Important flight mission monitoring method, equipment and medium

Abstract

The invention provides an important flight mission monitoring method and device, and a medium, and relates to the technical field of civil aviation. The method comprises the steps that an aircraft corresponding to an important flight task is determined, information of the aircraft is acquired, and the information comprises at least one of state information and position information; the area where the aircraft is located is determined according to the information, monitoring information corresponding to the aircraft is obtained according to the area, the monitoring information is displayed, and the monitoring information comprises at least one of situation information, voice monitoring information, control commander information and control site information. According to the embodiment of the invention, the whole process of an important flight task can be monitored, the integrity and timeliness of monitoring data are effectively improved, and the management requirements of the important flight task are effectively met.

Description

Technical Field

[0001] The present application relates to the field of civil aviation technology, and more specifically, to an important flight mission monitoring method, equipment, and medium. Background Art

[0003] The existing monitoring methods for important flight missions are to monitor important flight missions through air situation tracks or by receiving on-site duty calls. These monitoring methods can only monitor part of the process of important flight missions. The monitoring data is incomplete and has poor timeliness, which makes it difficult to meet the management requirements of important flight missions. Summary of the invention

[0004] The embodiments of the present application provide an important flight mission monitoring method, device, and medium, which can solve the problem that the existing important flight mission monitoring has incomplete monitoring data and poor timeliness, and is difficult to meet monitoring requirements. To achieve this purpose, the embodiments of the present application provide the following solutions.

[0005] According to one aspect of an embodiment of the present application, a method for monitoring an important flight mission is provided, the method comprising:

[0006] Determine an aircraft corresponding to an important flight mission, and obtain information of the aircraft, wherein the information includes at least one of status information and position information;

[0007] Determine the area where the aircraft is located based on the information, obtain monitoring information corresponding to the aircraft based on the area, and display the monitoring information, which includes at least one of situation information, voice monitoring information, control commander information, and control site information.

[0008] In a possible implementation, obtaining the status information of the aircraft includes:

[0009] The departure airport of the aircraft is determined according to the flight information of the aircraft, and the status data of the aircraft is obtained through the control tower of the departure airport.

[0010] In a possible implementation, determining the area where the aircraft is located according to the information, and acquiring the surveillance information corresponding to the aircraft according to the area includes:

[0011] If it is determined that the status information satisfies a first preset condition, the scene radar data of the departure airport is obtained, and the scene situation information is displayed based on the scene radar data and the map data of the departure airport, wherein the first preset condition includes that the status of the aircraft is one of door closing, start application, wheel block withdrawal, push-out start, and taxiing, and the scene situation information includes a scene surveillance screen of the departure airport and the aircraft is displayed on the scene surveillance screen.

[0012] In a possible implementation, determining the area where the aircraft is located according to the information, and acquiring the surveillance information corresponding to the aircraft according to the area includes:

[0013] If it is determined that the status information does not satisfy the first preset condition, then when it is determined that the status information is take-off but not landed, flight dynamic information is obtained, the jurisdiction corresponding to the aircraft is determined according to the flight dynamic information, and air situation information is displayed based on the data of the jurisdiction, the air situation information includes a flight situation screen, and the aircraft is displayed on the flight situation screen.

[0014] In a possible implementation, the information includes location information, and determining the area where the aircraft is located according to the information, and acquiring the monitoring information corresponding to the aircraft according to the area, includes:

[0015] If the aircraft is determined to be within the airport according to the location information, the command seat of the aircraft is determined according to the status information of the aircraft, the voice channel number corresponding to the command seat is obtained, and the voice monitoring information is obtained according to the voice channel number.

[0016] In a possible implementation, determining the area where the aircraft is located according to the information, and acquiring the surveillance information corresponding to the aircraft according to the area includes:

[0017] If it is determined according to the location information that the aircraft is not within the airport range, the command seat corresponding to the aircraft is determined according to the flight dynamic information of the aircraft, and the voice monitoring information is obtained according to the voice channel number corresponding to the command seat.

[0018] In a possible implementation, determining the command seat corresponding to the aircraft according to the flight dynamic information of the aircraft includes:

[0019] The air region where the aircraft is located is determined according to the flight dynamic information, the range to which the aircraft belongs is obtained based on radar information of the air region, and the corresponding command seat is determined according to the range, wherein the range includes any one of a terminal range and an area range.

[0020] In a possible implementation, the range to which the aircraft belongs is a regional range, and obtaining the control commander information includes:

[0021] Determine the control commander corresponding to the aircraft according to the command seat and the shift information, and obtain the information of the control commander;

[0022] Obtaining the control site information, including:

[0023] The location of the management object corresponding to the command seat is obtained, and the information of the management object is collected according to the location.

[0024] According to one aspect of an embodiment of the present application, an electronic device is provided, including a memory, a processor, and a computer program stored in the memory, wherein the processor executes the computer program to implement the steps of the method described above.

[0025] According to one aspect of an embodiment of the present application, a computer-readable storage medium is provided, on which a computer program is stored. When the computer program is executed by a processor, the steps of the method described above are implemented.

[0026] The beneficial effects of the technical solution provided by the embodiment of the present application are:

[0027] The important flight mission monitoring method provided in the present application determines the aircraft corresponding to the important flight mission, obtains the information of the aircraft, and the information includes at least one of status information and position information; determines the area where the aircraft is located based on the information, obtains the monitoring information corresponding to the aircraft based on the area, and displays at least one of situation information, voice monitoring information, control commander information, and control site information. The embodiment of the present application can determine the position of the aircraft based on the aircraft information, and then obtain the monitoring information of the aircraft based on the position, so that the entire process of the important flight mission can be monitored, effectively improving the integrity and timeliness of the monitoring data, and effectively meeting the management requirements of important flight missions. BRIEF DESCRIPTION OF THE DRAWINGS

[0028] In order to more clearly illustrate the technical solutions in the embodiments of the present application, the following is a brief introduction to the drawings required for use in describing the embodiments of the present application.

[0029] Figure 1 A flowchart of an important flight mission monitoring method provided in an embodiment of the present application;

[0030] Figure 2 A flowchart of situation information acquisition in an important flight mission monitoring method provided in an embodiment of the present application;

[0031] Figure 3A flowchart of obtaining voice monitoring information, control command personnel information, and control site information in an important flight mission monitoring method provided in an embodiment of the present application;

[0032] Figure 4 A structural diagram of an electronic device provided in an embodiment of the present application. DETAILED DESCRIPTION

[0033] The embodiments of the present application are described below in conjunction with the drawings in the present application. It should be understood that the implementation methods described below in conjunction with the drawings are exemplary descriptions for explaining the technical solutions of the embodiments of the present application and do not constitute a limitation on the technical solutions of the embodiments of the present application.

[0034] It will be understood by those skilled in the art that, unless specifically stated, the singular forms "one", "said", and "the" used herein may also include plural forms. It should be further understood that the terms "including" and "comprising" used in the embodiments of the present application refer to that the corresponding features can be implemented as the presented features, information, data, steps, operations, elements and / or components, but do not exclude the implementation of other features, information, data, steps, operations, elements, components and / or combinations thereof supported by the technical field. It should be understood that when we say that an element is "connected" or "coupled" to another element, the one element may be directly connected or coupled to the other element, or it may refer to that the one element and the other element establish a connection relationship through an intermediate element. In addition, the "connection" or "coupling" used herein may include wireless connection or wireless coupling. The term "and / or" used herein indicates at least one of the items defined by the term, for example, "A and / or B" indicates that it is implemented as "A", or is implemented as "A", or is implemented as "A and B".

[0035] In order to make the objectives, technical solutions and advantages of the present application clearer, the implementation methods of the present application will be further described in detail below in conjunction with the accompanying drawings.

[0036] The following describes several exemplary embodiments to illustrate the technical solutions of the embodiments of the present application and the technical effects produced by the technical solutions of the present application. It should be noted that the following embodiments can refer to, draw on or combine with each other, and the same terms, similar features and similar implementation steps in different embodiments will not be described repeatedly.

[0037] The important flight mission monitoring method, device, and medium provided in this application are intended to solve at least one technical problem existing in the prior art.

[0038] The embodiment of the present application provides an important flight mission monitoring method, which can be used for managing a smart terminal of a flight mission. The smart terminal can be a mobile phone, a computer, a server, a cloud platform, or other physical or virtual objects.

[0039] The important flight mission monitoring method of this application can provide the civil aviation operation supervision department with a comprehensive and full-chain real-time tracking and monitoring channel for important flight missions. This application collects real-time data such as flight plans, flight dynamics, control site call voice, air radar, scene surveillance radar, duty site video, on-site duty, etc. for processing, integrating the entire process of important flight mission support into a unified environment and dynamically correlating and aligning them. By automatically collecting important flight missions within the jurisdiction or manually adding them, they can be focused on; according to the flight trajectory and flight phase of important flight missions, the flight situation, controller calls, controller qualifications and capabilities, on-duty site conditions, and flight status passing through each jurisdiction are tracked and displayed.

[0040] Alternatively, if Figure 1-Figure 3 As shown, the important flight mission monitoring method of the present application includes:

[0041] S101: Determine the aircraft corresponding to the important flight mission and obtain the aircraft information.

[0042] Optionally, the information includes at least one of status information and location information. According to the status information and location information, situation information, voice monitoring information, control commander information, and control site information related to the aircraft are obtained to facilitate real-time monitoring of aircraft related to important flight missions.

[0043] Optionally, after obtaining the important flight mission, the aircraft corresponding to the important flight mission can be obtained through the flight plan information. The aircraft information can also be included in the important flight mission information, and the aircraft information is obtained according to the obtained important flight mission information.

[0044] Optionally, obtaining the status information of the aircraft includes: determining the departure airport of the aircraft according to the flight information of the aircraft, and obtaining the status data of the aircraft through the control tower of the departure airport.

[0045] In one embodiment, the flight information of the aircraft is obtained through the flight plan information, the departure airport of the aircraft is checked according to the flight information, and the status data of the aircraft is obtained from the control tower of the departure airport. The status data of the aircraft can be obtained through an automated information system installed in the control tower.

[0046] Optionally, the status data includes one of door closing, start application, gear removal, start push, taxiing, take-off, cruising, and landing. The current status of the aircraft can be identified through the status data, and then the area (such as an airport or air area) where the aircraft is located can be determined according to the status, and a corresponding monitoring information acquisition method can be adopted based on the area.

[0047] Alternatively, the position of the aircraft can be obtained through the aircraft-related control system and the aircraft status. Once the aircraft takes off, the control system will capture the longitude and latitude of the aircraft and determine the longitude and latitude as the position of the aircraft in the air. If the control system does not output longitude and latitude data, the position of the aircraft at the airport is determined in combination with the flight status, such as whether it is on the taxiway or the runway.

[0048] S102: Determine the area where the aircraft is located based on the information, obtain monitoring information corresponding to the aircraft based on the area, and display the monitoring information.

[0049] Optionally, the monitoring information includes at least one of situation information, voice monitoring information, control command personnel information, and control site information.

[0050] Optionally, when the monitoring information is situation information, the area where the aircraft is located is determined according to the information, and the monitoring information corresponding to the aircraft is obtained according to the area, including: if it is determined that the status information meets the first preset condition, the scene radar data of the departure airport is obtained, and the scene situation information is displayed according to the scene radar data and the map data of the departure airport, the first preset condition includes that the state of the aircraft is one of the following: door closing, start application, wheel block withdrawal, push start, taxiing, the scene situation information includes the scene monitoring screen of the departure airport and the aircraft is displayed on the scene monitoring screen. Among them, the aircraft can be highlighted by highlighting the identification of the aircraft.

[0051] Optionally, the aircraft logo may be highlighted by displaying it in a specific color, flashing the logo, displaying the aircraft logo in the center of the scene monitoring screen, and the like.

[0052] In one embodiment, when it is determined that the state information satisfies the first preset condition, it is determined that the aircraft is ready to take off, that is, the aircraft is in the airport. The real-time scene surveillance radar data (i.e., scene radar data) of the departure airport is received and processed, and the scene radar data is combined with the map data of the departure airport to obtain scene situation information. The scene surveillance screen of the departure airport is displayed according to the scene situation information, and the identification of the aircraft is highlighted in the scene surveillance screen.

[0053] Optionally, if it is determined that the status information does not meet the first preset condition, then when it is determined that the status information is taken off but not landed, flight dynamic information is obtained, the jurisdiction corresponding to the aircraft is determined according to the flight dynamic information, and the air situation information is displayed based on the data of the jurisdiction, the air situation information includes a flight situation screen, and the aircraft is displayed on the flight situation screen. The jurisdiction may be a command sector for managing the aircraft.

[0054] Optionally, if it is determined through status information that the aircraft has landed, it is determined that the monitoring task of the important flight mission is completed.

[0055] Optionally, the data of the jurisdiction include air radar data, automation data and boundary data of the jurisdiction, wherein the automation data include the aircraft's planned route, actual route, sector opening and closing data, the aircraft's own information such as aircraft number, aircraft model, take-off and landing locations, expected take-off time, expected landing time, actual take-off time and other data related to the important flight mission.

[0056] In one embodiment, Figure 2 As shown, if it is determined based on the acquired status information that the aircraft has taken off but not landed, the flight dynamic information corresponding to the aircraft is obtained, and the passing situation of the aircraft's waypoints is queried from the flight dynamic information. The position of the aircraft's most recent passed waypoint is determined based on the passing situation, and the scope of the route jurisdiction of the current aircraft is obtained based on the position (when the aircraft is flying, it flies according to the assigned route. There are many waypoints on the route, which will have longitude and latitude coordinates. These waypoints will fall within the command sector. The command sector where the point is located can be found based on the most recent passed waypoint), and the radar data of the jurisdiction is obtained. The air situation information is displayed based on the radar data, automation data, and boundary data of the jurisdiction.

[0057] Optionally, the flight situation picture includes an air map, sector boundaries, air routes and other data captured by the radar. The aircraft's logo is prominently displayed in the flight situation picture.

[0058] Optionally, real-time control and command conversations related to important flight missions can also be monitored based on the status information and location information. The area where the aircraft is located is determined based on the information, and the monitoring information corresponding to the aircraft is obtained based on the area, including: if the aircraft is determined to be within the airport range based on the location information, the command seat of the aircraft is determined based on the aircraft status information, the voice channel number corresponding to the command seat is obtained, and the voice monitoring information is obtained based on the voice channel number. The location information may include information on the real-time location of the aircraft.

[0059] Optionally, if the aircraft status is determined to be one of the following states: "door closed", "application for start", "wheel block withdrawal", or "start push", then the command seat of the aircraft can be determined to be the apron control seat; if the status is "taxiing", then the command seat of the aircraft can be determined to be the ground seat, otherwise it is the tower seat. After the command seat of the aircraft is determined, the voice channel number of the command seat corresponding to the aircraft is determined based on the command seat and pre-stored control voice basic configuration data, and the voice stream data in the voice channel corresponding to the voice channel number is monitored to obtain voice monitoring information.

[0060] Optionally, the control voice basic configuration data stores the correspondence between the command seat and the voice channel number, and the voice channel number corresponding to each command seat is queried according to the correspondence.

[0061] Optionally, when it is determined based on the location information that the aircraft is not within the airport, the area where the aircraft is located is determined based on the information, and monitoring information corresponding to the aircraft is obtained based on the area, including: if it is determined based on the location information that the aircraft is not within the airport, then the command seat corresponding to the aircraft is determined based on the aircraft's flight dynamics information, and voice monitoring information is obtained based on the voice channel number corresponding to the command seat.

[0062] Optionally, the command seat corresponding to the aircraft is determined according to the flight dynamics information of the aircraft, including: determining the air region where the aircraft is located according to the flight dynamics information, obtaining the range to which the aircraft belongs based on radar information of the air region, and determining the corresponding command seat according to the range, wherein the range includes any one of a terminal range and an area range.

[0063] Optionally, the flight dynamic information includes the aircraft's passing point (such as the most recently passed waypoint), and the current air region where the aircraft is located is determined based on the passing point, and radar data corresponding to the air region is received. The aircraft's altitude information is obtained based on the radar data, and the altitude information is used to determine whether the air region belongs to the terminal range or the regional range.

[0064] Optionally, the terminal range is a medium and low altitude area, which may be a range of 300 meters to 6000 meters in vertical altitude, and the area range is a high altitude area, which may be a range of more than 6000 meters in vertical altitude.

[0065] Alternatively, if Figure 3 As shown, if it is a terminal range, the automation data of the terminal range is received, the command sector of the aircraft is determined based on the automation data, and the command seat corresponding to the command sector where the aircraft is located is calculated according to the fan opening and closing data of the terminal range; if it is an area range, the automation data of the area under the jurisdiction of the aircraft is received, the command sector is determined based on the automation data, and the command seat corresponding to the command sector where the aircraft is located is calculated according to the fan opening and closing data of the area range.

[0066] Optionally, after determining the command seat corresponding to the command sector where the aircraft is located, the voice channel number corresponding to the command seat is determined based on the data of the command seat and the pre-stored basic configuration data of the control voice, and the voice stream data of the command sector where the current aircraft is located is obtained through the voice channel number, so as to use the obtained voice stream data to monitor the call instructions of the on-site control commander.

[0067] Optionally, the conversation content between the controller and the pilot at the command seat is monitored through voice stream data, so as to obtain the current workload of the controller based on the conversation content to prevent the controller from being overloaded.

[0068] Optionally, when the scope to which the aircraft belongs is a regional scope, the control command personnel information is obtained, including: determining the control command personnel corresponding to the aircraft based on the command seat and scheduling information, and obtaining the control command personnel information; obtaining control site information, including: obtaining the location of the management object corresponding to the command seat, and collecting the management object information based on the location.

[0069] Optionally, the scheduling information may include the scheduling and handover information of the control commander corresponding to the command seat, and the control commander of the area (command sector) where the aircraft corresponding to the important flight mission is currently located is determined based on the scheduling and handover information.

[0070] Optionally, the information of the control and command personnel includes basic information of the control and command personnel (such as name, contact information, etc.), qualification information, ability information (part of which is preset data, and the other part can be adjusted according to the current workload of the control and command personnel), working hours, foreman information and other information related to the work of the control and command personnel.

[0071] Optionally, the information of the operation department and department unit corresponding to the command seat can be obtained based on the operation management information of the management place to which the command seat belongs (including the information of the operation department and department unit corresponding to each command seat), and the operation department and department unit can be determined as the management object corresponding to the command seat. The camera used to collect the image of the management object is determined according to the location of the management object. The camera is connected to obtain the real-time video stream of the camera, and the information of the management object is obtained through the real-time video stream. Among them, the camera configuration information corresponding to the location of the management object can be obtained, and the camera gateway can be accessed according to the camera configuration information. The on-site duty video stream of the sector where the current aircraft is located is obtained through the camera gateway, and the on-site duty video is monitored using the video stream.

[0072] The important flight mission monitoring method of the present application determines the aircraft corresponding to the important flight mission, obtains the information of the aircraft, and the information includes at least one of status information and position information; determines the area where the aircraft is located based on the information, obtains the monitoring information corresponding to the aircraft based on the area, and displays at least one of situation information, voice monitoring information, control commander information, and control site information. The embodiment of the present application can determine the position of the aircraft based on the aircraft information, and then obtain the monitoring information of the aircraft based on the position, so that the entire process of the important flight mission can be monitored, effectively improving the integrity and timeliness of the monitoring data, and effectively meeting the management requirements of important flight missions.

[0073] In an optional embodiment, an electronic device is provided, such as Figure 4 As shown, Figure 4 The electronic device 4000 shown includes: a processor 4001 and a memory 4003. The processor 4001 and the memory 4003 are connected, such as through a bus 4002. Optionally, the electronic device 4000 may also include a transceiver 4004, which may be used for data interaction between the electronic device and other electronic devices, such as data transmission and / or data reception. It should be noted that in actual applications, the transceiver 4004 is not limited to one, and the structure of the electronic device 4000 does not constitute a limitation on the embodiments of the present application.

[0074] Processor 4001 may be a CPU (Central Processing Unit), a general-purpose processor, a DSP (Digital Signal Processor), an ASIC (Application Specific Integrated Circuit), an FPGA (Field Programmable Gate Array), or other programmable logic devices, transistor logic devices, hardware components, or any combination thereof. It may implement or execute various exemplary logic blocks, modules, and circuits described in conjunction with the disclosure of this application. Processor 4001 may also be a combination that implements computing functions, such as a combination of one or more microprocessors, a combination of a DSP and a microprocessor, and the like.

[0075] The bus 4002 may include a path to transmit information between the above components. The bus 4002 may be a PCI (Peripheral Component Interconnect) bus or an EISA (Extended Industry Standard Architecture) bus. The bus 4002 may be divided into an address bus, a data bus, a control bus, etc. For ease of representation, only one thick line is used in the figure, but it does not mean that there is only one bus or one type of bus.

[0076] Memory 4003 can be ROM (Read Only Memory) or other types of static storage devices that can store static information and instructions, RAM (Random Access Memory) or other types of dynamic storage devices that can store information and instructions, or it can be EEPROM (Electrically Erasable Programmable Read Only Memory), CD-ROM (Compact Disc Read Only Memory) or other optical disk storage, optical disk storage (including compressed optical disk, laser disc, optical disk, digital versatile disc, Blu-ray disc, etc.), magnetic disk storage medium, other magnetic storage devices or any other medium that can be used to carry or store computer programs and can be read by a computer, without limitation here.

[0077] The memory 4003 is used to store the computer program for executing the embodiment of the present application, and the execution is controlled by the processor 4001. The processor 4001 is used to execute the computer program stored in the memory 4003 to implement the steps shown in the above method embodiment.

[0078] Among them, the electronic device can be any electronic product that can interact with an object, such as a personal computer, a tablet computer, a smart phone, a personal digital assistant (PDA), a game console, an interactive network television (IPTV), a smart wearable device, etc.

[0079] The electronic device may also include a network device and / or an object device, wherein the network device includes, but is not limited to, a single network server, a server group consisting of multiple network servers, or a cloud consisting of a large number of hosts or network servers based on cloud computing.

[0080] The network where the electronic device is located includes but is not limited to the Internet, a wide area network, a metropolitan area network, a local area network, a virtual private network (Virtual Private Network, VPN), etc.

[0081] An embodiment of the present application provides a computer-readable storage medium, which includes a computer program. When the computer program is executed by a processor, the steps and corresponding contents of the aforementioned method embodiment can be implemented.

[0082] An embodiment of the present application provides a computer program product, which includes a computer program. When the computer program is executed by a processor, the steps and corresponding contents of the aforementioned method embodiment can be implemented.

[0083] The terms "first", "second", "third", "fourth", "1", "2", etc. (if any) in the specification and claims of this application and the above-mentioned drawings are used to distinguish similar objects, and are not necessarily used to describe a specific order or sequence. It should be understood that the numbers used in this way can be interchanged where appropriate, so that the embodiments of the present application described herein can be implemented in an order other than that shown or described in the drawings.

[0084] It should be understood that, although each operation step is indicated by arrows in the flowchart of the embodiment of the present application, the implementation order of these steps is not limited to the order indicated by the arrows. Unless clearly stated herein, in some implementation scenarios of the embodiment of the present application, the implementation steps in each flowchart can be performed in other orders according to demand. In addition, some or all of the steps in each flowchart may include multiple sub-steps or multiple stages based on actual implementation scenarios. Some or all of these sub-steps or stages may be executed at the same time, and each sub-step or stage in these sub-steps or stages may also be executed at different times respectively. In different scenarios of execution time, the execution order of these sub-steps or stages may be flexibly configured according to demand, and the embodiment of the present application does not limit this.

[0085] The above is only an optional implementation method for some implementation scenarios of the present application. It should be pointed out that for ordinary technicians in this technical field, without departing from the technical concept of the solution of the present application, other similar implementation methods based on the technical ideas of the present application are also within the protection scope of the embodiments of the present application.

Claims

1. A method for monitoring important flight missions, characterized in that: The method comprises: Determine an aircraft corresponding to an important flight mission, and obtain information of the aircraft, wherein the information includes at least one of status information and position information; Determine the area where the aircraft is located based on the information, obtain monitoring information corresponding to the aircraft based on the area, and display the monitoring information, which includes at least one of situation information, voice monitoring information, control commander information, and control site information.

2. The important flight mission monitoring method according to claim 1, characterized in that: Obtaining the status information of the aircraft, including: The departure airport of the aircraft is determined according to the flight information of the aircraft, and the status data of the aircraft is obtained through the control tower of the departure airport.

3. The important flight mission monitoring method according to claim 2, characterized in that: The determining the area where the aircraft is located according to the information, and acquiring the monitoring information corresponding to the aircraft according to the area, includes: If it is determined that the status information satisfies a first preset condition, the scene radar data of the departure airport is obtained, and the scene situation information is displayed based on the scene radar data and the map data of the departure airport, wherein the first preset condition includes that the status of the aircraft is one of door closing, start application, wheel block withdrawal, push-out start, and taxiing, and the scene situation information includes a scene surveillance screen of the departure airport and the aircraft is displayed on the scene surveillance screen.

4. The important flight mission monitoring method according to claim 3 is characterized in that: The determining the area where the aircraft is located according to the information, and acquiring the monitoring information corresponding to the aircraft according to the area, includes: If it is determined that the status information does not satisfy the first preset condition, then when it is determined that the status information is take-off but not landed, flight dynamic information is obtained, the jurisdiction corresponding to the aircraft is determined according to the flight dynamic information, and air situation information is displayed based on the data of the jurisdiction, the air situation information includes a flight situation screen, and the aircraft is displayed on the flight situation screen.

5. The important flight mission monitoring method according to claim 1, characterized in that: The information includes location information, and determining the area where the aircraft is located according to the information, and acquiring monitoring information corresponding to the aircraft according to the area, includes: If the aircraft is determined to be within the airport according to the location information, the command seat of the aircraft is determined according to the status information of the aircraft, the voice channel number corresponding to the command seat is obtained, and the voice monitoring information is obtained according to the voice channel number.

6. The important flight mission monitoring method according to claim 5, characterized in that: The determining the area where the aircraft is located according to the information, and acquiring the monitoring information corresponding to the aircraft according to the area, includes: If it is determined according to the location information that the aircraft is not within the airport range, the command seat corresponding to the aircraft is determined according to the flight dynamic information of the aircraft, and the voice monitoring information is obtained according to the voice channel number corresponding to the command seat.

7. The important flight mission monitoring method according to claim 6, characterized in that: The step of determining the command seat corresponding to the aircraft according to the flight dynamic information of the aircraft includes: The air region where the aircraft is located is determined according to the flight dynamic information, the range to which the aircraft belongs is obtained based on radar information of the air region, and the corresponding command seat is determined according to the range, wherein the range includes any one of a terminal range and an area range.

8. The important flight mission monitoring method according to claim 7, characterized in that: The range to which the aircraft belongs is the regional range, and the control commander information is obtained, including: Determine the control commander corresponding to the aircraft according to the command seat and the shift information, and obtain the information of the control commander; Obtaining the control site information, including: The location of the management object corresponding to the command seat is obtained, and the information of the management object is collected according to the location.

9. An electronic device comprising a memory, a processor and a computer program stored in the memory, characterized in that: The processor executes the computer program to implement the steps of the method according to any one of claims 1 to 8.

10. A computer-readable storage medium having a computer program stored thereon, characterized in that: When the computer program is executed by a processor, the steps of the method according to any one of claims 1 to 8 are implemented.

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