Patent classifications
B64D47/02
SYSTEM AND METHOD FOR QUANTIFYING AN EXPOSURE DOSE ON SURFACES
A method for quantifying an exposure dose for a surface is disclosed. The method may include emitting one or more beams of 222 nm light onto a portion of the surface using one or more far ultraviolet (UV) light sources capable of emitting 222 nm light, the portion of the surface being coated with one or more fluorescent coatings. The method may include capturing images of the portion of the surface. The method may include adjusting one or more image characteristics for the captured images using one or more filtering methods. The method may include generating a histogram of the adjusted images based on the one or more filtering methods. The method may include determining a pixel surface area for the generated histogram. The method may include calculating the exposure dose for the surface based on the generated pixel surface area and a predetermined calibration curve.
SYSTEM AND METHOD FOR QUANTIFYING AN EXPOSURE DOSE ON SURFACES
A method for quantifying an exposure dose for a surface is disclosed. The method may include emitting one or more beams of 222 nm light onto a portion of the surface using one or more far ultraviolet (UV) light sources capable of emitting 222 nm light, the portion of the surface being coated with one or more fluorescent coatings. The method may include capturing images of the portion of the surface. The method may include adjusting one or more image characteristics for the captured images using one or more filtering methods. The method may include generating a histogram of the adjusted images based on the one or more filtering methods. The method may include determining a pixel surface area for the generated histogram. The method may include calculating the exposure dose for the surface based on the generated pixel surface area and a predetermined calibration curve.
AIR TRANSPORTATION SYSTEMS AND METHODS
Systems and methods are disclosed for transporting people using air vehicles.
AIR TRANSPORTATION SYSTEMS AND METHODS
Systems and methods are disclosed for transporting people using air vehicles.
ACCESS MANAGEMENT SYSTEM
An access management system includes a mobile device with a processor and a memory and a software platform including at least a processor and a memory. The software platform is configured to analyze data obtained from the mobile device and other devices connected to the software platform. Specifically, the software platform is operable to determine if an access key received, read, or captured by a mobile device matches an access key for an authorized account, object, device, or space for the mobile device, and to provide access to the mobile device if the access key received, read, or captured by the mobile device matches the authorized access key.
ACCESS MANAGEMENT SYSTEM
An access management system includes a mobile device with a processor and a memory and a software platform including at least a processor and a memory. The software platform is configured to analyze data obtained from the mobile device and other devices connected to the software platform. Specifically, the software platform is operable to determine if an access key received, read, or captured by a mobile device matches an access key for an authorized account, object, device, or space for the mobile device, and to provide access to the mobile device if the access key received, read, or captured by the mobile device matches the authorized access key.
SYNTHETIC GEOREFERENCED WIDE-FIELD OF VIEW IMAGING SYSTEM
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.
SYNTHETIC GEOREFERENCED WIDE-FIELD OF VIEW IMAGING SYSTEM
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.
AIRCRAFT WING INSPECTION LIGHT WITH CAMERA
An aircraft wing inspection system includes a housing, a light source, a camera, and a display device. The housing is adapted to be mounted on an aircraft fuselage. The light source is disposed within the housing and is operable, upon being electrically energized, to emit a light beam. The camera is disposed within the housing and is configured to capture images of the aircraft wing, convert the captured images to digital image data, and transmit the digital image data. The display device is disposed remote from, and is in operable communication with, the camera. The display device is configured to receive the digital image data transmitted from the camera and to render the captured images.
AIRCRAFT WING INSPECTION LIGHT WITH CAMERA
An aircraft wing inspection system includes a housing, a light source, a camera, and a display device. The housing is adapted to be mounted on an aircraft fuselage. The light source is disposed within the housing and is operable, upon being electrically energized, to emit a light beam. The camera is disposed within the housing and is configured to capture images of the aircraft wing, convert the captured images to digital image data, and transmit the digital image data. The display device is disposed remote from, and is in operable communication with, the camera. The display device is configured to receive the digital image data transmitted from the camera and to render the captured images.