to make digital data available to the avionics application, a hardware monitoring module configured to implement an operating test by injecting predetermined test signals into the primary stage, and a software monitoring module configured to acquire digital data corresponding to the injected test signals, and to check that they correspond to predetermined values.
G01R 31/00 - Arrangements for testing electric propertiesArrangements for locating electric faultsArrangements for electrical testing characterised by what is being tested not provided for elsewhere
B64F 5/60 - Testing or inspecting aircraft components or systems
A centralized satellite quantum cryptographic key pairing method for ground stations includes a quantum key distribution step, wherein, for each station, a cryptographic key is shared through quantum communication between the station and a satellite; a centralized key storage step, wherein each key is first transmitted in encrypted form from the satellite to a terrestrial central key management unit (UC), and then stored by this unit (UC); and a pairing step between a first and a second of the stations, wherein, upon receipt of a communication request, the unit (UC) transmits the key linked to the second station, in encrypted form, to the first station.
A method for locating a GNSS signal-jamming source, including setting two antennas in rotation about a common axis of rotation so as to form N different respective positions corresponding to various angles of rotation, in each of the N positions, using each antenna to acquire a GNSS signal including a payload signal and a jamming signal, computing a phase offset between the acquired jamming signals, and determining a direction of the jamming source using a maximum value of the N computed phase shifts.
G01S 3/48 - Systems for determining direction or deviation from predetermined direction using antennas spaced apart and measuring phase or time difference between signals therefrom, i.e. path-difference systems the waves arriving at the antennas being continuous or intermittent and the phase difference of signals derived therefrom being measured
G01S 3/04 - Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received using radio waves Details
An input/output control system for at least one avionics application including at least two computing platforms implemented using similar hardware and software resources, each computing platform including a primary stage configured to acquire analogue signals and convert them into digital signals, an intermediate stage configured to digitally process the digital signals to form digital data, and a final stage configured to make the digital data available to the avionics application, the intermediate stage being further configured to encapsulate each processed digital data item, each computing platform further including a verification application configured to verify the encapsulation of each data item received.
A method for monitoring a Half Duplex Ethernet network including a plurality of nodes and having a PLCA operating mode and a CSMA/CD operating mode, each node being defined by an identifier. The method includes retrieving an internal state of the node describing the operating mode of the network, transmitting the internal state to all other nodes, analyzing the external states received corresponding to the internal states sent by other nodes, and based on the analysis, reconfiguring the node or conserving the current configuration thereof.
A method for establishing, for descent and approach phases of an aircraft, an efficient energy-dissipation strategy is provided, taking the form of a computation of an optimized descent and approach path, which aims to maximize employment of the idle regime while minimizing use of air brakes via more efficient deceleration.
An acoustic transducer (30) deployable in a sonobuoy application. The acoustic transducer (30) having a support structure (36) connecting a base plate (32) of an active assembly, comprising a base plate (32) and a piezoelectric body (34) supported by the base plate (32) to a passive vibrator (38) supported by the support structure (36). Such that bending vibration of the active assembly (32, 34) is mechanically coupled via the support structure (36) to drive bending vibration of the passive vibrator (38). Multiple acoustic transducers of this type can be used to form a transducer array for a sonobuoy.
B06B 1/06 - Processes or apparatus for generating mechanical vibrations of infrasonic, sonic or ultrasonic frequency making use of electrical energy operating with piezoelectric effect or with electrostriction
G10K 11/00 - Methods or devices for transmitting, conducting or directing sound in generalMethods or devices for protecting against, or for damping, noise or other acoustic waves in general
H04R 1/28 - Transducer mountings or enclosures designed for specific frequency responseTransducer enclosures modified by provision of mechanical or acoustic impedances, e.g. resonator, damping means
H04R 1/40 - Arrangements for obtaining desired frequency or directional characteristics for obtaining desired directional characteristic only by combining a number of identical transducers
H04R 1/44 - Special adaptations for subaqueous use, e.g. for hydrophone
Centre national de la recherche scientifique (France)
Institut Polytechnique de Bordeaux (France)
UNIVERSITÉ DE BORDEAUX (France)
Inventor
Ghiotto, Anthony
Varault, Stefan
Veyrac, Yoan
Lourenco Martins, Valentin
Abstract
An array antenna including a plurality of radiating elements fed in series and arranged along a vertical axis, operates under horizontal polarization, by connecting two successive radiating elements along the vertical axis by a pair of differential lines, each line having a length equal to the wavelength guided in the line, one end of a line being connected to a horizontal edge of a radiating element and the other end of the line being connected to the horizontal edge facing the other radiating element, a single radiating element being provided with at least one horizontal excitation point, positioned outside the vertical axis, preferably in proximity to a vertical edge of the single radiating element.
A handset device controls a vehicle entertainment system. The handset device includes an interface configured to communicate control signaling to the entertainment system, user selectable interface elements, light devices arranged to form light zones providing backlighting to corresponding groups of one or more of the user selectable interface elements, and controller circuitry. The controller circuitry is configured to respond to user selections among the user selectable interface elements by triggering corresponding control signaling to be communicated through the interface. The controller circuitry determines a lighting setting to select one of the light zones to activate to backlight the corresponding group of the one or more of the user selectable interface elements, and controls power flow to at least one light device in the selected light zone based on the light setting to backlight the corresponding group of the one or more of the user selectable interface elements.
G06F 3/023 - Arrangements for converting discrete items of information into a coded form, e.g. arrangements for interpreting keyboard generated codes as alphanumeric codes, operand codes or instruction codes
G06F 3/01 - Input arrangements or combined input and output arrangements for interaction between user and computer
H05B 47/175 - Controlling the light source by remote control
74.
SYSTEM FOR INTERACTING AT A DISTANCE WITH A POINTING MEANS OF AN HMI OF A VIEWING SYSTEM OF AN AIRCRAFT COCKPIT
A system for interacting at a distance with a pointing means of an HMI of a viewing system of an aircraft cockpit, including three layers including an upper layer in the shape of an inverted V, which itself acts as a handrest knob, including a module, with a touch-sensitive flat surface, configured to interact with the pointing means arranged on a front portion of the inverted V; at least one physical interactor configured to interact with the HMI arranged on a rear portion of the inverted V; and two lateral edges set back from the upper surface of the upper layer, each provided with at least one physical interactor.
B64D 43/00 - Arrangements or adaptations of instruments
G06F 3/0354 - Pointing devices displaced or positioned by the userAccessories therefor with detection of 2D relative movements between the device, or an operating part thereof, and a plane or surface, e.g. 2D mice, trackballs, pens or pucks
G06F 3/039 - Accessories therefor, e.g. mouse pads
A method for improving a shooting training with a shooting device on a target, the shooting device including a laser having an initial position and the target comprising one or more laser receivers, the method including acquiring image or video data relating to the target; analyzing the acquired image or video data of the target to determine pixels corresponding to at least one part of the target; determining a distance between the shooting device and the target based on the analysis and determining a position of one of the laser receivers; shooting a real or virtual projectile with the shooting device; determining the impact zone of the projectile on the target by calculating a trajectory from the shooting device to the target based on the distance determination and ballistic data from the projectile; deflecting the laser from the initial position to a new position based on the determined position of the of the one laser receiver; and transmitting with the laser at the new position to the laser receiver data relating to the determined impact zone and relating to the shot on the target.
A medical imaging system including a support having a frame and at least two wheels assembled directly or indirectly to the frame so as to allow the support to be moved; a medical imaging device; a control device configured to control the medical imaging device; and an electric power supply device configured to supply electrical energy to the medical imaging device and/or the control device, the medical imaging device, the control device and the electric power supply device each being configured to be removably assembled to the support.
The present invention relates to a method for decrypting a secret encrypted by a QC-MDPC mechanism, the decryption method being implemented by the receiver (14) and comprising the reception of a syndrome polynomial derived from the secret, the generation of random integers, the application of respective operations on the first and second sparse polynomials of the private key, the application of a third operation on the syndrome polynomial, the search for modified error polynomials such as the linear combination of modified error polynomials gives the modified syndrome polynomial, and the deduction of the shared secret by application of a respective operation on the first and second modified error polynomials, the five operations depending on the generated random integers and keeping the weight of the polynomial on which the operation is applied.
Thales Alenia Space Italia S.p.A. Con Unico Socio (Italy)
Sia "Allatherm" (Latvia)
Inventor
Mishkinis, Donatas
Gottero, Marco
Abstract
An evaporator assembly including at least one compensation chamber and at least one capillary pump that includes a primary wick, the evaporator assembly including a secondary wick extending through the at least one compensation chamber and the at least one capillary pump and contacting the primary wick thereof. The at least one compensation chamber and the at least one capillary pump are arranged parallel to one another along respective distinct axes.
F28D 15/04 - Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls in which the medium condenses and evaporates, e.g. heat-pipes with tubes having a capillary structure
F28D 15/02 - Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls in which the medium condenses and evaporates, e.g. heat-pipes
79.
Innovative Quantum Key Distribution Transmission System
Thales Alenia Space Italia S.p.A. Con Unico Socio (Italy)
Inventor
Catuogno, Tommaso
Verducci, Mattia
Iacurto, Cristian
Geraldi, Andrea
Abstract
The present invention concerns a Quantum Key Distribution transmission system comprising a transmitter and a receiver, wherein the transmitter is configured to transmit a multiphoton pulse to the receiver through a trusted area that extends from the transmitter towards the receiver up to a trusted distance from the transmitter; wherein the transmitter is configured to transmit the multiphoton pulse with a transmission power such that a single-photon pulse propagates out from the trusted area up to reach the receiver.
A ground-based content controller for managing content provided by an in-flight entertainment (“IFE”) system operating on an airplane can include a ground-based content processor and a non-transitory computer readable medium. The non-transitory computer readable medium can be communicatively coupled to the ground-based content controller and store program code executable by the ground-based content processor to perform operations. The operations can include retrieving information associated with a passenger of the airplane. The operations can further include determining content targeting rules based on the information. The content targeting rules can be used to select content to be made available to the passenger on the airplane. The operations can further include transmitting, prior to takeoff, the content targeting rules via a radio access network to an on-board content controller on the airplane.
H04N 21/214 - Specialised server platform, e.g. server located in an airplane, hotel or hospital
H04N 21/258 - Client or end-user data management, e.g. managing client capabilities, user preferences or demographics or processing of multiple end-users preferences to derive collaborative data
H04N 21/2668 - Creating a channel for a dedicated end-user group, e.g. by inserting targeted commercials into a video stream based on end-user profiles
A method for imaging a region of a moving blade of a wind turbine includes using a wider field-of-view (WFoV) camera to capture a plurality of WFoV images of at least part of the moving blade in a field-of-view (FoV) of the WFoV camera, determine a trigger time when an edge of the moving blade to calculate one or more NFoV image capture times when the edge of the moving blade, or a body of the moving blade, is, or will be, in the FoV of a NFoV camera, and using the NFoV camera to capture one or more NFoV images. The one or more NFoV images of the region of the moving blade may be analysed to identify any damage or defects in the moving blade without any need to interrupt the motion of the blades of the wind turbine.
Thales Alenia Space Italia S.p.A. Con Unico Socio (Italy)
Next One Film Group S.r.l. (Italy)
Inventor
Tedone, Domenico
Basso, Valter
Bonavina, Alessandra
Abstract
The invention concerns a method of providing a space extended reality service on earth, including: acquiring, by means of one or more acquisition systems/devices installed on a space platform, real-time data related to a surrounding space environment and/or to one or more astronauts in the space environment; generating, by means of a computer graphics processing device/system, based on the acquired real-time data and on synthetic data, a three-dimensional extended reality environment reproducing the space environment and one or more three-dimensional avatar(s) of the astronaut(s) reproducing movements and/or actions and/or facial expressions and/or voice of the astronaut(s), wherein the synthetic data digitally represent the space environment and/or the astronaut(s); and providing one or more users on earth with a space extended reality service based on the generated three-dimensional extended reality environment and avatar(s).
A method is provided of display of a dot-matrix digital image including controlling groups of three coloured elements, each element being of a different colour, each group forming one elementary element of a colour image, and carrying out anti-aliasing processing of the display. Each coloured element is a plano-convex assembly of a plurality of light-emitting diodes, each of the elements in a group being covered by a plate that is common to the diodes of the element and that scatters coloured light associated with the element, the anti-aliasing processing being carried out by applying commands for various light intensities to the light-emitting diodes inside a given element.
G09G 3/32 - Control arrangements or circuits, of interest only in connection with visual indicators other than cathode-ray tubes for presentation of an assembly of a number of characters, e.g. a page, by composing the assembly by combination of individual elements arranged in a matrix using controlled light sources using electroluminescent panels semiconductive, e.g. using light-emitting diodes [LED]
84.
METHOD OF CONTROLLING THE OBSERVATION OF A SPACE USING A TRACKING SYSTEM AND ASSOCIATED DEVICE
CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE (France)
Inventor
Atienza, Nicolas
Labreuche, Christophe
Sebag, Martine
Cohen, Johanne
Honore, Nicolas
Abstract
A method of monitoring observation uses a space tracking system. The method is implemented by a control module which is part of the tracking system. The method includes: a step of thumbnail training, each thumbnail gathering a set of data accessible to the tracking system over a respective zone and a predefined time interval, the zones associated with each thumbnail covering the space observed by the tracking system and the set of predefined time intervals covering an observation time interval, the data including at least: a step of monitoring the observation using a space tracking system corresponding to at least one thumbnail by applying a control function to all the data of the at least one thumbnail.
A production method for producing an anode for a cold cathode X-ray source, including the following steps: producing an element referred to as target from a first material adapted to generating X-rays from the absorption of an electron beam, the first material having a first thermal expansion coefficient Ce,1(Tu) at a predetermined temperature Tu of use of the anode in the X-ray source, producing an element referred to as target support from a second material having a second thermal expansion coefficient Ce,2(Tu) at the predetermined temperature Tu, joining the target to the target support by hard soldering using a solder material at a soldering temperature higher than the predetermined temperature Tu and higher than a melting point of the solder material, so as to form a film of solder interposed between the target and the target support.
A computer-implemented method includes receiving a series of measurements of distances generated, from a plurality of different positions each time, by a detection system operating by: transmitting a wave; receiving waves reflected by the environment; determining the distances by calculating differences between the wave transmission time and the time of reception of the reflected waves; generating, based on the series of distance measurements, a synthetic image representing the distances from the environment relative to a reference position; for each focal distance of a plurality of focal distances: generating, from the series of distance measurements or the synthetic image, a synthetic image that is focused at the focal distance, by applying compensation for penumbra effects; and detecting the presence of an object in the focused synthetic image.
A system for monitoring the operation of a computer including hardware blocks including a plurality of cores, a set of task schedulers capable of scheduling the execution of a task by assigning it an identifier, and of storing the identifier, the monitoring system including a collection unit capable of counting the number of queries of each hardware block during the execution of a task, of reading the identifier of the executed task in a first memory storage unit, of forming an association between a query and the corresponding identifier, and of storing each association formed on a second memory storage unit, and a monitoring unit capable of determining the state of operation (operating status) of the computer by using the stored associations.
A method for analysing the change between two frames of an uncompressed video stream, including estimating a shift and statistical deviation between all or part of the frames in at least one direction, and using the one or more computed shifts and statistical deviations to detect a significant change between the frames. A method for coding an uncompressed video stream, wherein information relating to a significant change is used to modify the uncompressed video stream or coding parameters of the uncompressed video stream, in order to avoid peaks in rate. A device implementing either of the methods, to a complete transmitting system, to a computer program product comprising program instructions allowing the steps of the methods to be executed, and to a recording medium comprising the computer program product.
H04N 19/159 - Prediction type, e.g. intra-frame, inter-frame or bidirectional frame prediction
G06V 10/75 - Organisation of the matching processes, e.g. simultaneous or sequential comparisons of image or video featuresCoarse-fine approaches, e.g. multi-scale approachesImage or video pattern matchingProximity measures in feature spaces using context analysisSelection of dictionaries
H04N 19/177 - Methods or arrangements for coding, decoding, compressing or decompressing digital video signals using adaptive coding characterised by the coding unit, i.e. the structural portion or semantic portion of the video signal being the object or the subject of the adaptive coding the unit being a group of pictures [GOP]
89.
Method for assisting with firing on a moving target, and associated device and assembly
A method for assisting with firing at a moving target, includes the steps of: displaying in a targeting window, superimposed onto the direct view of a scene, a main indicator creating a firing axis of a firing system; measuring a distance between the main indicator and a target in the scene; determining the speed of movement of the target; determining a targeting position, in the targeting window, anticipating an angular movement of the target relative to the firing axis, as a function of the speed of movement of the target, the speed of a projectile and the measured distance; and displaying, in the targeting window, a secondary indicator at the determined targeting position.
The present invention relates to an incremental magnetic encoder (10) defining an encoder axis (X) and comprising a fixed body and a movable body.
The present invention relates to an incremental magnetic encoder (10) defining an encoder axis (X) and comprising a fixed body and a movable body.
One of the bodies, called the first body (21), comprises a first support (33) comprising N arranged magnetic elements.
The present invention relates to an incremental magnetic encoder (10) defining an encoder axis (X) and comprising a fixed body and a movable body.
One of the bodies, called the first body (21), comprises a first support (33) comprising N arranged magnetic elements.
The other body, called second body (22), comprises:
a second support (41) comprising K*M magnetic elements arranged inhomogeneously along the direction of encoding (C1, C2) opposite the N magnetic elements, the K*M magnetic elements forming M groups of K magnetic elements, initial elements of the M different groups being spaced apart along the direction of encoding (C1, C2) by a homogeneous pitch P1, the K−1 magnetic elements of each group being spaced apart from the initial magnetic element of said group by variable pitches Pi;
at least one magnetic detector arranged opposite the first support (33).
G01D 5/245 - Mechanical means for transferring the output of a sensing memberMeans for converting the output of a sensing member to another variable where the form or nature of the sensing member does not constrain the means for convertingTransducers not specially adapted for a specific variable using electric or magnetic means influencing characteristics of pulses or pulse trainsMechanical means for transferring the output of a sensing memberMeans for converting the output of a sensing member to another variable where the form or nature of the sensing member does not constrain the means for convertingTransducers not specially adapted for a specific variable using electric or magnetic means generating pulses or pulse trains using a variable number of pulses in a train
A radar system with a radome is protected from lightning strikes by a conductive projection projecting into space outside the radome in the manner of a lightning rod, and passing through the wall of the radome to the inside, where its proximal part is in electrical contact with, or in so close proximity as to constitute a spark gap with an internal conductive member which passes within the radome to provide a conductive path for example via a platform on which an antenna may be mounted, to ground, so as to provide a viable path from the conductive projection to ground.
H01Q 3/02 - Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole
H01Q 1/42 - Housings not intimately mechanically associated with radiating elements, e.g. radome
H01Q 1/50 - Structural association of antennas with earthing switches, lead-in devices or lightning protectors
92.
Predicting monitoring device of the operation of a unit for estimating a physical value and associated system and methods
A predictive monitoring device for operation of a unit for estimating a physical quantity receiving data acquired by a detection unit and applying an estimation model to the acquired data, the predictive monitoring device including a generation unit for test data, applying a transformation to the acquired data, a computation unit estimating a value of the physical quantity by applying the model to the test data, an analysis unit for the test value, performing a comparison between the test value and an expected value according to a criterion for evaluating the performance of the model, and a warning unit issuing an alert according to the result of the comparison.
A mobile satellite communication (SATCOM) terminal for communication with non-terrestrial network (NTN) satellites. The SATCOM terminal performs operations to adapt signaling transmitted toward one of the NTN satellites operating as a cellular base station to compensate for at least one of: propagation delay in communications to the one of the NTN satellites; mobility management and handover to the one of the NTN satellites; and Doppler shift in the signaling transmitted toward the one of the NTN satellites.
Various embodiments of the present disclosure are directed to a computer server. The computer server includes at least one network interface, at least one processor connected to communicate through the at least one network interface with video display units (VDUs) and/or personal electronic devices (PEDs), and at least one memory. The one memory includes a sign language conversion module operative to translate digitized speech to a script of signs to be performed by a computer generated avatar. The one memory also includes a sign language animation module operative to generate video of an avatar performing signs forming a sign language responsive to the script of signs. The one memory also includes a distribution module operative to communicate the video of the avatar through the at least one network interface to VDUs and/or PEDs.
Method and electronic device for managing the execution of software application services on an avionics platform, related computer program and avionics system
A method of managing the execution of software services on an avionics platform including resources for the execution of the services is implemented by an electronic device and includes acquisition of contextual data for a group of software services to be executed, the contextual data including, for each software service: a maximum number of resources used by the service, an operating requirement of the service equal to resistance to breakdown/s or non-resistance to breakdown/s, and, if the operating requirement of the service is equal to resistance to breakdown/s, a number of breakdown/s the service should withstand, computation, from the acquired contextual data, of a context for the group of software services, and launching of the execution of software service/s of the group according to a set of distribution rule/s of the services and depending upon the computed context.
An electronic system (10) for a firearm (100) comprising a plurality of modules that are mechanically couplable to the firearm (100), the modules including: a wireless communication module (60); an optical sight module (30) comprising an optical sight (32) and an electronic display (34); a range finder module (40); a position and orientation module (70); a processing module (80); and a power module (90). The electronic system (10) is configured to determine coordinates of a first, in field of view, target object and wirelessly communicate the coordinates with another electronic system (10). The electronic system (10) is also configured to calculate based on received coordinates from another electronic system (10), a position of a second, outside field of view, target and display digital information containing movement directions on the electronic display (34) to instruct a user to orient the optical sight (32) to view the second target object in the field of view. The electronic system (10) operates independently of mechanical operation of the firearm (100).
H04L 67/12 - Protocols specially adapted for proprietary or special-purpose networking environments, e.g. medical networks, sensor networks, networks in vehicles or remote metering networks
H04W 4/029 - Location-based management or tracking services
H04W 4/70 - Services for machine-to-machine communication [M2M] or machine type communication [MTC]
An aircraft piloting assistance method, including the following steps implemented by an electronic piloting assistance device: detecting an event, with said event being an event for identifying a note class from among a set of predefined events for identifying N note classes, with N being an integer≥2; following the detecting step, triggering the acquisition of a voice signal currently being transmitted or received by the pilot and associated with the note class, and processing the acquired voice signal, with the processing being a function of the note class and comprising at least the conversion of the voice signal into text and the generation of a note as a function of the text.
An atom chip (Ach) for an ultra-cold atom sensor, includes a measurement plane XY of the atom chip comprising: a plurality of first pairs of waveguides, a plurality of second pairs of waveguides, the projections in the plane XY of the first pair furthest from X and of the second pair furthest from Y′ forming, at their intersection, a parallelogram with a centre O, a first conductive wire having a projection in the plane XY along X or Y′ or a diagonal of the parallelogram, the first conductive wire being designed to be flowed through by a DC current, the first wire having a flaring so as to take the form of a surface whose projection in the plane XY incorporates the parallelogram and exhibits symmetry about the point O.
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.
To limit interference between antennas such as radar patch antennas in a structure, rows of pin elements are provided intersecting a propagation path on the surface of the structure. These rows may comprise inner and outer rows separated by a predetermined distance determined as a function of the operating frequency of the antennas. One or more intermediate rows may be provided between the inner and outer rows. The length and diameter of pin elements as well as the spacing between pin elements of a given row, may equally be selected with a view to the operating frequency of the antennas. The pin elements of the inner and outer rows may be offset with respect to each other.