Abstract: A vector magnetometer comprises a cell to be filled with an atomic gas, an optical source and a photo-detection device. The optical source is configured to emit towards the cell: a first and a second optical beam, called probe beams, that are polarised linearly, a third optical beam, called the pump beam, linearly polarised. The polarisation directions of the probe beams and the polarisation direction of the pump beam are not coplanar. The photo-detection device is configured to receive light from the probe beams that have passed through the cell. The probe beams can have the same propagation direction. The polarisation direction of the pump beam can form an angle of 45°±10° with the polarisation direction of each of the probe beams.

Abstract: A device for measuring rotation including an NMR gyroscope having a sensing axis, a computer, a generating member configured to generate a magnetic field directed along the sensing axis, and a MEMS gyroscope rigidly connected to the NMR gyroscope, the MEMS gyroscope having a sensing axis aligned with the sensing axis of the NMR gyroscope, the MEMS gyroscope being suitable for delivering a MEMS signal representing a rotation about the sensing axis, the computer being configured to calculate, from an NMR signal output by the NMR gyroscope, information relating to a rotation about the sensing axis, and to analyse the MEMS signal over time in order to determine a current cut-off frequency, the computer also being configured to control the generating member in order to generate, over time, a magnetic field of which the amplitude is a function of the current cut-off frequency.

Abstract: A method for detecting rotation of a carrier utilizes a device embedded in said carrier that comprises an enclosure containing a gaseous mixture of an alkali metal and a noble gas. The method includes a step of starting up (DEM-MEOP) the device during which the noble gas is polarised by utilizing metastability exchange optical pumping. The start-up step is followed by a step of acquisition (MES-SEOP) by the device of a signal representative of said rotation during which the noble gas is maintained polarised by utilizing spin exchange optical pumping. The invention extends to the device and to an inertial navigation unit integrating said device and to an inertial navigation method implementing the method for detecting rotation of the carrier.

Abstract: A vector magnetometer comprises a cell to be filled with an atomic gas, an optical source and a photo-detection device. The optical source is configured to emit towards the cell: a first and a second optical beam, called probe beams, that are polarised linearly, a third optical beam, called the pump beam, linearly polarised. The polarisation directions of the probe beams and the polarisation direction of the pump beam are not coplanar. The photo-detection device is configured to receive light from the probe beams that have passed through the cell. The probe beams can have the same propagation direction. The polarisation direction of the pump beam can form an angle of 45°±10° with the polarisation direction of each of the probe beams.

Abstract: The invention relates to a navigational aid method for an inertial navigation system including at least one inertial sensor (4) having a sensitive axis (X-X), each inertial sensor (4) comprising an ASG gyroscope (8) able to deliver an ASG signal representative of a rotation about the corresponding sensitive axis (X-X), and a MEMS gyroscope (10) able to deliver a MEMS signal representative of a rotation about the corresponding sensitive axis (X-X), the method including the steps of: between a first date and a subsequent third date, calculating a path from the MEMS signals; from the third date, calculating the path from the ASG signals; estimating a bias vector introduced by the MEMS gyroscopes (10), from the MEMS signals and ASG signals; at a fourth date subsequent to the third date, resetting the path.

Abstract: A device for measuring rotation including an NMR gyroscope having a sensing axis, a computer, a generating member configured to generate a magnetic field directed along the sensing axis, and a MEMS gyroscope rigidly connected to the NMR gyroscope, the MEMS gyroscope having a sensing axis aligned with the sensing axis of the NMR gyroscope, the MEMS gyroscope being suitable for delivering a MEMS signal representing a rotation about the sensing axis, the computer being configured to calculate, from an NMR signal output by the NMR gyroscope, information relating to a rotation about the sensing axis, and to analyse the MEMS signal over time in order to determine a current cut-off frequency, the computer also being configured to control the generating member in order to generate, over time, a magnetic field of which the amplitude is a function of the current cut-off frequency.

Abstract: A method for detecting rotation of a carrier utilizes a device embedded in said carrier that comprises an enclosure containing a gaseous mixture of an alkali metal and a noble gas. The method includes a step of starting up (DEM-MEOP) the device during which the noble gas is polarised by utilizing metastability exchange optical pumping. The start-up step is followed by a step of acquisition (MES-SEOP) by the device of a signal representative of said rotation during which the noble gas is maintained polarised by utilizing spin exchange optical pumping. The invention extends to the device and to an inertial navigation unit integrating said device and to an inertial navigation method implementing the method for detecting rotation of the carrier.

Abstract: The invention relates to a navigational aid method for an inertial navigation system including at least one inertial sensor (4) having a sensitive axis (X-X), each inertial sensor (4) comprising an ASG gyroscope (8) able to deliver an ASG signal representative of a rotation about the corresponding sensitive axis (X-X), and a MEMS gyroscope (10) able to deliver a MEMS signal representative of a rotation about the corresponding sensitive axis (X-X), the method including the steps of: between a first date and a subsequent third date, calculating a path from the MEMS signals; from the third date, calculating the path from the ASG signals; estimating a bias vector introduced by the MEMS gyroscopes (10), from the MEMS signals and ASG signals; at a fourth date subsequent to the third date, resetting the path.

Abstract: A process for obtaining a material includes a substrate coated on at least one portion of at least one of its faces with a coating including at least one discontinuous metallic thin layer based on silver, on gold, or on any alloy thereof, the or each discontinuous metallic thin layer being encapsulated between at least two dielectric thin layers, and the or each discontinuous metallic thin layer being in the form of periodic geometric patterns, the process including a deposition step then a step wherein the substrate thus coated is made to run opposite at least one laser device emitting a laser radiation focused on the coating in the form of at least one line, the power of the radiation being adapted in order to render the or each metallic thin layer discontinuous by dewetting.

Abstract: A process for obtaining a material includes a substrate coated on at least one portion of at least one of its faces with a coating including at least one discontinuous metallic thin layer based on silver, on gold, or on any alloy thereof, the or each discontinuous metallic thin layer being encapsulated between at least two dielectric thin layers, and the or each discontinuous metallic thin layer being in the form of periodic geometric patterns, the process including a deposition step then a step wherein the substrate thus coated is made to run opposite at least one laser device emitting a laser radiation focused on the coating in the form of at least one line, the power of the radiation being adapted in order to render the or each metallic thin layer discontinuous by dewetting.

Abstract: The invention relates to a solar control glazing comprising a glass substrate provided, on one of its faces, with a stack of layers having a solar protection function, in which the stack comprises the sequence of the following layers, starting from the surface of the glass substrate: a lower layer for protecting the upper layers against the migration of the alkali metal ions resulting from the glass substrate, a layer of an indium tin oxide (ITO), an upper layer for protecting the ITO layer against atmospheric oxygen, said glazing being characterized in that said upper and lower layers are essentially composed of a dielectric material chosen from a silicon nitride, an aluminum nitride or their mixture and in that intermediate layers made of a chromium-comprising metal, which layers are optionally partially or completely oxidized and/or nitrided, are positioned on either side of and in contact with said ITO layer, the thickness of said intermediate layers being between 0.5 and 3 nanometers.

Abstract: A transparent electrode for an organic light-emitting diode including, on a transparent support made of mineral glass, n individual stacks of thin layers, each individual stack successively including, starting from the glass support, (a) a layer of mixed tin zinc oxide, (b) a crystalline layer of zinc oxide, optionally doped with aluminum, (c) a metallic silver layer, in contact with the zinc oxide layer, and positioned between each silver layer and the mixed tin zinc oxide layer or layers closest thereto is (d) a layer made of silicon nitride or made of silica, optionally doped with a metal. There is also provided It also relates to an an organic light-emitting diode device containing such an electrode and to a process for manufacturing such a device.