KR20190017400A - Flight Situation Management System of Light Plane - Google Patents

Abstract

The present invention relates to a management system of a small situation flight situation. A system according to the present invention comprises: an aircraft location part which receives location data of a small aircraft in flight, analyzes and processes received location data, and displays the same on a screen; a flight information part which collects and manages data which is required for flight and displays the data on the screen with an aircraft location unit; a flight plan management part which manages flight plan data entered from flight navigation; a flight security part which identifies a flight situation of the small aircraft on the basis of the location data of the small aircraft and checks the occurrence of abnormal situations; and a statistics part which collects data and processes the data to statistics data. According to the present invention, a real-time location of a small aircraft is monitored and all sorts of information which is required for flight is transferred and received by loading an ADS-B device on a small aircraft away from a conventional control method of a large aircraft which depends on radar. As a result, a flight situation of a small aircraft can be managed all together.

Description

Flight Situation Management System of Light Plane [

The present invention relates to a small-sized airplane flight situation management system, and more particularly, to a small-sized airplane that monitors the real-time position of a small-sized airplane by loading an ADS- And more particularly, to a small aircraft flight situation management system that can be integrally managed.

As the range of activities of modern people is expanded and personal business movements between continents increase, the proportion of aircraft as long distance transportation means is increasing. Accordingly, an air traffic control system is operated to handle the rapidly increasing air traffic volume.

The air traffic control system includes a flight data processing system (FDP) that processes and manages all data related to the flight plan, a surveillance data processing system that provides radar navigation information for the aircraft, (Controller Working Position), which supports and manages the control screen, a data recording system that backs up and manages all data exchanged in the air traffic control, or a management system that manages the status of the air traffic control systems and the processor .

Conventional air traffic control systems allow the aircraft to operate safely while transmitting and receiving flight information related to engine and aircraft system information, flight instruction, flight guidance, and various control functions through radars mounted on the aircraft. However, today, As the workload increases, safety, speed and efficiency problems are raised. Therefore, it is necessary to build a new and more precise and efficient new control system by using satellite and modern computer equipment away from current radio communication and radar-based control system. The need for

Accordingly, it is possible to provide terminals capable of displaying data acquired through aircraft navigation and ADS-B antennas, system equipment capable of processing, storing, and managing these data, and communication facilities for securing data linkage with related systems A Ground Flight Management Center became necessary.

Accordingly, the technical problem to be solved by the present invention is to provide an ADS-B device mounted on a small-sized aircraft, which monitors the real-time position of a small-sized aircraft, transmits and receives all information necessary for the flight, And to provide a small-sized aircraft flight status management system capable of integrally managing the flight status of a small-sized aircraft.

Further, the present invention includes other objects that can be achieved from the construction of the present invention described later, in addition to the objects explicitly mentioned.

According to an aspect of the present invention, there is provided a small-sized aircraft flight condition management system for receiving position data of a small-sized airplane in flight, analyzing and processing the received position data, An aviation information section for collecting and managing data necessary for flight and displaying the data on a screen together with the aircraft position section, a flight plan management section for managing flight plan data inputted from the air navigation, An aviation safety unit for checking the flight status of the small aircraft to check whether an abnormal situation has occurred, and a statistics unit for collecting the data and processing the data into statistical data.

The aircraft location unit may receive real-time location data of the small aircraft from the ADS-B server in conjunction with the ADS-B server.

The data displayed in the aviation information unit may include at least one of map, weather, airspace, obstacle, NOTAM information, landing area information, and AIP.

The air information unit can manage the data by each layer and display it on the screen.

The aeronautical information department may inform the small aircraft equipped with the ADS-B equipment of the information of the small aircraft not equipped with the ADS-B equipment.

The aviation safety department compares the flight plan path submitted before the flight with the flight position of the small aircraft to check whether the flight has departed, confirms whether the flight position of the small aircraft is invading the flight restricted area, It is possible to check whether the position of the small aircraft is normally moving and to check whether the altitude of the small aircraft is abnormally dropped and whether the track of the small aircraft is abnormally lost.

As described above, according to the small-sized airplane flight situation management system according to the embodiment of the present invention, the real-time position of the small-sized aircraft is monitored by mounting the ADS-B device on the small- It is possible to manage the flight situation of the small aircraft in an integrated manner by transmitting and receiving all the basic information necessary for the flight.

And it displays the NOTAM, aeronautical weather information, airspace and obstacle information based on the map information that comply with the national map standard provided in the National Space Information Center, so that it is easy to manage the situation necessary for the flight, .

In addition, it is possible to manage the flight plan data created by the air navigation system (dedicated / general purpose terminal) so that a small airplane pilot or a user can more easily prepare and receive the flight plan, Function can be provided.

In addition, it is possible to manage the flight of a small aircraft in an overall manner, so that it can flexibly cope with an abnormal situation, and can provide quick and smooth search support even in case of an accident.

It is also possible to manage statistics on flight time, flight frequency and accident history by systematically classifying and managing flight related information data.

On the other hand, the effects of the present invention are not limited to those described above, and other effects that can be derived from the constitution of the present invention described below are also included in the effects of the present invention.

1 is a block diagram of a small-sized aircraft flight situation management system according to an embodiment of the present invention.
2 is a diagram of a monitoring wall screen of a small-sized aircraft flight situation management system according to an embodiment of the present invention.
3 is a software configuration diagram of an aircraft position part according to an embodiment of the present invention.
4 is a block diagram illustrating an ADS-B server interworking function according to an embodiment of the present invention.
5 is a block diagram illustrating an ADS-B data management function according to an embodiment of the present invention.
FIG. 6 is a diagram showing the basic structure of Asterix Category 021.
FIG. 7 is a block diagram showing an aircraft position information display function according to an embodiment of the present invention.
8 is an exemplary diagram of an ADS-B server interworking management use case according to an embodiment of the present invention.
9 is an illustration of an ADS-B data management use case according to an embodiment of the present invention.
10 is an exemplary view of an airplane position information display use case according to an embodiment of the present invention.
FIG. 11 is an exemplary view showing a procedure of an aircraft position information management function according to an embodiment of the present invention.
FIG. 12 is an exemplary view showing a procedure of an aircraft position information display function according to an embodiment of the present invention.
13 is an exemplary view of an aircraft location database according to an embodiment of the present invention.
14 is an exemplary view of an aircraft location UI according to an embodiment of the present invention.
15 is a software configuration diagram of an aircraft information unit according to an embodiment of the present invention.
16 is a block diagram illustrating an air information update function according to an embodiment of the present invention.
FIG. 17 is a block diagram illustrating an air information display function according to an embodiment of the present invention.
Fig. 18 is a schematic diagram of Asterix format CAT. 022 is a diagram showing a basic structure.
FIG. 19 is a schematic diagram of an Asterix format CAT. 023 is a diagram showing a basic structure.
20 is an exemplary view of an air information update use case according to an embodiment of the present invention.
FIG. 21 is an illustration of an air information display use case according to an embodiment of the present invention. FIG.
22 is an exemplary view of an air information providing use case according to an embodiment of the present invention.
23 is an exemplary view showing a procedure of an air information update function according to an embodiment of the present invention.
24 is an exemplary diagram illustrating a procedure of an air information display function according to an embodiment of the present invention.
25 is an exemplary diagram of an aviation information section DB according to an embodiment of the present invention.
26 is an exemplary view of an aviation information unit UI according to an embodiment of the present invention.
27 is a software configuration diagram of a flight plan management unit according to an embodiment of the present invention.
28 is a configuration diagram showing a flight plan data checking function according to an embodiment of the present invention.
FIG. 29 is a configuration diagram illustrating a flight plan path display function according to an embodiment of the present invention.
30 is a configuration diagram illustrating a flight plan simulation function according to an embodiment of the present invention.
FIG. 31 is a configuration diagram showing a flight result data management function according to an embodiment of the present invention.
32 is an exemplary diagram of a user authentication use case according to an embodiment of the present invention;
33 is an exemplary diagram of a flight plan data management use case according to an embodiment of the present invention.
34 is an exemplary diagram of a flight plan data provision management use case according to an embodiment of the present invention.
35 is an exemplary view of a flight plan path display use case according to an embodiment of the present invention.
36 is an exemplary diagram of a flight plan simulation use case according to an embodiment of the present invention.
37 is an exemplary diagram of a flight result data management use case according to an embodiment of the present invention.
FIG. 38 is an exemplary view showing a procedure of a flight plan data checking function according to an embodiment of the present invention.
FIG. 39 is an exemplary diagram illustrating a procedure of a flight plan path display function according to an embodiment of the present invention.
FIG. 40 is an exemplary diagram illustrating a procedure of a flight plan simulation function according to an embodiment of the present invention.
FIG. 41 is an exemplary diagram illustrating a procedure of a flight result data management function according to an embodiment of the present invention.
42 is an exemplary diagram of a flight plan management DB according to an embodiment of the present invention.
43 is an exemplary diagram of a flight plan management UI according to an embodiment of the present invention.
44 is a software configuration diagram of the aviation safety department according to an embodiment of the present invention.
FIG. 45 is a configuration diagram showing an abnormal status checking function according to an embodiment of the present invention.
FIG. 46 is a configuration diagram showing an abnormal situation exposing function according to an embodiment of the present invention. FIG.
47 is an exemplary diagram of an abnormal situation check use case according to an embodiment of the present invention.
48 is an exemplary diagram of an abnormal situation exposing use case according to an embodiment of the present invention.
49 is an exemplary diagram of an abnormal situation environment information management use case according to an embodiment of the present invention.
50 is an exemplary diagram showing a procedure of an abnormal situation check function according to an embodiment of the present invention.
51 is an exemplary diagram illustrating a procedure of an abnormal situation exposing function according to an embodiment of the present invention.
52 is an exemplary diagram illustrating a procedure of an abnormal situation environment information management function according to an embodiment of the present invention.
53 is an exemplary diagram of an aviation safety department DB according to an embodiment of the present invention.
54 is an exemplary view of an aviation safety department UI according to an embodiment of the present invention.
55 is a software configuration diagram of a flight plan management unit according to an embodiment of the present invention.
56 is an exemplary diagram of a statistical data input use case according to an embodiment of the present invention.
57 is an exemplary diagram of a statistical data management use case according to an embodiment of the present invention.
58 is an exemplary diagram illustrating a procedure of a statistical data input function according to an embodiment of the present invention.
59 is an exemplary diagram illustrating a procedure of a statistical data management function according to an embodiment of the present invention.
60 is an exemplary diagram of a statistical DB according to an embodiment of the present invention.
61 is an exemplary diagram of a statistics unit UI according to an embodiment of the present invention.

Hereinafter, embodiments of the present invention will be described in detail with reference to the accompanying drawings so that those skilled in the art can easily carry out the present invention.

FIG. 1 shows a configuration diagram of a small-sized aircraft flight situation management system according to an embodiment of the present invention.

As shown in FIG. 1, the small-sized aircraft flight status management system includes an aircraft position unit, an aviation information unit, a flight plan management unit, an aviation safety unit, and a statistics unit.

A small aircraft flight situation management system receives real-time flight position monitoring function of aircraft by receiving position information of small aircraft in flight and collects map-based airspace information, no-fly zone, flight restricted zone, NOTAM and weather information It implements functions to provide to operators and pilots, and it is possible to implement functions to enable the creation and receipt of flight plans directly from the navigation terminal.

A small aircraft flight situation management system should link the FOIS system of the Ministry of Land, Transport and Maritime Affairs to the flight plan received, implement the function to display the actual location of the aircraft in flight together with the location information of the aircraft in flight, The system detects alarms by detecting dangerous situations such as departure of departure route and restricted area, communication disconnection, sudden drop in altitude, etc., which exceeds the error range, and records and manages necessary data in small aircraft and flight situation management system. You can implement features to provide the data and design the server in a redundant system so that the function is not interrupted in the event of an emergency such as equipment failure or system failure.

FIG. 2 is a diagram of a monitoring wall screen of a small-sized aircraft flight status management system according to an embodiment of the present invention. As shown in FIG. 2, the actual implementation of a small- It enables the flight plan of small aircraft, real-time flight monitoring, data of weather and NOTAM to be checked at once.

3 is a software configuration diagram of an aircraft position part according to an embodiment of the present invention.

Referring to FIG. 3, the aircraft position part receives and analyzes real-time position data of an aircraft in flight and displays it on a screen. The system includes a function of receiving position data provided by an ADS-B server for managing position data of an aircraft, And processing the position data and displaying it on the screen. The data to be displayed may include aircraft information (such as aircraft identification number) or flight information (altitude, latitude, longitude, speed, etc.), data provided by the ADS-B server may follow the Asterix format, So that the position of the aircraft can be monitored.

More specifically, the aircraft position unit can confirm the position information of the aircraft. The aircraft positioning unit receives the real-time position data of the aircraft through the ADS-B server, displays it on the screen, and can perform ADS-B server interlocking function and ADS-B data management function.

4 is a block diagram illustrating an ADS-B server interworking function according to an embodiment of the present invention.

In the ADS-B server interworking function shown in FIG. 4, since the position data of the aircraft in flight is managed through the ADS-B server, the interworking information with the ADS-B server must be defined. And may include a function of managing environment information and a function of receiving ADS-B data. ADS-B server environment information management function is to manage environment information for interworking with ADS-B server and ADS-B data reception management function can be function of receiving aircraft position data after interworking with ADS-B server have.

FIG. 5 is a block diagram illustrating an ADS-B data management function according to an embodiment of the present invention, and FIG. 6 is a diagram illustrating a basic structure of an Asterix Category 021.

As shown in FIG. 5, the ADS-B data management function is a function of processing the position data of the received aircraft, and may include a function of logging, data filtering, processing, storing, and transmitting.

The ADS-B data log management function records the reception history of the aircraft position data received through the ADS-B server. The ADS-B data filtering management function manages the environment for filtering valid data among the received aircraft position data The ADS-B data processing management function manages the environment in which the received aircraft position data is processed to the data format required for screen display. As shown in FIG. 6, the ADS- It can be constructed with the basic structure of category 021 corresponding to ADS-B. The CAT number 21 means that this data is the message of ADS-B, LEN is the length of the entire data block, FSPEC defines the values of the data fields in the data block, and ASTERIX CAT. User Application Profile of 021 can process and process data necessary for screen display.

The ADS-B data selection management function is to select only the data required for screen display from the processed ADS-B data. The ADS-B data storage management function is a function to record the processed aircraft position data in DB , And the ADS-B data transmission management function may be a function of transmitting the aircraft position data necessary for screen display.

FIG. 7 is a block diagram illustrating an airplane position information display function according to an embodiment of the present invention. As shown in FIG. 7, an aircraft position part can display position information of an aircraft. The location of the aircraft can be monitored by displaying the position of the aircraft in flight and periodically updating the position data of the aircraft provided by the ADS-B server to display the position of the aircraft in real time. Each data is composed of independent layers and can be managed by Layer Manager. The Layer Manager can include a Manage function for creating / deleting each layer, a processing function for converting to a coordinate required for screen display, and an Overlap function for displaying a screen.

The aircraft position information management function is a function of receiving position data and changing it to coordinate data necessary for screen display, and may include a data reception management function, a coordinate data management function, and a layer management function. The data reception management function is a function for receiving the position data of the aircraft and the coordinate data management function is a function for changing the aircraft position data to the coordinate data necessary for displaying the screen. The layer management function is a function for receiving the position information of the aircraft, It is displayed on the screen in a separate layer, and includes an aircraft layer management function and a flight information layer management function. The layer management function of the aircraft manages the position information of the aircraft in layers. The function of managing the flight information layer is a function of managing the flight information of the aircraft in a layer. The function of managing the flight information is a function of managing the flight information of the aircraft. The user can provide a function of playing back the flight path of the vehicle.

The following describes the use case design method for designing various functions of the aviation positioning.

FIG. 8 is an exemplary view of an ADS-B server interlock management use case according to an embodiment of the present invention, FIG. 9 is an exemplary view of an ADS-B data management use case according to an embodiment of the present invention, and FIG. FIG. 5 is an exemplary view of an airplane position information display use case according to an embodiment of the present invention.

As shown in FIG. 8, the use case of the ADS-B server interlocking management use function of the ADS-B server interlocking function for confirming the position information of the aircraft is as follows. ADS-B data reception start, ADS- Lt; / RTI >

The ADS-B data management use case of the ADS-B data management function shows data reception, data processing, data transmission, log recording, data filtering, aircraft flight information analysis, aircraft position information analysis and data storage diagram .

As shown in FIG. 10, the use case of the Aircraft Location Information Expression use case includes data reception, layer management, coordinate mapping, creation of a flight information layer, deletion of a flight information layer, creation of a position information layer, deletion of a position information layer, , Layer Playback environment check, and Layer Playback environment modification diagram.

11 is a diagram illustrating an exemplary procedure of an aircraft location information management function according to an exemplary embodiment of the present invention. Referring to FIG. 11, an ADS-B server interworking information, an ADS- , ADS-B data logging, ADS-B data processing, ADS-B data transmission, ADS-B data DB storage.

12 is a diagram illustrating a procedure of an aircraft position information display function according to an embodiment of the present invention. Referring to FIG. 12, ADS-B data transmission, ADS-B data reception, coordinate conversion, layer registration, , Layer Overlay, and procedures for layer playback, layer data check, layer DB data check, layer data transfer, data reception, and layer overlay.

13, an aircraft position database includes an aircraft number including an aircraft number, user information including a user number, a flight serial number, an aircraft number, , Flight information including the user number, and flight location information including the flight serial number.

FIG. 14 is a diagram illustrating an example of an aircraft position UI according to an embodiment of the present invention. As shown in FIG. 14, the aircraft position system UI includes flight-related statistics such as today's number of flights and today's flight times, , The position of the current aircraft in the current flight, and the detailed flight information of the aircraft in flight.

15 is a software configuration diagram of an aircraft information unit according to an embodiment of the present invention.

Referring to FIG. 15, the air information unit collects and manages data necessary for flight, and displays the data on the monitoring screen together with the aircraft position part. The data constituting the air information unit includes data such as map, weather, airspace, obstacle, Information, AIP, and the like. The meteorological and NOTAM data required by AERO should be constructed in conjunction with FOIS, and each data should be reflected in the update period.

The AIS is configured to manage the information that is the basis of the system operation, such as airspace information, airport and obstacle information, through user input and modification, and the data collected and collected by the flight status management system can be provided to the air navigation . ≪ / RTI >

The aeronautical information department may perform the aviation information update function. Each data should be updated with the latest information. Since each data may have different cycles according to characteristics, the aviation information update function can be made of the interlinking management function of aviation information and the aviation information management function.

16 is a block diagram illustrating an air information update function according to an embodiment of the present invention.

Among the aviation information update functions shown in FIG. 16, the linkage management function of aviation information is a function of managing environment information for updating aviation information since it must be able to link with an external server to update aviation information with the latest data, The function may be a function of identifying new information and processing new information. In addition to this, it has a function of checking new information for confirming aviation information for updating, a function for receiving new information for receiving new information that needs updating, a function for recording data log for recording each reception history of aviation information, A data processing function for processing the necessary data, and a data update function for storing the processed data in the DB to manage the change history of the data after updating.

FIG. 17 is a block diagram illustrating an aviation information display function according to an embodiment of the present invention. As shown in FIG. 17, the aviation information unit may perform aviation information display function for displaying aviation information required for aviation on a monitoring screen. The aeronautical information department can manage information necessary for flight by each layer and display it on the screen, and can include aviation information management function and aviation information layer management function.

The aviation information management function is a function for managing the received aviation information, an environmental information management function of aviation information for managing environment information for receiving aviation information for screen display, an aviation information receiving function for receiving aviation information for screen display And a coordinate data management function for processing the received aerial information into coordinate data necessary for screen display.

The aerial information layer management function may be a function of managing the aerial information to be displayed on each screen in order to display the aerial information on the screen.

In addition, it performs the manual input of the aerial information manually inputting the dangerous area which is not linked with security, and inputs the coordinates so that the dangerous area can be provided to the air navigation.

The aeronautical information department can provide the aeronautical information providing the aeronautical information necessary for the flight as the air navigation, and each air information can be managed in the same version as the air navigation using the data version.

Fig. 18 is a schematic diagram of Asterix format CAT. 022 is a diagram showing the basic structure and Fig. 023 is a diagram showing a basic structure.

The TIS-B (Traffic Information Service Broadcast) function is a function that notifies ADS-B equipped aircraft of information of an aircraft not equipped with ADS-B equipment. It is equipped with 1090ES, 978MHz frequency It can be applied regardless of Basically, if ADS-B "IN" function is implemented, more accurate situation recognition and useful information acquisition is possible. In addition to ADS-B equipment, it can also receive information from surveillance radar (SSR), ASDE and MLAT. In the first construction, the real-time monitoring function of the aircraft in flight is implemented first, and the stability of the system can be confirmed and then implemented in stages. As shown in FIG. 18, among the Asterix formats designated as EUROCONTROL standard, CAT. 022 < / RTI > A CAT number of 22 means that this data is a message of TIS-B, and LEN is the length of the entire data block. The FSPEC defines the values of the data fields in the data block, and ASTERIX CAT. User Application Profile of 022 can process the data needed for screen display processing.

The FIS-B (Flight Information Service Broadcast) function is a function to provide aeronautical information such as weather and NOTAM required for flight in the ground flight management system. Only UAT data linkable aircraft can be serviced. If the ADS-B "IN" function is implemented basically, more accurate situation recognition and useful information can be obtained. In the first construction, real-time flight monitoring function is implemented first, . As shown in Fig. 19, among the Asterix format used as a standard in EUROCONTROL, CAT corresponding to FIS-B. 023 < / RTI > A CAT number of 23 means that this data is a FIS-B message, and LEN is the length of the entire data block. The FSPEC defines the values of the data fields in the data block, and ASTERIX CAT. User Application Profile of 023 can process the data needed for screen display processing.

The following describes the use case design method for designing various functions of aviation information department.

FIG. 20 is an exemplary view of an air information update use case according to an embodiment of the present invention, FIG. 21 is an exemplary view of an air information disclosure use case according to an embodiment of the present invention, and FIG. FIG. 2 is an exemplary view of an air information providing use case according to FIG.

As shown in FIG. 20, the aviation information update use case shows a diagram of inputting aviation information, receiving aviation information, processing aviation information data, storing aviation information, confirming interworking information, and confirming new information. 21, the aeronautical information display use case includes data reception, layer management, coordinate mapping, map layer creation / deletion, weather information layer creation / deletion, airspace information layer creation / deletion, obstacle information layer creation / deletion, Creation / deletion, and creation / deletion of takeoff and landing information layer. As shown in FIG. 22, the aerial information providing use case shows a diagram of providing map data, providing weather data, providing airspace data, providing obstacle data, providing Notam data, and providing airport data.

23 is a diagram illustrating a procedure of an air information update function according to an exemplary embodiment of the present invention. As shown in FIG. 23, data input, interlocking information confirmation, air information server connection confirmation, data reception, data processing, 24 is a diagram illustrating a procedure of an aviation information exposing function according to an embodiment of the present invention. As shown in FIG. 24, data verification, DB data verification, data transmission, data reception, Coordinate transformation, Layer registration, Layer creation, Layer Overlay.

FIG. 25 is an exemplary view of an aviation information DB according to an embodiment of the present invention. As shown in FIG. 25, map information, airspace information, map version information, airport and airport information, NOTAM information, weather information, .

26 is an exemplary view of an aviation information unit UI according to an embodiment of the present invention. As shown in FIG. 26, the aviation information unit UI can display aviation information such as airspace, notam, obstacle, and corresponding zone information.

27 is a software configuration diagram of a flight plan management unit according to an embodiment of the present invention.

Referring to FIG. 27, the flight plan management unit manages the data of the flight plan received through the air navigation, manages the flight plan entered in the navigation, receives the flight plan of the small aircraft managed by the regional aviation authorities of the Ministry of Land Transportation It is configured to be able to interwork with the related system FOIS system. The flight plan prepared by flight navigation before flight is transferred from the flight situation management system to the FOIS system and accepted. have.

FIG. 28 is a block diagram showing a function of checking the flight plan data according to an embodiment of the present invention. As shown in FIG. 28, the flight plan management unit stores flight plan data received in the air navigation, Verification function, and may include user authentication, data reception, data processing, and data update functions. The user authentication function is a function of authenticating the user who has created the flight plan and has received the user information. The user authentication environment management function manages the environment information for the user authentication. The user authentication function that authenticates the information of the received user and notifies the authentication result .

The flight plan data management function includes flight plan data reception function for receiving flight plan data created by navigation, flight plan data processing function for processing data to store the received flight plan data in DB, And the like. The flight plan data provision management function can provide the flight plan data by linking the flight plan data created by the navigation with the FOIS system.

29, the flight plan management unit displays a route of the received flight plan together with the position information of the aircraft on the screen, as shown in FIG. 29. FIG. 29 shows a flight plan route display function according to an embodiment of the present invention. It can perform the plan route display function, and can be configured with the data management function of the flight plan path and the flight plan layer management function. The flight plan path data management function can include the flight plan path data environment information management function and the data reception and coordinate data management function. The flight plan path data environment information management function manages environment information for receiving flight plan path data The flight plan path data receiving function can receive the flight plan data, and the flight plan path coordinate data management function can change the received flight plan data to the coordinate data for displaying on the screen. Flight Plan Path The layer management function can display flight plan path data on the screen.

FIG. 30 is a block diagram illustrating a flight plan simulation function according to an embodiment of the present invention. As shown in FIG. 30, the flight plan management unit may perform a function of simulating the path of the received flight plan in advance, Simulation data management capabilities and simulation capabilities to simulate flight planning data. The flight planning simulation data management function includes an environmental information management function for managing environment information for receiving flight plan simulation data, a data receiving function for receiving flight plan simulation data, a coordinate data for displaying the position information of the received data Changing flight plan simulated coordinate data management functions.

FIG. 31 is a block diagram showing a flight result data management function according to an embodiment of the present invention. As shown in FIG. 31, the flight plan management unit can perform a flight result data management function for managing result data after completion of flight, A data reception function for receiving the result of flight completion from the navigation after completion of the flight, a data storage function for storing the received result of flight completion in the DB, and a data transmission function for transmitting the received flight result data to the FOIS system.

Next, the use case design method for designing various functions of the flight plan management section will be described.

FIG. 32 is an exemplary view of a user authentication use case according to an embodiment of the present invention, FIG. 33 is an exemplary view of a flight plan data management use case according to an embodiment of the present invention, and FIG. Fig. 35 is an exemplary view of a flight plan path display use case according to an embodiment of the present invention, Fig. 36 is an illustration of a flight plan simulation use case according to an embodiment of the present invention, Fig. And FIG. 37 is an exemplary view of a flight result data management use case according to an embodiment of the present invention.

32, the user authentication use case shows a diagram of user authentication, authentication result notification, and environment information confirmation. As shown in FIG. 33, the flight plan data management use case includes flight plan data reception, flight plan data processing, Data storage, and user authentication. As shown in FIG. 34, the flight plan data provision management use case shows a diagram of flight plan data storage, environment information confirmation, and data verification.

As shown in FIG. 35, the flight plan path display use case shows a diagram of data reception, layer management, coordinate mapping, path layer creation, and path layer deletion, and the flight plan simulation use case includes data reception, 37 shows a diagram of the flight result data management use case. The flight result data use case includes flight result data reception, flight result data storage, user authentication, flight result data transmission, and the like. Show the diagram.

FIG. 38 is a diagram illustrating a procedure of the flight plan data checking function according to an embodiment of the present invention. FIG. 38 shows a procedure for checking the flight plan data from the user authentication as shown in FIG. 38, and FIG. FIG. 40 is a flow chart illustrating a procedure of displaying a flight plan path from DB data verification to Layer Overlay as shown in FIG. 39, FIG. 41 is a diagram illustrating a procedure of a plan simulation function. FIG. 40 shows a flight plan simulation procedure from DB data verification to execution of a simulator. FIG. 41 shows a flowchart of a flight data management function according to an embodiment of the present invention. As shown in FIG. 41, the flight result data from the flight result data transmission to the flight result data storage It can show the procedure.

FIG. 42 is an exemplary diagram of a flight plan management DB according to an embodiment of the present invention. As shown in FIG. 42, flight plan information including a flight plan serial number and flight serial number mapping information may be stored in the flight plan management DB.

43 is a diagram illustrating an example of a flight plan management UI according to an embodiment of the present invention. As shown in FIG. 43, the flight plan management UI may display a simulation of a flight plan path and a flight plan path of a flying aircraft .

44 is a software configuration diagram of the aviation safety department according to an embodiment of the present invention.

Referring to FIG. 44, the aviation safety department grasps the flight situation of a small-sized aircraft and supports the search and rescue support quickly and smoothly in the event of an abnormal situation. It automatically detects the position of the small- And display the result of the analysis on the screen.

FIG. 45 is a block diagram showing an abnormal condition checking function according to an embodiment of the present invention. As shown in FIG. 45, the aviation safety unit can perform a function of checking the status of an aircraft through the position information of a small airplane in flight , The function may include a function of confirming whether the position of the aircraft is in a normal position and a function of transmitting the confirmation result.

The position check function is to check the abnormal situation through the position information of the received aircraft. It is a function to check whether or not the flight plan is out of route by comparing the flight plan route submitted before the flight and the flight position of the aircraft, , And a restricted area identification function to verify that the aircraft location is infiltrating the restricted area. And the position check function is to check whether the position information of the aircraft is being received properly, check whether the position of the aircraft is moving normally, check the altitude of the aircraft, , And a track loss checking function for checking whether the track of the aircraft is abnormally lost. Abnormal situation result transmission function can be a function to confirm whether or not each aircraft is in a dangerous situation and to transmit the result.

FIG. 46 is a block diagram illustrating an abnormal situation exposing function according to an embodiment of the present invention. As shown in FIG. 46, the aviation safety unit can perform a function of displaying a received abnormal condition result on a screen, Can include result confirmation, layer management functions. Abnormal situation result check function confirms received abnormal status result information. Abnormal situation layer management function displays and corrects received abnormal situation on the screen. Abnormal situation manual layer management function is a function to detect abnormality of received abnormal situation And to display and modify the manual information according to the result on the screen.

The following describes the use case design method for designing the various functions of aviation safety department.

FIG. 47 is an illustration of an abnormal situation check use case according to an embodiment of the present invention, FIG. 48 is an illustration of an abnormal situation display use case according to an embodiment of the present invention, and FIG. 49 is an example of the present invention Fig. 2 is an illustration of an abnormal situation environmental information use case according to the present invention; Fig.

As shown in FIG. 47, the abnormal situation check use case shows a diagram from receiving data to confirming whether an aircraft track is lost. As shown in FIG. 48, the abnormal situation display use case includes diagrams As shown in FIG. 49, the abnormal situation environment information management use case shows a diagram of abnormality situation environment information, abnormality situation environment information, abnormality situation manual information confirmation, and correction.

FIG. 50 is a view illustrating an example of a procedure of an abnormal status checking function according to an embodiment of the present invention. FIG. 51 is a view illustrating a procedure of an abnormal status displaying function according to an embodiment of the present invention. FIG. 8 is an exemplary diagram illustrating a procedure of an abnormal environment environment information management function according to an exemplary embodiment.

As shown in FIG. 50, the abnormal status check function shows procedures such as ADS-B data processing, position data check, abnormal situation environment information check, abnormal situation result check, abnormal condition result transmission, etc. Referring to FIG. 51, 52, the abnormal situation environment information management function checks abnormality situation environment information and stores abnormality situation manual environment information, etc. Lt; / RTI >

53 is an exemplary view of the aviation safety department DB according to an embodiment of the present invention. As shown in FIG. 53, the aviation safety department DB may store abnormal situation information, abnormal situation behavior information, related institution information, and abnormal situation display information .

54 is an exemplary view of an aviation safety unit UI according to an embodiment of the present invention. Referring to FIG. 54, the aviation safety unit UI can analyze the location information of an aircraft and notify an emergency situation in an abnormal situation.

Meanwhile, FIG. 55 is a software configuration diagram of a flight plan management unit according to an embodiment of the present invention.

Referring to FIG. 55, the statistics section is a system that utilizes statistical data through systematic management and collection of data handled in the flight situation management system. In the statistical system, the flight time and frequency are analyzed based on the flight information of the small aircraft, It can be configured to enable the status inquiry of emergency occurrence by condition based on the situation occurrence information.

The statistics department performs statistical data input function, and statistical data input function can be composed of data collection function and data update function. The functions may include flight information, flight plans, flight results, abnormal conditions, and aviation statistics data collection functions. The data collection function collects data by processing statistical data and collects data such as flight time and frequency based on flight plan information. The data update function updates the collected data to the statistical database. The statistical data management function is to check and manage the statistical data. It can check the statistical data in the report format, And a statistical data deletion function.

FIG. 56 is an exemplary view of a statistical data input use case according to an embodiment of the present invention; FIG. 57 is an exemplary view of a statistical data management use case according to an embodiment of the present invention; FIG.

Referring to FIG. 56, a statistical data input use case collects data, processes the statistical data into a statistical data format, and then updates the statistical data. Referring to FIG. 57, the statistical data management use- And displays a diagram that shows or deletes statistical data.

FIG. 58 is a view illustrating a procedure of a statistical data input function according to an embodiment of the present invention, and FIG. 59 is an exemplary view showing a procedure of a statistical data management function according to an embodiment of the present invention.

As shown in FIG. 58, the statistical data input function shows procedures such as data collection, statistical data processing, and statistical data update. As shown in FIG. 59, the statistical data management function includes statistical data confirmation, statistical data display, Show the procedure.

FIG. 60 is an exemplary diagram of a statistical DB according to an embodiment of the present invention. As shown in FIG. 60, the statistical DB includes a flight information history, a flight position information history, an abnormality situation information history, Mapping information, map information history, NOTAM information history, obstacle information history, statistical information, weather information history, and space information history can be stored.

61 is a diagram illustrating an example of a statistics unit UI according to an embodiment of the present invention. As shown in FIG. 61, the statistics unit UI may provide a list of flight statistics or a graph of flight statistics during a searched period.

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, Of the right.

Claims (6)

An aircraft position part for receiving position data of a small aircraft in flight, analyzing and processing the received position data and displaying the analyzed position data on a screen,
An aviation information part for collecting and managing data necessary for flight and displaying the data on a screen together with the aircraft position part,
A flight plan manager for managing the flight plan data input from the air navigation,
An aviation safety department for identifying the occurrence of an abnormal situation by checking the flight status of the small aircraft based on the position data of the small aircraft, and
A statistical unit for collecting the data and processing the statistical data
A small aircraft flight situation management system comprising: The method of claim 1,
The airplane-
A small-sized aircraft flight situation management system interfacing with an ADS-B server and receiving real-time position data of the small aircraft from the ADS-B server. The method of claim 1,
The data displayed on the aviation information unit may include:
A small aircraft flight situation management system comprising at least one of a map, weather, airspace, obstacle, NOTAM information, airport and AIP data. 4. The method of claim 3,
The air-
And the data is managed by each layer and is displayed on the screen. The method of claim 1,
The air-
A small aircraft flight situation management system that informs small aircraft equipped with ADS-B equipment of information on small aircraft without ADS-B equipment. The method of claim 1,
The aviation safety unit,
Checking whether or not the departure of the route is caused by comparing the flight plan route submitted before the flight with the flight position of the small aircraft, checking whether the flight position of the small aircraft is invading the flight restriction area, Checking whether the position of the small aircraft is normally moving, checking whether the altitude of the small aircraft is abnormally dropped, and whether the track of the small aircraft is abnormally lost.

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