Patent Publication Number: US-2023150686-A1

Title: System and method for separating avionics charts into a plurality of display panels

Description:
CROSS-REFERENCE TO RELATED APPLICATIONS 
     The present disclosure claims the benefit under 35 U.S.C. § 119(e) of U.S. Provisional Application Ser. No. 63/278,576, filed Nov. 12, 2021, entitled SYSTEMS AND METHODS FOR GENERATION, SELECTION, AND DISPLAY OF MAP-BASED CHART DATABASES FOR USE WITH CERTIFIED AVIONICS SYSTEMS, naming Jeff M. Henry, Kyle R. Peters, Todd E. Miller, Jason L. Wong, Reed A. Kovach, and Srinath Nandakumar as inventor, which is incorporated herein by reference in the entirety. 
    
    
     BACKGROUND 
     Avionics display systems often do not have ample data storage space available to store avionics chart data. There is a need for a system and method for lowering the individual chart data size. 
     SUMMARY 
     A method for separating avionics charts into a plurality of display panels is disclosed, in accordance with one or more embodiments of the present disclosure. The method includes receiving chart data for a virtual avionics chart. The method includes determining whether the received chart data exceeds a predetermined threshold. The method includes generating a plurality of display panels if the received chart data exceeds the predetermined threshold. The method includes determining one or more buffer lengths for the generated plurality of display panels. The method includes generating a plurality of output files based on the generated plurality of display panels and the determined one or more buffer lengths. 
     In some embodiments, the method may include providing the plurality of output files to an on-board aircraft controller for display on one or more display devices of an aircraft. 
     In some embodiments, the determine whether the received chart data exceeds a predetermined threshold may include comparing a data size of the received chart data to a predetermined data size threshold. 
     In some embodiments, the predetermined data size threshold may be between 1.2 Mb and 1.5 Mb. 
     In some embodiments, the predetermined data size threshold may be 1.3 Mb. 
     In some embodiments, the generate a plurality of display panels if the received chart data exceeds the predetermined threshold may further include determining one or more fold locations; determining one or more fold sizes; and assigning one or more fold numbers to one or more sections based on at least one of one or more x-values or one or more y-values. 
     In some embodiments, the one or more buffer lengths may be 1.00 inches. 
     In some embodiments, the method may further include determining whether chart data of the generated plurality of output files exceeds a predetermined threshold and adjusting a fold size of the one or more display panels if the chart data of the generated plurality of output files for the one or more display panels exceeds the predetermined threshold. 
     A system for separating avionics charts into a plurality of display panels is disclosed, in accordance with one or more embodiments of the present disclosure. The system includes one or more controllers including one or more processors configured to execute a set of program instructions stored in a memory, the set of program instructions configured to cause the one or more processors to: receive chart data for a virtual avionics chart; determine whether the received chart data exceeds a predetermined threshold; generate a plurality of display panels if the received chart data exceeds the predetermined threshold; determine one or more buffer lengths for the generated plurality of display panels; and generate a plurality of output files based on the generated plurality of display panels and the determined one or more buffer lengths. 
     In some embodiments, the one or more controllers may be configured to provide the plurality of output files to an on-board aircraft controller for display on one or more display devices of an aircraft. 
     In some embodiments, the determine whether the received chart data exceeds a predetermined threshold may include comparing a data size of the received chart data to a predetermined data size threshold. 
     In some embodiments, the predetermined data size threshold may be between 1.2 Mb and 1.5 Mb. 
     In some embodiments, the predetermined data size threshold may be 1.3 Mb. 
     In some embodiments, the generate a plurality of display panels if the received chart data exceeds the predetermined threshold may further include determining one or more fold locations; determining one or more fold sizes; and assigning one or more fold numbers to one or more sections based on at least one of one or more x-values or one or more y-values. 
     In some embodiments, the method may further include determining whether chart data of the generated plurality of output files exceeds a predetermined threshold and adjusting a fold size of the one or more display panels if the chart data of the generated plurality of output files for the one or more display panels exceeds the predetermined threshold. 
     This Summary is provided solely as an introduction to subject matter that is fully described in the Detailed Description and Drawings. The Summary should not be considered to describe essential features nor be used to determine the scope of the Claims. Moreover, it is to be understood that both the foregoing Summary and the following Detailed Description are examples and explanatory only and are not necessarily restrictive of the subject matter claimed. 
    
    
     
       BRIEF DESCRIPTION OF THE DRAWINGS 
       The detailed description is described with reference to the accompanying figures. The use of the same reference numbers in different instances in the description and the figures may indicate similar or identical items. Various embodiments or examples (“examples”) of the present disclosure are disclosed in the following detailed description and the accompanying drawings. The drawings are not necessarily to scale. In general, operations of disclosed processes may be performed in an arbitrary order, unless otherwise provided in the claims. In the drawings: 
         FIG.  1 A  illustrates a simplified block diagram of an aircraft including the system for separating avionics charts into a plurality of display panels, in accordance with one or more embodiments of the present disclosure; 
         FIG.  1 B  illustrates an aircraft including the system for separating avionics charts into a plurality of display panels, in accordance with one or more embodiments of the present disclosure; 
         FIG.  2    illustrates a flowchart depicting a method or process for separating avionics charts into a plurality of display panels, in accordance with one or more embodiments of the present disclosure; 
         FIG.  3    illustrates a flowchart depicting a method or process for separating avionics charts into a plurality of display panels, in accordance with one or more embodiments of the present disclosure; 
         FIG.  4    illustrates a simplified schematic of an avionic chart separated into a plurality of display panels, in accordance with one or more embodiments of the present disclosure; 
         FIG.  5    illustrates a simplified schematic of an avionic chart separated into a plurality of display panels, in accordance with one or more embodiments of the present disclosure. 
     
    
    
     DETAILED DESCRIPTION OF THE INVENTION 
     Reference will now be made in detail to the subject matter disclosed, which is illustrated in the accompanying drawings. 
     Before explaining one or more embodiments of the present disclosure in detail, it is to be understood the embodiments are not limited in their application to the details of construction and the arrangement of the components or steps or methodologies set forth in the following description or illustrated in the drawings. In the following detailed description of embodiments, numerous specific details may be set forth in order to provide a more thorough understanding of the present disclosure. However, it will be apparent to one of ordinary skill in the art having the benefit of the instant disclosure the embodiments disclosed herein may be practiced without some of these specific details. In other instances, well-known features may not be described in detail to avoid unnecessarily complicating the instant disclosure. 
     As used herein a letter following a reference numeral is intended to reference an embodiment of the feature or element that may be similar, but not necessarily identical, to a previously described element or feature bearing the same reference numeral (e.g., 1, 1a, 1b). Such shorthand notations are used for purposes of convenience only and should not be construed to limit the disclosure in any way unless expressly stated to the contrary. 
     Further, unless expressly stated to the contrary, “or” refers to an inclusive or and not to an exclusive or. For example, a condition A or B is satisfied by any one of the following: A is true (or present) and B is false (or not present), A is false (or not present) and B is true (or present), and both A and B are true (or present). 
     In addition, use of “a” or “an” may be employed to describe elements and components of embodiments disclosed herein. This is done merely for convenience and “a” and “an” are intended to include “one” or “at least one,” and the singular also includes the plural unless it is obvious that it is meant otherwise. 
     Finally, as used herein any reference to “one embodiment” or “some embodiments” means that a particular element, feature, structure, or characteristic described in connection with the embodiment is included in at least one embodiment disclosed herein. The appearances of the phrase “in some embodiments” in various places in the specification are not necessarily all referring to the same embodiment, and embodiments may include one or more of the features expressly described or inherently present herein, or any combination of or sub-combination of two or more such features, along with any other features which may not necessarily be expressly described or inherently present in the instant disclosure. 
       FIGS.  1 A- 5    generally illustrate a system and method for separating avionics charts into a plurality of display panels, in accordance with one or more embodiments of the present disclosure. 
     Aeronautical charts (or avionics charts) are widely used for air navigation. The Federal Aviation Administration (FAA) publishes charts for each stage of Visual Flight Rules (VFR) and Instrument Flight Rules (IFR) air navigation including training, planning, and departures, enroute (for low and high altitudes), approaches, and taxiing charts. These charts are frequently updated by the FAA. For example, the charts may be updated about once a month. As such, a pilot must ensure that they have the most-up-to-date charts on-board when flying. 
     In general, enroute charts provide aeronautical information for enroute instrument navigation. High altitude enroute charts are used to provide information for navigation at or above 18,000 ft MSL, while low altitude enroute charts are used to below information for navigation below 18,000 ft MSL. For example, high altitude enroute charts include jet and RNAV routes, identification and frequency of radio aids, selected airports, distances, time zones, special use air space, and the like. By way of another example, low altitude enroute charts include information regarding airports, NAVAIDs, communications, air traffic services, airspace, and the like. In general, these enroute charts are large in both physical size and chart data size. 
     Avionics display systems often do not have ample data storage space available on the display hardware to store the data for each aeronautical chart. For example, there may about approximately 1.3 Mb of available space in the display hardware (which is the upper limit that can be displayed at one time) and a given chart may be greater than 1.3 Mb (e.g., 25 Mb). Therefore, there is a need for a system and method for lowering the individual chart size, such that the system is able to display the chart. 
     As such, it would be desirable to provide a system and method for separating large avionics charts into multiple display panels. The system and method should allow charts to be processed off-line, such that the avionic resources have the bandwidth to display the processed charts during run-time. For example, the system and method may be configured to systematically break up the avionics charts into a plurality of panels to display on multiple display panels. By way of another example, the system and method may be configured to allow for overlapping panels to minimize panel swapping along the edges. By way of another example, the system and method may be configured to allow for program variance in choosing panel and buffer sizes. By way of another example, the system and method may be configured to modify the coordinates of the chart display items to new locations based on the panel boundaries (e.g., items outside the defined section are discarded, items that span sections are modified, and the like). By way of another example, the system and method may be configured to modify clip structures to the new boundaries (e.g., items outside the defined section are discarded, items that span sections are modified, or the like). By way of another example, the system and method may be configured to create new structures based on new boundaries by reassembling the modified lines and clip structures, such that each panel may be processed as an individual chart. 
       FIGS.  1 A- 1 B  illustrate an aircraft including a system for separating avionics charts into a plurality of display panels, in accordance with one or more embodiments of the present disclosure. 
     Referring now to  FIG.  1 A , the aircraft  100  may include an aircraft controller  102  (e.g., on-board/run-time controller). The aircraft controller  102  may include one or more processors  104 , memory  106  configured to store one or more program instructions  108 , and/or one or more communication interfaces  110 . 
     The aircraft  100  may include an avionics environment such as, but not limited to, a cockpit. The aircraft controller  102  may be coupled (e.g., physically, electrically, and/or communicatively) to one or more display devices  112 . The one or more display devices  112  may be configured to display three-dimensional images and/or two-dimensional images. Referring now to  FIG.  1 B , the avionics environment (e.g., the cockpit) may include any number of display devices  112  (e.g., one, two, three, or more displays) such as, but not limited to, one or more head-down displays (HDDs)  112 , one or more head-up displays (HUDs)  112 , one or more multi-function displays (MFDs), one or more adaptive flight displays (AFDs)  112 , one or more primary flight displays (PFDs)  112 , or the like. The one or more display devices  112  may be employed to present flight data including, but not limited to, situational awareness data (e.g., chart data) and/or flight queue data to a pilot or other crew member. For example, the situational awareness data (e.g., chart data) may be based on, but is not limited to, aircraft performance parameters, aircraft performance parameter predictions, sensor readings, alerts, or the like. 
     Referring again to  FIG.  1 A , the aircraft controller  102  may be coupled (e.g., physically, electrically, and/or communicatively) to one or more user input devices  114 . The one or more display devices  112  may be coupled to the one or more user input devices  114 . For example, the one or more display devices  112  may be coupled to the one or more user input devices  114  by a transmission medium that may include wireline and/or wireless portions. The one or more display devices  112  may include and/or be configured to interact with one or more user input devices  114 . 
     The one or more display devices  112  and the one or more user input devices  114  may be standalone components within the aircraft  100 . It is noted herein, however, that the one or more display devices  112  and the one or more user input devices  114  may be integrated within one or more common user interfaces  116 . 
     Where the one or more display devices  112  and the one or more user input devices  114  are housed within the one or more common user interfaces  116 , the aircraft controller  102 , one or more offboard controllers  124 , and/or the one or more common user interfaces  116  may be standalone components. It is noted herein, however, that the aircraft controller  102 , the one or more offboard controllers  124 , and/or the one or more common user interfaces  116  may be integrated within one or more common housings or chassis. 
     The aircraft controller  102  may be coupled (e.g., physically, electrically, and/or communicatively) to and configured to receive data from one or more aircraft sensors  118 . The one or more aircraft sensors  118  may be configured to sense a particular condition(s) external or internal to the aircraft  100  and/or within the aircraft  100 . The one or more aircraft sensors  118  may be configured to output data associated with particular sensed condition(s) to one or more components/systems onboard the aircraft  100 . Generally, the one or more aircraft sensors  118  may include, but are not limited to, one or more inertial measurement units, one or more airspeed sensors, one or more radio altimeters, one or more flight dynamic sensors (e.g., sensors configured to sense pitch, bank, roll, heading, and/or yaw), one or more weather radars, one or more air temperature sensors, one or more surveillance sensors, one or more air pressure sensors, one or more engine sensors, and/or one or more optical sensors (e.g., one or more cameras configured to acquire images in an electromagnetic spectrum range including, but not limited to, the visible light spectrum range, the infrared spectrum range, the ultraviolet spectrum range, or any other spectrum range known in the art). 
     The aircraft controller  102  may be coupled (e.g., physically, electrically, and/or communicatively) to and configured to receive data from one or more navigational systems  120 . The one or more navigational systems  120  may be coupled (e.g., physically, electrically, and/or communicatively) to and in communication with one or more GPS satellites  122 , which may provide vehicular location data (e.g., aircraft location data) to one or more components/systems of the aircraft  100 . For example, the one or more navigational systems  120  may be implemented as a global navigation satellite system (GNSS) device, and the one or more GPS satellites  122  may be implemented as GNSS satellites. The one or more navigational systems  120  may include a GPS receiver and a processor. For example, the one or more navigational systems  120  may receive or calculate location data from a sufficient number (e.g., at least four) of GPS satellites  122  in view of the aircraft  100  such that a GPS solution may be calculated. 
     It is noted herein the one or more aircraft sensors  118  may operate as a navigation device  120 , being configured to sense any of various flight conditions or aircraft conditions typically used by aircraft and output navigation data (e.g., aircraft location data, aircraft orientation data, aircraft direction data, aircraft speed data, and/or aircraft acceleration data). For example, the various flight conditions or aircraft conditions may include altitude, aircraft location (e.g., relative to the earth), aircraft orientation (e.g., relative to the earth), aircraft speed, aircraft acceleration, aircraft trajectory, aircraft pitch, aircraft bank, aircraft roll, aircraft yaw, aircraft heading, air temperature, and/or air pressure. By way of another example, the one or more aircraft sensors  118  may provide aircraft location data and aircraft orientation data, respectively, to the one or more processors  104 ,  126 . 
     The aircraft controller  102  of the aircraft  100  may be coupled (e.g., physically, electrically, and/or communicatively) to one or more offboard controllers  124 . 
     The one or more offboard controllers  124  may include one or more processors  126 , memory  128  configured to store one or more programs instructions  130  and/or one or more communication interfaces  132 . 
     The aircraft controller  102  and/or the one or more offboard controllers  124  may be coupled (e.g., physically, electrically, and/or communicatively) to one or more satellites  134 . For example, the aircraft controller  102  and/or the one or more offboard controllers  124  may be coupled (e.g., physically, electrically, and/or communicatively) to one another via the one or more satellites  134 . For instance, at least one component of the aircraft controller  102  may be configured to transmit data to and/or receive data from at least one component of the one or more offboard controllers  124 , and vice versa. By way of another example, at least one component of the aircraft controller  102  may be configured to record event logs and may transmit the event logs to at least one component of the one or more offboard controllers  124 , and vice versa. By way of another example, at least one component of the aircraft controller  102  may be configured to receive information and/or commands from the at least one component of the one or more offboard controllers  124 , either in response to (or independent of) the transmitted event logs, and vice versa. 
     It is noted herein that the aircraft  100  and the components onboard the aircraft  100 , the one or more offboard controllers  124 , the one or more GPS satellites  122 , and/or the one or more satellites  134  may be considered components of a system  138 , for purposes of the present disclosure. The system may be generally discussed in concurrently filed U.S. patent application Ser. No. ______, filed on Nov. 12, 2021, entitled TOOL TO FACILITATE CUSTOMER GENERATED CHART DATABASES FOR USE WITH A CERTIFIED AVIONICS SYSTEM and having attorney docket number 131418US01, which is incorporated herein by reference in the entirety. 
     The one or more processors  104 ,  126  may include any one or more processing elements, micro-controllers, circuitry, field programmable gate array (FPGA) or other processing systems, and resident or external memory for storing data, executable code, and other information accessed or generated by the aircraft controller  102  and/or the one or more offboard controllers  124 . In this sense, the one or more processors  104 ,  126  may include any microprocessor device configured to execute algorithms and/or program instructions. It is noted herein, however, that the one or more processors  104 ,  126  are not limited by the materials from which it is formed or the processing mechanisms employed therein and, as such, may be implemented via semiconductor(s) and/or transistors (e.g., using electronic integrated circuit (IC) components), and so forth. In general, the term “processor” may be broadly defined to encompass any device having one or more processing elements, which execute a set of program instructions from a non-transitory memory medium (e.g., the memory), where the set of program instructions is configured to cause the one or more processors to carry out any of one or more process steps. 
     The memory  106 ,  128  may include any storage medium known in the art suitable for storing the set of program instructions executable by the associated one or more processors. For example, the memory  106 ,  128  may include a non-transitory memory medium. For instance, the memory  106 ,  128  may include, but is not limited to, a read-only memory (ROM), a random access memory (RAM), a magnetic or optical memory device (e.g., disk), a magnetic tape, a solid state drive, flash memory (e.g., a secure digital (SD) memory card, a mini-SD memory card, and/or a micro-SD memory card), universal serial bus (USB) memory devices, and the like. The memory  106 ,  128  may be configured to provide display information to the display device (e.g., the one or more display devices  112 ). In addition, the memory  106 ,  128  may be configured to store user input information from a user input device of a user interface. The memory  106 ,  128  may be housed in a common controller housing with the one or more processors. The memory  106 ,  128  may, alternatively or in addition, be located remotely with respect to the spatial location of the processors and/or a controller. For instance, the one or more processors and/or the controller may access a remote memory (e.g., server), accessible through a network (e.g., internet, intranet, and the like). 
     The aircraft controller  102  and/or the one or more offboard controllers  124  may be configured to perform one or more process steps, as defined by the one or more sets of program instructions  108 ,  130 . The one or more process steps may be performed iteratively, concurrently, and/or sequentially. The one or more sets of program instructions  108 ,  130  may be configured to operate via a control algorithm, a neural network (e.g., with states represented as nodes and hidden nodes and transitioning between them until an output is reached via branch metrics), a kernel-based classification method, a Support Vector Machine (SVM) approach, canonical-correlation analysis (CCA), factor analysis, flexible discriminant analysis (FDA), principal component analysis (PCA), multidimensional scaling (MDS), principal component regression (PCR), projection pursuit, data mining, prediction-making, exploratory data analysis, supervised learning analysis, boolean logic (e.g., resulting in an output of a complete truth or complete false value), fuzzy logic (e.g., resulting in an output of one or more partial truth values instead of a complete truth or complete false value), or the like. For example, in the case of a control algorithm, the one or more sets of program instructions  108 ,  130  may be configured to operate via proportional control, feedback control, feedforward control, integral control, proportional-derivative (PD) control, proportional-integral (PI) control, proportional-integral-derivative (PID) control, or the like. 
     The one or more communication interfaces  110 ,  134  may be operatively configured to communicate with one or more components of the aircraft controller  102  and/or the one or more offboard controllers  124 . For example, the one or more communication interfaces  110 ,  134  may also be coupled (e.g., physically, electrically, and/or communicatively) with the one or more processors  104 ,  126  to facilitate data transfer between components of the one or more components of the aircraft controller  102  and/or the one or more offboard controllers  124  and the one or more processors  104 ,  126 . For instance, the one or more communication interfaces  110 ,  134  may be configured to retrieve data from the one or more processors  104 ,  126 , or other devices, transmit data for storage in the memory  106 ,  128 , retrieve data from storage in the memory  106 ,  128 , or the like. By way of another example, the aircraft controller  102  and/or the one or more offboard controllers  124  may be configured to receive and/or acquire data or information from other systems or tools by a transmission medium that may include wireline and/or wireless portions. By way of another example, the aircraft controller  102  and/or the one or more offboard controllers  124  may be configured to transmit data or information (e.g., the output of one or more procedures of the inventive concepts disclosed herein) to one or more systems or tools by a transmission medium that may include wireline and/or wireless portions (e.g., a transmitter, receiver, transceiver, physical connection interface, or any combination). In this regard, the transmission medium may serve as a data link between the aircraft controller  102  and/or the one or more offboard controllers  124  and the other subsystems (e.g., of the aircraft  100  and/or the system  138 ). In addition, the aircraft controller  102  and/or the one or more offboard controllers  124  may be configured to send data to external systems via a transmission medium (e.g., network connection). 
     The one or more display devices  112  may include any display device known in the art. For example, the display devices  112  may include, but are not limited to, one or more head-down displays (HDDs), one or more HUDs, one or more multi-function displays (MFDs), or the like. For instance, the display devices  112  may include, but are not limited to, a liquid crystal display (LCD), a light-emitting diode (LED) based display, an organic light-emitting diode (OLED) based display, an electroluminescent display (ELD), an electronic paper (E-ink) display, a plasma display panel (PDP), a display light processing (DLP) display, or the like. Those skilled in the art should recognize that a variety of display devices may be suitable for implementation in the present invention and the particular choice of display device may depend on a variety of factors, including, but not limited to, form factor, cost, and the like. In a general sense, any display device capable of integration with the user input device (e.g., touchscreen, bezel mounted interface, keyboard, mouse, trackpad, and the like) is suitable for implementation in the present invention. 
     The one or more user input devices  114  may include any user input device known in the art. For example, the user input device  114  may include, but is not limited to, a keyboard, a keypad, a touchscreen, a lever, a knob, a scroll wheel, a track ball, a switch, a dial, a sliding bar, a scroll bar, a slide, a handle, a touch pad, a paddle, a steering wheel, a joystick, a bezel input device, or the like. In the case of a touchscreen interface, those skilled in the art should recognize that a large number of touchscreen interfaces may be suitable for implementation in the present invention. For instance, the display device may be integrated with a touchscreen interface, such as, but not limited to, a capacitive touchscreen, a resistive touchscreen, a surface acoustic based touchscreen, an infrared based touchscreen, or the like. In a general sense, any touchscreen interface capable of integration with the display portion of a display device is suitable for implementation in the present invention. In another embodiment, the user input device may include, but is not limited to, a bezel mounted interface. 
       FIG.  2    illustrates a flowchart depicting a method or process  200  for separating large avionics charts into multiple display panels, in accordance with one or more embodiments of the disclosure.  FIGS.  4 - 5    generally illustrate graphical representations of a plurality of display panels of a separated avionics chart, in accordance with one or more embodiments of the disclosure. 
     In a step  202 , chart data may be received from a third-party chart provider. For example, the offboard controller  124  may be configured to receive chart data from a third-party chart provider. In one instance, the offboard controller  124  may be configured to receive enroute chart data from a third-party enroute chart provider. In another instance, the offboard controller  124  may be configured to receive terminal chart data from a third-party terminal chart provider. 
     It is noted that the offboard controller  124  may be configured to receive any type of chart known from any suitable third-party chart provider. 
     In a step  204 , it is determined whether the received chart data exceeds a predetermined threshold. For example, the offboard controller  124  may be configured to compare a size of the received chart data to a predetermined threshold to determine whether the received chart data exceeds the predetermined threshold. In one instance, the offboard controller  124  may be configured to compare a data size of the received chart data to a predetermined chart data size threshold to determine whether the received chart data exceeds the predetermined chart data size threshold (e.g., whether the received chart data is too large in data size). It is noted that the predetermined chart data size threshold may be any threshold suitable for the display system. For example, the predetermined chart data size threshold may be between 1.2-1.5 Mb. For instance, the predetermined chart data size threshold may be 1.3 Mb. 
     If the received chart data size does not exceed the predetermined threshold (i.e., the data size is less than that predetermined threshold), then in a step  206 , the chart data may be provided to the on-board aircraft controller  102  for display on the one or more display devices  112 . In this regard, the chart is not separated into a plurality of display panels prior to display on the one or more display devices  112 . 
     If the received chart data size exceeds the predetermined threshold (i.e., the data size is greater than that predetermined threshold), then in a step  208 , a plurality of display panels  402  may be generated. It is noted that the display panels may be labeled using any labeling mechanism suitable for defining each individual display panel. The labels (e.g., 00, 01, 02, . . . ) shown in  FIG.  4    are provided merely for illustrative purposes and shall not be construed as limiting the scope of the present disclosure. 
       FIG.  3    illustrates a flowchart depicting a method or process  208  for generating the plurality of display panels, in accordance with one or more embodiments of the disclosure. 
     In a step  302 , one or more fold locations may be determined. For example, the offboard controller  124  may be configured to generate a plurality of display panels  402  by determining one or more fold locations. For instance, the offboard controller  124  may be configured to adjust one or more dimensions of the received chart image and determine a size of the adjusted image. In this regard, the offboard controller  124  may be configured to remove one or more portions of the received chart image (e.g., title page, legend, or the like) to generate an adjusted image and determine a size of the adjusted image. 
     In a step  304 , one or more fold sizes may be determined. For example, the offboard controller  124  may be configured to determine an x-axis fold size (F x ) and further configured to determine a y-axis fold size (F y ). For instance, the offboard controller  124  may be configured to adjust the size of the adjusted image based on a folding algorithm. In this regard, the adjusted image may be divided by a predetermined fold size threshold (e.g., divided by 10 inches) to generate one or more pages (P) and a remainder (R). If the remainder (R) is less than a predetermined threshold, then the offboard controller  124  may be configured to distribute that amount to each page (P). At that point, each page may have a size of S+R/p. For example, S may be 10, P may be 5, and R may be 2 for a 52-inch wide chart, such that the panel size may be 10.4 inches (10+⅖). If the remainder (R) is more than 4, then the offboard controller  124  may be configured to add another page (P). For example, for a 57-inch wide chart, the chart may have five (5) panels of 10 inches and one (1) of 7 inches. It is noted that the aforementioned process may be performed for both the x- (horizontal) and y-axis (vertical). 
     Referring to  FIG.  5   , the fold size may be configurable. For example, where the virtual avionics chart includes a chart legend  320 , the offboard controller  124  may be configured to determine a fold size based on the dimensions of the chart legend  320 . For instance, where a panel includes data that exceeds a predetermined threshold, the offboard controller  124  may be configured to adjust the size of the panel to generate an adjusted panel  502  that is smaller than the original panel  402 . For purposes of simplicity,  FIG.  5    depicts only the panels  402 ,  502  of the chart  400 . It is noted that  FIG.  5    is provided merely for illustrative purposes and shall not be construed as limiting the scope of the present disclosure. 
     In a step  306 , the offboard controller  124  may be configured to assign a fold number (Fn y  below, Fn x  below) based on the F x  and F y  values. For instance, the first value (e.g., Fn y  below value) may represent the fold number down and the second value (e.g., Fn y  below value) may represent the fold number across. It is noted that the y-value is given first because it facilitates that left-to-right reading of the numbers and many charts do not have horizontal folds. 
     Referring to  FIG.  4   , the offboard controller  124  may be configured to place each graphical object of the received chart into one or more sections (SS) by comparing the X and Y coordinates to Section Begin and End coordinates (e.g., SB X/Y  and SE X/Y ). It is noted that objects may be placed in more than one section. The new coordinates of each object may then be determined. Given the fold number and the .svg X/Y position, the new X and Y positions follow. 
     Equations 1-4 are shown and described by: 
       When  Fnx= 0, New  X  coordinate= X   Equation 1
 
       When  Fnx!= 0, New  X  coordinate= X−FnxFx+B   Equation 2
 
       When  Fny= 0, New  Y  coordinate= Y   Equation 3
 
       When  Fnv!= 0, New  Y  coordinate= Y−FnyFy+B   Equation 4
 
     For example, the offboard controller  124  may be configured to assign the left panel in each row an X index of zero, increasing by one across the row, as illustrated by Equation 1 (e.g., Fnx). By way of another example, the offboard controller  124  may be configured to assign the top panel in each column a Y index of 0, increasing by one down each column, as illustrated by Equation 3 (e.g., Fny). It is noted that together, Fny and Fnx make up the labels/cell numbers shown in  FIG.  4    (e.g., 00,01, . . . 23). 
     It is noted that the offboard controller  124  may be configured to receive data with positions based on the entire chart. However, the original position (X) may need to have a new position calculated (using Equation 2) because the panels are displayed independently. For example, in one illustrative example, X may be 35, Fnx is 3, Fx is 10, and B is 1, such that the new calculated X coordinate is 6. In this example, the line might start at an X location about 35 inches from the left edge, or about half way across the fourth panel, such that the X of 35 inches would be at a position 5 inches into its panel if there was no buffer and it would be in the 4th panel over which is panel number 3 (e.g., Fnx=3) since they are zero based. Thus, with a 1 inch buffer the new coordinate would be 6. 
     In a step  210 , one or more buffer lengths may be determined. For example, the offboard controller  124  may be configured to determine one or more buffer lengths (B)  404 . For instance, as shown in  FIGS.  4 - 5 B , the offboard controller  124  may be configured to determine a buffer length  404  and add such buffer length  404  to each side of the display panel  402  to form a section  406 . For purposes of the present disclosure, the term “buffer length” and variants thereof may be defined as an amount added to the virtual fold so that there is some overlap between adjacent display panels. Further, for purposes of the present disclosure, the term “section” and variants thereof may be defined as the display panel (e.g., displayed image of the fold) plus the buffer. It is noted that the section is what the offboard controller  124  products and stores as a displayable entity. 
     It is noted that the buffer length  404  may be any buffer length. For example, the buffer length  404  may be 1.00 inches. 
     Referring to  FIG.  4   , a first display panel  402  (e.g., display panel 00) may include a first buffer length  404  added to a first side of the display panel (e.g., left side of the display panel 00), a second buffer length  404  added to a second side of the display panel (e.g., top side of the display panel 00), a third buffer length  404  added to a third side of the display panel (e.g., right side of the display panel 00), and a fourth buffer length  404  added to a fourth side of the display panel (e.g., bottom side of the display panel 00), where the first display panel  402  (e.g., display panel 00) and the four buffer lengths  404  may form a first section  406 . Continuing with this example, a second display panel  402  (e.g., display panel 01) may include a first buffer length  404  added to a first side of the display panel (e.g., left side of the display panel 01), a second buffer length  404  added to a second side of the display panel (e.g., top side of the display panel 01), a third buffer length  404  added to a third side of the display panel (e.g., right side of the display panel 01), and a fourth buffer length  404  added to a fourth side of the display panel (e.g., bottom side of the display panel 01), where the second display panel  402  (e.g., display panel 01) and the four buffer lengths  404  may form a second section  406 . In this regard, a buffer length  404  is added around the perimeter of the display panels  402  (e.g., display panel 00 and display panel 01), such that there is some overlap between the adjacent sections 00, 01, respectively. In particular, as shown in  FIG.  3   , a user viewing display panel 00 may pan through the right buffer of the first panel 00 and the left buffer of the second panel 01, such that any chart data on either side of the fold line may be easily viewed. 
     In an optional step  212 , one or more pre-processing chart image steps may be performed. For example, the offboard controller  124  may be configured to determine whether any part of the symbol (e.g., arrowhead, or the like) is in a section. If any part of the symbol is in a section then the offboard controller  124  may be configured to add a whole symbol. Further, the offboard controller  124  may be configured to apply a clipping region to restrict the symbol to a visual boundary. 
     By way of another example, the offboard controller  124  may be configured determine whether there is an embedded Clip Path for each group. If there is an embedded clip path then the offboard controller  124  may be configured to process the full related Path and convert to a set of clipped lines or a clipped shape. Further, the offboard controller  124  may be configured to process the full related path and convert the set of clipped lines (or clipped shape). 
     By way of another example, the offboard controller  124  may be configured to allocate the clipped lines or clipped shapes. 
     By way of another example, for each line Path, the offboard controller  124  may be configured to step through the Path, each line and arc command within the path comparing it to each set of section boundaries. If the start and end points of each line are within a section boundary, the offboard controller  124  may be configured to add the line command to the appropriate section(s). If the start and end points of each arc are within a section boundary, the offboard controller  124  may be configured add the arc to the appropriate section(s). If the radius and center of an arc would place part of it within a section boundary, the offboard controller  124  may be configured to add the arc to the appropriate section(s). It is noted that very long arcs can be broken at section boundaries if desired. If the start point of a line or the end point of a line is within a section boundary, but not both, the offboard controller  124  may be configured to clip the line at the section boundary (to remove very long lines from being drawn, if necessary). If the end point of a line or arc is outside a section, the offboard controller  124  may be configured to track the absolute coordinates in case the lines within the path re-enter the section. 
     By way of another example, for each fill Path, the offboard controller  124  may be configured to step through the Path. If the entire path is within a section, the offboard controller  124  may be configured to output the path. If the path enters or exits a section, the offboard controller  124  may be configured to mark the point on the section boundary. The offboard controller  124  may be configured to mark all entries and exits along a boundary. It is noted that these points are sorted and then connected with straight lines along the boundary to complete the shape within each section. Further, it is noted that sorting may be by y value when the break occurs along an x border and by x value when the break occurs along a y border. If the end point of a line or arc is outside a section, the offboard controller  124  may be configured to track the absolute coordinates to determine where the path re-enters the section. It is noted that the completed path may be unchanged or may be multiple paths separated across multiple sections. A method for fills may be generally discussed in concurrently filed U.S. patent application Ser. No. ______, filed on Nov. 12, 2021, entitled CONVERSION OF FILLED AREAS TO RUN LENGTH ENCODED VECTORS and having attorney docket number 131427US01, which is incorporated herein by reference in the entirety. 
     In a step  214 , a plurality of output files are generated based on the separated plurality of display panels  402 . For example, the offboard controller  124  may be configured to generate a plurality of output files including section data. For instance, the plurality of output files may be an SVG file. 
     In an optional step  216 , the generated output files may be provided to the aircraft controller  102  for display on the one or more display panels  112 . For example, the generated output files from the offboard controller  124  may be provided to the aircraft controller  102  via the communication interfaces  110 ,  134 . A system and method for display of the panels may be generally discussed in U.S. patent application Ser. No. ______, filed Nov. 12, 2021, entitled SYSTEM AND METHOD FOR ENHANCING SITUATIONAL AWARENESS VIA PANEL SELECTOR DISPLAY WHILE VIEWING MULTIPANEL AVIONICS CHARTS and having attorney docket number 131438US01, which is incorporated herein by reference in the entirety. 
     In an optional step  218 , prior to providing the plurality of output files to the on-board aircraft controller  102  (step  216 ), it is determined whether the chart data of the generated output files exceeds a predetermined threshold. If the chart data of the generated output file exceeds the predetermined threshold (as discussed previously herein), then the offboard controller  124  may be configured to break up at least a portion of the previously separated chart (using steps  208 - 216 ) such that the aircraft controller  102  may have ample storage to store/run the output file when displaying the chart. 
     For example, as shown in  FIG.  5   , the offboard controller  124  may be configured to break up the display panel 11 into two additional display panels  502 . In this regard, each display panel  502  may be stored individually as its own separate chart, rather than stored as a single display panel. 
     Although the disclosure has been described with reference to the embodiments illustrated in the attached drawing figures, equivalents may be employed and substitutions made herein without departing from the scope of the claims. Components illustrated and described herein are merely examples of a system/device and components that may be used to implement embodiments of the present disclosure and may be replaced with other devices and components without departing from the scope of the claims. Furthermore, any dimensions, degrees, and/or numerical ranges provided herein are to be understood as non-limiting examples unless otherwise specified in the claims.