Brevet FR3126055A1 — publié le 20230210

An imaging system for an aircraft is disclosed. A plurality of image sensors are attached, affixed, or secured to the aircraft. Each image sensor is configured to generate sensor-generated pixels based on an environment surrounding the aircraft. Each of the sensor-generated pixels is associated with respective pixel data including, position data, intensity data, time-of-acquisition data, sensor-type data, pointing angle data, latitude data, and longitude data. A controller generates a buffer image including synthetic-layer pixels, maps the sensor-generated pixels to the synthetic-layer pixels in the buffer image, fills a plurality of regions of the buffer image with the sensor-generated pixels, and presents the buffer image on a head-mounted display (HMD) to a user of the aircraft. Figure 1 Synthetic georeferenced wide-field of view imaging system Summary An imaging system for an aircraft system is disclosed in accordance with one or more illustrative embodiments of the present disclosure. In one illustrative embodiment, the system comprises a plurality of image sensors attached, affixed, or secured to the aircraft, wherein each image sensor is configured to generate sensor-generated pixels based on an environment surrounding the aircraft, wherein each of the sensor-generated pixels is associated with respective pixel data including: position data, intensity data, time-of-acquisition data, sensor-type data, pointing angle data, and latitude data and longitude data derived from the pointing angle data. In another illustrative embodiment, the system comprises a controller communicatively coupled to the plurality of image sensors, configured to: generate a buffer image including synthetic-layer pixels, wherein each of the synthetic-layer pixels is associated with latitude data and longitude data derived from a synthetic vision database; map the sensor-generated pixels to the synthetic-layer pixels in the buffer image by matching the latitude data and the longitude data derived from the pointing angle data with the latitude data and the longitude data derived from the synthetic vision database; fill a plurality of regions of the buffer image with the sensor-generated pixels, wherein each respective one of the regions of the buffer image is respectively filled by the sensor-generated pixels generated by a respective one of the image sensors; and present the buffer image on a head-mounted display (HMD) to a user of the aircraft. Advantageously, the pointing angle data is generated by a respective position encoder embedded with or communicatively coupled to each of the image sensors. Advantageously, the pointing angle data is generated by a respective inertial measurement unit (IMU) embedded with or communicatively coupled to each of the image sensors. Advantageously, the pointing angle data is generated by a respective attitude and heading reference system (AHRS) embedded with or communicatively coupled to each of the image sensors. Advantageously, the plurality of image sensors includes at least one fixed image sensor and at least one rotatable image sensor. Advantageously, the aircraft includes a winch attached, affixed, or secured thereto, wherein the winch includes a winch cable extendable in a first direction, and the at least one fixed image sensor comprises a winch image sensor configured to capture the environment in the first direction. Advantageously, the aircraft includes a rotatable searchlight, and the at least one rotatable image sensor comprises a searchlight image sensor configured to rotate in conjunction with the rotatable searchlight. Advantageously, the at least one rotatable image sensor includes a turreted image sensor. Advantageously, at least one of the plurality of image sensors is configured to detect visual light or infrared light. Advantageously, at least one of the plurality of image sensors comprises a charge-coupled device (CCD) or a complementary metal-oxide-semiconductor (CMOS) device. Advantageously, at least one of the plurality of image sensors comprises an imaging radar configured to detect radio frequency radiation. It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not necessarily restrictive of the invention as claimed. The accompanying drawings, which are incorporated in and constitute a part of the specification, illustrate embodiments of the invention and together with the general description, serve to explain the principles of the invention. The numerous advantages of the disclosure may be better understood by those skilled in the art by reference to the accompanying figures in which: is a side view of an imaging system for an aircraft, in accordance with one or more embodiments of the present disclosure. is a georeferenced buffer image constructed by sensor fusion, in accordance with one or more embodiments of the present disclosure. and are isometric views of a head mounted display (HMD), in accordance with one or more embodiments of the present disclosure. An imaging system for an aircraft, comprising: a plurality of image sensors attached, affixed, or secured to the aircraft, wherein each image sensor is configured to generate sensor-generated pixels based on an environment surrounding the aircraft, wherein each of the sensor-generated pixels is associated with respective pixel data including: position data, intensity data, time-of-acquisition data, sensor-type data, pointing angle data, and latitude data and longitude data derived from the pointing angle data; and a controller communicatively coupled to the plurality of image sensors, configured to: generate a buffer image including synthetic-layer pixels, wherein each of the synthetic-layer pixels is associated with latitude data and longitude data derived from a synthetic vision database, map the sensor-generated pixels to the synthetic-layer pixels in the buffer image by matching the latitude data and the longitude data derived from the pointing angle data with the latitude data and the longitude data derived from the synthetic vision database, fill a plurality of regions of the buffer image with the sensor-generated pixels, wherein each respective one of the regions of the buffer image is respectively filled by the sensor-generated pixels generated by a respective one of the image sensors, present the buffer image on a head-mounted display (HMD) to a user of the aircraft. The imaging system of claim 1, wherein the pointing angle data is generated by a respective position encoder embedded with or communicatively coupled to each of the image sensors. The imaging system of claim 1, wherein the pointing angle data is generated by a respective inertial measurement unit (IMU) embedded with or communicatively coupled to each of the image sensors. The imaging system of claim 1, wherein the pointing angle data is generated by a respective attitude and heading reference system (AHRS) embedded with or communicatively coupled to each of the image sensors. The imaging system of claim 1, wherein the plurality of image sensors includes at least one fixed image sensor and at least one rotatable image sensor. The imaging system of claim 5, wherein the aircraft includes a winch attached, affixed, or secured thereto, wherein the winch includes a winch cable extendable in a first direction, and the at least one fixed image sensor comprises a winch image sensor configured to capture the environment in the first direction. The imaging system of claim 5, wherein the aircraft includes a rotatable searchlight, and the at least one rotatable image sensor comprises a searchlight image sensor configured to rotate in conjunction with the rotatable searchlight. The imaging system of claim 5, wherein the at least one rotatable image sensor includes a turreted image sensor. The imaging system of claim 1, wherein at least one of the plurality of image sensors is configured to detect visual light or infrared light. The imaging system of claim 1, wherein at least one of the plurality of image sensors comprises a charge-coupled device (CCD) or a complementary metal-oxide-semiconductor (CMOS) device. The imaging system of claim 1, wherein at least one of the plurality of image sensors comprises an imaging radar configured to detect radio frequency radiation.