Abstract:
A touch screen display assembly including, but not limited to, a touch sensitive screen, a bezel at least partly framing the touch sensitive screen, and a stabilizing member connected to the bezel and disposed proximate the touch sensitive screen. The stabilizing member is configured to stabilize a hand of an operator at multiple positions around a periphery of the touch sensitive screen when the operator interacts with the touch sensitive screen.
Abstract:
A dynamic runway indicator is displayed overlying a conformal runway for assisting a pilot in completing an approach to landing on a runway. The dynamic runway indicator includes a polygon, that by changing position with respect to the conformal runway, provides advanced instrumentation cues to the pilot for adjusting the aircraft flight path to a normal, or recommended, path to the runway for landing, thereby assisting the pilot to improve the accuracy and safety of the approach and landing.
Abstract:
Methods and systems are provided for identifying objects of interest during an air search and rescue (SAR) operation. The method comprises detecting an object of interest near a SAR pattern with a sensor onboard an aircraft. The location of the object of interest is input into a visual display system that is shown to an aircrew member. Distinct symbols are automatically added to categorize the object of interest on the visual display system. The distinct symbols are confirmed by the aircrew member accurately categorize the object of interest.
Abstract:
Avionic display systems and methods are provided for generating avionic displays including symbology decreasing the likelihood of boom tolerance threshold exceedance (an overpressure events) due to potential constructive interference between pressure waves occurring during supersonic flight. In various embodiments, the avionic display system includes a display device on which an avionic display is generated. A controller architecture is operably coupled to the display device and configured to determine when there exists a possibility for an overpressure event to occur in a future timeframe due to constructive interference between colliding pressure waves, which are forecast to occur during the impending supersonic flight of one or more A/C. When determining that there exists a possibility for an overpressure event to occur in the future timeframe due to constructive interference between pressure waves, the controller architecture further generates symbology or other graphics on the avionic display indicative of the potential occurrence of the overpressure event.
Abstract:
Avionic display systems and methods are provided for generating avionic displays, which include symbology and other graphics pertaining to forecast overpressure events, which are forecast to occur during supersonic aircraft flight. In various embodiments, the avionic display system includes a display device on which an avionic display is produced. A controller architecture is operably coupled to the display device. Storage media contains computer-readable code or instructions that, when executed by the controller architecture, cause the avionic display system to determine whether an overpressure event is forecast to occur due to the predicted future occurrence of a sonic boom, which has a magnitude exceeding a boom tolerance threshold. When the controller architecture determines that an overpressure event is forecast to occur, the avionic display system further generates symbology on the avionic display indicative of or visually signifying the forecast overpressure event.
Abstract:
A method and system are described for enhancing ground situational awareness to an aircrew via an alphanumeric display of an air traffic control ground clearance, including displaying a symbol for each stage of the clearance. A crewmember may accept or change each stage via a graphical user interface within the alphanumeric display.
Abstract:
A dynamic runway indicator is displayed overlying a conformal runway for assisting a pilot in completing an approach to landing on a runway. The dynamic runway indicator includes a polygon, that by changing position with respect to the conformal runway, provides advanced instrumentation cues to the pilot for adjusting the aircraft flight path to a normal, or recommended, path to the runway for landing, thereby assisting the pilot to improve the accuracy and safety of the approach and landing.
Abstract:
Methods and systems for improving presentation of terrain/obstacle alerting information in a composite (synthetic and sensor) image. An exemplary system includes an imaging device that obtains image data for a region exterior to the vehicle, a processing system, and a display device. The processing system is in data communication with the display device and the imaging device. The processing system receives information from an alerting (e.g., a terrain awareness and warning) system and the obtained image data, colors, or makes transparent at least a portion of the obtained image data, if the received information indicates that an alert condition exists for the portion of the obtained image data, and generates a composite image comprising a previously generated synthetic image and the obtained image data with the enhanced portion. The display device displays the composite image. The obtained image data overlie the synthetic image.
Abstract:
A system and methods of displaying airport field features on a flight deck display element of an aircraft are provided. The flight deck display system obtains geographic position data and heading data for the aircraft, accesses airport feature data associated with synthetic graphical representations of an airport field, and renders a dynamic synthetic display of the airport field on the flight deck display element. The dynamic synthetic display is rendered in accordance with the geographic position data, the heading data, and the airport feature data. In certain embodiments the synthetic display includes graphical representations of taxiways/runways, along with signage that is conformally rendered on the exposed taxiway surfaces. Display characteristics of the signage may be influenced by the actual physical and/or temporal proximity of the aircraft relative to reference locations on the airport field. In some embodiments, the taxiway/runway signage includes dynamic directional indicators corresponding to the intended directions of travel on the taxiways/runways. Moreover, the taxiway/runway signage can be dynamically rendered in a forward-facing manner at all times on the flight deck display element.
Abstract:
A panoramic image system with parallax mitigation includes a controller that can generate on a display an IFOV that includes image data from both a first image sensor having a first FOV and a second image sensor having a second FOV which are overlapping FOVs. The IFOV includes a portion of the non-overlapping section of a first FOV, the overlapping sections of both the first and second FOVs, and a portion of the non-overlapping section of the second FOV. The overlapping section of the first FOV is blended with the overlapping section of the second FOV, wherein the first FOV and the second FOV both have a level of contribution to the blended overlapping section. The level of contribution to the blending from the first FOV increases as the viewer’s head moves in a first angular direction and decreases as the viewer’s head moves in a second angular direction.