Abstract:
A display system configured for displaying critical aeronautical information on an aircraft display that is not certified for displaying critical aeronautical information comprises a mounting adapter and an application server. The mounting adapter is configured to mount, in an aircraft cockpit, a personal electronic device (PED) wherein the PED is not certified to display critical aeronautical information. The mounting adapter further comprises a surface with an actuatable covering that is configured to be overlaid on a PED display and an actuation source configured to actuate the covering. The application server is configured to execute a module that generates critical aeronautical information, transmit the generated critical aeronautical information to the PED for display, determine whether a problem exists with the image displayed on the PED display, and enable the actuation source to cause the covering to annunciate a message indicating a problem with the image displayed on the PED display.
Abstract:
An augmented display system with dynamic see-through transmittance control is disclosed. The augmented display system includes: an augmented display screen; a tandem electrochromic (EC) filter disposed over the augmented display screen. The tandem EC filter includes a first window having a dominant first transmittance characteristic and a second window having a dominant second transmittance characteristic; and an augmented display transmittance controller configured to individually control the activation of the first window and the second window of the tandem EC filter, wherein the augmented display transmittance controller is configured to: determine from an ambient light sensor output the transmittance required from the first window and the second window for a selected augmented display luminance; and apply appropriate drive voltage waveforms to the first window and the second window to achieve the determined transmittance.
Abstract:
A method for verifying the integrity, continuity, and availability (ICA) of information displayed on an uncertified display is provided. The method comprises creating, on the high integrity device, application data for display on an uncertified display device; transmitting the application data to the uncertified display device for display; receiving, at the high integrity device from the uncertified display device, a captured image of the display captured using a screen capture feature on the uncertified display device; determining, at the high integrity device, an expected display image; comparing, at the high integrity device, the captured image of the display to the expected display image; identifying, at the high integrity device, a loss of ICA if one or more frames in the captured image fails the comparison with the expected display image; and causing the annunciation of a message indicating the loss of ICA when a loss of ICA is identified.
Abstract:
A mounting apparatus configured to mount a personal electronic device (PED) in an aircraft flight deck and provide a visible indication on the PED display when a fault condition exists includes an optical sensor positioned to view the PED display and configured to record an image of the PED display; an optically transparent surface configured to be overlaid on the PED display; an actuatable covering on the surface wherein the actuatable covering has a first optically transparent state and a second optically emissive state; an excitation source configured to cause the covering to switch from the first state to the second state; and a controller configured to transmit an image of the PED display recorded by the optical sensor to a server and command, responsive to receipt of an enable signal from the server, the actuation source to actuate the covering to indicate that the fault condition exists.
Abstract:
A system and method of displaying a conformal-capable head-up display image is provided. Distortions caused by combiner curvature, for example, are removed by pre-distorting and projecting separate images for each eye. Shutter-based eyewear controls the visibility as the imagery is cycled, e.g., shuttered, between left and right eyes. The combined image generator, projector and eyewear system maintains minimal vergence errors, minimal dipvergence errors, acceptable average transmittance, and optionally, high conformality.
Abstract:
Apparatus for a smudge-resistant structure and related fabrication methods are provided. An exemplary smudge-resistant structure includes a transparent substrate having a macrostructured surface configured to reduce contact with the transparent substrate and an oxidizing layer overlying the macrostructured surface.
Abstract:
A system and method of displaying a conformal-capable head-up display image is provided. Distortions caused by combiner curvature, for example, are removed by pre-distorting and projecting separate images for each eye. Shutter-based eyewear controls the visibility as the imagery is cycled, e.g., shuttered, between left and right eyes. The combined image generator, projector and eyewear system maintains minimal vergence errors, minimal dipvergence errors, acceptable average transmittance, and optionally, high conformality.
Abstract:
A display integrity system for use in a mounting adapter configured to mount a personal electronic device (PED) on an aircraft is disclosed. The display integrity system includes a transparent surface configured to overlay the display surface of a PED when the PED is mounted in the mounting adapter. The transparent surface includes one or more regions embedded with one or more coating layers that when activated with a select excitation wavelength are configured to emit visible light to annunciate a message indicating a problem with an image displayed on the PED. The display integrity system further includes a lighting source housed in the mounting adapter and configured to provide light in the select excitation wavelength when activated to illuminate the transparent surface and an imaging device mounted in the mounting adapter and configured to capture an image of the PED display for transmission to a server for integrity checking.
Abstract:
An addressable display system configured for use in a mounting adapter configured to mount a personal electronic device (PED) on an aircraft includes a transparent surface configured to overlay the display surface of a PED when the PED is mounted in the mounting adapter wherein the transparent surface includes a region that is uniformly coated with a coating layer that when activated with a select excitation wavelength is configured to emit visible light to annunciate a message indicating a problem with an image displayed on a PED display; a lighting source configured to provide light in at an excitation wavelength; a MEMS (microelectromechanical systems) scanner module that is controllable to write desired symbology for annunciation at different addressable locations on the transparent surface; and an imaging device configured to capture an image of the PED display for an integrity check of data displayed on the PED display.
Abstract:
A server system on an aircraft is provided. The server system is configured to allow critical aeronautical information to be displayed on a cockpit display that is not certified for displaying critical aeronautical information. The server system includes an aircraft interface device configured to interface with one or more aeronautical systems on the aircraft to retrieve critical aeronautical information; an application module configured to generate application data for display on the cockpit display wherein the application data includes at least some of the critical aeronautical information; an interface module configured to transmit the application data to the cockpit display for display; and an integrity checking module configured to retrieve image data from an image sensor trained on a display device in the cockpit display and configured to perform an integrity check on the image data from the image sensor.