Low-altitude airspace management system and method

Abstract

The invention provides a low-altitude airspace management system and method, and the system comprises a channel planning module which is used for determining a current flight channel of a target aircraft according to the flight data of the target aircraft and the target airspace data of a target low-altitude airspace through which the target aircraft passes; the flight adjustment module is used for adjusting the current flight state of the dangerous aircraft with the flight risk; the airspace coordination module is used for establishing real-time information sharing and controlling the multiple aircrafts to perform coordination work according to the shared information; and the fault response module is used for determining a target processing strategy of the fault aircraft for the fault aircraft with the fault condition, and processing the fault aircraft according to the target processing strategy. Therefore, an intelligent, efficient and safe low-altitude aircraft management scheme is provided, the flight safety can be guaranteed, and the airspace resource utilization rate can be improved.

Description

Technical Field

[0001] This application relates to the field of airspace management technology, and in particular to a management system and method for low-altitude airspace. Background Technology

[0002] With the rapid development of the low-altitude airspace, especially the widespread application of low-altitude aircraft such as drones and air taxis, the demand for low-altitude airspace has increased significantly. Low-altitude aircraft are widely used in logistics, air travel, agricultural spraying, environmental monitoring, and many other fields, greatly promoting economic and social progress. However, low-altitude aircraft face numerous challenges during flight, particularly in high-density flight environments, where issues such as mutual interference between aircraft, airway congestion, and insufficient airspace resources are becoming increasingly prominent.

[0003] Currently, there has been some technical research on flight path planning and airspace management for low-altitude aircraft, but most technologies are still in their initial stages and have some problems and shortcomings: Static airway planning problems. Traditional airway planning methods are usually static, meaning that airways and flight paths are fixed in advance and lack the ability to be dynamically adjusted. This method can easily lead to safety hazards such as airway congestion and aircraft collisions when there are many aircraft, diverse mission types, and complex airspace environments.

[0004] Lack of real-time adaptability. Existing low-altitude airspace control systems and airway allocation mechanisms typically rely on simple rules and models, making intelligent adjustments difficult. This results in slow response and limited effectiveness when faced with unexpected situations or airspace changes.

[0005] Insufficient airspace coordination. Most low-altitude aircraft's airspace control systems can only achieve one-way communication between the aircraft and the airspace management system. The coordination and information sharing mechanisms between aircraft are relatively weak, making it impossible to effectively avoid interference and conflicts between aircraft. In high-density flight environments, the lack of efficient coordination mechanisms will exacerbate flight safety hazards.

[0006] Therefore, how to intelligently perform dynamic flight path planning and allocation in complex low-altitude flight environments, enhance the coordination capabilities between aircraft, ensure flight safety, and improve the utilization rate of airspace resources has become an urgent technical challenge. Summary of the Invention

[0007] In view of this, the purpose of this application is to provide a management system and method for low-altitude airspace. Through the coordinated operation of a route planning module, a flight adjustment module, an airspace coordination module, and a fault response module, dynamic route planning and allocation can be carried out, improving the coordination capabilities between aircraft, ensuring flight safety, and increasing the utilization rate of airspace resources. This provides an intelligent, efficient, and safe low-altitude aircraft management solution and promotes the sustainable development of the low-altitude field.

[0008] This application provides a management system for low-altitude airspace, the management system comprising: The flight path planning module is used to determine the current flight path of the target aircraft based on the flight data of the target aircraft and the target airspace data of the target low-altitude airspace through which the target aircraft passes. The flight adjustment module is used to predict flight risks based on the flight data of each aircraft in the aircraft cluster, and to adjust the current flight status of dangerous aircraft with flight risks. The airspace coordination module is used to establish real-time information sharing between aircraft and between aircraft and the air traffic management system, and to control multiple aircraft to coordinate their work based on the shared information. The fault response module is used to monitor the fault status of the aircraft cluster in real time. For the faulty aircraft, it determines the target processing strategy for the faulty aircraft according to the specific fault status, and processes the faulty aircraft according to the target processing strategy.

[0009] Optionally, when the flight path planning module determines the current flight path of the target aircraft based on the target aircraft's flight data and the target airspace data of the target low-altitude airspace through which the target aircraft passes, the flight path planning module is used to: Acquire real-time flight data and planned flight data of the target aircraft; wherein, the real-time flight data includes the current position and current speed of the target aircraft, and the planned flight data includes the mission planning information of the target aircraft, the mission planning information including mission position planning information and mission priority; Based on the mission location planning information in the target aircraft's planned flight data, determine the target low-altitude airspace that the target aircraft will pass through, and obtain the target airspace data of the target low-altitude airspace. Based on the real-time flight data, planned flight data, and target airspace data, the current flight path of the target aircraft is determined according to a preset flight path planning algorithm.

[0010] Optionally, when the flight adjustment module is used to predict flight risks based on the flight data of each aircraft in the aircraft cluster and to adjust the current flight status of dangerous aircraft with flight risks, the flight adjustment module is used to: Based on the real-time flight data and planned flight data of each aircraft in the aircraft cluster, and combined with the obstacle information in the current airspace, identify whether there are overlapping aircraft in flight. Aircraft that have overlapping flight paths are identified as dangerous aircraft. For each dangerous aircraft, the current flight status of the dangerous aircraft is adjusted based on its flight data, the flight data of other aircraft besides the dangerous aircraft, and the current airspace conditions; wherein, adjusting the current flight status of the dangerous aircraft includes adjusting the flight data of the dangerous aircraft and / or adjusting the current flight path of the dangerous aircraft.

[0011] Optionally, the flight adjustment module is also used for: In response to a flight adjustment command, determine the aircraft to be adjusted as indicated by the flight adjustment command; The flight adjustment command is parsed to determine the specific adjustment parameters; The flight data of the aircraft to be adjusted are adjusted according to the specific adjustment parameters.

[0012] Optionally, when the fault response module is used to monitor the fault status of the aircraft cluster in real time and determine the target handling strategy for a faulty aircraft based on the specific fault status, the fault response module is used to: Monitor the flight parameters of each aircraft in the aircraft cluster under the current flight status to determine whether the fault conditions are met; If the fault conditions are met, determine the fault type and severity of the corresponding faulty aircraft based on the fault conditions met. Based on the identified fault type and severity of the faulty aircraft, a target solution processing strategy for the faulty aircraft is determined.

[0013] Optionally, the waterway planning module is also used for: The flight path allocation order of the aircraft is determined based on the mission priority of each aircraft to be assigned a flight path; The current flight path for each aircraft is determined according to the flight path allocation order.

[0014] Optionally, the flight adjustment module is also used for: Based on the flight data of each aircraft in the aircraft cluster, determine whether flight congestion has occurred; If congestion occurs, the scheduling order of each aircraft will be determined based on the mission priority of each aircraft under congestion conditions. According to the scheduling order, control the flight of each aircraft in sequence.

[0015] This application also provides a method for managing low-altitude airspace, the method comprising: Based on the flight data of the target aircraft and the target airspace data of the low-altitude airspace that the target aircraft passes through, the current flight path of the target aircraft is determined; Based on the flight data of each aircraft in the aircraft cluster, flight risk is predicted, and the current flight status of dangerous aircraft with flight risks is adjusted. Establish real-time information sharing between aircraft and between aircraft and air traffic management systems, and control multiple aircraft to coordinate their work based on the shared information; The system monitors the fault status of the aircraft cluster in real time. For faulty aircraft, it determines the target processing strategy for the faulty aircraft based on the specific fault status and processes the faulty aircraft according to the target processing strategy.

[0016] This application also provides an electronic device, including: a processor, a memory, and a bus. The memory stores machine-readable instructions executable by the processor. When the electronic device is running, the processor communicates with the memory via the bus. When the machine-readable instructions are executed by the processor, the steps of the management method described above are performed.

[0017] This application also provides a computer-readable storage medium storing a computer program, which, when executed by a processor, performs the steps of the management method described above.

[0018] This application provides a management system and method for low-altitude airspace, the management system comprising: The flight path planning module is used to determine the current flight path of the target aircraft based on the flight data of the target aircraft and the target airspace data of the target low-altitude airspace through which the target aircraft passes. The flight adjustment module is used to predict flight risks based on the flight data of each aircraft in the aircraft cluster, and to adjust the current flight status of dangerous aircraft with flight risks. The airspace coordination module is used to establish real-time information sharing between aircraft and between aircraft and the air traffic management system, and to control multiple aircraft to coordinate their work based on the shared information. The fault response module is used to monitor the fault status of the aircraft cluster in real time. For the faulty aircraft, it determines the target processing strategy for the faulty aircraft according to the specific fault status, and processes the faulty aircraft according to the target processing strategy.

[0019] Thus, the technical solution provided in this application can solve the problems of airway congestion, inter-aircraft interference, and efficient utilization of airspace resources for low-altitude aircraft in high-density airspace environments. By combining airway planning, flight adjustment, airspace coordination, and fault response modules, this application can achieve intelligent management and efficient collaboration of low-altitude aircraft, improve airspace utilization, ensure flight safety, and provide strong technical support for the rapid development of the low-altitude field. Furthermore, it can be widely applied to low-altitude applications such as drone delivery, air taxis, patrol monitoring, and agricultural spraying, possessing significant commercial value and application prospects.

[0020] To make the above-mentioned objectives, features and advantages of this application more apparent and understandable, preferred embodiments are described below in detail with reference to the accompanying drawings. Attached Figure Description

[0021] To more clearly illustrate the technical solutions of the embodiments of this application, the accompanying drawings used in the embodiments will be briefly introduced below. It should be understood that the following drawings only show some embodiments of this application and should not be regarded as a limitation of the scope. For those skilled in the art, other related drawings can be obtained based on these drawings without creative effort.

[0022] Figure 1 This is one of the structural schematic diagrams of a low-altitude airspace management system provided in an embodiment of this application; Figure 2 A second schematic diagram of the structure of a low-altitude airspace management system provided in an embodiment of this application; Figure 3 A flowchart illustrating a low-altitude airspace management method provided in an embodiment of this application; Figure 4 This is a schematic diagram of the structure of an electronic device provided in an embodiment of this application. Detailed Implementation

[0023] To make the objectives, technical solutions, and advantages of the embodiments of this application clearer, the technical solutions of the embodiments of this application will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of this application, and not all embodiments. The components of the embodiments of this application described and shown in the accompanying drawings can generally be arranged and designed in various different configurations. Therefore, the following detailed description of the embodiments of this application provided in the accompanying drawings is not intended to limit the scope of the claimed application, but merely represents selected embodiments of this application. Based on the embodiments of this application, every other embodiment obtained by those skilled in the art without inventive effort falls within the scope of protection of this application.

[0024] With the rapid development of the low-altitude airspace, especially the widespread application of low-altitude aircraft such as drones and air taxis, the demand for low-altitude airspace has increased significantly. Low-altitude aircraft are widely used in logistics, air travel, agricultural spraying, environmental monitoring, and many other fields, greatly promoting economic and social progress. However, low-altitude aircraft face numerous challenges during flight, particularly in high-density flight environments, where issues such as mutual interference between aircraft, airway congestion, and insufficient airspace resources are becoming increasingly prominent.

[0025] Currently, there has been some technical research on flight path planning and airspace management for low-altitude aircraft, but most technologies are still in their initial stages and have some problems and shortcomings: Static airway planning problems. Traditional airway planning methods are usually static, meaning that airways and flight paths are fixed in advance and lack the ability to be dynamically adjusted. This method can easily lead to safety hazards such as airway congestion and aircraft collisions when there are many aircraft, diverse mission types, and complex airspace environments.

[0026] Lack of real-time adaptability. Existing low-altitude airspace control systems and airway allocation mechanisms typically rely on simple rules and models, making intelligent adjustments difficult. This results in slow response and limited effectiveness when faced with unexpected situations or airspace changes.

[0027] Insufficient airspace coordination. Most low-altitude aircraft's airspace control systems can only achieve one-way communication between the aircraft and the airspace management system. The coordination and information sharing mechanisms between aircraft are relatively weak, making it impossible to effectively avoid interference and conflicts between aircraft. In high-density flight environments, the lack of efficient coordination mechanisms will exacerbate flight safety hazards.

[0028] Therefore, how to intelligently perform dynamic flight path planning and allocation in complex low-altitude flight environments, enhance the coordination capabilities between aircraft, ensure flight safety, and improve the utilization rate of airspace resources has become an urgent technical challenge.

[0029] Based on this, embodiments of this application provide a management system and method for low-altitude airspace, which can intelligently perform dynamic flight path planning and allocation in complex low-altitude flight environments, enhance the coordination capabilities between aircraft, ensure flight safety, and improve the utilization rate of airspace resources.

[0030] Please see Figure 1 , Figure 2 , Figure 1 This is one of the structural schematic diagrams of a low-altitude airspace management system provided in an embodiment of this application; Figure 2 This is a second schematic diagram of a low-altitude airspace management system provided in an embodiment of this application. Figure 1 As shown in the illustration, the management system 100 provided in this application embodiment includes: The flight path planning module 110 is used to determine the current flight path of the target aircraft based on the flight data of the target aircraft and the target airspace data of the target low-altitude airspace through which the target aircraft passes. The flight adjustment module 120 is used to predict flight risks based on the flight data of each aircraft in the aircraft cluster, and to adjust the current flight status of dangerous aircraft with flight risks. The airspace coordination module 130 is used to establish real-time information sharing between aircraft and between aircraft and the air traffic management system, and to control multiple aircraft to coordinate their work based on the shared information. The fault response module 140 is used to monitor the fault status of the aircraft cluster in real time. For the faulty aircraft with faulty status, it determines the target solution processing strategy for the faulty aircraft according to the specific fault status and processes the faulty aircraft according to the target processing strategy.

[0031] The functions of each module in the above embodiments and the specific technical means used to implement the corresponding functions are described below: Regarding the flight path planning module 110, this module can perform flight path planning before the aircraft takes off, and can also replan the flight path during flight.

[0032] In one embodiment provided in this application, when the flight path planning module 110 determines the current flight path of the target aircraft based on the flight data of the target aircraft and the target airspace data of the target low-altitude airspace traversed by the target aircraft, the flight path planning module 110 is used to: Acquire real-time flight data and planned flight data of the target aircraft; determine the target low-altitude airspace through which the target aircraft will pass based on the mission position planning information in the planned flight data of the target aircraft, and acquire the target airspace data of the target low-altitude airspace; determine the current flight path of the target aircraft according to a preset flight path planning algorithm based on the real-time flight data, planned flight data and target airspace data.

[0033] In the above embodiments, the real-time flight data includes the current position and current speed of the target aircraft, and the planned flight data includes the mission planning information of the target aircraft, which includes mission location planning information and mission priority.

[0034] The real-time flight data may also include the aircraft's current heading and current altitude.

[0035] The task location planning information includes the task start position and the task end position, and may even include intermediate path positions.

[0036] The above-mentioned determination of the target low-altitude airspace through which the target aircraft will pass, based on the mission position planning information in the planned flight data of the target aircraft, can specifically be based on the mission start position and mission end position, or even intermediate path positions in the mission position planning information, and determined according to a preset expansion rule.

[0037] Once the target low-altitude airspace is determined, the target airspace data obtained may include airspace density and weather conditions, or it may also include data on aircraft currently flying in the target low-altitude airspace.

[0038] In the above embodiments, the preset route planning algorithm includes the mapping relationship between flight data and airspace data and routes.

[0039] Furthermore, in another embodiment provided in this application, the flight path planning module 110 is also used to: determine the flight path allocation order of the aircraft according to the mission priority of each aircraft to be allocated a flight path; and determine the current flight path of each aircraft according to the flight path allocation order.

[0040] Here, when allocating flight paths to each aircraft according to the flight path allocation order, if the number of remaining flight paths is greater than the number of aircraft, the remaining unallocated flight paths for the aircraft will wait for flight path allocation.

[0041] Specifically, when allocating airways according to mission priority, airways can be intelligently allocated based on factors such as the mission type of the aircraft, the urgency of the flight mission, the characteristics of the cargo, and the delivery time requirements. In the event of airspace congestion, high-priority flight missions will be prioritized for scheduling.

[0042] Furthermore, the flight path planning module 110 can also be used to automatically adjust the flight path allocation results of aircraft based on airspace usage and changes in flight missions. The flight paths planned by the flight path planning module 110 will ensure a safe distance between aircraft to avoid collisions.

[0043] Furthermore, the flight path planning module 110 can employ machine learning and deep learning algorithms to optimize flight path allocation and adjustment strategies based on historical data of the aircraft, airspace change trends, and real-time monitoring information. The flight path planning module 110 can perform hierarchical management of airspace based on real-time data and, in conjunction with the aircraft's altitude and flight direction, perform multi-level, cross-altitude flight path allocation.

[0044] The flight adjustment module 120 can be used to adjust the flight status of the aircraft during flight.

[0045] In one embodiment provided in this application, when the flight adjustment module 120 is used to predict flight risks based on flight data of each aircraft in the aircraft cluster and adjust the current flight status of dangerous aircraft with flight risks, the flight adjustment module is used to: Based on the real-time and planned flight data of each aircraft in the aircraft cluster, and combined with the obstacle information in the current airspace, identify whether there are overlapping aircraft; identify overlapping aircraft as dangerous aircraft; for each dangerous aircraft, adjust the current flight status of the dangerous aircraft based on the flight data of the dangerous aircraft, the flight data of the other aircraft, and the current airspace conditions.

[0046] In the above embodiments, if the distance between any two aircraft is less than the safe distance at the same time, it can be determined that the aircraft overlap.

[0047] Here, when the flight adjustment module 120 is used to adjust the current flight status of the dangerous aircraft, it specifically includes adjusting the flight data of the dangerous aircraft and / or adjusting the current flight path of the dangerous aircraft.

[0048] For example, when the flight paths of aircraft A and aircraft B overlap, the system will dynamically adjust the flight path based on one or more of the data such as the aircraft's mission priority, flight altitude, and flight time window to ensure a safe distance between the aircraft.

[0049] It should be noted that during the adjustment process, obstacle detection and emergency collision avoidance mechanisms are combined to automatically adjust the flight path to avoid collisions when aircraft conflicts or temporary obstacles occur.

[0050] For example, when aircraft A detects that it is too close to aircraft B, the system will instruct aircraft A to adjust its flight path or change its flight altitude to ensure flight safety.

[0051] Furthermore, in another embodiment provided in this application, the flight adjustment module 120 is further configured to: in response to a flight adjustment command, determine the aircraft to be adjusted indicated by the flight adjustment command; parse the flight adjustment command to determine specific adjustment parameters; and adjust the flight data of the aircraft to be adjusted according to the specific adjustment parameters.

[0052] The flight adjustment command can be issued by the target personnel, or it can be automatically triggered when the conditions are met, based on real-time flight data and preset trigger conditions.

[0053] Furthermore, the flight adjustment module 120 is also used to: determine whether flight congestion has occurred based on the flight data of each aircraft in the aircraft cluster; if congestion occurs, determine the scheduling order of each aircraft under congestion conditions based on the task priority of each aircraft under congestion conditions; and control each aircraft to fly sequentially according to the scheduling order.

[0054] For example, in flight missions, there are tasks with different priorities. Some urgent transport missions need to be completed first, while some routine flight missions can be carried out during idle time. The flight adjustment module 120 dynamically adjusts the aircraft's flight path allocation based on the urgency of the flight mission, the aircraft's real-time status, and airspace usage. When airspace resources are scarce, the system prioritizes the successful completion of high-priority tasks while optimizing the flight path allocation for low-priority tasks. For instance, if an urgent mission needs to be completed within a short time, and the airspace is nearing saturation, the system will automatically allocate the optimal flight path for that mission and adjust the paths and priorities of other missions to ensure the urgent mission is completed in a timely manner.

[0055] Regarding the airspace coordination module 130, this module can establish real-time information sharing between aircraft and between aircraft and the air traffic management system. Specifically, it can achieve real-time information sharing between aircraft and the air traffic management system, as well as among aircraft, through ad-hoc networking technology. Each aircraft can receive the position, flight path information, and flight status of other aircraft in real time, thereby enabling dynamic coordination during flight. When an aircraft's flight path overlaps with the paths of other aircraft, the management system will automatically calculate and instruct the aircraft to adjust its path to avoid collisions or interference. This module can also adjust the aircraft's path according to airspace usage to achieve efficient utilization of airspace resources.

[0056] The airspace collaboration module 130 is compatible with the operating systems of different types of aircraft and supports cross-platform collaboration and information sharing.

[0057] Regarding the fault response module 140, this module can promptly and accurately identify the faulty aircraft and determine specific target handling strategies based on the specific causes of the faulty aircraft.

[0058] Furthermore, when the fault response module 140 is used to monitor the fault status of the aircraft cluster in real time, and to determine the target solution processing strategy for the faulty aircraft based on the specific fault status, the fault response module 140 is used to: monitor the flight parameters of each aircraft in the aircraft cluster under the current flight state to determine whether the fault conditions are met; if the fault conditions are met, determine the fault type and fault severity of the corresponding faulty aircraft based on the met fault conditions; and determine the target solution processing strategy for the faulty aircraft based on the determined fault type and fault severity of the faulty aircraft.

[0059] For example, when the system detects a malfunction in an aircraft, it will automatically activate the emergency response mechanism based on the type and severity of the malfunction. For instance, if an aircraft engine malfunctions, the system will instruct the aircraft to change its altitude or heading to return to a predetermined safe area. For more serious malfunctions, the system will alert the airspace management system and coordinate with other aircraft and the airspace management system to provide support to the malfunctioning aircraft, ensuring flight safety.

[0060] Furthermore, such as Figure 2 As shown, the management system 100 also includes a status monitoring module 150, which is used to monitor the flight status of the aircraft in real time and automatically adjust the flight parameters of the aircraft through an adaptive algorithm to ensure flight safety.

[0061] In summary, this management system can play an important role in various scenarios such as urban air travel, drone logistics delivery, and low-altitude tourism.

[0062] In low-altitude urban travel scenarios, this system can plan and allocate flight paths in real time, ensuring that low-altitude aircraft can fly efficiently in urban airspace. When multiple aircraft depart simultaneously, the system can automatically allocate different flight paths based on real-time data and avoid collisions between aircraft through path adjustment and collision avoidance mechanisms. In addition, the system can also intelligently adjust the flight paths of aircraft based on the usage of urban airspace to avoid traffic congestion.

[0063] In drone logistics delivery scenarios, this solution can dynamically adjust flight paths based on different delivery tasks. Through the task priority processing module, urgent delivery tasks can receive priority flight path allocation, while ensuring the normal operation of other delivery tasks. The system can also intelligently adjust the aircraft's flight path based on real-time aircraft data and airspace changes, ensuring the efficiency and safety of delivery tasks.

[0064] In low-altitude tourism scenarios, aircraft need to avoid obstacles such as high-density buildings and traffic routes in cities. Through the path adjustment and collision avoidance mechanism of this invention, the system can calculate the optimal flight path for the aircraft in real time and avoid conflicts with other aircraft or obstacles. When multiple low-altitude aircraft are simultaneously conducting low-altitude tourism, the system can adjust the path based on real-time data to ensure flight safety.

[0065] Through the detailed description of the above implementation methods, it can be seen that the management system provided by this solution has a high level of intelligence and practical application value, and can efficiently and safely manage and schedule aircraft in various low-altitude scenarios.

[0066] Based on the same inventive concept, this application also provides a management method corresponding to the management system. Since the principle of the method in this application is similar to that of the management system described above in this application, the implementation of the method can refer to the implementation of the system, and the repeated parts will not be described again.

[0067] Please see Figure 3 , Figure 3 This is a flowchart illustrating a low-altitude airspace management method provided in an embodiment of this application. Figure 3 As shown, the management method includes: S301. Determine the current flight path of the target aircraft based on the flight data of the target aircraft and the target airspace data of the target low-altitude airspace through which the target aircraft passes. S302. Based on the flight data of each aircraft in the aircraft cluster, predict flight risks and adjust the current flight status of dangerous aircraft with flight risks. S303. Establish real-time information sharing between aircraft and between aircraft and air traffic management systems, and control multiple aircraft to coordinate their work based on the shared information. S304. Monitor the fault status of the aircraft cluster in real time. For faulty aircraft, determine the target processing strategy for the faulty aircraft based on the specific fault status, and process the faulty aircraft according to the target processing strategy.

[0068] Optionally, determining the current flight path of the target aircraft based on its flight data and the target airspace data of the low-altitude airspace it traverses includes: Acquire real-time flight data and planned flight data of the target aircraft; wherein, the real-time flight data includes the current position and current speed of the target aircraft, and the planned flight data includes the mission planning information of the target aircraft, the mission planning information including mission position planning information and mission priority; Based on the mission location planning information in the target aircraft's planned flight data, determine the target low-altitude airspace that the target aircraft will pass through, and obtain the target airspace data of the target low-altitude airspace. Based on the real-time flight data, planned flight data, and target airspace data, the current flight path of the target aircraft is determined according to a preset flight path planning algorithm.

[0069] Optionally, the step of predicting flight risks based on flight data from each aircraft in the aircraft cluster, and adjusting the current flight status of dangerous aircraft posing flight risks, includes: Based on the real-time flight data and planned flight data of each aircraft in the aircraft cluster, and combined with the obstacle information in the current airspace, identify whether there are overlapping aircraft in flight. Aircraft that have overlapping flight paths are identified as dangerous aircraft. For each dangerous aircraft, the current flight status of the dangerous aircraft is adjusted based on its flight data, the flight data of other aircraft besides the dangerous aircraft, and the current airspace conditions; wherein, adjusting the current flight status of the dangerous aircraft includes adjusting the flight data of the dangerous aircraft and / or adjusting the current flight path of the dangerous aircraft.

[0070] Optionally, the management method further includes: In response to a flight adjustment command, determine the aircraft to be adjusted as indicated by the flight adjustment command; The flight adjustment command is parsed to determine the specific adjustment parameters; The flight data of the aircraft to be adjusted are adjusted according to the specific adjustment parameters.

[0071] Optionally, the real-time monitoring of the aircraft cluster's fault status, and for faulty aircraft, determining the target handling strategy for the faulty aircraft based on the specific fault condition, includes: Monitor the flight parameters of each aircraft in the aircraft cluster under the current flight status to determine whether the fault conditions are met; If the fault conditions are met, determine the fault type and severity of the corresponding faulty aircraft based on the fault conditions met. Based on the identified fault type and severity of the faulty aircraft, a target solution processing strategy for the faulty aircraft is determined.

[0072] Optionally, the management method further includes: The flight path allocation order of the aircraft is determined based on the mission priority of each aircraft to be assigned a flight path; The current flight path for each aircraft is determined according to the flight path allocation order.

[0073] Optionally, the management method further includes: Based on the flight data of each aircraft in the aircraft cluster, determine whether flight congestion has occurred; If congestion occurs, the scheduling order of each aircraft will be determined based on the mission priority of each aircraft under congestion conditions. According to the scheduling order, control the flight of each aircraft in sequence.

[0074] Please see Figure 4 , Figure 4 This is a schematic diagram of the structure of an electronic device provided in an embodiment of this application. Figure 4 As shown, the electronic device 400 includes a processor 410, a memory 420, and a bus 430.

[0075] The memory 420 stores machine-readable instructions executable by the processor 410. When the electronic device 400 is running, the processor 410 communicates with the memory 420 via the bus 430. When the machine-readable instructions are executed by the processor 410, they can perform the operations described above. Figure 3 The steps in the method embodiment shown are specifically implemented in the method embodiment and will not be repeated here.

[0076] This application also provides a computer-readable storage medium storing a computer program, which, when executed by a processor, can perform the above-described actions. Figure 3 The steps in the method embodiment shown are specifically implemented in the method embodiment and will not be repeated here.

[0077] Those skilled in the art will understand that, for the sake of convenience and brevity, the specific working processes of the systems, devices, and units described above can be referred to the corresponding processes in the foregoing method embodiments, and will not be repeated here.

[0078] In the several embodiments provided in this application, it should be understood that the disclosed systems, apparatuses, and methods can be implemented in other ways. The apparatus embodiments described above are merely illustrative. For example, the division of units is only a logical functional division, and in actual implementation, there may be other division methods. Furthermore, multiple units or components may be combined or integrated into another system, or some features may be ignored or not executed. Additionally, the shown or discussed mutual couplings, direct couplings, or communication connections may be through some communication interfaces; indirect couplings or communication connections between devices or units may be electrical, mechanical, or other forms.

[0079] The units described as separate components may or may not be physically separate. The components shown as units may or may not be physical units; that is, they may be located in one place or distributed across multiple network units. Some or all of the units can be selected to achieve the purpose of this embodiment according to actual needs.

[0080] In addition, the functional units in the various embodiments of this application can be integrated into one processing unit, or each unit can exist physically separately, or two or more units can be integrated into one unit.

[0081] If the aforementioned functions are implemented as software functional units and sold or used as independent products, they can be stored in a processor-executable, non-volatile, computer-readable storage medium. Based on this understanding, the technical solution of this application, in essence, or the part that contributes to the prior art, or a portion of the technical solution, can be embodied in the form of a software product. This computer software product is stored in a storage medium and includes several instructions to cause a computer device (which may be a personal computer, server, or network device, etc.) to execute all or part of the steps of the methods described in the various embodiments of this application. The aforementioned storage medium includes various media capable of storing program code, such as USB flash drives, portable hard drives, read-only memory (ROM), random access memory (RAM), magnetic disks, or optical disks.

[0082] Finally, it should be noted that the above-described embodiments are merely specific implementations of this application, used to illustrate the technical solutions of this application, and not to limit them. The scope of protection of this application is not limited thereto. Although this application has been described in detail with reference to the foregoing embodiments, those skilled in the art should understand that any person skilled in the art can still modify or easily conceive of changes to the technical solutions described in the foregoing embodiments, or make equivalent substitutions for some of the technical features, within the scope of the technology disclosed in this application. Such modifications, changes, or substitutions do not cause the essence of the corresponding technical solutions to deviate from the spirit and scope of the technical solutions of the embodiments of this application, and should all be covered within the scope of protection of this application. Therefore, the scope of protection of this application should be determined by the scope of the claims.

Claims

1. A low airspace management system, characterized by, The management system comprises: a flight path planning module, configured to determine a current flight path of a target aircraft according to flight data of the target aircraft and target airspace data of a target low-altitude airspace through which the target aircraft passes; a flight adjustment module, configured to perform flight risk prediction according to flight data of each aircraft in a cluster of aircrafts, and adjust a current flight state of a dangerous aircraft that has flight risk; an airspace coordination module, configured to establish real-time sharing of information among aircrafts and between the aircrafts and an air traffic management system, and control multiple aircrafts to work in coordination according to shared information; a fault response module, configured to monitor fault conditions of the cluster of aircrafts in real time, determine a target processing strategy of a fault aircraft that has a fault condition according to a specific fault condition corresponding to the fault aircraft, and process the fault aircraft according to the target processing strategy.

2. The management system according to claim 1, characterized by When the flight path planning module is configured to determine a current flight path of a target aircraft according to flight data of the target aircraft and target airspace data of a target low-altitude airspace through which the target aircraft passes, the flight path planning module is configured to: obtain real-time flight data and planned flight data of the target aircraft; wherein the real-time flight data comprises a current position and a current speed of the target aircraft, and the planned flight data comprises task planning information of the target aircraft, the task planning information comprising task position planning information and task priority; determine the target low-altitude airspace through which the target aircraft passes according to the task position planning information in the planned flight data of the target aircraft, and obtain target airspace data of the target low-altitude airspace; determine the current flight path of the target aircraft according to the real-time flight data, the planned flight data and the target airspace data according to a preset flight path planning algorithm.

3. The management system of claim 1, wherein, When the flight adjustment module is configured to perform flight risk prediction according to flight data of each aircraft in a cluster of aircrafts, and adjust a current flight state of a dangerous aircraft that has flight risk, the flight adjustment module is configured to: identify whether there are aircrafts with flight overlap according to real-time flight data and planned flight data of each aircraft in the cluster of aircrafts, in combination with obstacle information in a current airspace; determine aircrafts with flight overlap as dangerous aircrafts; for each dangerous aircraft, adjust a current flight state of the dangerous aircraft according to flight data of the dangerous aircraft, flight data of the remaining aircrafts except the dangerous aircraft, and a current situation of the current airspace; wherein adjusting the current flight state of the dangerous aircraft comprises adjusting flight data of the dangerous aircraft and / or adjusting a current flight path of the dangerous aircraft.

4. The management system of claim 1, wherein, The flight adjustment module is further configured to: determine a to-be-adjusted aircraft indicated by a flight adjustment instruction in response to the flight adjustment instruction; analyze the flight adjustment instruction to determine specific adjustment parameters; adjust flight data of the to-be-adjusted aircraft according to the specific adjustment parameters.

5. The management system of claim 1, wherein, The fault response module is configured to: monitor flight parameters of each aircraft in the aircraft cluster under the current flight state, and determine whether a fault condition is met; if the fault condition is met, determine a fault type and a fault degree of the corresponding fault aircraft according to the met fault condition; determine a target processing strategy of the fault aircraft according to the determined fault type and fault degree of the fault aircraft.

6. The management system of claim 1, wherein, The route planning module is further configured to: determine a flight route allocation sequence of the aircraft according to a task priority of the aircraft of each to-be-allocated flight route; determine a current flight route of each aircraft according to the flight route allocation sequence.

7. The management system of claim 1, wherein, The flight adjustment module is further configured to: determine whether flight congestion occurs according to flight data of each aircraft in the aircraft cluster; if the flight congestion occurs, determine a scheduling sequence of each aircraft under the congestion according to a task priority of each aircraft under the congestion; control each aircraft to fly in sequence according to the scheduling sequence.

8. A method of managing low airspace, characterized by, The management method comprises: determine a current flight route of the target aircraft according to flight data of the target aircraft and target airspace data of a target low-altitude airspace to be passed through by the target aircraft; perform flight risk prediction according to flight data of each aircraft in the aircraft cluster, and adjust a current flight state of a dangerous aircraft having flight risk; establish real-time information sharing between the aircraft and between the aircraft and an air traffic management system, and control multiple aircraft to work coordinately according to the shared information; monitor fault conditions of the aircraft cluster in real time, determine a target processing strategy of a fault aircraft having a fault condition according to a corresponding specific fault condition of the fault aircraft, and process the fault aircraft according to the target processing strategy.

9. An electronic device, comprising: comprise: a processor, a memory and a bus, the memory stores machine readable instructions executable by the processor, when the electronic device is running, the processor and the memory communicate through the bus, and the machine readable instructions are executed by the processor to perform the steps of the management method of claim 8.

10. A computer-readable storage medium, characterized in that, The computer readable storage medium stores a computer program, and the computer program is executed by the processor to perform the steps of the management method of claim 8.

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