Abstract: A method and apparatus are provided for adapting (modifying) input requirements, such as a required touch force or a touch screen format, in response to an event, for example, important situations, detection of an increased input error rate, aircrew activation, and motion such as turbulence, aircraft vibration, and/or gravitational forces.

Abstract: Methods and systems are provided for providing information relating to taxiing an aircraft at an airport having a plurality of taxi paths. One exemplary method involves identifying a first aircraft location on a first taxi path and a first aircraft heading along the first taxi path, and determining a first subset of possible taxi paths from the plurality of taxi paths based on the first aircraft location and the first aircraft heading, such that each respective taxi path of the first subset intersects the first taxi path at a respective intersection location in the first aircraft heading from the first aircraft location. The method continues by receiving a first input, and when the first input corresponds to a second taxi path of the first subset, providing indication of the second taxi path.

Abstract: A display system and method for an aircraft simultaneously displays the terrain under the flight plan, or under the current track of the aircraft, as both a two-dimensional lateral situation view image and as a perspective vertical situation view image. This provides improved tactical flight planning, and that does not erroneously show the flight plan passing through the displayed terrain.

Abstract: A flight deck display system for an aircraft or other vehicle includes a first data source of visual feature data that is indicative of visual features of a location of interest, a second data source of flight data for the aircraft, a processor architecture, and a display element. The processor architecture is operatively coupled to the first data source and to the second data source, and it is configured to process the visual feature data, process the flight data, and, based upon the visual feature data and the flight data, generate image rendering display commands. The display element receives the image rendering display commands and, in response thereto, renders a dynamic graphical representation of the location of interest using the visual feature data. The dynamic graphical representation of the location conveys an amount of visible detail that varies as a function of the flight data.

Abstract: A method for displaying information on a flight deck display element of an aircraft begins by obtaining a user interface command that represents a user-entered selection of a designated target. Relevant data is accessed and processed in response to this command, including aircraft status data for the aircraft, terrain data corresponding to terrain proximate the designated target, and graphics data corresponding to the designated target. Then, a target-focused display is rendered on the flight deck display element. The target-focused display includes a real-time synthetic perspective view of the designated target and the terrain proximate the designated target, wherein content of the target-focused display is influenced by the aircraft status data, the terrain data, and the graphics data.

Abstract: Methods and systems for operating a display device that is viewable by a user of an aircraft are provided. A first image is caused to be displayed on the display device. The first image is at least representative of a field of view from on-board the aircraft of an actual terrain. A second image is rendered over the first image on the display device. The second image includes a vertical position indicator indicating a vertical position of the aircraft relative to a selected flight path. The vertical position indicator is moved in a pitch direction on the display device in response to the aircraft moving relative to the actual terrain. The pitch direction corresponds to a change in the pitch of the aircraft.

Abstract: A method and system is provided for displaying aircraft symbology. The method includes displaying (302, 502, 702, 902, 1002) a symbol (202) for a first aircraft in a predetermined format, processing (304, 504, 704, 904, 1004) data related to flight conditions of the first aircraft and a second aircraft, determining (306, 506, 706, 906, 1006) a format for the display of the second aircraft based on the processed data, and displaying (308, 508, 708, 908, 1008) a symbol (212, 214, 216, 412, 416, 612, 614, 616, 812, 814, 816) for the second aircraft in accordance with the determined format.

Abstract: A methods, apparatus and system are provided for a vehicle with a ground navigational display. The system may include a display, a navigation system determining a location of the vehicle, a database storing a map including locations of buildings on the map and a processor. The processor may be configured to display the map on the display based upon the location of the vehicle, assign a fixed height to all of the buildings displayed on the display, and render the buildings displayed on the display in three-dimensions and having the assigned fixed height.

Abstract: A system for enhancing a vehicle operator's orientation and ability to navigate a vehicle includes, but is not limited to, a display unit, a data storage unit, a position determining unit and a processor communicatively connected to the display unit, the data storage unit and the position determining unit. The processor is configured to obtain a position and heading of the vehicle from the position determining unit, to obtain terrain data from the data storage unit, and to control the display unit to display a three-dimensional representation of a terrain representative of an actual terrain proximate the vehicle. The processor controls the display unit to overlay a three-dimensional compass onto the three-dimensional representation of the terrain to display both the heading of the vehicle and the location of the vehicle with respect to the actual terrain.

Abstract: Methods and systems for displaying a digital terrain to a user of a vehicle are provided. First, second, and third actual terrain data points are received. The third actual terrain data point is between the first and second actual terrain data points. If the third actual terrain data point is above a line interconnecting the first and second actual terrain data points, the first actual terrain data point is modified such that the third actual terrain data point is not above a line interconnecting said modified first actual terrain data point and the second actual terrain data point. A digital terrain is displayed to the user of the vehicle. The digital terrain includes a first digital terrain data point corresponding to the modified first actual terrain data point.

Abstract: A vehicle display system displays enhanced vision (EV) and captured images, for example synthetic vision (SV) images, to an operator of a vehicle. The display system includes an EV vision system for generating EV images, an SV database containing information regarding terrain and objects of interest for a travel path of a vehicle, an SV system for generating SV images based on travel of the vehicle and information from the SV database, a processor for filtering the EV images and merging the filtered EV image with the SV image, and a display for displaying the merged SV and filtered EV images.

Abstract: A display system for an aircraft includes a processing unit configured to determine a touchdown point for the aircraft and to supply display commands associated with the touchdown point; and a display device coupled the processing unit and configured to receive the display commands and operable to render symbology representing the touchdown point.

Abstract: A system for enhancing a vehicle operator's orientation and ability to navigate a vehicle includes, but is not limited to, a display unit, a data storage unit, a position determining unit and a processor communicatively connected to the display unit, the data storage unit and the position determining unit. The processor is configured to obtain a position and heading of the vehicle from the position determining unit, to obtain terrain data from the data storage unit, and to control the display unit to display a three-dimensional representation of a terrain representative of an actual terrain proximate the vehicle. The processor controls the display unit to overlay a three-dimensional compass onto the three-dimensional representation of the terrain to display both the heading of the vehicle and the location of the vehicle with respect to the actual terrain.

Abstract: Methods and systems are provided for displaying a symbol that is representative of an aircraft in flight. The method includes, but is not limited to, the steps of detecting an attitude of the aircraft and a view direction of an operator of the aircraft, and displaying with a near-to-eye display unit a three-dimensional symbol in an exocentric manner. The three-dimensional symbol is displayed to appear to be oriented in a manner that is representative of the attitude of the aircraft. The three-dimensional symbol is further displayed to rotate in a manner that corresponds with the view direction.

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.

Abstract: Methods and systems are provided for providing information relating to taxiing an aircraft at an airport having a plurality of taxi paths. One exemplary method involves identifying a first aircraft location on a first taxi path and a first aircraft heading along the first taxi path, and determining a first subset of possible taxi paths from the plurality of taxi paths based on the first aircraft location and the first aircraft heading, such that each respective taxi path of the first subset intersects the first taxi path at a respective intersection location in the first aircraft heading from the first aircraft location. The method continues by receiving a first input, and when the first input corresponds to a second taxi path of the first subset, providing indication of the second taxi path.

Abstract: A method and system is described for enhancing ground situational awareness to an aircrew via a display (116) within an aircraft (202, 310, 404) operating at an airport, including displaying (602, 704) at least one taxiway (A, B, C, D, E, G, K, 302, 408) for the airport, displaying (602, 704) at least one runway (210, 312, 406) for the airport, displaying (604, 706) a landmark related to the at least one taxiway (A, B, C, D, E, G, K, 302, 408), determining (606, 708) the position of the aircraft (202, 310, 404), displaying (608, 710) the aircraft (202, 310, 404), and blossoming (610, 712) the landmark (208, 304) as the aircraft (202, 310, 404) approaches the landmark (208, 304, 408).

Abstract: A flight deck display system for an aircraft or other vehicle includes a first data source of visual feature data that is indicative of visual features of a location of interest, a second data source of flight data for the aircraft, a processor architecture, and a display element. The processor architecture is operatively coupled to the first data source and to the second data source, and it is configured to process the visual feature data, process the flight data, and, based upon the visual feature data and the flight data, generate image rendering display commands. The display element receives the image rendering display commands and, in response thereto, renders a dynamic graphical representation of the location of interest using the visual feature data. The dynamic graphical representation of the location conveys an amount of visible detail that varies as a function of the flight data.

Abstract: Provided are methods and systems for automatically inserting intermediate waypoint information between travel critical waypoint information in an electronic waypoint list. The electronic waypoint list may contain travel critical waypoint information representing a planned track for a ship, an aircraft, a train or a terrestrial motor vehicle such as a truck. Two collinear, travel critical waypoints are received and inserted into the electronic list of waypoints. The location of an intermediate waypoint is then determined from a database containing records of a plurality of waypoints. If the location of the intermediate waypoint exists on a line between the at least two collinear, travel critical waypoints, then the intermediate waypoint is inserted in the electronic list of waypoints. If not, then the intermediate waypoint is discarded and another waypoint is examined to see if it exists on the line.

Abstract: A method for displaying information on a flight deck display element of an aircraft begins by obtaining a user interface command that represents a user-entered selection of a designated target. Relevant data is accessed and processed in response to this command, including aircraft status data for the aircraft, terrain data corresponding to terrain proximate the designated target, and graphics data corresponding to the designated target. Then, a target-focused display is rendered on the flight deck display element. The target-focused display includes a real-time synthetic perspective view of the designated target and the terrain proximate the designated target, wherein content of the target-focused display is influenced by the aircraft status data, the terrain data, and the graphics data.