Abstract: Part for a motor vehicle includes an opacification coating, associated manufacturing method and luminous device including the part. The part for a motor vehicle includes a polymer-based body having a surface, an opacification coating covering at least one portion of the surface. The coating is formed by at least one thin iron-based layer and includes at least one compound from among an iron oxide and an iron nitride, and has a thickness that is greater than or equal to 100 nm over at least 50% of the at least one portion of the surface. Furthermore, the coating exhibits incident light radiation absorption that is greater than 70% of the incident light radiation. Thus, the coating allows reliable and reproducible opacification of the surface of the part.

Abstract: The invention relates to a disruption detection method and device for a positioning measurement correction message of a satellite geolocation device, able to receive a composite radio signal including a plurality of signals each emitted by a satellite in view of the geolocation device, and a positioning measurement differential correction message (MC) emitted by a satellite geolocation precision augmentation system. The device (20) according to the invention includes modules (32) computing, for each of the satellites in view, at least one differential correction coherence metric depending on a positioning measurement differential correction (CAS) extracted from the received differential correction message (MC). The device (20) also includes a module (34) detecting a disruption of the correction message when the number of satellites for which the differential correction coherence metric is above a predetermined threshold exceeds a predetermined number of satellites (N0), strictly greater than one.

Abstract: The invention relates to a disruption detection method and device for a positioning measurement correction message of a satellite geolocation device, able to receive a composite radio signal including a plurality of signals each emitted by a satellite in view of the geolocation device, and a positioning measurement differential correction message (MC) emitted by a satellite geolocation precision augmentation system. The device (20) according to the invention includes modules (32) computing, for each of the satellites in view, at least one differential correction coherence metric depending on a positioning measurement differential correction (CAS) extracted from the received differential correction message (MC). The device (20) also includes a module (34) detecting a disruption of the correction message when the number of satellites for which the differential correction coherence metric is above a predetermined threshold exceeds a predetermined number of satellites (NO), strictly greater than one.