KR20140057438A - Controller working position and display method for air traffic control - Google Patents

Abstract

Disclosed is a display system and a method for the air traffic control. The display system for the air traffic control includes: an air traffic situation display management unit for displaying a current air traffic situation including a track and a line of an aircraft on the basis of air traffic control data; and a flight data management unit for displaying the flight plan of the aircraft and a predicted route of the aircraft which is derived from the flight plan.

Description

TECHNICAL FIELD [0001] The present invention relates to a control system for an air traffic control system,

The following description relates to the present system for air traffic control, and more specifically, the present system for displaying the air traffic control data in the air traffic control system and providing convenience facilities for the control.

In order to prevent the smooth operation of airplanes and the prevention of air accidents, the civilian or military air traffic control system currently operates an air traffic control information processing system that processes and controls various air traffic control data. The air traffic control system provides the controller with identification and display of aircraft, presentation and distribution of flight plan data, flight safety warnings, and handling controller requirements.

Such an air traffic control system prevents the collision between the aircraft and the obstacle between the aircraft in advance and maintains the safety of the air traffic by managing the flight status of the aircraft and improves the efficiency of the air traffic operation.

Research on the development of a next-generation integrated air traffic control system is continuously required to secure the design technology of the integrated control system for air traffic control, to secure the safety of the air traffic through the development and standardization of the pilot operation system, and to improve the efficiency.

The CWP (controller working position) is a kind of human machine interface (HMI) that provides controllers with the ability to display and manage the necessary control data for air traffic control. In order to be a more efficient display system, access functions of the present system should be designed in a concise manner considering the convenience of the controller, and the inputs, requirements, control data and risk alarms should be logically presented to the controller. In addition, it is necessary to minimize the possibility of errors in processing and to be able to process data reliably. Continuous technological development is required to solve the above requirements.

According to an embodiment of the present invention, there is provided an air traffic control system for an air traffic control system, comprising: an air traffic situation management unit for presenting an aviation state including an aerial and a route of an aircraft based on air traffic control data; And a flight data management unit for displaying the flight plan of the aircraft and the predicted course of the aircraft derived from the flight plan.

The present system for air traffic control according to an embodiment may further include a system management unit for managing resources of an application and a system based on a control signal, and displaying state data of other subsystems.

The method for presenting an air traffic control according to an embodiment includes the steps of: displaying a current air condition including a flight and a route of an aircraft based on air traffic control data; And displaying the flight plan of the aircraft and the predicted course of the aircraft derived from the flight plan.

In the method for presenting an air traffic control according to an embodiment, the step of presenting the current air condition can include the step of synthesizing or overlaying weather data synchronized with the current air condition to the current air condition .

In the method of presenting an aviation control according to an embodiment, the step of presenting the current aviation situation may comprise the step of displaying APM data on an airport runway in a vertical or horizontal view.

Wherein the step of presenting the approach path monitoring (APM) data in a vertical view or in a horizontal view comprises, in the vertical view, Generating an approach path monitoring alert if the access path monitoring alert is located; And generating an approach path monitoring alert when the aircraft is located outside the range defined in the horizontal view based on the landing point and the runway axis of the aircraft.

BRIEF DESCRIPTION OF THE DRAWINGS Fig. 1 is a diagram showing an overall configuration of an air traffic control display system according to an embodiment.
FIG. 2 is a diagram illustrating a detailed configuration of a general display management unit according to an embodiment.
FIG. 3 is a view showing the detailed configuration of the aviation situation display management unit according to an embodiment.
FIG. 4 is a diagram illustrating a detailed configuration of a flight data management unit according to an embodiment.
5 is a detailed block diagram of a data input / output management unit according to an embodiment of the present invention.
FIG. 6 is a diagram illustrating a detailed configuration of a system management unit according to an embodiment.
7 is a view for explaining the operation of the data log management unit according to an embodiment.
8 is a flow chart illustrating an aviation control method for an air traffic control according to an embodiment.

Hereinafter, embodiments will be described in detail with reference to the accompanying drawings. The specific structural or functional descriptions below are merely illustrative for purposes of illustrating embodiments of the invention and are not to be construed as limiting the scope of the invention to the embodiments described in the text. The method of presenting an air traffic control according to an embodiment can be performed by an air traffic control system, and the same reference numerals shown in the drawings denote the same members.

BRIEF DESCRIPTION OF THE DRAWINGS Fig. 1 is a diagram showing an overall configuration of an air traffic control display system according to an embodiment.

1, the air navigation control system 100 includes an air condition display unit 110, a general appearance management unit 120, a flight data management unit 130, a system management unit 140, a data input / output management unit 150, And a data log management unit 160.

The CWP (controller working position) 100 is a system for presenting air traffic control data to controllers or providing convenience functions to controllers for air traffic control.

The present system 100 can display all the information for indicating an air condition such as a wake or an air route of an aircraft and can display a graphical user interface (GUI) for displaying inputs, requirements, air traffic data, alarms and warnings to the controller, graphical user interface (GUI) based windows. In addition, the present system 100 can exchange flight information with people related to the air traffic control service, support the operations of the approach control station and the air traffic control station, and provide the output information related to the flight information and the alarm. In addition, the present system 100 can store and reproduce all the air traffic control data in preparation for the system suspension due to an emergency situation, can support the manual control mode in case of failure of the other subsystems, Can be managed. Finally, the present system 100 can support next generation air traffic control functions such as controller-pilot data link communications (CPDLC) and automatic dependent surveillance-broadcast (ADS-B).

The aviation situation indication management unit 110 can display the current aviation situation. The aviation situation indication management unit 110 can display aircraft, weather data and the like and can perform functions such as filtering function, warning and alarm function, coupling function, manual mode function, holding, control transfer and recording data reproduction have.

Specifically, the aviation state occurrence management unit 110 can display the current aviation state including the wake and the air route of the aircraft based on the air traffic control data. Air traffic data may include radar data sensed by various radars, flight data including flight plans, next generation surveillance sensor data, weather data related to weather observation, and the like. The next generation surveillance sensor data may include PSR (Primary Surveillance Radar) sensing data, SSR (Second Surveillance Radar) mode-S sensing data, ADS-B (Automatic Dependent Surveillance-Broadcast) sensing data, and MALT .

The aviation situation creation management unit 110 analyzes the aviation control data as described above, and can display a route representing the trail of the aircraft and a route indicating the merit of passing by the aircraft.

The aviation state occurrence management unit 110 may synthesize or overlay the weather data synchronized with the current aviation state to the current aviation state. When the controller selects the display of the weather data, the aviation condition display management unit 110 can simultaneously display the air condition and the weather condition based on weather data such as weather radar measurement data, satellite weather data, or cloud image data. The weather data can be updated according to the setting.

In addition, the air condition-presenting management unit 110 may display the information about the wake-up of the aircraft as a data block and display the wake-up status according to the wakeup of the aircraft.

Then, the aviation situation indication management unit 110 can display APM (approach path monitoring) data on an airport runway in a vertical view or a horizontal view. For example, if the controller selects a runway for use at a jurisdiction airport, the aviation status indication manager 110 may present access path monitoring data for the runway. In the vertical view, when the aircraft is positioned below an axis defined on the basis of the landing point and the glide angle of the aircraft, the air condition-occurrence management unit 110 can generate an approach path monitoring warning, and in the horizontal view, If an aircraft is located outside the defined range based on the axis, an approach path monitoring alert can be generated.

The general display management unit 120 can configure a main frame for the display of an actual screen. The general appearance management unit 120 can manage windows, graphic tools, measurement tools, maps, screens, log-in / out, and perform functions such as time functions, snapshot and supervisory management.

The flight data management unit 130 can manage and display the flight plan and ICAO telegram of the aircraft. The flight data management unit 130 may include flight data strip function, flight plan and professional management functions, passive flight data function, predictive route display, aircraft departure / arrival management, air traffic flow management, data communication, Function can be performed.

Specifically, the flight data management unit 130 displays the predicted route of the aircraft as a 4D (dimension) orbit including latitude, longitude, altitude, and time, and can display the predicted route according to a predefined time. The flight data management unit 130 can display the predicted route based on the time designated by the controller. If the controller selects each aircraft and selects the predicted route time, the flight data management unit 130 may display the predicted route of the selected aircraft on the screen. The forecast route can be displayed as a line on the control screen and can be updated.

In addition, the flight data management unit 130 may store the performance data of the aircraft including performance based navigation (PBN), area navigation (RNAV), and reduced vertical separation minimum (RVSM) It can be displayed together with the flight plan of the aircraft. For example, if the controller selects a wake, the flight data manager 130 may display the aircraft performance data in a data block, a flight plan window, or a strip.

The system management unit 140 manages resources of an application and a system based on a control signal and manages resources such as a surveillance data processor (SDP) 170 and a flight data processor (FDP) Status data of other subsystems can be displayed.

The data input / output management unit 150 provides communication with external functions and can process external input and output. Specifically, the data input / output management unit 150 includes a flight data processing system 175, a monitoring data processing system (SDP) 170, a data recording system (DRS) 165, a monitoring control system (SMC) monitor and control 185, software management system 180, simulation system 190, and surveillance data emergency bypass system 195, as shown in FIG. .

The surveillance data processing system 170 can receive, filter, calibrate, convert and track the data sensed by the surveillance sensor, and can perform a safety alarm function for the surveillance. The flight data processing system 175 may process the reception, maintenance, processing, distribution, and modification of the flight data. The recording / playback system 165 can store and provide the control data, the control screen, and the statistical data. The software maintenance system 180 can manage the parameters of the entire system and manage the version of the software used. The supervisory control system 185 may monitor and control the network and the hardware and software status of each system. The surveillance data emergency bypass system 195 can receive radar data directly in the event of a functional problem of the surveillance data processing system 170. The simulation system 190 may provide training or training data for the controller to the airborne control system 100.

The data log management unit 160 can manage the data log, specifically, can record the data log of all the functions, and can transmit the error log and the related data log to the recording and reproducing system 165 when an error occurs

FIG. 2 is a diagram illustrating a detailed configuration of a general display management unit according to an embodiment.

2, the general display management unit 200 includes a window management unit 205, a time management unit 210, a timer alarm unit 215, a graphic tool management unit 220, a map management unit 225, a general screen management unit 230 A log management unit 235, an operation mode information output unit 240, an administrator management unit 245, a console setting unit 250, an electronic message providing unit 255, a latitude and longitude output unit 260, 265, a distance orientation measurement unit 270, and a snapshot generation unit 275. [

The window management unit 205 can provide different windows according to respective functions on the control screen. A window may include an indication window, a function window, a notification window, and an error window. The currently displayed window is a window that is always displayed on the screen, and it is impossible to move, resize, or close the window, and the main screen and the lower information panel may correspond. The function window is a window displayed by a request and an instruction, and may include a general function window and a special function window.

General function windows can be moved and closed, and can include all windows related to the function. It is impossible to change the size of the general function window, but it is possible to change the size of the window in which the list is displayed. The special function window can not be moved, resized and closed, and may include sub-screens (SN-2, SN-3) and a strip window. The notification window may include a timer notification window, a list warning message window, and a global map storage confirmation window, which are displayed as windows for notifying and confirming a specific status. Notice windows can be moved and closed, but they can not be resized. The error window includes a list error message window, an error message window for adding a flight plan (FPL), and an error message window for adding a repetitive flight plan (RPL) to the window displayed when an operator has an operational error. . Error windows can be moved and closed, but not resizable. In the case of the function window displayed by the operator's request or command, the window can be browsed by using the keyboard shortcut key. In addition, in order to prevent all the windows from covering the control screen, the general screen manager 230 can adjust the initial position of the window.

The time management unit 210 may receive the system time from the time reference system (TRS) and display the current time (UTC). Time information is always displayed in the lower information panel and can not be changed by the operator. The time consists of "hour: minute: second" and can be used for all functions that use time. In particular, the time management unit 210 may transmit a current time to the timer alarm unit 215 to provide a timer function.

The timer alarm unit 215 can provide a timer function to the control station. The timer can be set for each control and alarm is provided at the set time. The set time is configured as "hour: minute: second", and when the system time (current time) received from the time management unit 210 is reached, an alarm can be displayed through the notification window. The timer function may include a countdown setting in which a notification window is displayed after a preset time from the current time, and an alarm function in which a notification window is displayed when the current time matches the set time.

The graphic tool management unit 220 can create and manage graphic objects on the control screen by using graphic tools. The controller can use the graphic tool management unit 220 to generate a user map. Graphic objects that the graphical tool management unit 220 can generate include text, lines, polylines, polygons, squares, rectangles, circles, and arcs. A graphic object can be created by selecting a line color, a face tile, or a face color. The color can be composed of red, blue, yellow, green, black, white, gray, dark red, dark blue, have. The color of the generated graphic object can be changed, and the graphic object can be automatically generated by inputting the latitude and longitude coordinates after selecting the graphic type. The management functions of the generated graphic objects include moving to a desired position, deleting the corresponding graphic object, deleting all the graphic objects created on the control screen, restoring and selecting the graphic object in the order of recently deleted, moving, deleting, .

The map management unit 225 can select a map designated by the controller and display it on the control screen. The map may include a system map, a user map (global map, local map), an xml map, and a weather map. The map management unit 225 can manage the map for each controller ID received from the login management unit 235, and can receive the system map from the SMS input unit. In addition, the map manager 225 can create a user map through the graphical tool manager 220, and the global map can be managed in the administrator manager 245. The map management unit 225 can receive the xml map and the weather map from the SDP input unit.

The system map type is Coast, FIR, KADIZ, SECTOR, TCA, RA, DA, PA, AA, MOA, MSAW, CATA, AIRPORT, RUNWAY, FIX, T_FIX, VORTAC, VORDME, NDB, ROUTE, HOLD, SID, STAR , APCH, and CVFR, respectively, which can be either present or absent. The system map can display or hide the corresponding layer by ID, show / hide the map name (label) stored in the system map, and change and save the system map color for each controller. The user map is a map that the controller can generate using the graphic tool management unit 220. The user map can be divided into a global map, which is generated by a supervisor, and a local map, which is a map generated and managed by each controller. The xml map represents the MSAW, APW, QNH, STCA, and blanking area maps received from the SDP into the xml file. The map manager 225 can display or not display each xml map. The map manager 225 can receive the weather map from the SDP to ASTERIX Cat.008 (ASTERIX Cat. 008 Monoradar Weather Data). The weather map is shown in the form of a polygon, and the map manager 225 maps the weather map High, Medium, and Low, respectively. For example, 0, 1, 2 can be classified as Low, 3, 4, 5 as Medium, 6, 7 as High.

The general screen management unit 230 can change the text font or color of the lower information panel and the data block and can adjust the initial position of the window. The general screen management unit 230 may provide a text font size change function, a text color change function, and a window initial position adjustment function. In the text font size change function, the font size is changed according to the font of the text, and the fonts are the default FontSmall and FONT_1 and FnLabel. In the text color change function, the color of the text changes to the selected color, and the colors are black, red, and blue, which are the default colors. You can adjust the initial position of all windows by adjusting the initial position of the window. After activating the window to adjust the position, place it at the desired position on the control screen and save it, Can be displayed. The general screen management unit 230 can manage the IDs of the controllers, and the functions set based on the setting of each controller can be displayed. The general screen management unit 230 can transmit the changed text to the data block management unit and can transmit the initial position value of the window to the window management unit 205. [

The log-in management unit 235 provides log-on and log-off functions when the controller inputs a unique ID. When the log-in management unit 235 logs in with the registered ID, the ID can be displayed on the lower information panel, and the log-on time and the connection time until log-off can be recorded. The login management unit 235 can load the map information, the general screen information, and the strip information according to the ID of the controller, receives the latest user list from the administrator management unit 245, and transmits the login information to the operation mode information output unit 240 ). The login management unit 235 can display an alert window when logging in with a non-registered ID or when logging in with an already logged-in ID. When the controller logs in, the console setting unit 250 sets the console setting, such as supervisor function, flight data operator (FDO) function, RPL function, FLOW function, and the like A unique function can be activated.

The operation mode information output unit 240 may display general information on the lower information panel according to the data of interest and the control system. The operation mode information output unit 240 may provide an operator mode display function, an assignment sector information display function, a login status display function, and an SSR code filtering setting function. Operator mode In the display function, "OPS" when a sector is assigned, "SUP" when a supervisor, "FREE" when a sector is not allocated, "REP" In this case, "MONO" is displayed. In the assignment sector information display function, the allocated sector information is displayed, and the sector information can be received from the console setting unit 250. [ The login status display function confirms the information on the login status (controller ID), and the controller information can be received from the login management unit 235. The SSR code filtering setting function sets the Min and Max values of SSR code filtering, and the setting value can be applied even if two digits are input.

The administrator management unit 245 can provide a unique management function of the supervisor. Specifically, the administrator management unit 245 uses a global map management function, a sector management function, a minimum safe altitude warning (MSAW) function, a proximity warning (APW) management function, a safety alert Setting management function, manual altimeter setting value (QNH) management function, user information update function, user information distribution function, upper layer wind height management function and automatic control management function.

In connection with the global map management function, the global map is created in the graphic tool management unit 220, and may be transmitted to the CWP output unit (FIG. 5) and provided to all the consoles. The maximum number of cluster maps is 10, and each can be distributed.

The sector management function indicates a function of changing a sector of a console to be reassigned. When the sector information is received through the console setting set by the console setting unit 250 and the reassigned sector information is transmitted to the console setting unit 250, the sector information is changed to the lower information panel of the corresponding console. The administrator management unit 245 may transmit the reassigned sector change message to the FDP output unit (FIG. 5), receive the result from the FDP input unit (FIG. 5), monitor other sectors through a shadow have.

The MASW and APW management functions are functions for activating or scheduling MASW and APW layer by layer and adding, modifying and deleting APW. The administrator management unit 245 may transmit a change request of the MASW and APW to the SDP output unit (FIG. 5) and receive the result from the SDP input unit (FIG. 5). The modified MASW and APM may be displayed on all consoles. The manager management unit 245 may receive the NOTAM (notice to air man) information from the NOTAM management unit (FIG. 4) and add the NOTAM map to the APW layer have.

Using the safety alarm The configuration management function indicates the function of activating or deactivating the MSAW, APM, short-term conflict alert (STCA), and APW. The administrator management unit 245 can transmit to the SDP output unit whether the safety alarm is active or inactive and receive the result from the SDP input unit. Depending on whether it is active or inactive, MSAW, APM, STCA and APW can be displayed on all consoles.

Manual altimeter setpoint (QNH) management function indicates changing the QNH value of the corresponding point. After receiving the QNH value from the FDP input unit, the modified QNH value can be transmitted to the FDP output unit and the result can be received from the FDP input unit. The QNH value of the changed point can be displayed on all consoles.

The user information update function is performed upon execution of the user information update command, and receives the latest user list from the SMC input unit (FIG. 5). The user information distribution function indicates that the received latest user list is provided to the login management unit 235.

The upper-layer wind elevation management function is a function for inputting and managing the upper-layer wind elevation. It receives the upper wind height value from the FDP input unit and then transmits the corrected upper wind level elevation value to the FDP output unit and receives the result from the FDP input unit.

The automatic control management function indicates that automatic control transfer permission or denial message is transmitted to the FDP output unit at the same time as the system starts. The manager management unit 245 may process the request message in the flight data processing system and send the confirmation message to the FDP input unit. In the automatic control transfer mode, the aircraft is automatically transferred or transferred to the aircraft, otherwise the procedure of the manual control transfer function is followed.

The console setting unit 250 can set the role of the console by console setting. Console configuration consists of xml file. Console configuration that is managed includes Console.xml which is status information of each console, roles.xml which defines the role of role, and sectors.xml where information of sector is defined. In the case of the sector, the NO, NW, SO, SW, EA, HC, LC, and JE in the case of the sector, NO, WE , EA, LC, HC, and SO. The console setting unit 250 receives the changed sector information from the administrator management unit 245, and transmits the changed sector information to the administrator management unit 245 after applying it to the console setting. The console setting unit 250 can transmit the set role information of the set console to the login management and provide the set information of the console setting to the other units.

The electronic message provision unit 255 may provide an electronic message (E-message) between the internal operator (SMC or CWP). When the message is input to the message window, the electronic message providing unit 255 can transmit the message to the internal operator and display the received message on the control screen. The electronic message providing unit 255 receives a message from the SMC input unit, transmits a message to the SMC output unit, receives a message from the CWP input unit with another CWP, and transmits the message to the CWP output unit.

The latitude and longitude output unit 260 can display the latitude and longitude on the control screen. The latitude and longitude output unit 260 can display latitude and longitude values corresponding to the mouse cursor position on the control screen on the lower information panel, and latitude and longitude can be displayed as "degrees: minutes: seconds". The latitude and longitude output unit 260 may display a grid of latitude and longitude on the control screen, and the fineness of the grid may vary depending on the zoom in or zoom out of the control screen , The grid can be displayed or not displayed in accordance with the selection. The latitude and longitude output unit 260 can display the position of the coordinate where the latitude and longitude values are input on the control screen by using the symbol "*", and the coordinates can be displayed up to 100, Lt; / RTI >

The current screen management unit 265 provides a current screen management function for control purposes. The current screen management unit 265 can zoom in or zoom out the control screen based on the operation of the mouse wheel and can provide a compass function. The compass function can be provided via a large circle with angles displayed in units of 15 degrees, and can be displayed or not displayed at any time. The current screen management unit 265 can display the control screen based on true north or magnetic north and has a difference of 8 degrees between the true north and the magnetic north and can set the magnetic north as a default value have. In addition, the current screen management unit 265 can display a range ring on the control screen. The range circle may have a set value with a radial distance (NM) of 1, 2, 5, 10, 20, 30, 50 and the numbers 10, 20, 30, 40, 50, If a mono radar plot is selected, the center of the range circle can be automatically updated to the center of the radar site.

When the measurement tool is selected, the distance-bearing-degree measurement unit 270 can measure the distance between the two points and the bearing degree. There are static points and dynamic points (aircraft) in the two kinds of points, so there may be three cases as follows. First, when a static point and a static point are selected, the distance bearing degree measurement unit 270 measures the distance between two points and the bearing degree. Secondly, when a static point and a dynamic point are selected, the measuring unit 270 measures the distance, azimuth and velocity between two points, and when the dynamic point and the dynamic point are selected, Measure the degree and altitude difference. The unit of measurement distance is NM and can be measured up to the second decimal place. The range of the bearing is 0 ~ 359 (degrees). The unit of the measurement speed is min (min) and can be measured up to the second decimal point. The unit of altitude difference is FL and the absolute value difference can be measured. In the case of a dynamic point, the measured value can be updated depending on the position. Up to 5 measurement tools can be displayed simultaneously, each of which can be selectively released.

The snapshot generation unit 275 can periodically generate a snapshot of the display screen. The snapshot generation unit 275 can generate a snapshot according to the set period and output the stored snapshot.

FIG. 3 is a view showing the detailed configuration of the aviation situation display management unit according to an embodiment.

3, the aviation condition occurrence management unit 300 includes a weather data output unit 305, a control mode management unit 310, a flight configuration management unit 315, a flight status output unit 317, a call filtering unit 320, An APM information output unit 325, a FPASD output unit 330, an FDP alarm management unit 335, a holding function management unit 340, a control data playback unit 345, an ASDE information output unit 350, a data block management unit And the navigation control unit 385. The SDP alarm management unit 360 includes an SDP alarm management unit 360, an SPI output unit 365, a wake up condition alarm management unit 370, a manual control right acquisition management unit 375, a manual control right acquisition management unit 380, A plan providing unit 390 and a SID / STAR management unit 395.

The track configuration manager 315 can receive the wake from the SDP input, and the display of each data block and wake follows international standards and facilitates operator identification. The track configuration manager 315 may provide management functions regarding the symbols, Halo, the leader line, the vector line, and the trace component of the trace history. Symbols can be changed by the controller. The track configuration management unit 315 can display Halo of each wakeup or all wakeups, and can adjust the set value of Halo from 0 to 10 in one unit. A leader line represents a line connecting a data block and a trace. The track configuration manager 315 can adjust the thickness of the leader line to 0, 1, 2, and 3 (0 indicates no-show), adjust the position to 9 basic directions, You can adjust the data block to the desired position. In addition, the trace configuration managing unit 315 can adjust the vector lengths to 1MIN, 2MIN, 3MIN, 1NM, 2NM, and 3NM. The history configuration management unit 315 can display the history history, and can change the number of history history to 2, 4, 6, 8, and 10.

The data block management unit 355 can display in the data block the information about the miniplan received from the FDP input unit and the trace of the aircraft received from the SDP input unit. The data block manager 355 may provide a highlight of the data block to identify the selected snapshot and provide a control popup window (SSR?) To allow a control command on the selected snapshot.

The data block management unit 355 can set the information of the data block in the normal mode or the extended mode to display the snapshot information and the set value. In addition, the data block management unit 355 can automatically or manually select a user to offset the data blocks of the overlapping traces. The data block management unit 355 receives the text setting value from the general screen management unit, receives the FDP alarm from the FDP alarm management unit 335, and receives and displays SDP alarm and alarm information from the SDP alarm management unit 360 .

The data block management unit 355 receives the alarm information from the SPI output unit 365 and receives the emergency emergency condition code information from the alarm emergency condition alarm management unit 370. The data block management unit 355 acquires the manual control right from the manual control right acquisition management unit 375 And release information. The data block management unit 355 receives manual control transference information from the manual control right management unit 380 and receives manual coupling / decoupling information from the flight plan providing unit 390, Label labeling information from the label management unit 385. [

The data block management unit 355 receives the SSR code allocation information from the SSR code management unit, receives the permission flight altitude or cleared flight level (CFL) information from the CFL management unit, And receive flight plan air status display (FPASD) information. The data block management unit 355 receives the aircraft performance information from the aircraft performance output unit, receives the automatic control transfer information from the automatic control right management unit (not shown), receives MTCD from the MTCD output unit, detection information from the control mode management unit 310. [

The wake state output unit 317 can display the state of the wake according to the type of wake received from the SDP input unit. The trajectory state output unit 317 can display only the selected trajectory. The trajectory state output unit 317 can display only the selected trajectory. The wake state output unit 317 can set priorities of wakes, and the basic priority is Plot < ADS-B < System Track order. In addition, the wake state output unit 317 can confirm the priorities of the wake-ups, and display the wake ups on the uppermost screen as the numbers are assigned higher. The wake state output unit 317 can distinguish symbols and colors so that the wake state can be identified and identified. For example, the wakeup status output unit 317 may be configured such that the controlled track is light green, the limited track is dark green, and the partial track is the other track It can be displayed in dark gray, and the ADS-B wake can be displayed in dark white.

The trajectory filtering unit 320 may filter the trajectory based on the trajectory received from the SDP input unit, the miniplan received from the FDP input unit, or the setting value to display a required trajectory among the trajectories within the present range. The types of filtering performed by the trajectory filtering unit 320 include Plot generated by each radar site (Plot only when the radar mode is changed to Plot), Plot state (PSR / SSR / Combination), Correlated / Uncorrelated Track, VFR (1200), Altitude (Filter by setting the altitude value, setting the altitude to filter the altitude below the altitude, If it is set, the wake above the corresponding altitude is filtered), and there is an area (sector). The wake-up filtering unit 320 may display all the wake-ups by using the Quick All function.

The SDP alarm management unit 360 can display the SDP warning and alarm conditions received from the SDP input unit in a visual and audible manner so that the controller can recognize the SDP warning and alarm condition. The SDP alert management unit 360 can receive sector information from the console setting unit and can inform the operator of the warning through the visual effect when the warning that the warning and the warning are generated are hidden in the window. The warning and alarm are displayed in the warning window and transmitted to the data block management unit 355. If the operator recognizes (ecks), the auditory notification is removed. In addition, the warning and alarm may be changed in color when the operator performs a cognitive operation, and the warning and alarm may be color-coded. The warning and alarm may optionally include only warning / alert , It should always be displayed in the data block, and the beep and warning window will occur only in the corresponding sector. The Warning / Alert message window is displayed for each safety function, Warning / Alert is turned on / off for each wake, and the alarm information includes the occurrence time. SDP alerts and alerts can include MSAW, APM, APW, STCA. The warning of MSAW Warning status is displayed in yellow warning message, the data block is highlighted, and the highlight of data block disappears when the operator confirms that the MSAW Warning occurred. Trace information generated by the MSAW is displayed in the alert list, and an audible signal may be generated in the MSAW Alerting state. The warning of the MSAW Alerting state is displayed in a red warning message in the data block, the data block is highlighted, and the highlight and audible signals of the data block disappear when the operator confirms the MSAW Alerting state trace. Can transmit the APM information to the APM information output unit 325 and can display the navigation information generated by the APM in the warning list and generate the auditory signal in the APM Alerting state. The APM Alerting state trace is displayed as a red warning message in the data block, the data block is highlighted, and the highlight and audible signals of the data block disappear when the operator confirms the wake of the APM Alerting state.

The SDP alarm management unit 360 can transmit the APW information to the NOTAM management unit, display the navigation information in which the APW has occurred, and generate the audible signal in the APW Alerting state. The APW Warning status is displayed as a yellow warning message, the data block is highlighted, and the highlight of the data block disappears when the operator acknowledges the wake of the APW Warning status. The wake of the APW Alerting state is indicated by a red warning message in the data block, the data block is highlighted, and the highlight and audible signals of the data block disappear when the operator confirms the wake of the APW Alerting state. When accessing a hazardous area, the warning information may include the name of the alert area. The STCA warning status is displayed as a yellow warning message, the data block is highlighted, and the highlight of the data block disappears when the operator confirms that the STCA Warning has occurred. The STCA Alerting state trace is displayed as a red warning message in the data block, the data block is highlighted, and an audible signal may be generated in the STCA Alerting state. When the operator identifies the wake of the STCA Alerting state, the highlight and audible signals of the data block disappear. The SDP alarm management unit 360 can display the navigation information in which STCA has occurred as a warning list.

When an FDP alarm condition received from the FDP input unit occurs, the FDP alarm management unit 335 can display it in a visual and audible manner so that the controller can identify the FDP alarm condition. The FDP alarm management unit 335 displays an alarm in an alarm window and can send an alarm to the data block management unit 355. When the operator recognizes the alarm, the audible notification is removed and the hourly notification is changed. The FDP alarm management unit 335 receives setting information from the console setting unit, and a warning / alert is generated only in the corresponding control sector. The Warning / Alert message window is displayed for each safety function, and Warning / Alert is turned on / off for each wake. The alarm may be classified into a color, the alarm information includes the occurrence time, and the FDP alarm management unit 335 can notify the operator through the visual effect when the alarm in which the alarm occurs is hidden in the window. The FDP alarm received from the FDP input unit may include RAM (route adherence monitoring), clearance level adherence monitoring (CLAM), missed position report (MPR), and estimated time over significant point (ETO).

The SPI output unit 365 can visually indicate the SPI (special position identification) when the special position identification (SPI) occurs, so that the controller can recognize the special position identification. The SPI represents, for example, the ability of the pilot to report its position when the controller requests it. The SPI output unit 365 can display the SPI in the alert window, send the SPI to the data block management unit 355, and receive the sector information from the console setting unit. If the operator recognizes the occurrence of an SPI, the audible notification is removed and the visual notification changed. The SPI can be color-coded, and a Warning / alert message window can be displayed for each safety function, and Warning / alert is turned on / off for each wake. The path information may include an occurrence time, and the SPI output unit 365 may display the SPI through blinking and color change. If the warning is generated and the window where the alarm occurs, the visual effect To inform the operator of the relevant information.

The wake-up emergency condition alarm management unit 370 can display the wake-up emergency condition code in a visual and audible manner so that the controller can recognize the wake-up emergency condition code. The warfare emergency condition alarm management unit 370 can receive sector information from the console setting unit and can send an alarm to the data block management unit 355. [ Trace information where an emergency condition code occurred can be displayed in the warning list. EMERGENCY EMERGENCY CONDITIONS EMERGENCY EMERGENCY CONDITION CODE ALARMS MANAGED BY ALARM MANAGEMENT 370 (1) EM: SSR code -> 7700, (2) RF: SSR code -> 7600, (3) HJ: SSR code -> 7500 have. In the EM, RF or HJ state, a red warning message appears on the data block, the data block is highlighted, and an audible signal is generated. Also, the highlight and audible signals of the data block disappear by the operator's confirmation operation.

The manual control right acquisition control unit 375 can provide the manual control right acquisition function and the release function. Trails without control are displayed in dark gray, and control orders are executed through Assumes. The wake-up log is displayed in bright green, and the command to release the control right is executed through Release. The manual control right acquisition management unit 375 transmits a control command to the FDP through the FDP output unit, receives the control right acquired normally from the FDP from the FDP input unit, and transmits the result to the data block management unit 355. The wake-up log is normally a Controlled Track and is displayed in bright green. In addition, the manual control right acquisition control unit 375 transmits the control right release command to the FDP through the FDP output unit, receives the control point from the FDP input unit that has been normally released from the control right, and transmits the result to the data block management unit 355 . A wake in which control is normally released becomes a Limited Track, and is displayed in dark gray. The manual control right acquisition management unit 375 can receive the sector information from the console setting unit.

The manual control right acquisition management unit 380 can provide the function of acquiring the manual control right and the transfer function. The handover command is executed using Initiate, and the manual control right argument management unit 380 can receive the sector information from the console setting unit. The manual control right acquisition management unit 380 transmits the control right command to the FDP output unit through the FDP output unit, receives the execution result through the FDP input unit, and transmits the result to the data block management unit 355. When the control transfer command is executed on the control transfer side, the transfer request message is transmitted from the FDP to the control acceptance side, and the control acceptance request window can be confirmed on the control acceptance side. In the case of rejection of transfer from the control acceptance side, it can be confirmed through a message from the control transfer side. The sectors to be transferred to the control can be selected with a mouse click. If you do not assemble for a certain period of time defined by the control acceptance side after the control transfer, the control transfer is canceled automatically. In case of control transfer, the control transfer order can be canceled or changed.

The holding function managing unit 340 provides an aircraft holding setting and holding releasing function, and can receive the miniplan from the FDP input unit. The holding function management unit 340 may transmit the holding setting request and the holding release request to the FDP through the FDP output unit and receive the execution result from the FDP input. A hold command can be executed on a data block of a trace (green) having a control point during a correlation track. When hold information is input to the hold window, information can be transferred to the FDP to be stored and updated, The hold status is displayed. The holding function management unit 340 may perform an end-hold command to the hold state to release the hold, and the initial information of holding can be automatically inputted and corrected.

The ASDE information output unit 350 can display an airport surface detection equipment (ASDE) in a separate window on the control screen. The ASDE information output unit 350 can provide clear and accurate traffic information for all aircraft and vehicles covered by the ground surveillance radar.

The control mode management unit 310 automatically switches the control mode to By-Pass when all the nodes of the SDP are degraded or down, and monitors the air condition using monoradar tracking data It can be continuously displayed. The control mode management unit 310 can use the subsystem status information received from the SMC input unit to check the node status of the SDP. When the controller switches to the By-Pass mode, the control mode management unit 310 can continuously display the air condition using the mono radar tracking data. The control mode management unit 310 receives an ASTERIX Cat. 034 Monoradar Service Messages, ASTERIX Cat. 048 Monoradar Target Reports, ASTERIX Cat. 062 Track Data, ASTERIX Cat. 062 (1062/380 Flight plan related data: Mini plan). When the function of the control mode management unit 310 is activated, the function of the SDP alarm management unit 360 can not be used. If any one of the FDP nodes is active, all functions of the flight data management unit can be used.

The APM information output unit 325 can receive the wake from the SDP input unit and can display the APM information of each airport runway in a vertical view or a horizontal view. The APM information output 325 generates an APM alert in the vertical view if the aircraft is located below an axis defined by considering the system parameters of the angle at the landing point and glide angle (3 degrees) of the aircraft. The APM information output 325 is used to determine, in a horizontal view, the aircraft is located outside the form defined by adding the width of the strip at a radial distance above a side angle (150 degrees) corresponding to the landing point of the aircraft and each side of the runway axis Occurs when an APM warning occurs.

The FPASD output unit 330 can display the aviation status using the FPASD received from the FDP input unit when all nodes of SDP and EBP are in the degraded or down state. When the function of the FPASD output unit 330 is activated, all functions of the flight data management unit can be used. However, the flight status output unit 317, the SDP alarm management unit 360, the SID / STAR management unit 395, The alarm management unit 370, the weather data output unit 305, and the control mode management unit 310 can not be used.

The SID / STAR management unit 395 can set and display a standard instrument departure procedure (SID) and a standard terminal arrival route (STAR) of a jurisdiction aircraft. SID and STAR exist for each runway, and the route of the aircraft can be changed according to the set SID and STAR. The SID / STAR management unit 395 transmits the set SID and STAR to the FDP output unit based on the runway information received from the runway direction management unit, and can receive the execution result from the FDP input unit.

The weather data output unit 305 can display the received weather data superimposed on the control screen. The weather data output unit 305 can display or not display the weather data, and the weather data can be updated according to the setting.

The flight plan supply unit 390 can add the flight plan received from the FDP input unit to the wake-up plan without the flight plan, add or delete the flight plan to the FDP output unit, receive the execution result from the FDP input unit To the data block management unit 355. The flight plan supply unit 390 may provide a manual coupling function between the flight plan and the wake. Specifically, the flight plan supply unit 390 adds a flight plan, and inputs the SSR code of the wake-up request. The flight plan providing unit 390 can provide a manual decoupling function between wakes and receive sector information from the console setting unit.

The navigation label manager 385 may generate a radar tag. Specifically, the navigation label management unit 385 can execute a navigation label creation command by using a start command for an uncorrelated unstatement, transmits the generated flight plan to the FDP through the FDP output unit, The result of the execution can be received from the FDP input unit and transmitted to the memory block management unit. As a result, the worms normally processed in the FDP are displayed in bright green.

The navigation label manager 385 can delete the navigation label. Specifically, the navigation label management unit 385 can execute a navigation label delete command using a drop command on the generated navigation, and transmits the deleted flight plan to the FDP through the FDP output unit. And transmit the result of the execution to the memory block management unit. Accordingly, the wand normally processed in the FDP is displayed in dark gray. The navigation label management unit 385 can receive sector information from the console setting unit.

The control data playback unit 345 transmits a recording data request of the corresponding time to the DRS through the DRS output unit, receives the recording data from the DRS input unit, and reproduces (passively replay) and reproduces the stored control data . The control data reproducing unit 345 can reproduce the control screen by setting a specific time and reproduce the control screen of another control station. The control data playback unit 345 can provide start, pause, restart, and end functions when the recorded data is played back. The control data playback unit 345 can provide normal speed (real time), low speed Times), and high-speed (5 times, 10 times) playback functions.

FIG. 4 is a diagram illustrating a detailed configuration of a flight data management unit according to an embodiment.

4, the flight data management unit 400 includes a flight plan management unit 405, an aircraft route management unit 410, an ICAO professional management unit 415, an error specialty management unit 420, an RPL management unit 425, A CPDLC message management unit 440, a PDC message management unit 445, an FDP defect management unit 450, an ATA / ATD management unit 455, an SSR code management unit 460, a CFL management unit 450, An aircraft data output unit 475, a NOTAM management unit 480, an air data strip management unit 485, a runway direction management unit 490 and an aircraft statistics management unit 495 have.

The flight plan management unit 405 may generate a request message to request the flight plan corresponding to the route and the aircraft identification code (ACID) to be searched at normal times, and transmit the request message to the FDP output unit. The FDP transmits a corresponding single flight plan or a list of multiple flight plans to the CWP, and the corresponding message is transmitted to the flight plan management unit 405 through the FDP input unit. The flight plan manager 405 can read the flight plan from the message and display it in the flight plan window and the list. The flight plan management unit 405 transmits the flight plan generated by the controller to the FDP output unit. The FDP sends a confirmation and an error message to the CWP, and the corresponding message is transmitted to the flight plan management unit 405 through the FDP input unit. The flight plan management unit 405 outputs the flight plan modified by the controller to the FDP output . The FDP transmits the confirmation / warning and error message to the CWP, and the corresponding message can be transmitted to the flight plan management unit 405 through the FDP input unit. The flight plan management unit 405 may generate a request message and transmit it to the FDP output unit when the controller desires to delete the flight plan. The FDP sends the confirmation / warning and error message to the CWP, and the corresponding message is transmitted to the flight plan management unit 405 through the FDP input unit. The flight plan management unit 405 can display each confirmation message in a window. The flight plan manager 405 may buffer the flight plan modified by the controller and the flight plan to be deleted in case of a system failure (local operation).

The aircraft route management unit 410 may request a route to the aircraft from the FDP output unit. The request message transmitted to the FDP output unit may include the ACID and the SSR code of the corresponding aircraft. The aircraft route management unit 410 may receive the route calculated for the aircraft from the FDP input unit. FID-ACID-Fixed_Point (5) ET (4) LEVEL (4) -Fixed_Point (5) ET (4) LEVEL (4) -Fixed_Point (5) ET (4) LEVEL (4) ). The aircraft route managing unit 410 transmits the flight plan whose route has been modified by the input of the controller to the FDP input unit. The flight plan management unit 405 transmits the route change due to the mouse click of the controller to the FDP input unit 406. When the FDP passes the validation route, Can be changed and displayed.

The ICAO professional management unit 415 manages ICAO telegrams such as ALR, ARR, CHG, CNL, DEP, DLA, FPL, RCF, RQP, RQS, SPL, AIDC, NOTAM, TEXT, TEL_CPL, TEL_EST, TEL_CDN, TEL_ACP, TEL_LAM, can do. The ICAO professional management unit 415 can transmit the ICAO text inputted by the controller to the FDP output unit at a usual time, and the controller can provide a GUI for inputting the text. The GUI is configured to fit the field of the expert, and the ICAO professional management unit 415 can receive the ICAO message from the FDP input unit and display it on the window. The ICAO professional management unit 415 can store the ICAO text entered by the controller in a buffer in case of a system failure (local operation)

The error message management unit 420 can receive the Role information from the login management unit and enable the corresponding function only when the received Role is FDO. The error message management unit 420 can activate the FDO function through the Adaptation value set from the login management unit. Only the controller with the Adaptation value will be given the right to modify the error text, otherwise the error text can not be modified. The error message management unit 420 may request an error message to be corrected by the FDP output unit. After receiving the request message, the FDP sends a message containing the error message to the FDP input. The error management unit 420 can receive the error message and display it in the form of a list. The list is composed of fields of type of expert, ACID, From, To, Originator, and an error field number. The error message management unit 420 can provide the corrected error message to the FDP through the FDP output unit. If there is no abnormality in the provided error message, the error message management unit 420 can receive a confirmation message from the FDP input unit. If there is an error, the error message management unit 420 receives a message including the erroneous field from the FDP input unit. The error message management unit 420 receives an error message to be automatically transmitted by the FDP through the FDP input unit, and the received error message is displayed under the current list. The error message management unit 420 may transmit an error message to the FDP output unit of the controller, and may receive the acknowledgment message through the FDP input unit when the FDP receives and processes the message.

The RPL management unit 425 can receive the Role information from the? Log-in management unit, and can activate the function only when the received Role is the RPL. The RPL management unit 425 normally generates a request message and transmits it to the FDP output unit. Upon receipt of the request, the FDP sends a message containing the RPL list to the CWP. The corresponding message is transmitted from the FDP input unit to the RPL management unit 425. The RPL management unit 425 can read the RPL list from the message and display it in the window. The RPL management unit 425 transmits the corresponding field to the FDP output unit when the controller selects a field desired to be filtered. The RPL management unit 425 receives the filtered RPL from the FDP input unit and displays it in a window. When the controller clears the filtering, the RPL management unit 425 transmits a request message to the FDP output unit, receives the filtered RPL list from the FDP input unit, The RPL management unit 425 may generate a request message to request the FDP for detailed information on a specific RPL and transmit the request message to the FDP output unit. The FDP can send a message to the CWP containing details of the requesting RPL. The corresponding message is transmitted from the FDP input unit to the RPL management unit 425. The RPL management unit 425 displays the RPL window in the case of the Waiting / Modeled state and the flight plan window in the Prepared state according to the state of the RPL. The RPL management unit 425 can provide a GUI so that the controller can modify / delete the RPL. When the controller has modified / deleted the RPL, the RPL management unit 425 generates a request message and transmits the request message to the FDP output unit. The FDP sends a response message to the CWP in response to the request message. The message is transmitted from the FDP input unit to the RPL management unit 425, and the RPL management unit 425 can display a response message from the message in the window.

The prediction route output unit 430 can output a prediction result based on the flight plan of each aircraft. In the predictive route modeling performed by the predicted route output unit 430, the predicted route from the aircraft is displayed in the form of the 4D orbit (latitude, longitude, altitude, and time) processed by the FDP. The forecasting route can be displayed according to the time specified by the controller, for example, 5 minutes, 10 minutes, 15 minutes. The forecast route is displayed as a line on the control screen and can be updated.

The aircraft output unit 435 can display departure and arrival plans of existing and changed aircraft for each airport. Specifically, the aircraft output unit 435 can display the aircraft departing for each airport and the arriving aircraft by time zone and displaying statistics. The aircraft output unit 435 can display a list generated based on the departing aircraft, the arriving aircraft, the time zone, the airline, the departure / arrival airport or the usage route of each airport, and calculates the departure order and the arrival order of the aircraft And can be displayed graphically. The aircraft output unit 435 can receive and display statistics on the flight plan and departure and arrival of the aircraft through the FDP input unit.

The CPDLC message management unit 440 can receive the CPDLC message from the FDP input unit and can provide a GUI for the controller to input the CPDLC message. The controller can select the format of the input message using the combo box. The message format is Air Traffic Management Doc. 4444 Based on the table in Appendix 5, Uplink messages. The message format reads the text file at the same time the system is started and displays it in the input window. The CPDLC message management unit 440 may enable voice communication with the pilot by activating the voice communication mode according to the controller selection, and may transmit a message including the controller input to the FDP output unit.

The PDC message management unit 445 receives the pre-departure clearance (PDC) request message from the FDP input unit and can display it on the window. The PDC message management unit 445 may generate a message including PDC permission or denial of the controller and transmit the message to the FDP output unit.

The FDP defect management unit 450 may receive the FDP request message and provide the necessary information to support recovery of the system failure. The FDP defect management unit 450 can confirm the system status received from the SMS input unit in order to recognize the failure of the FDP. The FDP defect management unit 450 recognizes a system failure when all the nodes of the FDP are degraded or down, and switches the control mode to the local mode. The information that the FDP defect management unit 450 transmits to the FDP may have characteristics such as a request message of the CWP, a function (flight plan creation / modification / deletion, local coupling, etc.) performed locally by the CWP. The FDP defect management unit 450 can store events occurring during the FDP and the system failure, and can automatically transmit the stored data to the FDP output unit in response to the transmission request of the FDP. The FDP defect management unit 450 can transmit the recovery status to the SMC output unit during the failure recovery process and the recovery status can be set to, for example, "0: initial value, 1: failure occurrence, 2: : Occurrence of recovery error ".

The ATA / ATD management unit 455 may provide a GUI that can change the actual time of arrival (ATA) and the actual time of arrival (ATD). The ATA / ATD management unit 455 may generate a request message including ATA and ATD changed by the controller and transmit the request message to the FDP output unit. The FDP may transmit a confirmation message to the CWP, and the corresponding message may be delivered to the ATA / ATD management unit 455 through the FDP input unit. The ATA / ATD management unit 455 can display the confirmation message in the window.

The SSR code management unit 460 may generate a request message for requesting the SSR code list and transmit the request message to the FDP output unit. The FDP transmits a response message to the CWP, and the corresponding message can be transmitted to the SSR code management unit 460 via the FDP input unit. The SSR code management unit 460 can read the information including the SSR code from the response message and display it in the list window. In addition, the SSR code management unit 460 may generate a request message for changing the SSR code of the controller and transmit the request message to the FDP output unit. The FDP sends confirmation / warning and error messages to the CWP, and the corresponding message can be delivered to the SSR code management unit 460 via the FDP input unit. The SSR code management unit 460 can display confirmation / warning and error messages in a window.

The CFL management unit 465 can receive the sector information from the console setting unit, provide the GUI for allowing the allocation altitude change to be made in the control state, and changing the CFL. The CFL management unit 465 may generate a request message including the CFL changed by the controller and transmit the request message to the FDP output unit, and the FDP may transmit the confirmation message to the CWP. The confirmation message may be transmitted to the CFL management unit 465 through the FDP input unit, and the confirmation message may be displayed in the window.

The MTCD output unit 470 can display an MTCD between aircraft to provide a notification related to a medium-term collision. The MTCD output unit 470 can receive and display the MTCD information from the FDP input unit and set the collision expected distance. The MTCD output unit 470 can display an alert with an image or a sound, indicate a risk of a collision in a window, and display an expected collision path on a control screen. The MTCD output unit 470 can display MTCD status graphically, for example, using the "Conflict and Risk Display" window and the "Vertical Aid" window.

The aircraft performance output unit 475 can receive the performance information of the aircraft from the FDP and display it. The performance information of the aircraft is received from the FDP input unit. The aircraft performance output unit 475 transmits performance information of the aircraft to the data block management unit, the flight plan management unit 405, and the air data strip management unit 485. For example, the aircraft performance output unit 475 may determine whether the performance of the aircraft in the data block is "PBN-> P or none (speed side)", "RNP (RNAV) RVSM -> * or none (side of speed) ". The aircraft performance output unit 475 outputs the performance of the aircraft to the strip as "PBN -> P, N / A (R), RNP , None (next to the model) ". The aircraft performance output unit 475 displays the performance of the aircraft in the flight plan window as "PBN -> P, none (equipment side), RNP (RNAV) -> R, > *, None (beside equipment) ".

The NOTAM management unit 480 can display the NOTAM map on the control screen and set the area to APW. The NOTAM management unit 480 can display the start time, end time, location (latitude and longitude), limitations, map type, and altitude information of the NOTAM on the control screen. In addition, the NOTAM management unit 480 may receive the NOTAM message in the ATS message format from the? FDP input unit, then request the SDP to add the APW layer to the NOTAM map through the manager management unit, and set the NOTAM map to the APW layer .

The air data strip management unit 485 can receive the posting message through the FDP input unit and display the received posting message in an electronic strip window or output it as a paper strip. The air data strip management unit 485 can receive the sector information from the console setting unit and display only postings related to the control sector in the strip window through the received sector information. Can receive the ID of the controller from the log-in management unit, load the configuration file through the received ID, and provide the electronic strip and paper strip set by the controller. The air data strip management unit 485 may provide different kinds of electronic strips and paper strips depending on the state of posting. The states displayed on the electronic strip include, for example, " Preactive: 30 minutes + EOBT based on EOBT flight schedule to be departed + Modeled ", "Announced: Prepared or Departed status "," Handover- , And "Controlled". For example, "Announced: Prepared", "1 hour prior to Incheon FIR Pass", and "10 minutes before Jurisdiction entry" The strip management unit 485 can receive the deletion request message received from the FDP and delete the strip, and the deletion request message is transmitted to the air data strip management unit 485 through the FDP input unit. When the controller sets a strip to output a paper strip, the air data strip management unit 485 may generate a file in an output format using the strip, and then transmit the file to the CWP input unit. The air data strip management unit 485 may receive the paper strip file from the CWP output unit and output it to the strip printer.

The runway direction management unit 490 can set and change the runway direction of the airports or airplanes to be controlled. The runway direction management unit 490 can transmit the set and changed runway directions to the FDP output unit, receive the process results from the FDP input unit, and transmit the runway direction to the SID / STAR management unit.

The aircraft statistical management unit 495 can receive the Role information from the login management unit and activate the function only when the received Role is FLOW. The airplane statistical management unit 495 may be configured to provide a list of airplanes that are scheduled to depart, arrive, or are scheduled to depart or arrive at a particular airport, It can be displayed graphically. The aircraft statistics management unit 495 can manage the aircraft statistics through the set values. If the aircraft statistics management unit 495 is expected to exceed the air traffic flow management (AFTM) limit set in the near future, the label icon and bar graph of that point (fix, airport) or sector will be highlighted in red Can be displayed and can be emphasized and displayed in yellow if it is predicted that the predetermined time is exceeded but exceed the limit value. The aircraft statistics management unit 495 receives the aircraft statistical data from the FDP input unit, and when the setting value is changed, transmits the changed setting value to the FDP output unit and receives the processing result from the FDP input unit.

5 is a detailed block diagram of a data input / output management unit according to an embodiment of the present invention.

5, the data input / output management unit 500 includes a DRS input unit 505, a DRS output unit 510, an FDP input unit 515, an FDP output unit 520, an SDP input unit 525, an SDP output unit 530 An SMS input unit 535, an SMC input unit 540, an SMC output unit 545, a CWP input unit 550, and a CWP output unit 555.

The FDP input unit 515 can forward information received from the FDP in the CWP. The FDP input unit 515 is used for the flight planning, the flight planning route, the ICAO specialization, the SSR code, the CFL, the posting data, the error flight plan, the RPL, the forecast route, the departure and arrival information, MTCD, PBN, RVSM, CPDLC, AIDC SID / STAR, Coupling / Decoupling, Label, ASTERIX Cat., FACILITY Data Communication), Runway, Traffic Information, PDC, Sector Information, QNH, FDP Alarm, FPASD, Holding, 062 (1062/380 Flight plan related data: Mini plan). The FDP input unit 515 can receive information through an external channel connected to the FDP as an MQ (message queue). The MQ may be, for example, a middleware (program) used for stable data communication between systems. The FDP input unit 515 can perform validation by reading the header of the received information. If an error occurs in the validity check, the FDP input unit 515 transmits the error message to the data log management unit. If the information is valid, the FDP input unit 515 can transmit the information to each unit.

The FDP output unit 520 can receive information sent to the FDP from the units in the CWP and transmit the information to the outside. The FDP output unit 520 includes:? Flight plan request / add / modify / delete, ICAO special request, PDC authorization / denial, QNH request / modification, SSR code request / reassign / change, Request, CFL input, ATD / ATA input, control transfer / acquisition request, control acquisition / release request, coupling / decoupling request, label generation / drop request, flight planning route request, sector allocation / change / It can manage information such as information request, RPL list search / add / modify / delete request, FDO list request / modification, runway setting / status / change request, CPDLC message transmission, sector information request, SID / STAR request. The FDP output unit 520 can transmit information to an external channel connected to the FDP as an MQ. The FDP output unit 520 can perform the validity check by reading the header of the received information, and when an error occurs in the validity check, the FDP output unit 520 transmits the error message to the data log management unit. If the information is valid, the FDP output unit 520 can transmit the information to the FDP through an external channel.

The SDP input unit 525 can transmit information received from the SDP in the CWP. The SDP input unit 525 is connected to the ASTERIX Cat. 004 Safety Nets Messages, ASTERIX Cat. 008 Monoradar Weather Data, ASTERIX Cat. 021 ADS-B Messages, ASTERIX Cat. 034 Monoradar Service Messages, ASTERIX Cat. 048 Monoradar Target Reports, ASTERIX Cat. 062 System Track Data can be managed. The SDP input unit 525 can receive information through an external channel connected to the SDP as an MQ. The SDP input unit 525 reads the header of the received information and performs validity checking. When an error occurs in the validation, the SDP input unit 525 transmits the error message to the data log management unit. The SDP input unit 525 can transmit the information to each unit when the information is valid.

The SDP output unit 530 can receive information to be transmitted through the SDP from the units in the CWP and transmit the information to the outside. The SDP output unit 530 can manage information such as MSAW, APW change request, SafetyNet enable / disable, and the like.

The SMS input unit 535 can receive information from the SMS and deliver it to a unit inside the CWP. The SMS input unit 535 can manage information such as a system map and an airport map. The SMS input unit 535 can use the SFTP file transfer protocol. The SMS transmits a map to each console of the CWP, and the SMS input unit 535 can deliver it to the map management unit. When the system is restarted, the system can perform the control using the updated map.

The SMC input unit 540 receives the control signal from the SMC and can transmit the control signal to the unit in the CWP. In addition, the SMC input unit 540 can receive the status of the subsystem, the electronic message, and the user list from the SMC and transmit the status to the units in the CWP. The SMC input unit 540 manages information such as application status request, hardware (CPU, memory, hard disk) status request, system status request, system shutdown request, strip printer status request, electronic message, subsystem status, can do. The SMC input unit 540 uses the SNMP protocol. The SMC transmits an SNMP request message to each console of the CWP, and the SMC input unit 540 can transmit the SNMP request message to the SMC control signal processing unit and the SMC request message processing unit. The SMC input unit 540 uses the MQ, and can provide the status of the subsystem to the subsystem output unit, the electronic message to the electronic message providing unit, and the user list to the administrator management unit.

The SMC output unit 545 can transmit information to the SMC. The SMC output unit 545 can manage information such as application status, hardware (CPU, memory, hard disk) status, system status, strip printer status, electronic message, user list update request, The SMC output unit 545 uses the SNMP protocol and MQ. A response message corresponding to the request of the SMC is generated and transmitted to the SMC output unit 545, or a trap message is generated when an event such as application termination, system termination, power off of the strip printer occurs, . A message for transmitting the electronic message created by the controller to the SMC is sent to the SMC output unit 545. When the controller requests the user list update, a message is generated and transmitted to the SMC output unit 545. [

The DRS input unit 505 may receive the reproduction data from the DRS and transmit it to the control data reproduction unit.

The DRS output unit 510 may transmit a request message regarding the reproduction data to the DRS. When the controller inputs the date and time of the reproduction material, a request message is generated and transmitted to the DRS output unit 510.

The CWP input unit 550 can receive a message from another CWP. The CWP input unit 550 can manage information such as an electronic message, paper strip data, user information, login information, and global map.

The CWP output unit 555 can transmit a message to another CWP. The CWP output unit 555 can manage information such as an electronic message, paper strip data, user information, login information, and global map.

FIG. 6 is a diagram illustrating a detailed configuration of a system management unit according to an embodiment.

6, the system management unit 600 may include an SMC request message processing unit 610, an SMC control signal processing unit 620, and a subsystem output unit 630. The system management unit 600 controls the system, and requests and executes application status requests / responses / traps, system status requests / responses / traps, strip printer status requests / And can execute data such as execution.

The SMC request message processing unit 610 may process the request message received from the monitoring control system (SMC). The received request message is related to MAMB status, system recovery status, application status (On, Off), hardware status (CPU, memory, hard disk), and system status (On, Off). The SMC request message processing unit 610 may generate a response message for the request message and transmit the response message to the SMC output unit, generate a trap message for the event, and transmit the trap message to the SMC output unit. Events are related to the start or end of an application, the start or end of a system.

The SMC control signal processor 620 can process the control signal received from the SMC. The control signal is related to the start and end of the application, and the termination of the system. The SMC control signal processor 620 continuously monitors the state of the application and can automatically re-execute the application when the application is abnormally terminated.

The subsystem output unit 630 can display the status of the subsystem received from the SMC. Specifically, the subsystem output unit 630 may display states of subsystems such as a monitoring data processing system (SDP), a flight data processing system (FDP), and a radar site.

7 is a view for explaining the operation of the data log management unit according to an embodiment.

Referring to FIG. 7, the data log management unit 700 can manage the flight data log and the error log stored in the present system. The present system can periodically transmit the log to the recording / playback system and use the log transmitted at the time of system recovery. The data log management unit 700 can collect or manage all the data logs and error logs generated in the air status occurrence management unit 110, the general appearance management unit 120, the flight data management unit 130, and the system management unit 140 , And transmits the collected log through the data input / output management unit 150.

8 is a flow chart illustrating an aviation control method for an air traffic control according to an embodiment.

In step 810, the air traffic control display system may display the current air condition, including the wake and flight of the aircraft, based on the air traffic control data. The airborne monitoring system can display information about the wake of the aircraft as a data block and display the state of the wake according to the wake of the aircraft.

In this case, the aeronautical monitoring system can be displayed by synthesizing or overlaying weather data synchronized with the present air condition to the current air condition.

In addition, the airborne monitoring system can display APM data for the airport runway in a vertical or horizontal view. In this case, the aeronautical monitoring system can generate an approach path monitoring warning if the aircraft is located below an axis defined on the basis of the landing and gliding angles of the aircraft in the vertical view, and in the horizontal view, If an aircraft is located outside the defined range based on the axis, an approach path monitoring alert can be generated.

In step 820, the airborne monitoring system may display the predicted course of the aircraft derived from the flight plan and flight plan of the aircraft. In this case, the air traffic control system can display the predicted route of the aircraft as a 4D (dimension) orbit including latitude, longitude, altitude and time, and display the predicted route according to the predefined time.

In addition, the aeronautical monitoring system can display performance data of an aircraft including performance based navigation (PBN), local navigation (RNAV) and vertical separation interval reduction (RVSM) along with the flight plan of the aircraft.

The method according to an embodiment may be implemented in the form of a program command that can be executed through various computer means and recorded in a computer-readable medium. The computer-readable medium may include program instructions, data files, data structures, and the like, alone or in combination. The program instructions to be recorded on the medium may be those specially designed and configured for the embodiments or may be available to those skilled in the art of computer software. Examples of computer-readable media include magnetic media such as hard disks, floppy disks and magnetic tape; optical media such as CD-ROMs and DVDs; magnetic media such as floppy disks; Magneto-optical media, and hardware devices specifically configured to store and execute program instructions such as ROM, RAM, flash memory, and the like. Examples of program instructions include machine language code such as those produced by a compiler, as well as high-level language code that can be executed by a computer using an interpreter or the like. The hardware devices described above may be configured to operate as one or more software modules to perform the operations of the embodiments, and vice versa.

While the present invention has been particularly shown and described with reference to exemplary embodiments thereof, it is to be understood that the invention is not limited to the disclosed exemplary embodiments. For example, it is to be understood that the techniques described may be performed in a different order than the described methods, and / or that components of the described systems, structures, devices, circuits, Lt; / RTI &gt; or equivalents, even if it is replaced or replaced.

Therefore, other implementations, other embodiments, and equivalents to the claims are also within the scope of the following claims.

Claims (16)

An aviation situation indication management unit for presenting the current aviation condition including the trajectory and route of the aircraft based on the aviation control data; And
A flight data management unit for presenting the flight plan of the aircraft and the predicted course of the aircraft derived from the flight plan,
And an airborne control system. The method according to claim 1,
Wherein the air condition-
An aeronautical monitoring system that combines and overlays weather data synchronized with current weather conditions to the current weather conditions. The method according to claim 1,
Wherein the air condition-
Wherein the information about the wake of the aircraft is displayed as a data block, and the state of the wake according to the wake of the aircraft is displayed. The method according to claim 1,
Wherein the air condition-
An aeronautical monitoring system that displays APM data on an airport runway in a vertical or horizontal view. 5. The method of claim 4,
Wherein the air condition-
Generating an approach path monitoring alert if the aircraft is located below an axis defined on the basis of the landing and gliding angles of the aircraft in the vertical view,
And generates an approach path monitoring alert when an aircraft is located outside the defined range based on the landing point and the runway axis of the aircraft in the horizontal view. The method according to claim 1,
The flight data management unit,
A flight control system in which a predicted route of an aircraft is displayed in a 4D (dimension) orbit including latitude, longitude, altitude and time, and a predicted route is displayed according to a predefined time. The method according to claim 1,
The flight data management unit,
An aeronautical monitoring system that displays performance data of an aircraft including performance based navigation (PBN), local navigation (RNAV) and vertical separation interval reduction (RVSM) along with the flight plan of the aircraft. The method according to claim 1,
A system management unit for managing resources of an application and a system based on a control signal,
Further comprising: an air navigation system for air traffic control. Presenting the current aviation situation including the wake and flight of the aircraft based on the air traffic control data; And
A step of displaying the flight plan of the aircraft and the predicted course of the aircraft derived from the flight plan
The method comprising the steps of: 10. The method of claim 9,
The method of claim 1,
A step of synthesizing or overlaying weather data synchronized with current weather conditions to current weather conditions
The method comprising the steps of: 10. The method of claim 9,
The method of claim 1,
Wherein the information about the wake of the aircraft is displayed as a data block, and the status of the wake according to the wake of the aircraft is displayed. 10. The method of claim 9,
The method of claim 1,
Stepping up APM data for airport runway to vertical or horizontal view
The method comprising the steps of: 13. The method of claim 12,
Wherein the step of presenting the approach path monitoring (APM) data as a vertical view or a horizontal view comprises:
Generating an approach path monitoring alert if the aircraft is located below an axis defined on the basis of the landing and gliding angles of the aircraft in the vertical view; And
Generating an approach path monitoring alert when the aircraft is located outside the range defined in the horizontal view based on the landing point of the aircraft and the runway axis;
The method comprising the steps of: 10. The method of claim 9,
Wherein the step of displaying the flight plan of the aircraft and the predicted course of the aircraft comprises:
A method of presenting an air traffic control system in which a predicted route of an aircraft is displayed as a 4D (dimension) orbit including latitude, longitude, altitude and time, and a predicted route is displayed according to a predefined time. 10. The method of claim 9,
Wherein the step of displaying the flight plan of the aircraft and the predicted course of the aircraft comprises:
An aeronautical display method that displays performance data of an aircraft including performance based navigation (PBN), local navigation (RNAV) and vertical separation interval reduction (RVSM) along with flight plan of aircraft. A computer-readable recording medium on which a program for executing the method of any one of claims 9 to 15 is recorded.

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