Abstract: Presented herein is a system and method for graphically displaying intruder aircraft symbology on an avionics display system onboard a host aircraft. The method comprises receiving data from the intruder aircraft, determining the reference altitude of the intruder aircraft, displaying intruder symbology on the display, and generating symbology on the display to visually distinguish the intruder symbology when the barosetting of the intruder is not substantially equal to the barosetting of the host aircraft.

Abstract: Embodiments of a flight deck display system for deployment onboard a host aircraft are provided, as are embodiments of a method carried-out by a flight deck display system. In one embodiment, the flight deck display system includes a cockpit display, a wireless communication module, and a controller operatively coupled to the cockpit display and to the wireless communication module. The controller is configured to generate a vertical In-Trail Procedure (ITP) window on the cockpit display, which includes graphics representative of the current position of the host aircraft, the current position of an intruder aircraft when present within a predetermined distance of the host aircraft, and a plurality of flight levels. The controller is further configured to receive data from which the current flight path of the intruder aircraft can be derived; and periodically update the vertical ITP window to include flight path symbology indicative of the current flight path of the intruder aircraft.

Abstract: An aircraft display system is provided and configured to render a cockpit display having a field-of-view. The system comprises a monitor and a processor coupled to the monitor and configured to generate a vertical situation display on the monitor. The vertical situation display includes at least one graphic indicative of a region of the terrain encompassed by the field-of-view.

Abstract: A display system and method for an aircraft are provided. The display device includes a processing unit configured to receive arrestor bed information associated with a runway and to generate display commands based on the arrestor bed information; and a display device coupled the processing unit and configured to receive the display commands and to display symbology representing the arrestor bed information.

Abstract: Embodiments of a flight deck display system for deployment onboard a host aircraft are provided, as are embodiments of a method carried-out by a flight deck display system. In one embodiment, the flight deck display system includes a cockpit display, a wireless communication module, and a controller operatively coupled to the cockpit display and to the wireless communication module. The controller is configured to generate a vertical In-Trail Procedure (ITP) window on the cockpit display, which includes graphics representative of the current position of the host aircraft, the current position of an intruder aircraft when present within a predetermined distance of the host aircraft, and a plurality of flight levels. The controller is further configured to receive data from which the current flight path of the intruder aircraft can be derived; and periodically update the vertical ITP window to include flight path symbology indicative of the current flight path of the intruder aircraft.

Abstract: A display system and method for an aircraft are provided. The display device includes a processing unit configured to receive arrestor bed information associated with a runway and to generate display commands based on the arrestor bed information; and a display device coupled the processing unit and configured to receive the display commands and to display symbology representing the arrestor bed information.

Abstract: A method is provided for displaying information on a display device of an aircraft. The method comprises determining graphics data for visual aids that represent segmented circle airport marker (SCAM) information, incorporating the graphics data into a user interface, and generating the user interface for display on the display device of the aircraft.

Abstract: An aircraft display system is provided and configured to render a cockpit display having a field-of-view. The system comprises a monitor and a processor coupled to the monitor and configured to generate a vertical situation display on the monitor. The vertical situation display includes at least one graphic indicative of a region of the terrain encompassed by the field-of-view.