Abstract: Methods and systems are provided for resolving a selected graphical element corresponding to a tactile user input associated with a graphical user interface display on a display device associated with a vehicle, such as an aircraft. The tactile user input is classified based on its temporal duration, and the classification of the tactile user input influences the identification of the selected graphical element or other response to the tactile user input.

Abstract: Systems and methods for displaying a scorecard for rating pilot performance by registering a wearable device based on the identification of the wearable device through pilot profile data, location data, and an identification key data received from the wearable device; linking, the wearable device to the avionic system to receive flight data, and to a cloud server to receive computed performance scores for in-flight display by the wearable device; alternately, in response to a manual input action, authenticating pilot identity to enable pilot access and linking of the flight data to the cloud server for display; generating a set of flight components via a model specified for a flight phase based on data from the wearable device if available, and the flight data, the model includes flight performance score values; displaying a flight phase performance score; and displaying on the graphical user interface in a cockpit display the performance scorecard.

Abstract: Methods and systems for providing landing area information on an active avionic display on a display device in a cockpit of an aircraft. The system includes an avionic display module configured to render an avionic display on a display device; and a landing area guidance module configured to: construct a graphical insert that is smaller than the avionic display, the graphical insert depicting the landing area environment as a two-dimensional area that includes a landing location rendered therein in a first visualization scheme; overlay the graphical insert on a small portion of the avionic display; indicate a target exit on the landing location; determine whether a runway overrun awareness alerting system (ROAAS) alert has been received; determine whether a surface indication alerts (SurfIA) alert has been received; responsive to the ROAAS alert and the SurfIA alert, alter the rendering within the graphical insert.

Abstract: Methods and systems are provided for assisting operation of a vehicle by monitoring a physiological state of an operator and automatically initiating a remedial action responsive to a change in the physiological state. One method involves determining a biometric indication of the current physiological state based on measurement data from one or more sensing devices, determining an activity-based indication of the current physiological state based on output signals from one or more user interface elements and determining an aggregate indicator of the current physiological state as a function of the biometric indication and the activity-based indication using one or more weighting factors that vary during operation of the vehicle. One or more remedial actions are automatically initiated based on the aggregate indicator, for example, in response to a change in physiological state indicated by the value of the aggregate indicator.

Abstract: Systems and methods for presenting a qualitative risk assessment for an aircraft to perform a flight procedure. Methods include determining: a pilot support value that is representative of a human-machine interface (HMI) onboard the aircraft; a crew factors value representative of a number of pilots and respective experience; an equipment state value of the aircraft, representing available and functioning avionic systems; a type of procedure for the flight procedure; a remaining trip length; an airport facilities state value; an Airport facilities state value; a physical environment value; and, an environmental state value. The method calculates the qualitative risk assessment, as a function of the determined values/factors and presents the qualitative risk assessment in a predefined area on an avionic display in the aircraft.

Abstract: Methods and systems of displaying weather data for a cockpit display system of an aircraft. The methods and systems include generating a display to include a first graphical map of real-time weather data from a weather radar. The display further includes a notification graphic associated with a portion of part of a displayed flight plan in which a significant weather condition exists. When the notification graphic is selected, the display includes the first graphical map of the real time weather data based on weather data from the weather radar and a second graphical map of significant weather conditions data derived from transmitted weather data.

Abstract: Systems and methods for presenting an RTA waypoint with associated time constraints. The system includes a flight management system (FMS) providing an assigned flight plan with a plurality of waypoints; a display device configured to render a current location and trajectory of the aircraft in a navigation display and in a vertical display; and a controller circuit. The system locates the RTA waypoint among the plurality of waypoints, as a function of the flight plan and the current location and trajectory of the aircraft. The system identifies a time constraint associated with the RTA waypoint. The system uses the time constraint to determine a type, from among an “at”, a “before”, and an “after”, for the RTA waypoint; and, assigns a preprogrammed visual encoding scheme for the type to the RTA waypoint. The system presents the RTA waypoint, using the visual encoding scheme, on the display device.

Abstract: Systems and methods for suggesting, on an avionic display in an aircraft, a communication frequency that is relevant to a context of the aircraft. The method includes determining a location and orientation of the aircraft and referencing an intended flight path to determine, based thereon, the context of the aircraft. The method uses the context to reference an on-board source of a plurality of stored navigation communication frequencies. The method identifies one or more relevant navigation communication frequencies for the context and presents the relevant navigation communication frequencies in a predefined area on an avionic display.

Abstract: Systems and methods for displaying a scorecard for rating pilot performance by registering a wearable device based on the identification of the wearable device through pilot profile data, location data, and an identification key data received from the wearable device; linking, the wearable device to the avionic system to receive flight data, and to a cloud server to receive computed performance scores for in-flight display by the wearable device; alternately, in response to a manual input action, authenticating pilot identity to enable pilot access and linking of the flight data to the cloud server for display; generating a set of flight components via a model specified for a flight phase based on data from the wearable device if available, and the flight data, the model includes flight performance score values; displaying a flight phase performance score; and displaying on the graphical user interface in a cockpit display the performance scorecard.

Abstract: Methods and systems are provided for guiding or otherwise assisting operation of an aircraft when diverting from a flight plan. One method involves determining a gliding trajectory for the aircraft based at least in part on a current altitude of the aircraft, providing a graphical representation of the gliding trajectory for the aircraft, identifying a plurality of landing locations within a range defined by the gliding trajectory from the aircraft, and for each landing location of the plurality of landing locations, providing a graphical representation of a respective landing location with respect to the gliding trajectory at a respective altitude associated with the respective landing location and at a respective distance with respect to a graphical representation of the aircraft corresponding to a respective geographic distance between a current location of the aircraft and the respective landing location.

Abstract: Methods and systems for providing landing area information on an active avionic display on a display device in a cockpit of an aircraft. The system includes an avionic display module configured to render an avionic display on a display device; and a landing area guidance module configured to: construct a graphical insert that is smaller than the avionic display, the graphical insert depicting the landing area environment as a two-dimensional area that includes a landing location rendered therein in a first visualization scheme; overlay the graphical insert on a small portion of the avionic display; indicate a target exit on the landing location; determine whether a runway overrun awareness alerting system (ROAAS) alert has been received; determine whether a surface indication alerts (SurfIA) alert has been received; responsive to the ROAAS alert and the SurfIA alert, alter the rendering within the graphical insert.

Abstract: Methods and systems for low visibility surface movement guidance for an aircraft navigating an airport environment. The system includes an avionic display module on an aircraft, configured to receive ownship data and generate an avionic display on a display device, and to respond to display commands. The system also includes a low voltage (LV) conditions module, configured to: receive weather data and determine when low voltage LV conditions are occurring; and, responsive to determining that LV conditions are occurring, (i) generate display commands to reconfigure the avionic display to present the LVO plan, rendered in accordance with a preprogrammed visualization scheme for rendering LV features in the LVO plan, and (ii) calculate an optimized taxi route for the aircraft to a target airport point of interest, as a function of the LVO plan. The system generates display commands to render the optimized taxi route on the reconfigured avionic display.

Abstract: Methods and systems are provided for propagating a free-form user input across different displays. One method involves receiving a free-form user input on a navigational map display, assigning a geographic location to the free-form user input based on a position of the free-form user input on the navigational map display, and generating a graphical indication influenced by the free-form user input on a second display at a respective position on the second display corresponding to the geographic location assigned to the free-form user input.

Abstract: A controller for selectively displaying information from raster charts is disclosed. The controller is configured to: retrieve raster data; assign a different priority level to each of a plurality of types of raster data; cause raster data having a predetermined priority level to be displayed with first augmentation information and prevent from being displayed raster data not having the first predetermined priority level, wherein the first augmentation information comprises database data retrieved from a database and is assigned a first predetermined augmentation information priority level; generate a hidden layer of second augmentation information comprising database data from the database that is correlated to a geographical location of the displayed raster data and assigned a second predetermined augmentation information priority level; and cause the hidden layer of second augmentation information to be displayed over a portion of the displayed raster data when the geographical location is selected.

Abstract: Systems and methods for presenting an RTA waypoint with associated time constraints. The system includes a flight management system (FMS) providing an assigned flight plan with a plurality of waypoints; a display device configured to render a current location and trajectory of the aircraft in a navigation display and in a vertical display; and a controller circuit. The system locates the RTA waypoint among the plurality of waypoints, as a function of the flight plan and the current location and trajectory of the aircraft. The system identifies a time constraint associated with the RTA waypoint. The system uses the time constraint to determine a type, from among an “at”, a “before”, and an “after”, for the RTA waypoint; and, assigns a preprogrammed visual encoding scheme for the type to the RTA waypoint. The system presents the RTA waypoint, using the visual encoding scheme, on the display device.

Abstract: A system and method of operating a correlative display system for a plurality of display systems on an aircraft includes receiving, by a processor, an identification of a feature from a user interface associated with a first display system of the plurality of display systems. The processor determines a location of the identified feature relative to data displayed on each other display system of the plurality of display systems, wherein the identified feature is not previously displayed on at least one of the other display systems of the plurality of display systems. The processor generates instructions to highlight the identified feature on each other display system of the plurality of display systems at the determine location relative to data displayed on each other display system.

Abstract: Methods and systems are provided for resolving a selected graphical element corresponding to a tactile user input associated with a graphical user interface display on a display device associated with a vehicle, such as an aircraft. The tactile user input is classified based on its temporal duration, and the classification of the tactile user input influences the identification of the selected graphical element or other response to the tactile user input.

Abstract: Methods and systems are provided for guiding or otherwise assisting operation of an aircraft when diverting from a flight plan. One method involves determining a gliding trajectory for the aircraft based at least in part on a current altitude of the aircraft, providing a graphical representation of the gliding trajectory for the aircraft, identifying a plurality of landing locations within a range defined by the gliding trajectory from the aircraft, and for each landing location of the plurality of landing locations, providing a graphical representation of a respective landing location with respect to the gliding trajectory at a respective altitude associated with the respective landing location and at a respective distance with respect to a graphical representation of the aircraft corresponding to a respective geographic distance between a current location of the aircraft and the respective landing location.

Abstract: A system and method for operating a dynamic vertical situation display on an aircraft includes generating display data for a dynamic vertical situation display displayed on a display based upon flight plan data from a flight management system, where the flight plan data includes a plurality of waypoints and one or more phases of flight. A current phase of flight of the aircraft and a number of waypoints currenting displayed on the dynamic vertical situation display on the display is determined, and instructions to dynamically change a size of the dynamic vertical situation display on the display are generated based upon at least one of the number of waypoints currenting displayed on the display and the current phase of flight of the aircraft.

Abstract: A method for displaying objects in an aerial vehicle is disclosed. The method includes: determining if sensed objects or calculated virtual objects around the travel path of the aerial vehicle are within a field of view of a three-dimensional view in front of the aerial vehicle displayed on a display screen in the aerial vehicle; selecting, for each graphical object representing an object within the field of view of the three-dimensional view, a graphical object display size for the object, wherein the display size of an object is determined based on a non-linear projection per distance between the object and the view point that is scaled based on a continuous, non-linear scaling function, which causes the object to be displayed smaller at certain distances and larger at other distances than it would if linear scaling alone were applied; causing the display of the one or more graphical objects with the selected display size.