Abstract: A method for integration of a portable electronic device (PED) with a flight deck display in some embodiments includes providing an onboard network coupled to a flight-deck-installed, multi-function display and coupling the PED to the onboard network. The method may also include receiving information from a PED hosted application in the PED, routing information through a gateway and/or a plurality of firewalls, and displaying information on the flight-deck-installed, multi-function display. In some embodiments, a pilot control interface is coupled to the PED through the onboard network, and a plurality of functions on the PED is controlled via the pilot control interface. An airplane in some embodiments includes a fuselage portion, a wing portion, and a system that carries out the method, possibly through use of computer readable storage medium with stored instructions.

Abstract: Systems and methods for compensating for latency in a touch screen controlled by a coupled processor, including maintaining historical data of delays in displaying a graphical response from the coupled processor after an input at the interactive touch screen, using the historical data to provide a graphical feedback signal at the interactive touch screen to reduce entry error by a user due to a delayed graphical response to the input, and displaying the graphical feedback on the interactive touch screen.

Abstract: Systems and methods for compensating for latency in a touch screen controlled by a coupled processor, including maintaining historical data of delays in displaying a graphical response from the coupled processor after an input at the interactive touch screen, using the historical data to provide a graphical feedback signal at the interactive touch screen to reduce entry error by a user due to a delayed graphical response to the input, and displaying the graphical feedback on the interactive touch screen.

Abstract: A method for integration of a portable electronic device (PED) with a flight deck display in some embodiments includes providing an onboard network coupled to a flight-deck-installed, multi-function display and coupling the PED to the onboard network. The method may also include receiving information from a PED hosted application in the PED, routing information through a gateway and/or a plurality of firewalls, and displaying information on the flight-deck-installed, multi-function display. In some embodiments, a pilot control interface is coupled to the PED through the onboard network, and a plurality of functions on the PED is controlled via the pilot control interface. An airplane in some embodiments includes a fuselage portion, a wing portion, and a system that carries out the method, possibly through use of computer readable storage medium with stored instructions.

Abstract: A method for integration of a portable electronic device (PED) with a flight deck display in some embodiments includes providing an onboard network coupled to a flight-deck-installed, multi-function display and coupling the PED to the onboard network. The method may also include receiving information from a PED hosted application in the PED, routing information through a gateway and/or a plurality of firewalls, and displaying information on the flight-deck-installed, multi-function display. In some embodiments, a pilot control interface is coupled to the PED through the onboard network, and a plurality of functions on the PED is controlled via the pilot control interface. An airplane in some embodiments includes a fuselage portion, a wing portion, and a system that carries out the method, possibly through use of computer readable storage medium with stored instructions.

Abstract: A method for integration of a portable electronic device (PED) with a flight deck display in some embodiments includes providing an onboard network coupled to a flight-deck-installed, multi-function display and coupling the PED to the onboard network. The method may also include receiving information from a PED hosted application in the PED, routing information through a gateway and/or a plurality of firewalls, and displaying information on the flight-deck-installed, multi-function display. In some embodiments, a pilot control interface is coupled to the PED through the onboard network, and a plurality of functions on the PED is controlled via the pilot control interface. An airplane in some embodiments includes a fuselage portion, a wing portion, and a system that carries out the method, possibly through use of computer readable storage medium with stored instructions.

Abstract: A method, apparatus and computer program product are provided for displaying forecast weather products in relation to a planned flight path of an air vehicle. The method, apparatus and computer program product may display a representation of future weather conditions along with the planned flight path of the air vehicle and a representation of the anticipated location of the air vehicle during the time period during which the future weather forecast is valid in order to provide context for the future weather information. Additionally, the method, apparatus and computer program product may display the weather information as well as information regarding the time period during which the weather information is valid in a graphical manner that is intuitive to the crew of the air vehicle so as not to distract or otherwise increase the workload upon the crew.

Abstract: A method identifies turbulence information from turbulence data generated by a set of remote aircraft based on a request to form identified turbulence information. The turbulence information is identified in response to the request received at an aircraft to view the turbulence information. The identified turbulence information is displayed on a display device in the aircraft.

Abstract: A method, apparatus and computer program product are provided for displaying forecast weather products in relation to a planned flight path of an air vehicle. The method, apparatus and computer program product may display a representation of future weather conditions along with the planned flight path of the air vehicle and a representation of the anticipated location of the air vehicle during the time period during which the future weather forecast is valid in order to provide context for the future weather information. Additionally, the method, apparatus and computer program product may display the weather information as well as information regarding the time period during which the weather information is valid in a graphical manner that is intuitive to the crew of the air vehicle so as not to distract or otherwise increase the workload upon the crew.

Abstract: A method identifies turbulence information from turbulence data generated by a set of remote aircraft based on a request to form identified turbulence information. The turbulence information is identified in response to the request received at an aircraft to view the turbulence information. The identified turbulence information is displayed on a display device in the aircraft.