A method is present for presenting a flight deck. A model of the flight deck is identified having a number of locations for a number of displays. Aircraft data is obtained. A number of panels is generated from the aircraft data. A display of the flight deck is generated containing the number of pane
A method is present for presenting a flight deck. A model of the flight deck is identified having a number of locations for a number of displays. Aircraft data is obtained. A number of panels is generated from the aircraft data. A display of the flight deck is generated containing the number of panels in the number of locations to form a presentation of the flight deck.
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1. A method for evaluating a configuration of a flight deck design, the method comprising: a physical processor identifying a model of a flight deck, the model comprising: a computer aided design model of a structure of the flight deck, a display panel design, and a number of locations corresponding
1. A method for evaluating a configuration of a flight deck design, the method comprising: a physical processor identifying a model of a flight deck, the model comprising: a computer aided design model of a structure of the flight deck, a display panel design, and a number of locations corresponding to a number of display panels on the structure of the flight deck; such that each display panel, in the number of display panels, corresponds to a location in the number of locations, the display panel design configured to receive inputs for changing a particular location corresponding to a particular display panel within the model of the flight deck, as well as an orientation and a scale of the particular display panel;receiving, from a user interface, a selection for: a display preference between performance and quality;evaluating the configuration before creating a prototype of and a simulator using the flight deck design the prototype comprising at least one of: wood, and core;identifying each location in the number of locations by a 3-D coordinate from a center of gravity of an aircraft comprising the flight deck;a panel, in the number of display panels, comprising a window display system and an instrument display system;the physical processor obtaining aircraft data comprising aircraft state data;the physical processor generating video data from the aircraft data;processing the video data and providing screen capture video data to display panels in the structure;the physical processor generating a display of the structure and the number of display panels of the flight deck responding to inputs from the aircraft data and an input device; andevaluating the configuration of the flight deck design via evaluating changes, responsive to inputs received from the input device, in the display of the structure and the number of display panels of the flight deck. 2. The method of claim 1 further comprising: displaying a number of controls within the flight deck communicating with an input device for controlling the number of controls;the physical processor generating new aircraft data responsive to receiving an input from the input device; andthe physical processor modifying the number of display panels based on the new aircraft data. 3. The method of claim 2, wherein the step of generating the video data from the aircraft data comprises: the physical processor sending inputs received from the input device to a simulation program; andthe physical processor receiving the new aircraft data from the simulation program. 4. A method for evaluating a configuration of a flight deck design, the method comprising: a physical processor identifying a model of a flight deck, the model comprising: a computer aided design model of a structure of the flight deck, a display panel design, and a number of locations corresponding to a number of display panels on the structure of the flight deck; such that each display panel, in the number of display panels, corresponds to a location in the number of locations, the display panel design configured to receive inputs for changing a particular location corresponding to a particular display panel within the model of the flight deck, as well as an orientation and a scale of the particular display panel;the physical processor obtaining aircraft data from at least one of: a simulation program, recorded flight data, and real time flight data, the aircraft data comprising aircraft state data;the physical processor generating video data from the aircraft data;processing the video data and providing screen capture video data to display panels in the structure;the physical processor generating a display of the structure and the number of display panels of the flight deck responding to inputs from the aircraft data and an input device; andevaluating the configuration of the flight deck design via evaluating changes, responsive to inputs received from the input device, in the display of the structure and the number of display panels of the flight deck. 5. The method of claim 4, further comprising the physical processor identifying the model of the flight deck comprising: the flight deck design, the display panel design, a digital terrain, and the number of locations for the number of display panels. 6. A method for evaluating a configuration of a flight deck design, the method comprising: a physical processor identifying a model of a flight deck, the model comprising: a computer aided design model of a structure of the flight deck, a display panel design, and a number of locations corresponding to a number of display panels on the structure of the flight deck; such that each display panel, in the number of display panels, corresponds to a location in the number of locations, the display panel design configured to receive inputs for changing a particular location corresponding to a particular display panel within the model of the flight deck, as well as an orientation and a scale of the particular display panel;the physical processor obtaining aircraft data comprising aircraft state data;the physical processor generating video data from the aircraft data;processing the video data and providing screen capture video data to display panels in the structure;the physical processor generating a display of the structure and the number of display panels of the flight deck responding to inputs from the aircraft data and an input device;evaluating the configuration of the flight deck design via evaluating changes, responsive to inputs received from the input device, in the display of the structure and the number of display panels of the flight deck; andtesting and reviewing alternative flight deck designs by changing the model of the flight deck. 7. A data processing system configured to evaluate, prior to a creation a prototype of and a simulator for a flight deck design, such that: the flight deck design comprises a flight deck structure and a number of panels located on the flight deck structure;the prototype comprises the at least one of: wood, and core;at least one panel in the number of panels comprises a window display system and an instrument display system; andthe data processing system comprises: a bus;a communications unit connected to the bus;a storage device connected to the bus, wherein the storage device includes program code; anda processor unit connected to the bus, the processor unit configured to: receive, from a user interface, a selection for: a display preference between performance and quality;execute the program code to identify a model of a flight deck that comprises: a flight deck design, a display panel design, and a number of locations on the flight deck structure for assigning a number of panels for displays that comprise at least one of: instruments and controls, and display a number of controls within the flight deck configured to: receive an input from an input device applied to the number of controls;generate new aircraft data from the input; andmodify a number of the number of panels based on the new aircraft data;execute the program code to send the input to a simulation program;receive the new aircraft data from the simulation program;receive an input, from an input device, to change a location of a panel, in the number of panels, in the model, the location being defined by a 3-D coordinate from a center of gravity of an aircraft that comprises the flight deck;obtain aircraft data;generate video data from the aircraft data;process the video data to provide instrument displays for presentation within the panels for the flight deck; andgenerate a display of the flight deck that comprises the number of panels that forms a tool for an evaluation of the input to change to the location of the panel in the model of the flight deck. 8. A data processing system configured to evaluate, prior to a creation a prototype of and a simulator for a flight deck design, the flight deck design that comprises a flight deck structure and a number of panels located on the flight deck structure, such that the data processing system comprises: a bus;a communications unit connected to the bus;a storage device connected to the bus, wherein the storage device includes program code; anda processor unit connected to the bus, the processor unit configured to: execute the program code to: and identify a model of a flight deck that comprises: a flight deck design, a display panel design, and a number of locations on the flight deck structure for assigning a number of panels for displays that comprise at least one of: instruments and controls; andtest and to review the flight deck design responsive to a change of the model of the flight deck;receive an input, from an input device, to change a location of a panel, in the number of panels, in the model, the location being defined by a 3-D coordinate from a center of gravity of an aircraft that comprises the flight deck;obtain aircraft data;generate video data from the aircraft data;process the video data to provide instrument displays for presentation within the panels for the flight deck; andgenerate a display of the flight deck that comprises the number of panels that forms a tool for an evaluation of the input to change to the location of the panel in the model of the flight deck. 9. The data processing system of claim 8, further comprising the processor unit configured to execute the program code to identify the model of the flight deck that comprises: the flight deck design, the display panel design, a digital terrain, and the number of locations for the number of panels. 10. A non-transitory computer recordable storage medium that comprises a computer program product programmed to: evaluate a configuration of a flight deck;identify a model of the flight deck that comprises: a flight deck design, a display panel design, and a number of locations, on a structure of the flight deck, that comprise a number of panels that comprise displays, each panel in the number of panels associated respectively with a location in the number of locations;receive an input, from an input device, to change a location in the number of location for a panel in the number of panels;obtain aircraft data that comprises aircraft state data;generate a video data from the aircraft data, and process the video data to provide instrument displays for presentation within the panels for the flight deck;generate a display of the flight deck that comprises the number of panels that forms a tool for an evaluation of the input to change to the location of the panel in the model of the flight deck; andtest and review flight deck designs based upon a change of the model for the flight deck. 11. The non-transitory computer recordable storage medium of claim 10, further comprising: the evaluation being a prerequisite to a prototype or simulator for the flight deck; andthe number of panels comprise at least one panel that comprises a window display system and an instrument display system. 12. The non-transitory computer recordable storage medium of claim 11 further comprising program code, stored on the non-transitory computer recordable storage medium, programmed to: receive, from a user interface, a selection for: a display preference between performance and quality;display a number of controls within the flight deck configured for manipulation via an input applied to the number of controls via an input device;generate new aircraft data from the input; andmodify a number of the number of panels based on the new aircraft data. 13. The non-transitory computer recordable storage medium of claim 12, further comprising program code, stored on the non-transitory computer recordable storage medium, programmed to: send the input to a simulation program; andreceive the new aircraft data from the simulation program. 14. The non-transitory computer recordable storage medium of claim 10, further comprising program code, stored on the non-transitory computer recordable storage medium, programmed to obtain the aircraft data from at least one of: a simulation program, recorded flight data, and real time flight data. 15. The computer program product of claim 10, further comprising: the location defined by a 3-D coordinate from a center of gravity of an aircraft that comprises the flight deck; andprogram code, stored on the non-transitory computer recordable storage medium, for identifying the model of the flight deck having the flight deck design, the display panel design, a digital terrain, and the number of locations for the number of panels.
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