Abstract: Processing of image data derived from radiation emanating from a scene and acquired by a multi-channel enhanced vision system renders an image of the scene for display. Detected first and second wavelength bands of radiation produce respective first and second sets of image data that include representations of relatively low contrast, high spatial frequency detail of features of the scene. Nonlinear intensity transformation of data derived from the first and second sets of image data produces, respectively, first and second sets of low dynamic range image data representing, respectively, first and second sets of intensity values. Different pairs of associated intensity values of the first and second sets correspond to different pixels forming an image. The associated intensity values of the different pairs are combined to form fused image data representing brightness levels of the pixels forming a displayed image that exhibits with high brightness and in great detail the features of the scene.

Abstract: A system for and a method of synchronous acquisition of pulsed source light performs monitoring of aircraft flight operation. Diode sources of illumination (18, 108, 208) are pulsed (16, 106, 206) at one-half the video frame rate of an imaging camera (36, 136, 236). Alternate frames view the world-scene with lights of interest pulsed on, and then off, respectively. Video differencing (34, 134, 234) eliminates the background scene, as well as all lights not of interest. Suitable threshholding over a resulting array of camera pixel-differences acquires the desired lights and represents them as point symbology on a display (40, 140, 240). In an enhanced vision landing system embodiment, the desired lights (symbols) overlay or are fused on a thermal image of the scene; alternatively, the symbols overlay a visible scene (TV) image.

Abstract: A technique for assessing runway visibility to airborne infrared vision devices (EVS) determines the range performance of airborne infrared EVS sensors at a given destination and in real time by extending the modern RVR philosophy to the infrared spectrum. The technique measures extinction coefficients at the infrared sensor wavelengths of interest through deployment of ground-based infrared transmissometer systems. These infrared extinction coefficients are used with computational algorithms that are analogous to those used at visible wavelengths to determine the respective distances at which the background scene and runway lights are discernible using infrared cameras with appropriate image processing. In this technique, infrared sensors replace the human eye as a basic mechanism of sensing through the atmospheric path. The algorithms also account for the image processing and cockpit display functions, in accordance with the ultimate discernment by the pilot's eye when viewing an appropriate display device.

Abstract: Preferred embodiments of an image display system achieve mapping of high dynamic range image data to render on a lower dynamic range display device a corresponding image characterized by stable global intensity levels and visually perceptible local area detail. The high dynamic range image data include representations of relatively low intensity contrast, high spatial frequency details and relatively low spatial frequency intensities. Data derived from the high dynamic range image data are applied to a nonlinear intensity transform. The nonlinear intensity transform preserves or enhances the low intensity contrast, high spatial frequency details and maintains a visually perceptible representation of the relatively low spatial frequency intensities to thereby provide visually perceptible local area detail. An exemplary embodiment derives high dynamic range image data from a thermal infrared camera for use with aircraft.

Abstract: A system for and a method of synchronous acquisition of pulsed source light performs monitoring of aircraft flight operation. Diode sources of illumination (18, 108, 208) are pulsed (16, 106, 206) at one-half the video frame rate of an imaging camera (36, 136, 236). Alternate frames view the world-scene with lights of interest pulsed on, and then off, respectively. Video differencing (34, 134, 234) eliminates the background scene, as well as all lights not of interest. Suitable threshholding over a resulting array of camera pixel-differences acquires the desired lights and represents them as point symbology on a display (40, 140, 240). In an enhanced vision landing system embodiment, the desired lights (symbols) overlay or are fused on a thermal image of the scene; alternatively, the symbols overlay a visible scene (TV) image.

Abstract: A system for and a method of synchronous acquisition of pulsed source light performs monitoring of aircraft flight operation. Diode sources of illumination (18, 108, 208) are pulsed (16, 106, 206) at one-half the video frame rate of an imaging camera (36, 136, 236). Alternate frames view the world-scene with lights of interest pulsed on, and then off, respectively. Video differencing (34, 134, 234) eliminates the background scene, as well as all lights not of interest. Suitable threshholding over a resulting array of camera pixel-differences acquires the desired lights and represents them as point symbology on a display (40, 140, 240). In an enhanced vision landing system embodiment, the desired lights (symbols) overlay or are fused on a thermal image of the scene; alternatively, the symbols overlay a visible scene (TV) image.

Abstract: A system for and a method of synchronous acquisition of pulsed source light performs monitoring of aircraft flight operation. Diode sources of illumination (18, 108, 208) are pulsed (16, 106, 206) at one-half the video frame rate of an imaging camera (36, 136, 236). Alternate frames view the world-scene with lights of interest pulsed on, and then off, respectively. Video differencing (34, 134, 234) eliminates the background scene, as well as all lights not of interest. Suitable threshholding over a resulting array of camera pixel-differences acquires the desired lights and represents them as point symbology on a display (40, 140, 240). In an enhanced vision landing system embodiment, the desired lights (symbols) overlay or are fused on a thermal image of the scene; alternatively, the symbols overlay a visible scene (TV) image.