Coordinated Control Method, Device, Equipment and Storage Medium for Aircraft

Abstract

The coordinated control method, device, equipment and storage medium for an aircraft provided by the present invention determine the placard position of an aircraft to be controlled in an airport plane map through the track data collected by a radar device; then, determine the identity identifier of the aircraft to be controlled through the radar device; then, look up the flight plan information of the aircraft to be controlled according to the identity identifier; subsequently, generate a track placard of the aircraft to be controlled at the placard position according to the flight plan information. This method uses track dynamic data as the control operation target, simplifies the number of auxiliary screens in the controller's operation process by generating track placards to display the core status information of the aircraft, reduces the controller's attention range and work fatigue, and improves the control efficiency and surface safety.

Description

Technical Field

[0001] The present invention relates to the field of aerospace transportation control technology, and in particular to a coordinated control method, device, equipment and storage medium for aircraft. Background Art

[0002] With the expansion of routes, the increase in the types of passenger and cargo aircraft, and the differences in the nature of flight missions, the workload of controllers has increased, and the procedural control mode of paper progress sheets is difficult to meet the complex flight missions and safety requirements. Since 2001, large airports have gradually introduced tower automation control systems with electronic progress sheets as the core.

[0003] However, with the improvement of living standards, the number of flights at major airports will continue to grow. The increase in the number of flights has put forward higher requirements for the efficiency of the use and command of airport surfaces and airspace. At the same time, the increasing attention to safety risks has also prompted airports to introduce new technologies that are conducive to improving safety and efficiency. At present, the domestic automated control system conducts control and command through electronic progress sheets. Because the electronic progress sheet is essentially a text of the aircraft's planned status, there are differences and lags with the actual dynamics of the scene, which poses a safety risk.

[0004] In summary, the problems existing in the prior art need to be solved urgently. Summary of the invention

[0005] The present invention provides a coordinated control method, device, equipment and storage medium for aircraft, which are used to solve the defects in the prior art and improve the control efficiency and scene safety.

[0006] The present invention provides a coordinated control method for aircraft, comprising:

[0007] Determine the sign position of the aircraft to be governed in the airport plan map through the track data, the track data is collected by one or more radar devices, and the sign position corresponds to the track of the aircraft to be governed in real time;

[0008] Determining the identity of the aircraft to be regulated by means of the radar equipment;

[0009] According to the identity identifier, searching for the flight plan information of the aircraft to be governed;

[0010] A track sign of the aircraft to be governed is generated at the sign position according to the flight plan information; the track sign displays first status information, and the first status information is used by the operating user to coordinate and control the target aircraft.

[0011] According to a method for coordinated control of an aircraft provided by the present invention, after the step of generating a track label of the target aircraft at the label position, the method further includes:

[0012] Determine the planned status of the aircraft to be controlled according to the flight plan information;

[0013] Screen the track label according to the planned status and the user management authority to obtain a target track label;

[0014] Highlight the target track label.

[0015] According to a method for coordinated control of an aircraft provided by the present invention, after the step of screening the track label according to the planned status and the user management authority, the method further includes:

[0016] Obtain a label operation instruction issued by an operating user;

[0017] In response to the label operation instruction, display second status information of the corresponding track label on a preset interface, and the content of the second status information is more than the content of the first status information;

[0018] In response to the label operation instruction, generate common operation options according to the flight plan information, and the common operation options are generated by sorting the operation options according to the usage priority.

[0019] According to a method for coordinated control of an aircraft provided by the present invention, after the step of screening the track label according to the planned status and the user management authority, the method further includes:

[0020] Obtain a label jurisdiction instruction issued by an operating user and used to wake up subsequent operation options;

[0021] In response to the label jurisdiction instruction, judge whether the operating user has jurisdiction according to the flight plan information;

[0022] When the operating user has jurisdiction, determine the switchable status of the target aircraft according to the flight plan information and the current status information of the target aircraft;

[0023] Generate the subsequent operation options according to the switchable status.

[0024] According to a method for coordinated control of an aircraft provided by the present invention, the step of generating subsequent operation options according to the switchable status specifically includes:

[0025] Based on the switchable state and the flight plan information, determine whether the operating user has jurisdiction over the spacecraft in the switchable state;

[0026] When the operating user has jurisdiction, switch the current state of the target aircraft to the switchable state.

[0027] According to a method for coordinated control of an aircraft provided by the present invention, the step of generating a track sign of the target aircraft at the sign position according to the flight plan information specifically includes:

[0028] Determine a set of state information of the target aircraft according to the flight plan information;

[0029] Determine the jurisdiction sector of the target aircraft according to the set of state information;

[0030] According to the jurisdiction sector, screen the first state information from the set of state information for display.

[0031] The present invention also provides an aircraft coordinated control device, including:

[0032] A position determination module, configured to determine the sign position of the aircraft to be jurisdictioned on the airport plane map through track data, where the track data is collected by one or more radar devices, and the sign position corresponds to the track of the aircraft to be jurisdictioned in real time;

[0033] An identity recognition module, configured to determine the identity identifier of the aircraft to be jurisdictioned through the radar device;

[0034] An information search module, configured to search for the aircraft plan information of the aircraft to be jurisdictioned according to the identity identifier;

[0035] A sign generation module, configured to generate a track sign of the aircraft to be jurisdictioned at the sign position according to the flight plan information; the track sign displays first state information, and the first state information is used for the operating user to perform coordinated control on the target aircraft.

[0036] The present invention also provides an electronic device, including a memory, a processor, and a computer program stored on the memory and executable on the processor, where when the processor executes the program, it implements the aircraft coordinated control method as described in any one of the above.

[0037] The present invention also provides a non-transitory computer-readable storage medium, on which a computer program is stored, and when the computer program is executed by a processor, it implements the aircraft coordinated control method as described in any one of the above.

[0038] The present invention also provides a computer program product, including a computer program which, when executed by a processor, implements the aircraft coordination control method as described in any one of the above.

[0039] The aircraft coordination control method, device, equipment and storage medium provided by the present invention determine the sign position of an aircraft to be controlled in an airport plane map through the track data collected by a radar device; then determine the identity identifier of the aircraft to be controlled through the radar device; then, according to the identity identifier, search for the flight plan information of the aircraft to be controlled; subsequently, generate a track sign of the aircraft to be controlled at the sign position according to the flight plan information. This method uses track dynamic data as the control operation target, and simplifies the number of auxiliary screens in the controller's operation process by generating track signs to display the core status information of the aircraft, reduces the controller's attention range and work fatigue, and improves the control efficiency and surface safety. Brief Description of the Drawings

[0040] In order to more clearly illustrate the technical solutions in the present invention or the prior art, the following will briefly introduce the drawings required for the description of the embodiments or the prior art. Obviously, the drawings in the following description are some embodiments of the present invention. For those of ordinary skill in the art, other drawings can be obtained based on these drawings without creative efforts.

[0041] Figure 1 is a schematic flowchart of the aircraft coordination control method provided by the present invention;

[0042] Figure 2 is a schematic structural diagram of the aircraft coordination control device provided by the present invention;

[0043] Figure 3 is a schematic structural diagram of the electronic device provided by the present invention. Detailed Embodiments

[0044] To make the objectives, technical solutions and advantages of the present invention clearer, the following will clearly and completely describe the technical solutions in the present invention with reference to the drawings in the present invention. Obviously, the described embodiments are some, but not all, of the embodiments of the present invention. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present invention without creative efforts fall within the scope of protection of the present invention.

[0045] In air traffic control, the tower is the key location for directing the takeoff and landing of aircraft. Traditional controllers visually direct flights and use paper flight progress strips to record flight information and control status. With the increase in flight routes and the variety of flight types, paper progress strips are difficult to meet the requirements of efficient control. Since 2001, large airports have introduced an automated control system with electronic progress strips as the core. This system improves control efficiency through standardized processes and convenient data sharing. However, since the electronic progress strip is essentially a text of the planned state of the aircraft, there are differences and lags with the actual situation on the ground, posing safety risks.

[0046] To solve the problems existing in the prior art, the present invention proposes a coordinated control method for aircraft to improve control efficiency and ground safety. The following describes the coordinated control method for the aircraft, as Figure 1 shown, including but not limited to the following steps:

[0047] Step 110: Determine the placard position of the aircraft to be controlled on the airport plane map through the track data, and the track data is collected by one or more radar devices.

[0048] In step 110, it is necessary to determine the position of the aircraft to be controlled on the electronic map based on the track data, where the aircraft to be controlled can be one or multiple. Specifically, the track data of the aircraft is collected by one or more radar devices. The track data includes information such as the position, speed, and heading of the aircraft. Then, the collected track data is processed, including data cleaning, noise removal, etc., to ensure the accuracy and reliability of the data. After data cleaning, the position of the aircraft is calculated through one or multiple paths of track data. The position information in the track data can be used, combined with information such as the speed and heading of the aircraft, and the actual position of the aircraft can be calculated using a mathematical model or algorithm. The placard position of the aircraft is determined on the airport plane map, usually corresponding to the current position of the aircraft. The placard position can be represented by symbols or icons, and relevant information of the aircraft, such as flight number, destination, etc., can be marked on it. It can be understood that different styles and colors of placards can be drawn to facilitate the distinction by the controller.

[0049] Step 120: Determine the identity identifier of the aircraft to be controlled through the radar device.

[0050] In step 110, the spacecraft can be displayed on the electronic map, but only that there is a spacecraft at that location is known, and the identity information of the spacecraft is not known. Therefore, in step 120, it is necessary to obtain the identity identifier of the aircraft through the radar device. Specifically, a transponder is carried on the spacecraft. When the ground radar sends an interrogation signal to the spacecraft, the transponder will receive the signal and send a response, which contains the identification information of the spacecraft, such as a secondary response code, a 24-bit address code, a flight number, etc. After the ground radar receives the response signal, it can determine the identification information of the aircraft.

[0051] It can be understood that it can also be obtained through ADS-B. ADS-B is an avionics device that can broadcast its position, speed, and other relevant information on the aircraft. The ADS-B information contains the identification information of the aircraft, such as the ICAO 24-bit address code (ICAO 24 address), etc. The ground station can receive and decode the ADS-B information to obtain the identification information of the spacecraft.

[0052] Step 130: According to the identity identifier, search for the flight plan information of the aircraft to be jurisdictioned.

[0053] In step 120, the identity identifier of the spacecraft has been obtained. Therefore, in step 130, only according to the identity identifier of the spacecraft, the corresponding flight plan information of the spacecraft can be matched. Specifically, find the corresponding query page or function in the system, input the identity identifier of the aircraft to be queried, and execute the query operation. The system will return the flight plan information related to the aircraft, such as the flight number, takeoff and landing time, flight route, expected flight altitude, etc.

[0054] Step 140: According to the flight plan information, generate a track label of the aircraft to be jurisdictioned at the label position; the track label displays first status information, and the first status information is used for the operating user to conduct coordinated control of the target aircraft.

[0055] A track label usually refers to a label or sign used in an air traffic control system to display the track and related information of an aircraft, which is a virtual label on an electronic display screen. In step 140, according to the flight plan information, a track label of the target aircraft can be generated at the label position, and the first status information is displayed on the label. This information is used for the operating user to conduct coordinated control of the target aircraft. The first status information may include information such as the altitude, speed, and heading of the aircraft, as well as any situations that require special attention or coordination. According to the information displayed on the track label, the operating user can conduct coordinated control, including adjusting the flight plan, providing route guidance, coordinating air traffic, etc., to ensure the safe flight and smooth operation of the target aircraft.

[0056] The coordinated control method for an aircraft provided by the present invention determines the placard position of an aircraft to be controlled in an airport plane map based on the track data collected by a radar device; then determines the identity identifier of the aircraft to be controlled through the radar device; then looks up the flight plan information of the aircraft to be controlled according to the identity identifier; and subsequently generates a track placard of the aircraft to be controlled at the placard position according to the flight plan information. This method uses track dynamic data as the target of control operations, and simplifies the number of auxiliary screens in the controller's operation process by generating track placards to display the core status information of the aircraft, reduces the controller's attention range and work fatigue, and improves control efficiency and surface safety.

[0057] As a further optional embodiment, after the step of generating a track placard of the target aircraft at the placard position, the method further includes:

[0058] Determine the planned status of the aircraft to be controlled according to the flight plan information;

[0059] Screen the track placard according to the planned status and user management authority to obtain a target track placard;

[0060] Highlight the target track placard.

[0061] In this embodiment, after generating the track placard of the target aircraft, according to the flight plan information, the track placard can be further screened and highlighted to facilitate the user to more easily manage and monitor the operation of the aircraft. Screen the track placard according to the planned status and the user's management authority, and only display the target track placards that meet the conditions. For example, when the user permission indicates that the user is a controller at the release desk, the aircraft that has not taken off can be screened out according to the planned takeoff time and the current time. Highlight the target track placards that meet the conditions to make it easier for the user to identify and monitor. The highlighting can be carried out in different ways such as using different colors, fonts or icons to highlight the target track placards.

[0062] Preferably, in actual applications, the controller needs to face all the aircraft on the airport. To facilitate the controller to quickly identify the flights that need to be controlled by himself, the placards can be differentially displayed according to information such as track status, planned status, and control jurisdiction status. For example, use a specific color (such as blue) and a dynamic icon to indicate that the aircraft is in flight; or use gray to display the track placards of the landed aircraft to indicate that it has completed the flight mission; or use orange to mark the delayed track placards and add the corresponding delay time information; or use the default color to display the track placards within the jurisdiction to ensure that the controller can clearly identify the flights within his jurisdiction, and use a light color to display the track placards of other jurisdictions, but still retain the basic information for reference.

[0063] It is understandable that controllers in different positions handle different flights. For example, after a flight is boarded and the cabin door is closed, the captain will apply to the release desk for release. When the release desk determines that the time is appropriate, it will approve the release. The planned status will then change to apron relationship, preparing for pushback. After pushback, the ground desk will conduct taxiing guidance.

[0064] As a further optional embodiment, after the step of screening the track signs according to the planned status and user management authority, the method further includes:

[0065] Obtain a sign operation instruction issued by an operating user;

[0066] In response to the sign operation instruction, display second status information of the corresponding track sign on a preset interface, where the content of the second status information is more than that of the first status information;

[0067] In response to the sign operation instruction, generate common operation options according to the flight plan information, where the common operation options are generated by sorting the operation options according to the usage priority.

[0068] In this embodiment, the operating user can issue a sign operation instruction to obtain more information and operate on the track sign. The user can click on the track sign on the electronic map to trigger the sign operation instruction to obtain more information or perform specific operations. In response to the sign operation instruction, the system will display the second status information of the corresponding track sign on a preset interface. The content of the second status information is more than that of the first status information, and may include detailed flight information of the aircraft, the current route and flight segment, the estimated arrival time, etc. In response to the sign operation instruction, the system will also generate common operation options according to the flight plan information. These options are generated by sorting according to the usage priority, so that the operating user can quickly select and execute common control commands, such as changing the route, providing air traffic guidance, etc.

[0069] As a further optional embodiment, after the step of screening the track signs according to the planned status and user management authority, the method further includes:

[0070] Obtain a sign jurisdiction instruction issued by the operating user and used to wake up subsequent operation options;

[0071] In response to the sign jurisdiction instruction, judge whether the operating user has jurisdiction according to the flight plan information;

[0072] When the operating user has jurisdiction, determine the switchable states of the target aircraft according to the flight plan information and the current status information of the target aircraft;

[0073] Generate subsequent operation options according to the switchable states.

[0074] In this embodiment, the operating user can issue a sign jurisdiction instruction, which is used to wake up subsequent operation options. The controller can generate a sign jurisdiction instruction by clicking on the sign with an input device such as a mouse. Subsequently, the system will determine whether the user who issues the sign jurisdiction instruction has jurisdiction. When the operating user has jurisdiction, the system determines the switchable states of the target aircraft according to the flight plan information and the current status information of the target aircraft. These states may include waiting for takeoff, in flight, about to land, etc. According to the switchable states, the system generates subsequent operation options. For example, for an aircraft waiting for takeoff, the operation options may include confirming the takeoff time, adjusting the takeoff sequence, etc.; for an aircraft in flight, the operation options may include providing air traffic guidance, adjusting the flight route, etc.

[0075] The core control operations are state switching and position handover. The essence of state switching is to perform the transition state under the jurisdiction of the position, which has a certain correlation with position handover. Its calculation logic is as follows:

[0076] (1) Check the takeoff and landing type of the current flight and the current position jurisdiction status, and determine whether the current operating user has jurisdiction.

[0077] (2) If jurisdiction is available, query the surface control sector operation process based on the target takeoff and landing type, aircraft position, and takeoff and landing runway, and query the flight status change process from this sector operation process.

[0078] (3) Check the position where the current target plan status is located, determine the target's next permission switch state, and sort it by priority (system configuration, the more commonly used, the higher the priority) to complete the state switching query.

[0079] (4) According to the status of the next operation, query the control sector to which the status belongs, and determine whether this sector belongs to the current control position. If not, record the position handover target.

[0080] (5) According to the status of the next operation, check whether it is necessary to set information such as the approach flight mode, departure intersection, crossing intersection, and handover position while switching states, and merge it into the next operation options.

[0081] (6) According to the query results of steps (3) and (4), package and generate state switching and position handover operation options.

[0082] As a further optional embodiment, the step of generating subsequent operation options according to the switchable state specifically includes:

[0083] Based on the switchable state and the flight plan information, determine whether the operating user has jurisdiction over the spacecraft in the switchable state;

[0084] When the operating user has jurisdiction, switch the current state of the target aircraft to the switchable state.

[0085] In this embodiment, for the case where the jurisdiction over the aircraft is no longer available after the state is switched, an ad-hoc handover is performed - transfer the management authority to the next seat, and display the track label in light color, but still retain the basic information for reference.. It can be understood that after the seat handover, the controller no longer needs to control the aircraft. To simplify the interface, in this embodiment, the highlighting display of the track label of the target aircraft is cancelled, or the style and color of the track label can be changed to distinguish it from the aircraft that needs to be controlled.

[0086] As a further optional embodiment, the step of generating the track label of the target aircraft at the label position according to the flight plan information specifically includes:

[0087] Based on the flight plan information, determine the set of status information of the target aircraft;

[0088] Based on the set of status information, determine the jurisdiction sector of the target aircraft;

[0089] Based on the jurisdiction sector, screen the first status information from the set of status information for display.

[0090] In this embodiment, the set of status information refers to the set of all status information of the target aircraft. These status information include flight plan information, current position, flight altitude, speed, heading, estimated arrival time, etc. According to different jurisdiction sectors or operation requirements, specific status information that needs to be displayed or concerned can be screened from the set of status information to better manage and monitor the operation of the aircraft.

[0091] As a further optional embodiment, the controller selects control operations according to the actual on-site control needs:

[0092] (1) When the controller performs a state switch, the system calculates control instruction conflicts:

[0093] a. Detect whether the next state requires the use of apron facilities such as parking positions and runways

[0094] b. If necessary, check whether there are other aircraft using the target facility as well.

[0095] c. If the facility is being used jointly, check whether there are conflicts in the usage scenarios. For example, if the parking bay has been occupied, if the next state of this aircraft requires crossing the runway but there is an aircraft taking off or landing on the runway, or if the next state of this aircraft requires entering the runway for takeoff but there is an aircraft landing, etc. Conflicts in the parking bay may lead to congestion in surface operations and flight delays, while conflicts on the runway may cause safety accidents or pose safety risks.

[0096] d. If there are conflicts, remind the controller to confirm whether to perform this operation.

[0097] (2) When the controller performs an operation, the system backend automatically completes the data modification corresponding to the operation and updates and synchronizes it to all users:

[0098] a. Modify the flight plan data, such as the target state, jurisdiction seat, handover target seat, coordination information, etc.

[0099] b. Update information such as status identification, handover identification, coordination identification, etc.

[0100] c. Update the control guidance, such as the taxi route, waiting position, handover position, etc.

[0101] d. If there is a seat handover, check whether it is a cross-department handover. If so, prompt coordination and frequency change (notify the captain to leave the original control frequency band).

[0102] e. Complete other automated control processes, such as automatic transmission of messages, automatic allocation of parking bays and runways, nearest allocation of departure and crossing points, synthesis of control instructions, release and verification of control instructions.

[0103] The following describes the coordinated control device for an aircraft provided by the present invention. As Figure 2 shown, the coordinated control device for an aircraft described below can be correspondingly referred to the coordinated control method for an aircraft described above.

[0104] A coordinated control device for an aircraft, comprising:

[0105] A position determination module 210, configured to determine the label position of an aircraft to be jurisdiction in an airport plane map through track data, where the track data is collected by one or more radar devices;

[0106] An identity recognition module 220, configured to determine the identity label of the aircraft to be jurisdiction through the radar device;

[0107] An information search module 230, configured to search for the aircraft plan information of the aircraft to be jurisdiction according to the identity label;

[0108] A sign generation module 240, configured to generate a track sign of the aircraft to be controlled at the sign position according to the flight plan information; the track sign displays first status information, and the first status information is used for an operating user to perform coordinated control on the target aircraft.

[0109] Figure 3 An example of a schematic physical structure diagram of an electronic device is shown as Figure 3 shown. The electronic device may include: a processor 310, a communication interface 320, a memory 330, and a communication bus 340. Among them, the processor 310, the communication interface 320, and the memory 330 communicate with each other through the communication bus 340. The processor 310 may call logic instructions in the memory 330 to execute a method for coordinated control of an aircraft. The method includes:

[0110] Determine the sign position of the aircraft to be controlled in the airport plane map through track data, where the track data is collected by one or more radar devices;

[0111] Determine the identity identifier of the aircraft to be controlled through the radar device;

[0112] Find the flight plan information of the aircraft to be controlled according to the identity identifier;

[0113] Generate a track sign of the aircraft to be controlled at the sign position according to the flight plan information; the track sign displays first status information, and the first status information is used for an operating user to perform coordinated control on the target aircraft.

[0114] In addition, when the logic instructions in the above-mentioned memory 330 are implemented in the form of a software functional unit and sold or used as an independent product, they may be stored in a computer-readable storage medium. Based on such an understanding, the technical solution of the present invention essentially or the part that contributes to the prior art or a part of the technical solution may be embodied in the form of a software product. The computer software product is stored in a storage medium and includes several instructions for causing a computer device (which may be a personal computer, a server, or a network device, etc.) to execute all or part of the steps of the methods described in various embodiments of the present invention. The foregoing storage medium includes: various media such as a USB flash drive, a mobile hard disk, a read-only memory (ROM, Read-Only Memory), a random access memory (RAM, Random Access Memory), a magnetic disk, or an optical disc that can store program codes.

[0115] On the other hand, the present invention also provides a computer program product, which includes a computer program that can be stored on a non-transitory computer-readable storage medium. When the computer program is executed by a processor, the computer can execute the aircraft coordination control method provided by the above-mentioned various methods, and the method includes:

[0116] Determine the placard position of the aircraft to be controlled in the airport plane map through the track data, and the track data is collected by one or more radar devices;

[0117] Determine the identity identifier of the aircraft to be controlled through the radar device;

[0118] Search for the flight plan information of the aircraft to be controlled according to the identity identifier;

[0119] Generate a track placard of the aircraft to be controlled at the placard position according to the flight plan information; the track placard displays first status information, and the first status information is used for the operating user to perform coordination control on the target aircraft.

[0120] On another aspect, the present invention also provides a non-transitory computer-readable storage medium, on which a computer program is stored. When the computer program is executed by a processor, it is implemented to execute the aircraft coordination control method provided by the above-mentioned various methods, and the method includes:

[0121] Determine the placard position of the aircraft to be controlled in the airport plane map through the track data, and the track data is collected by one or more radar devices;

[0122] Determine the identity identifier of the aircraft to be controlled through the radar device;

[0123] Search for the flight plan information of the aircraft to be controlled according to the identity identifier;

[0124] Generate a track placard of the aircraft to be controlled at the placard position according to the flight plan information; the track placard displays first status information, and the first status information is used for the operating user to perform coordination control on the target aircraft.

[0125] The device embodiments described above are merely illustrative. The units described as separate components may or may not be physically separated, and the components shown as units may or may not be physical units, that is, they may be located in one place or distributed to multiple network units. Some or all of the modules can be selected according to actual needs to achieve the purpose of the solution of this embodiment. Those of ordinary skill in the art can understand and implement it without creative labor.

[0126] Through the description of the above embodiments, those skilled in the art can clearly understand that each embodiment can be implemented by means of software plus a necessary general hardware platform, and of course, it can also be implemented by hardware. Based on such an understanding, the essence of the above technical solution, or the part that contributes to the prior art, can be embodied in the form of a software product. This computer software product can be stored in a computer-readable storage medium, such as ROM / RAM, magnetic disk, optical disk, etc., and includes several instructions for causing a computer device (which can be a personal computer, a server, or a network device, etc.) to execute the methods described in each embodiment or some parts of the embodiments.

[0127] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention, rather than to limit them; although the present invention has been described in detail with reference to the foregoing embodiments, those of ordinary skill in the art should understand that they can still modify the technical solutions described in the foregoing embodiments, or perform equivalent replacements for some of the technical features; and these modifications or replacements do not make the essence of the corresponding technical solutions deviate from the spirit and scope of the technical solutions of the embodiments of the present invention.

Claims

1. A coordinated control method for an aircraft, characterized in that, Including: Determine the sign position of the aircraft to be managed in the airport plane map through the track data, where the track data is collected by one or more radar devices, and the sign position corresponds in real time to the track of the aircraft to be managed; Determine the identity identifier of the aircraft to be managed through the radar device; Search for the flight plan information of the aircraft to be managed according to the identity identifier; Generate a track sign of the aircraft to be managed at the sign position; the track sign displays first status information, and the first status information is used for the operating user to conduct coordinated control over the aircraft to be managed; After the step of generating the track sign of the aircraft to be managed at the sign position, the method further includes: Determine the planned status of the aircraft to be managed according to the flight plan information; Filter the track signs according to the planned status and the user management authority to obtain target track signs; Highlight the target track signs; The step of highlighting the target track signs includes: Highlight the target track signs through color, font or icon; After the step of filtering the track signs according to the planned status and the user management authority, the method further includes: Obtain a sign operation instruction issued by the operating user; In response to the sign operation instruction, display second status information of the corresponding track sign on a preset interface, and the content of the second status information is more than the content of the first status information; In response to the sign operation instruction, generate common operation options according to the flight plan information, and the common operation options are generated by sorting the operation options according to the usage priority; Wherein, the second status information includes the detailed flight information of the aircraft, the current route and flight segment, and the estimated arrival time; the common operation options include: status switching and seat handover; After the step of filtering the track signs according to the planned status and the user management authority, the method further includes: Obtain a sign jurisdiction instruction issued by the operating user and used to wake up subsequent operation options; In response to the sign jurisdiction instruction, judge whether the operating user has jurisdiction according to the flight plan information; When the operating user has jurisdiction, determine the switching status of the aircraft to be managed according to the flight plan information and the current status information of the aircraft to be managed; Generate the subsequent operation options according to the switching status; The step of generating subsequent operation options according to the switching status specifically includes: Judge whether the operating user has jurisdiction over the aircraft in the switching status according to the switching status and the flight plan information; When the operating user has jurisdiction, switch the current status of the aircraft to be managed to the switching status; Check the current flight takeoff and landing type and the current seat jurisdiction status, and judge whether the current operating user has jurisdiction; If there is jurisdiction, query the surface control sector operation process based on the target takeoff / landing type, aircraft position, and runway, and query the flight status change process from this sector operation process; Check the position of the current target plan status, determine the next permission switching status of the target, sort by priority, and complete the status switching query; According to the status of the next operation, query the control sector to which the status belongs, and determine whether this sector belongs to the current control seat. If not, record the target of seat handover; According to the status of the next operation, check whether it is necessary to set the approach flight mode, departure intersection, crossing intersection, and handover position information while switching the status, and merge them into the next operation option.

2. The coordinated control method for an aircraft according to claim 1, characterized in that The step of generating the track sign of the aircraft to be controlled at the sign position according to the flight plan information specifically includes: Determine the set of status information of the aircraft to be controlled according to the flight plan information; Determine the control sector of the aircraft to be controlled according to the set of status information; According to the control sector, screen the first status information from the set of status information for display.

3. An aircraft coordinated control device, characterized in that, Including: A position determination module for determining the sign position of the aircraft to be controlled on the airport plane map through track data, where the track data is collected by one or more radar devices, and the sign position corresponds to the track of the aircraft to be controlled in real time; An identity recognition module for determining the identity identifier of the aircraft to be controlled through the radar device; An information search module for searching for the flight plan information of the aircraft to be controlled according to the identity identifier; A sign generation module for generating the track sign of the aircraft to be controlled at the sign position according to the flight plan information; the track sign displays the first status information, and the first status information is used for the operating user to conduct coordinated control of the aircraft to be controlled; After the step of generating the track sign of the aircraft to be controlled at the sign position, it further includes: Determine the planned status of the aircraft to be controlled according to the flight plan information; Screen the track sign according to the planned status and the user management authority to obtain the target track sign; Highlight the target track sign; The step of highlighting the target track sign includes: Highlight the target track sign through color, font, or icon; After the step of screening the track sign according to the planned status and the user management authority, it further includes: Obtain a sign operation instruction issued by the operating user; In response to the sign operation instruction, display the second status information of the corresponding track sign on a preset interface, and the content of the second status information is more than the content of the first status information; In response to the sign operation instruction, generate common operation options according to the flight plan information, and the common operation options are generated by sorting the operation options according to the usage priority; Wherein, the second status information includes the detailed flight information of the aircraft, the current route and flight segment, and the estimated arrival time; the common operation options include: status switching and seat handover; After the step of screening the track signs according to the planned status and user management authority, the following steps are further included: Obtain a sign jurisdiction instruction, which is issued by an operating user and is used to wake up subsequent operation options; In response to the sign jurisdiction instruction, judge whether the operating user has jurisdiction authority according to the flight plan information; When the operating user has jurisdiction authority, determine the switching state of the aircraft to be jurisdiction according to the flight plan information and the current status information of the aircraft to be jurisdiction; Generate the subsequent operation options according to the switching state; The step of generating subsequent operation options according to the switching state specifically includes: Judge whether the operating user has jurisdiction authority over the aircraft in the switching state according to the switching state and the flight plan information; When the operating user has jurisdiction authority, switch the current state of the aircraft to be jurisdiction to the switching state; Check the takeoff and landing type of the current flight and the jurisdiction status of the current seat, and judge whether the current operating user has jurisdiction authority; If having jurisdiction authority, query the surface control sector operation process according to the target takeoff and landing type, aircraft position and landing / takeoff runway, and query the flight status change process from the sector operation process; Check the position where the current target plan status is located, determine the target next permission switching state, and sort by priority to complete the status switching query; According to the status of the next operation, query the control sector to which the status belongs, and determine whether the sector belongs to the current control seat. If not, record the seat handover target; According to the status of the next operation, check whether it is necessary to set the approach flight mode, departure crossing, passing crossing, and handover position information while switching the state, and merge them into the next operation option.

4. An electronic device, comprising a memory, a processor, and a computer program stored on the memory and running on the processor, characterized in that, When the processor executes the program, it implements the coordinated control method of the aircraft according to any one of claims 1 to 2.

5. A non-transitory computer-readable storage medium having a computer program stored thereon, characterized in that, When the computer program is executed by the processor, it implements the coordinated control method of the aircraft according to any one of claims 1 to 2.

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