Abstract: An inertial head-tracking system includes light emitting diodes (LEDs) and photoreceptors. The LEDs and photoreceptors are positioned around the environment and helmet respectively. A processor periodically receives measurements from the photoreceptors and resets inertial drift based on those measurements. Either the LEDs or the photoreceptors are constrained to a specified range to allow for more accurate drift estimation.

Abstract: A head worn display (HWD) includes a head attachment region, an internal display and a controller. The internal display is viewable by a user and includes variable transparency areas. The internal display is arranged to display at least a portion of an external region external to the HWD. The controller is configured to control the variable transparency areas to block view of a region of the external region and to control the internal display to overlay information in a region of the internal display corresponding to the region of the external region which is blocked.

Abstract: A system and method are disclosed for design of a suite of multispectral (MS) sensors and processing of enhanced data streams produced by the sensors for autonomous aircraft flight. The suite of MS sensors is specifically configured to produce data streams for processing by an autonomous aircraft object identification and positioning system processor. Multiple, diverse MS sensors image naturally occurring, or artificial features (towers buildings etc.) and produce data streams containing details which are routinely processed by the object identification and positioning system yet would be unrecognizable to a human pilot. The object identification and positioning system correlates MS sensor output with a-priori information stored onboard to determine position and trajectory of the autonomous aircraft. Once position and trajectory are known, the object identification and positioning system sends the data to the autonomous aircraft flight management system for autopilot control of the autonomous aircraft.

Abstract: An apparatus interfaces with a light stanchion associated with a runway. The apparatus can include a first interface for attaching to the light stanchion, second interface for attaching to runway light, and a radar reflective member. The radar reflective member can be a corner reflector. The radar reflector can be part of set of reflectors arranged in accordance with visual approach slope indications or precision approach path indications.

Abstract: An optical device includes an electrochromic layer, a plurality of electronic drivers, and a controller. The electrochromic layer includes a plurality of electrochromic regions separated from each other. The plurality of electronic drivers are arranged to electrically connect with and drive respective of the electrochromic regions. The controller is configured to control the plurality of electronic drivers to individually address each of the plurality of electrochromic regions to selectively drive some of the plurality of electrochromic regions to change light transmission of the selectively driven plurality of electrochromic regions.

Abstract: An optical display system includes a first display, a plurality of electronic drivers, a controller, and a combiner. Light from a scene is combined with image light from the first display, and the combined light presented to an observer. The combiner includes an electrochromic layer comprising one or more electrochromic regions separated from each other. The electronic drivers are arranged to electrically connect with and drive respective of the electrochromic regions. The controller is configured to control the plurality of electronic drivers to individually address each of the electrochromic regions to selectively drive some of the electrochromic regions to change light transmission of the selectively driven electrochromic regions.

Abstract: An integrity monitoring system for a first image sensor includes an electronic processor configured to receive sensor data for the provision of image data associated with an environment of the avionic sensor. The electronic processor is configured to monitor the avionic sensor for integrity. The electronic processor is configured to perform at least one of: determining a presence of an optical feature associated with optics of the first image sensor, comparing overlap information derived from the sensor data and other sensor data, comparing characteristics of a digital output stream of the sensor data to expected characteristics, or comparing a first motion derived from the image data and a second motion derived from avionic position equipment.

Abstract: A system and method operate to leverage high assurance positioning systems to determine a hybrid deviation from an expected position, altitude, and path to generate a lateral and vertical signal indicating deviation from a desired position. As a filtered or alternative to conventional precision landing systems, the hybrid positioning system receives sensor data from a plurality of sensors and compares the received sensor data to known values to determine a deviation of position and trajectory. Extending the capability of existing auto-land systems, relative-to-runway sensors and/or filtered high assurance hybrid solutions are employed as an alternative to conventional precision landing systems. The sensors provide position data that is compared to an expected position and path to provide deviations in lateral, vertical, and speed augmenting traditional RF-based systems.

Abstract: An airfield visibility monitoring system may include a measurement unit to emit one or more pulses of electromagnetic radiation along an aircraft glideslope associated with a runway and detect backscattered radiation from the glideslope associated with the emitted pulses. The measurement unit may further determine round-trip times between emission of the one or more pulses and detection of the backscattered radiation. The system may further include a controller. The controller may determine values of a visibility metric for multiple distances from the measurement unit along the glideslope based on the detected backscattered radiation and round-trip times, determine values of the visibility metric for multiple altitudes based on the values of the visibility metric along the glideslope, and direct an airfield communication unit to broadcast values of the visibility metric for at least some of the altitudes.

Abstract: An infrared emitter is described. The infrared emitter comprises an infrared source, a housing, and infrared optics. The infrared source emits electromagnetic radiation with a peak intensity at a radiation wavelength within the range of 2 to 15 microns. The housing has an aperture, and is arranged to house the infrared source. The infrared optics is arranged to direct the electromagnetic radiation emitted from the infrared source through the aperture to outside the housing.

Abstract: An apparatus is for use with an aircraft radar system having a radar antenna. The apparatus includes processing electronics configured to cause the radar antenna to emit radar pulses having a pulse width less than 6 microseconds and configured to receive radar data associated with signals associated with the radar antenna. The radar data is processed to identify centroids associated with indications of the runway lights for a runway in the radar data. A best fit analysis of the centroids is used to identify a runway centerline associated with the runway.

Abstract: An integrity monitoring system for a first image sensor includes an electronic processor configured to receive sensor data for the provision of image data associated with an environment of the avionic sensor. The electronic processor is configured to monitor the avionic sensor for integrity. The electronic processor is configured to perform at least one of: determining a presence of an optical feature associated with optics of the first image sensor, comparing overlap information derived from the sensor data and other sensor data, comparing characteristics of a digital output stream of the sensor data to expected characteristics, or comparing a first motion derived from the image data and a second motion derived from avionic position equipment.

Abstract: An on-board computer system includes a first neural network trained to receive a video stream of a landing approach, runway data, and aircraft state data and identify environmental landmarks corresponding to components of the runway and environmental obstacles that might interfere with autonomous landing. The on-board computer system also includes a second neural network that receives a flight path vector and a flight director corresponding to vectors based on the aircraft energy state and a desired aircraft flight path respectively. The second neural network determines flight control inputs to bring the flight path vector into conformity with the flight director.

Abstract: A computer system with one or more cameras monitors the head poses produced by a head-tracking system and produces a pass/fail indication that the head poses are reliable in a high assurance environment. The system may identify individual fiducials and independently verifying that they conform to the computed pose; and/or compute a location of fiducials as would be observed by a single verification camera and compare the computed locations to actual observed locations. The verification camera may be part of a second head-tracking system, utilized while not operating in its ordinary capacity. The computer system may also calibrate the head-tracking system to account for temperature and pressure fluctuations and perform image stabilization before the image frames are passed to the head-tracking system for processing by observing separate fiducials in fixed locations relative to the camera.

Abstract: A system and method are disclosed for design of a suite of multispectral (MS) sensors and processing of enhanced data streams produced by the sensors for autonomous aircraft flight. The onboard suite of MS sensors is specifically configured to sense and use a MS variety of sensor-tuned objects, either strategically placed objects and/or surveyed and sensor significant existing objects to determine a position and verify position accuracy. The received MS sensor data enables an autonomous aircraft object identification and positioning system to correlate MS sensor data output with a-priori information stored onboard to determine and verify position and trajectory of the autonomous aircraft. Once position and trajectory are known, the object identification and positioning system commands the autonomous aircraft flight management system and autopilot control of the autonomous aircraft.

Abstract: A system and method for augmenting synthetic vision system (SVS) databases with spectrum diverse features that are matched to the observations of natural scenes derived from non-visible band sensors. The system correlates sensor output with a-priori information in databases to enhance system precision and robustness. Multiple diverse sensors image naturally occurring, or artificial features (towers buildings etc.) and store the multi-spectral attributes of those features within the enhanced multi-spectral database and share the information with other systems. The system, upon “live” observation of those features and attributes, correlates current observations with expected fiducial observations in the multi-spectral database and confirms operation, navigation, precise position, and sensor fidelity to enable autonomous operation of an aircraft employing the system.

Abstract: A system for presentation of visual information to a user includes an image generator operatively coupled to an information source, a projector operatively coupled to the image generator and configured to project light indicative of the image within a defined region of space comprising a head box, a head worn viewing device comprising an optical element configured to receive the light indicative of the image when the optical element is positioned in the head box and to convert the light indicative of the image into a final image viewable by the user.

Abstract: A system and method for controlling display characteristics is disclosed. The system and method can receive a control signal from a user interface and a video input signal. The system and method can filter the video input signal in accordance with a spatial frequency threshold related to the control signal to provide a filtered video output signal. The system and method can provide the filtered video output signal for display of an image on the translucent display and non-translucent display. The translucent display can be a head up display (HUD) and the non-translucent display can be a head down display. The user interface can be a brightness, contrast or combination brightness and contrast control.

Abstract: A system may include a structure, a head wearable device, emitters, receivers, and a processor. The emitters may be configured to emit signals and may be implemented on at least one of the structure or the head wearable device. The receivers may be configured to receive at least some of the signals from the emitters, to detect at least one signal property including signal intensity of the received signals, and to output information of the at least one signal property as signal data. The receivers may be implemented on at least one of the structure or the head wearable device. A processor may be configured to: receive the signal data from the receivers; determine a position and an orientation of the head wearable device based on the signal data; and output image or symbolic data to the head wearable device to be displayed by the head wearable device.

Abstract: A head worn display (HWD) includes a head attachment region, an internal display and a controller. The internal display is viewable by a user and includes variable transparency areas. The internal display is arranged to display at least a portion of an external region external to the HWD. The controller is configured to control the variable transparency areas to block view of a region of the external region and to control the internal display to overlay information in a region of the internal display corresponding to the region of the external region which is blocked.