Abstract: Methods, apparatuses, systems, and computer program products are disclosed for determining a flight plan. An example method includes determining one or more potential flight plans from an originating location to a destination location, each potential flight plan comprising a different combination of one or more flight plan segments forming a potential flight plan from the originating location to the destination location. The method further includes calculating a projected cost for each of the one or more potential flight plans wherein the projected cost is based at least in part on dynamic cost data, dynamic navigation data, or a combination thereof. The method further includes determining an optimal flight plan from among the one or more potential flight plans, the optimal flight plan having a lowest aggregate cost of the calculated projected costs associated with each of the one or more potential flight plans.

Abstract: Methods, apparatuses, systems, and computer program products are disclosed for determining a flight plan. An example method includes determining one or more potential flight plans from an originating location to a destination location, each potential flight plan comprising a different combination of one or more flight plan segments forming a potential flight plan from the originating location to the destination location. The method further includes calculating a projected cost for each of the one or more potential flight plans wherein the projected cost is based at least in part on dynamic cost data, dynamic navigation data, or a combination thereof. The method further includes determining an optimal flight plan from among the one or more potential flight plans, the optimal flight plan having a lowest aggregate cost of the calculated projected costs associated with each of the one or more potential flight plans.

Abstract: A method for providing aircraft descent data and approach data onboard an aircraft is provided. The method determines a safe descent area bounded by an outer boundary region, by a processor communicatively coupled to a system memory element, based on an optimum glideslope angle, variable glideslope data, and a continuously monitored boundary exceedance condition; and presents graphical elements associated with the safe descent area, the optimum glideslope angle, and the outer boundary region, by a display device communicatively coupled to the processor.

Abstract: Methods and systems are provided for monitoring conformance of an aircraft to an actual and predicted 4-dimensional (4D) trajectory with respect to a reference business trajectory (RBT). First, a flight plan for the aircraft is acquired from an onboard flight management system (FMS) computer. A predicted flight trajectory is generated based on the latitude, longitude, altitude, speed and time of the flight plan for the aircraft. An onboard trajectory conformance monitor that is independent of the FMS computer, monitors the present flight trajectory of the aircraft and anticipates any actual or future deviations from the RBT. The trajectory conformance monitor will generate an advisory of any actual or anticipated deviations from the RBT.

Abstract: A method and system of monitoring aural and message alerts received during flight in an internet of things (IOT) cockpit of an aircraft generated by systems within the cockpit, the method includes: receiving a plurality of alerts which include at least one of an aural alert or message alert; applying a first natural language processing (NLP) process to the aural alert to convert the aural alert to a text alert consistent in structure with the message alert for aggregating together with the message alert to form a concatenated message alert; and identifying the context of the concatenated message alert by applying a second NLP process to the concatenated message alert in its entirety and subsequent tagging the concatenated message alert to associate a tagged message with a display element wherein the tagged message is a concatenated message.

Abstract: The present disclosure generally relates to display systems in the flight deck of an aircraft, and also to methods for providing such displays. More particularly, the displays and methods of the present disclosure are configured to integrate airport surface lighting information with information received from multiple air traffic control (ATC) communication channels, for purposes of increasing aircrew situational awareness and preventing runway incursions.

Abstract: A method for providing surface collision warning data onboard a first airport vehicle comprising an aircraft or other airport vehicle configured for ground-based travel, by a processor communicatively coupled to a system memory element, is provided.

Abstract: A method for providing surface collision warning data onboard a first airport vehicle comprising an aircraft or other airport vehicle configured for ground-based travel, by a processor communicatively coupled to a system memory element, is provided.

Abstract: A method for providing aircraft descent data and approach data onboard an aircraft is provided. The method determines a safe descent area bounded by an outer boundary region, by a processor communicatively coupled to a system memory element, based on an optimum glideslope angle, variable glideslope data, and a continuously monitored boundary exceedance condition; and presents graphical elements associated with the safe descent area, the optimum glideslope angle, and the outer boundary region, by a display device communicatively coupled to the processor.

Abstract: A method of operating an augmented reality processed terrain and obstacle threat scouting service is provided. The method includes using at least one sensor of a monitoring vehicle to monitor terrain and obstacle data. The monitored terrain and obstacle data is compared with terrain and obstacle data in a terrain and obstacle database. A non-validated georeferenced delta is determined when the comparison of the monitored terrain and obstacle data with terrain and obstacle data in the terrain and obstacle database finds non-matching terrain and obstacle data. The non-validated georeferenced delta is transmitted to a ground distribution center, consumer vehicle and/or cloud based server. Non-validated georeferenced delta received at a consumer vehicle is differentiated from other terrain and obstacle data on a synthetic vision display.

Abstract: Methods and systems are provided for monitoring conformance of an aircraft to an actual and predicted 4-dimensional (4D) trajectory with respect to a reference business trajectory (RBT). First, a flight plan for the aircraft is acquired from an onboard flight management system (FMS) computer. A predicted flight trajectory is generated based on the latitude, longitude, altitude, speed and time of the flight plan for the aircraft. An onboard trajectory conformance monitor that is independent of the FMS computer, monitors the present flight trajectory of the aircraft and anticipates any actual or future deviations from the RBT. The trajectory conformance monitor will generate an advisory of any actual or anticipated deviations from the RBT.

Abstract: A system and method for contextual tagging of data on at least one display associated with a vehicle is provided. The method includes: receiving data regarding the vehicle from at least one of a source of verbal data and a source of non-verbal data; determining a context associated with the data and a variable parameter associated with the context; determining a display element associated with the at least one display that corresponds to the determined variable parameter; generating a symbol for the display to display adjacent to the determined display element based on at least one of the determined context and the determined variable parameter; generating a selectable icon for the display to render adjacent to the symbol based on received verbal data; associating the received verbal data to the selectable icon; and outputting the received verbal data to an audio device based on a selection of the selectable icon.

Abstract: A method and system of monitoring aural and message alerts received during flight in an internet of things (IOT) cockpit of an aircraft generated by systems within the cockpit, the method includes: receiving a plurality of alerts which include at least one of an aural alert or message alert; applying a first natural language processing (NLP) process to the aural alert to convert the aural alert to a text alert consistent in structure with the message alert for aggregating together with the message alert to form a concatenated message alert; and identifying the context of the concatenated message alert by applying a second NLP process to the concatenated message alert in its entirety and subsequent tagging the concatenated message alert to associate a tagged message with a display element wherein the tagged message is a concatenated message.

Abstract: A method of operating an augmented reality processed terrain and obstacle threat scouting service is provided. The method includes using at least one sensor of a monitoring vehicle to monitor terrain and obstacle data. The monitored terrain and obstacle data is compared with terrain and obstacle data in a terrain and obstacle database. A non-validated georeferenced delta is determined when the comparison of the monitored terrain and obstacle data with terrain and obstacle data in the terrain and obstacle database finds non-matching terrain and obstacle data. The non-validated georeferenced delta is transmitted to a ground distribution center, consumer vehicle and/or cloud based server. Non-validated georeferenced delta received at a consumer vehicle is differentiated from other terrain and obstacle data on a synthetic vision display.

Abstract: A system and method for displaying a current state and a future state of a vehicle on a display associated with the vehicle are provided. The method includes: receiving flight plan data for a selected flight plan and a plurality of legs associated with the selected flight plan from a source of flight plan data; determining, with a processor, a current state of the vehicle with respect to one of the plurality of legs based on sensor data; determining, with the processor, a current target state for the vehicle with respect to one of the plurality of legs based on the flight plan data; determining a divergence of the current state based on a difference between the current state and the current target state; and generating a user interface for display that illustrates the divergence of the current state with respect to the one of the plurality of legs.

Abstract: Methods provide for guidance without sensing data about an ownship, the method includes: pre-loading, from an airport mapping database to an lateral guidance computer within a cockpit, airport mapping data for use in guidance of the ownship from a lateral guidance computer; executing airport moving map applications to process the airport mapping data to form a synthesized view for displaying on a display within the cockpit; receiving by the electronic information device within the cockpit at least one of a 3D spatial representation of the ownship; overlaying the 3D spatial representation of the ownship onto the synthesized view for providing a visual 3D representation of the ownship; and providing, without using the sensing data about the ownship, one or more cues, by a digital taxi application based on only airport mapping data and dimensions associated with the 3D spatial representation of the ownship, on the display within the cockpit.

Abstract: A method of operating an augmented reality processed terrain and obstacle threat scouting service is provided. The method includes using at least one sensor of a monitoring vehicle to monitor terrain and obstacle data. The monitored terrain and obstacle data is compared with terrain and obstacle data in a terrain and obstacle database. A non-validated georeferenced delta is determined when the comparison of the monitored terrain and obstacle data with terrain and obstacle data in the terrain and obstacle database finds non-matching terrain and obstacle data. The non-validated georeferenced delta is transmitted to a ground distribution center, consumer vehicle and/or cloud based server. Non-validated georeferenced delta received at a consumer vehicle is differentiated from other terrain and obstacle data on a synthetic vision display.

Abstract: The present disclosure generally relates to display systems in the flight deck of an aircraft, and also to methods for providing such displays. More particularly, the displays and methods of the present disclosure are configured to integrate airport surface lighting information with information received from multiple air traffic control (ATC) communication channels, for purposes of increasing aircrew situational awareness and preventing runway incursions.

Abstract: A system and method for contextual tagging of data on at least one display associated with a vehicle is provided. The method includes: receiving data regarding the vehicle from at least one of a source of verbal data and a source of non-verbal data; determining a context associated with the data and a variable parameter associated with the context; determining a display element associated with the at least one display that corresponds to the determined variable parameter; generating a symbol for the display to display adjacent to the determined display element based on at least one of the determined context and the determined variable parameter; generating a selectable icon for the display to render adjacent to the symbol based on received verbal data; associating the received verbal data to the selectable icon; and outputting the received verbal data to an audio device based on a selection of the selectable icon.

Abstract: A system and method for displaying a current state and a future state of a vehicle on a display associated with the vehicle are provided. The method includes: receiving flight plan data for a selected flight plan and a plurality of legs associated with the selected flight plan from a source of flight plan data; determining, with a processor, a current state of the vehicle with respect to one of the plurality of legs based on sensor data; determining, with the processor, a current target state for the vehicle with respect to one of the plurality of legs based on the flight plan data; determining a divergence of the current state based on a difference between the current state and the current target state; and generating a user interface for display that illustrates the divergence of the current state with respect to the one of the plurality of legs.