Multi-model combined ground anchor arrangement method and device, electronic equipment and storage medium

Abstract

The invention discloses a multi-model combined ground anchor arrangement method and device, electronic equipment and a storage medium. The method comprises the following steps: loading an existing camera ground anchor point location resource map, coordinate data of each stop line and a proportional scale; loading a ground anchor arrangement diagram of the corresponding model based on the model information of the ground anchor to be combined; performing superposition processing on each ground anchor arrangement diagram and the existing camera ground anchor point location resource diagram to obtain a combined ground anchor arrangement diagram; carrying out image processing on the combined ground anchor arrangement diagram to extract a ground anchor demand area and an existing machine position ground anchor point position; and a clustering algorithm is adopted to determine and output the minimum ground anchor arrangement number and the corresponding point positions meeting the mooring requirements of all the aircraft types. According to the method, the existing aircraft position ground anchor point location resource map and the ground anchor arrangement maps of different aircraft types are loaded, and superposition processing and optimization are carried out, so that the mooring compatibility of multiple aircraft types is realized, and meanwhile, the dual targets of facility reduction and pavement operation intensification are achieved through topology recombination and efficiency improvement of the existing anchor point resources.

Description

Technical Field

[0001] The present invention belongs to the technical field of aircraft ground anchor design and maintenance, and more specifically, relates to a multi-aircraft combined ground anchor layout method, device, electronic device, and storage medium. Background Art

[0002] With the rapid development of the air transportation industry, the contradiction between the limitedness of airport apron resources and the increasing flight demand has become increasingly prominent. In order to improve the utilization efficiency of the airport apron, modern airports generally adopt the design of composite aircraft positions, enabling a single position to meet the parking requirements of multiple aircraft types. The aircraft stop point refers to the final stop position of the aircraft when docking at the jet bridge or remote position, ensuring the precise alignment of the aircraft door with the boarding bridge or maintaining the necessary safety distance from ground equipment. Due to the differences in the sizes and door positions of different aircraft types, the stop points of different aircraft types on the same position will also vary, resulting in the situation of multiple stop points on the position. Although this design improves the flexibility of the position, it also poses higher requirements for ground anchor layout.

[0003] In the apron operation management of civil airports, aircraft ground anchors, as the core facilities to ensure the mooring safety of aircraft, the rationality of their layout directly affects the fixing efficiency of aircraft and the ground operation efficiency. The current mainstream ground anchor configuration mode has significant limitations: traditional designs are statically planned based on the mooring requirements of a single aircraft type, resulting in redundant ground anchor points, insufficient multi-aircraft compatibility, and easy spatial interference with the pavement operation flow line. Particularly crucial is that there are two fundamental deficiencies in the existing technical system: firstly, there is a lack of a collaborative configuration mechanism for ground anchor resources for multi-aircraft dynamic berthing scenarios; secondly, there is a systematic lack of functional reuse and spatial optimization strategies for existing ground anchor points. This blank in the ability to reuse existing anchor point resources directly restricts the flexible adaptation ability in the mooring scenario of composite aircraft types and exacerbates the redundancy of pavement facilities and operation conflicts. Therefore, it is urgent to construct a new ground anchor configuration system with intelligent optimization characteristics to achieve the dual goals of facility reduction and pavement operation intensification while realizing multi-aircraft mooring compatibility through topological reorganization and efficiency improvement of existing anchor point resources.

[0004] The information disclosed in the background art section of the present invention is only intended to deepen the understanding of the general background art of the present invention and should not be regarded as an admission or any form of suggestion that this information constitutes the prior art known to those skilled in the art. Summary of the Invention

[0005] The object of the present invention is to propose a method, device, electronic device and storage medium for combined ground anchor arrangement of multiple aircraft types, so as to solve the problems of poor adaptability, excessive number of ground anchors and adverse effects on the operation efficiency of the airport pavement existing in the traditional ground anchor arrangement method. While realizing the mooring compatibility of multiple aircraft types, through the topological recombination and efficiency improvement of the existing anchor point resources, the dual goals of facility reduction and pavement operation intensification are achieved.

[0006] To achieve the above object, the present invention proposes a method, device, electronic device and storage medium for combined ground anchor arrangement of multiple aircraft types.

[0007] According to the first aspect of the present invention, a method for combined ground anchor arrangement of multiple aircraft types is proposed, including:

[0008] Loading the existing apron ground anchor point resource map, the coordinate data of each stop line and the scale;

[0009] Loading the ground anchor arrangement map of the corresponding aircraft type based on the aircraft type information of the ground anchors to be combined;

[0010] Performing superposition processing on each of the ground anchor arrangement maps and the existing apron ground anchor point resource map based on the scale and the coordinate data of each stop line to obtain a combined ground anchor arrangement map;

[0011] Performing image processing on the combined ground anchor arrangement map to extract the ground anchor demand area and the existing apron ground anchor points;

[0012] Based on the ground anchor demand area and the existing apron ground anchor point resources, using a clustering algorithm to determine the minimum number of ground anchor arrangements and the corresponding point information that meet the mooring requirements of each aircraft type;

[0013] Generating and outputting a combined ground anchor arrangement map of multiple aircraft types based on the number of ground anchor arrangements and the corresponding point information.

[0014] Optionally, before loading the ground anchor arrangement map of the corresponding aircraft type based on the aircraft type information of the ground anchors to be combined, it further includes:

[0015] Verifying the validity of the coordinate data of each stop line based on the existing apron ground anchor point resource map.

[0016] Optionally, the image processing of the combined ground anchor arrangement map includes:

[0017] Marking the ground anchor demand area and the existing apron ground anchor points of the combined ground anchor arrangement map as shaded areas;

[0018] Converting the combined ground anchor arrangement map with the marking completed into a picture;

[0019] Extract the shadow area from the picture based on the HSV color space, and convert the shadow area into a binary mask.

[0020] Optionally, the clustering algorithm includes:

[0021] K-Means algorithm.

[0022] Optionally, the determination of the minimum number of ground anchor arrangements and the corresponding point position information that meet the mooring requirements of each aircraft type by using a clustering algorithm based on the ground anchor demand area and the existing ground anchor point position resources of the aircraft positions includes:

[0023] Extract the overlapping area based on the ground anchor demand area and the existing ground anchor point position resources of the aircraft positions;

[0024] Determine the minimum number of ground anchor arrangements and the corresponding point position information that meet the mooring requirements of each aircraft type by using a clustering algorithm based on the overlapping area.

[0025] Optionally, mark the corresponding aircraft type at each stop line of the combined ground anchor layout diagram.

[0026] Optionally, the generation and output of the multi-aircraft type combined ground anchor layout diagram based on the ground anchor arrangement quantity and the corresponding point position information include:

[0027] Calculate the distance from each ground anchor point to the first stop line based on the minimum number of ground anchor arrangements and the corresponding point position information and the coordinate data of the first stop line;

[0028] Generate a multi-aircraft type combined ground anchor layout diagram based on the minimum number of ground anchor arrangements and the corresponding point position information and each of the distances;

[0029] Output the multi-aircraft type combined ground anchor layout diagram.

[0030] According to the second aspect of the present invention, a multi-aircraft type combined ground anchor layout device is proposed, including:

[0031] Loading module: used to load the existing aircraft position ground anchor point position resource map, the coordinate data of each stop line and the scale; load the ground anchor layout diagram of the corresponding aircraft type based on the aircraft type information of the ground anchor to be combined;

[0032] Overlay module, used to perform overlay processing on each of the ground anchor layout diagrams and the existing aircraft position ground anchor point position resource map based on the scale and the coordinate data of each stop line to obtain a combined ground anchor layout diagram;

[0033] Image processing module, used to perform image processing on the combined ground anchor layout diagram to extract the ground anchor demand area and the existing aircraft position ground anchor points;

[0034] An optimization module, configured to determine the minimum number of ground anchor arrangements and corresponding point information that meet the mooring requirements of each aircraft type by using a clustering algorithm based on the ground anchor demand area and the existing ground anchor point resources of the aircraft positions;

[0035] A generation and output module, configured to generate and output a multi-aircraft combined ground anchor arrangement diagram based on the number of ground anchor arrangements and the corresponding point information.

[0036] According to a third aspect of the present invention, an electronic device is provided, and the electronic device includes:

[0037] At least one processor; and,

[0038] A memory communicatively connected to the at least one processor; wherein,

[0039] The memory stores instructions executable by the at least one processor, and the instructions are executed by the at least one processor so that the at least one processor can execute the multi-aircraft combined ground anchor arrangement method according to any one of the first aspects.

[0040] According to a fourth aspect of the present invention, a non-transitory computer-readable storage medium is provided, and the non-transitory computer-readable storage medium stores computer instructions for causing a computer to execute the multi-aircraft combined ground anchor arrangement method according to any one of the first aspects.

[0041] The beneficial effects of the present invention are as follows: By loading the existing ground anchor point resource map of the aircraft positions and the ground anchor arrangement diagrams of different aircraft types, and performing superposition processing and optimization, the present invention can scientifically and reasonably determine the ground anchor arrangement plan in the scenario of a composite aircraft type position, so that a single position can better meet the parking requirements of multiple aircraft types, making full use of the limited airport apron resources and alleviating the contradiction between the limited airport apron resources and the growing flight demand; while realizing the mooring compatibility of multiple aircraft types, through the topological reorganization and efficiency improvement of the existing anchor point resources, the dual goals of facility reduction and pavement operation intensification are achieved.

[0042] The system of the present invention has other characteristics and advantages, which will be obvious from the accompanying drawings incorporated herein and the subsequent specific embodiments, or will be described in detail in the accompanying drawings incorporated herein and the subsequent specific embodiments, and these accompanying drawings and specific embodiments are jointly used to explain the specific principles of the present invention. BRIEF DESCRIPTION OF THE DRAWINGS

[0043] By describing the exemplary embodiments of the present invention in more detail in conjunction with the accompanying drawings, the above and other objects, features, and advantages of the present invention will become more obvious. In the exemplary embodiments of the present invention, the same reference numerals generally represent the same components.

[0044] Figure 1 The flowchart showing the steps of a multi - type combined ground anchor layout method according to Embodiment 1 of the present invention.

[0045] Figure 2 The schematic diagram showing the existing aircraft position ground anchor position resource map according to Embodiment 1 of the present invention.

[0046] Figure 3 The schematic diagram showing the ground anchor layout map of a single aircraft type according to Embodiment 1 of the present invention.

[0047] Figure 4 The schematic diagram showing the multi - type combined ground anchor layout map according to Embodiment 1 of the present invention. Detailed implementation manners

[0048] The present invention will be described in more detail below with reference to the accompanying drawings. Although the preferred embodiments of the present invention are shown in the drawings, it should be understood that the present invention can be implemented in various forms and should not be limited by the embodiments set forth herein. On the contrary, these embodiments are provided to make the present invention more thorough and complete, and to fully convey the scope of the present invention to those skilled in the art.

[0049] Embodiment 1

[0050] As Figure 1 shown, this embodiment provides a multi - type combined ground anchor layout method, including:

[0051] S1. Load the existing aircraft position ground anchor position resource map, the coordinate data of each stop line, and the scale;

[0052] Specifically, the existing aircraft position ground anchor position resource map is as Figure 2 shown. This map records the specific position information of the existing ground anchor positions on the existing aircraft positions, including the accurate coordinate markings of the ground anchor positions, the records of relevant attribute information such as the types and specifications of the ground anchors. This map can exist in the form of drawings (such as CAD drawings) or electronic images (such as JPEG, PNG, PDF, etc.); the stop line coordinate data refers to the relevant coordinate information of the final stop position of the aircraft when docking at the jetty or remote position; the scale is a parameter used to represent the proportional relationship between the distance on the map or image and the actual distance.

[0053] After this step, verify the validity of each stop line coordinate data based on the existing aircraft position ground anchor position resource map.

[0054] Specifically, check the coordinate system of the existing aircraft position ground anchor position resource map and the stop line coordinate data; if they are inconsistent, use professional geographic information software or relevant algorithms to convert the stop line coordinate data into the same coordinate system as the resource map to ensure that subsequent operations are carried out under the same spatial reference; check whether the coordinates of the stop line are within the geographical boundaries of the airport and whether the coordinates are within the corresponding aircraft position area; for the coordinates of the stop line, it is required that they have a certain continuity, that is, the distance between adjacent coordinate points cannot be too large; check whether the stop line coordinate data is consistent with the stop line coordinate data in the existing aircraft position ground anchor position resource map.

[0055] S2. Load the ground anchor layout diagram of the corresponding aircraft type based on the aircraft type information of the ground anchors to be combined;

[0056] Specifically, in this step, the ground anchor layout diagram of the corresponding aircraft type is loaded according to the aircraft type information of the ground anchors to be combined, that is, the ground anchor layout diagram of the corresponding aircraft type is loaded according to the aircraft type information of all the aircraft to be parked at a single aircraft position. Among them, the ground anchor layout diagrams of all aircraft types can be stored in the database of the airport for subsequent retrieval and loading; the ground anchor layout diagram is a drawing used to show the position, quantity, specifications and related layout requirements of the ground anchors in the airport aircraft positions, including information such as the position of the ground anchors, the requirements for uplift resistance, and the position of the tie points.

[0057] S3. Perform superposition processing on each ground anchor layout diagram and the existing aircraft position ground anchor position resource map based on the scale and each stop line coordinate data to obtain a combined ground anchor layout diagram;

[0058] Specifically, in this step, the scales adopted by each ground anchor layout diagram and the existing aircraft position ground anchor position resource map are uniformly converted by setting the scale to ensure that the scales of the existing aircraft position ground anchor position resource map and each ground anchor layout diagram are consistent to ensure the accuracy of superposition; through the stop line coordinate data, the ground anchor layout diagrams of different aircraft types can be accurately aligned with the existing aircraft position ground anchor position resource map in terms of spatial position, so as to ensure the accurate corresponding relationship between each ground anchor layout diagram and the existing aircraft position ground anchor position resource map in space.

[0059] S4. Perform image processing on the combined ground anchor layout diagram to extract the ground anchor demand area and the existing aircraft position ground anchor positions;

[0060] In this step, the ground anchor demand area and the existing aircraft position ground anchor positions of the combined ground anchor layout diagram are marked as shaded areas;

[0061] Convert the marked combined ground anchor layout diagram into a picture;

[0062] Extract the shaded area from the picture based on the HSV color space and convert the shaded area into a binary mask.

[0063] In one embodiment, it is also possible to perform image processing on the existing aircraft position ground anchor position resource map and the ground anchor layout maps of each aircraft type respectively and then overlay them. The existing aircraft position ground anchor position resource map after image processing is as Figure 2 shown. The aircraft position stop line 2 is a key reference position for aircraft parking, used to ensure the precise alignment of the aircraft cabin door with the boarding bridge 1. The present invention achieves high-precision positioning of the ground anchor layout by tangentially aligning the origin of the aircraft head with the stop line. The position of the stop line 2 is determined by the airport aircraft position layout and is precisely described through the coordinate system 3. The existing aircraft position ground anchor positions 4 are marked in the form of circles, providing basic data support for the optimization of the ground anchor layout. The stop lines are named TO, T1, T2, etc., where the stop line TO is the first stop line. The coordinate system 3 includes L1 (the distance between the stop line T1 and the stop line TO), L2 (the distance between the stop line T2 and the stop line TO), L3 (the distance between the stop line T3 and the stop line TO), and so on. These distance parameters are determined according to the actual layout requirements of the airport. The ground anchor layout maps of each aircraft type after image processing are as Figure 3 shown. The ground anchor demand area for a single aircraft type is represented by the shaded area 7. Taking the A319 aircraft as an example, when it is parked, the origin of the aircraft head is tangentially aligned with the stop line 5, and the aircraft type 6 (A319) allowed to park is marked beside the stop line.

[0064] S5. Based on the ground anchor demand area and the existing aircraft position ground anchor position resources, use a clustering algorithm to determine the minimum number of ground anchor layouts and the corresponding position information that meet the mooring requirements of each aircraft type;

[0065] In this step, the clustering algorithm includes: the K-Means algorithm.

[0066] Specifically, the principle of the K-Means algorithm is as follows: The algorithm first randomly selects K data points as the initial cluster centers, then assigns each data point to the cluster where the nearest cluster center is located, and continuously updates the positions of the cluster centers, that is, calculates the mean value of all data points in each cluster as the new cluster center until the cluster centers no longer change significantly or reach the preset number of iterations. Other clustering algorithms can also be used, such as the K-Medoids algorithm, etc.

[0067] In this step, using a clustering algorithm based on the ground anchor demand area and the existing aircraft position ground anchor position resources to determine the minimum number of ground anchor layouts and the corresponding position information that meet the mooring requirements of each aircraft type includes:

[0068] Extract the overlapping area based on the ground anchor demand area and the existing aircraft position ground anchor position resources;

[0069] Based on the overlapping area, use a clustering algorithm to determine the minimum number of ground anchor layouts and the corresponding position information that meet the mooring requirements of each aircraft type.

[0070] Specifically, due to differences in their structures, sizes, and mooring requirements, different aircraft models have different corresponding ground anchor demand areas. At the same time, the existing ground anchor point resources at the aircraft positions are the actual existing ground anchor distribution. Extracting the overlapping areas can visually show which existing ground anchor points at the aircraft positions are in the common areas of the ground anchor demands of different aircraft models, and which ground anchor demand areas have overlapping parts; by identifying the overlapping areas, potential resource conflicts or sharing situations can be discovered. For example, if some existing ground anchor points at the aircraft positions are located at the overlapping parts of the ground anchor demand areas of multiple aircraft models, then these ground anchors may be able to meet the mooring requirements of multiple aircraft models simultaneously, improving the utilization rate of the ground anchors; conversely, if there are conflicts between the ground anchor demand areas and no suitable existing ground anchor points at the aircraft positions cover them, further planning and adjustment are required. In airport operation, the layout of ground anchors needs to consider costs and space utilization efficiency. If the overlapping areas are not extracted, it may lead to the independent layout of ground anchors in the ground anchor demand areas of different aircraft models, resulting in duplicate setting of ground anchors. By extracting the overlapping areas, this situation can be avoided, unnecessary ground anchor layout can be reduced, and construction and maintenance costs can be lowered. The determination of the overlapping areas provides accurate input data for subsequent optimization of the ground anchor layout using clustering algorithms. The clustering algorithm can analyze and classify the ground anchor demands and the existing ground anchor points in the overlapping areas to find the smallest set of ground anchors that can cover the mooring requirements of all aircraft models. In this way, an optimal ground anchor layout plan can be formulated to minimize the number of ground anchors used to the greatest extent while meeting the mooring safety requirements of each aircraft model. The space of airport aircraft positions is limited, and a reasonable ground anchor layout can make full use of the limited space. The minimum number of ground anchor layouts determined by the clustering algorithm and the corresponding point information can ensure that the distribution of ground anchors in the aircraft position is more compact and reasonable, avoiding the ground anchors being too scattered or concentrated, and improving the overall utilization efficiency of the aircraft position space; ensuring that the mooring requirements of each aircraft model can be met. The determined ground anchor layout plan takes into account the overlapping situation of the ground anchor demands of each aircraft model, can provide stable mooring support, guarantee the safety and reliability of the aircraft during parking, and reduce the risk of safety accidents caused by improper mooring. The steps to determine the minimum number of ground anchor layouts and the corresponding point information that meet the mooring requirements of each aircraft model based on the overlapping areas using the clustering algorithm are as follows: 1. Initialization: Set the initial number of anchor points N = 1; Cluster to generate candidate points: 2. Use a clustering algorithm (such as K-Means), with N as the number of clusters, to cluster the ground anchor demand points in the overlapping areas to obtain N candidate ground anchor points; 3. Verify the coverage range: Check whether these candidate points can cover the mooring requirements of all aircraft models. If they cannot cover, increase the value of N and repeat steps 2 and 3; if they can cover, stop the optimization process to obtain the minimum number of ground anchor layouts and the corresponding point information that meet the mooring requirements of each aircraft model.

[0071] S6. Generate and output a multi-aircraft model combined ground anchor layout diagram based on the number of ground anchor layouts and the corresponding point information.

[0072] In this step, based on the number of ground anchor arrangements and the corresponding point position information, a multi-aircraft combined ground anchor arrangement diagram is generated and output, including:

[0073] Calculate the distance from each ground anchor point to the first stop line based on the minimum number of ground anchor arrangements, the corresponding point position information, and the coordinate data of the first stop line;

[0074] Generate a multi-aircraft combined ground anchor arrangement diagram based on the minimum number of ground anchor arrangements, the corresponding point position information, and each distance;

[0075] Output the multi-aircraft combined ground anchor arrangement diagram

[0076] Specifically, the multi-aircraft combined ground anchor arrangement diagram is as Figure 4 shown. The aircraft types allowed to park are marked beside the stop line. The clear indication of applicable aircraft types for this position supports the parking of aircraft such as A319, A320-100, B737-800, A321-100, etc.; The overlapping area 8 between the ground anchor demand area and the existing ground anchor point positions of the aircraft positions is used to determine the minimum number of ground anchor arrangements and the corresponding point position information that meet the mooring requirements of each aircraft type using a clustering algorithm. The number and position of the ground anchors 9 are the minimum number and position of the ground anchor arrangements. The dimension marking 10 shows the distance from the ground anchor 9 to the first stop line; The multi-aircraft combined ground anchor arrangement diagram clearly presents the ground anchor arrangement plan for multiple aircraft types in a visual manner. The specific number of ground anchors and the point position information of each ground anchor are clearly marked in the figure, enabling relevant personnel to clearly understand the distribution of ground anchors on the aircraft position at a glance; The ground anchor arrangement diagram provides accurate installation position guidance for ground anchor installers. Installers can accurately determine the installation positions of ground anchors on the airport aircraft position according to the point position information marked on the figure, ensuring the accuracy and standardization of ground anchor installation, thereby improving the quality and efficiency of ground anchor installation. By optimizing the ground anchor arrangement, the repeated setting and unreasonable distribution of ground anchors are avoided, and the utilization efficiency of airport aircraft position resources is improved.

[0077] Embodiment 2

[0078] This embodiment provides a multi-aircraft combined ground anchor arrangement device, including:

[0079] Loading module: used to load the existing ground anchor point position resource map of the aircraft position, the coordinate data of each stop line, and the scale; load the ground anchor arrangement diagram of the corresponding aircraft type based on the aircraft type information of the ground anchor to be combined;

[0080] Overlay module, used to perform overlay processing on each ground anchor arrangement diagram and the existing ground anchor point position resource map of the aircraft position based on the scale and the coordinate data of each stop line to obtain a combined ground anchor arrangement diagram;

[0081] Image processing module, used to perform image processing on the combined ground anchor arrangement diagram to extract the ground anchor demand area and the existing ground anchor points of the aircraft position;

[0082] An optimization module, configured to determine the minimum number of ground anchor arrangements and the corresponding point information that meet the mooring requirements of each aircraft type by using a clustering algorithm based on the ground anchor demand area and the existing ground anchor point resources of the aircraft positions;

[0083] A generation and output module, configured to generate and output a multi-aircraft combined ground anchor arrangement diagram based on the number of ground anchor arrangements and the corresponding point information.

[0084] Embodiment 3

[0085] This embodiment of the present disclosure further provides an electronic device, which includes:

[0086] At least one processor; and,

[0087] A memory communicatively connected to the at least one processor; wherein,

[0088] The memory stores instructions executable by the at least one processor, and the instructions are executed by the at least one processor so that the at least one processor can execute the multi-aircraft combined ground anchor arrangement method in Embodiment 1.

[0089] The electronic device according to the embodiment of the present disclosure includes a memory and a processor, and the memory is used to store non-temporary computer-readable instructions. Specifically, the memory may include one or more computer program products, and the computer program products may include various forms of computer-readable storage media, such as volatile memory and / or non-volatile memory. The volatile memory may include, for example, random access memory (RAM) and / or cache memory, etc. The non-volatile memory may include, for example, read-only memory (ROM), hard disk, flash memory, etc.

[0090] The processor may be a central processing unit (CPU) or other forms of processing units with data processing capabilities and / or instruction execution capabilities, and may control other components in the electronic device to perform desired functions. In an embodiment of the present disclosure, the processor is used to run the computer-readable instructions stored in the memory.

[0091] Those skilled in the art should understand that, in order to solve the technical problem of how to obtain good user experience effects, this embodiment may also include well-known structures such as communication buses and interfaces, and these well-known structures should also be included in the protection scope of the present disclosure.

[0092] For a detailed description of this embodiment, reference may be made to the corresponding descriptions in the foregoing embodiments, and details will not be repeated here.

[0093] Embodiment 4

[0094] An embodiment of the present disclosure provides a non-transitory computer-readable storage medium storing computer instructions for causing a computer to execute the multi-model combined ground anchor arrangement method in Embodiment 1.

[0095] A computer-readable storage medium according to an embodiment of the present disclosure stores non-temporary computer-readable instructions. When the non-temporary computer-readable instructions are run by a processor, all or part of the steps of the methods of the various embodiments of the present disclosure described above are executed.

[0096] The above computer-readable storage medium includes but is not limited to: optical storage media (such as CD-ROMs and DVDs), magneto-optical storage media (such as MOs), magnetic storage media (such as magnetic tapes or external hard drives), media with built-in rewritable non-volatile memories (such as memory cards), and media with built-in ROMs (such as ROM cartridges).

[0097] The various embodiments of the present invention have been described above. The above description is exemplary and not exhaustive, and is also not limited to the disclosed embodiments. Many modifications and variations are obvious to those of ordinary skill in the art without departing from the scope and spirit of the described embodiments.

Claims

1. A method for arranging a multi-type combined ground anchor, characterized in that: include: Load the existing anchor point resource map, coordinate data and scale of each stop line; Load the anchor layout diagram of the corresponding model based on the model information of the anchor to be combined; Based on the scale and the coordinate data of each stop line, each of the ground anchor arrangement diagrams and the existing ground anchor point resource map are superimposed to obtain a combined ground anchor arrangement diagram; Performing image processing on the combined ground anchor arrangement diagram to extract the ground anchor requirement area and the existing ground anchor points; Based on the anchor demand area and the existing anchor point resources, a clustering algorithm is used to determine the minimum number of anchor arrangements and corresponding point information that meet the mooring requirements of each aircraft type; A multi-model combined ground anchor layout diagram is generated and output based on the number of ground anchor layouts and the corresponding point information.

2. The method for arranging multiple types of combined ground anchors according to claim 1, characterized in that: Before the model information of the ground anchor to be combined is loaded with the ground anchor layout diagram of the corresponding model, the method further includes: The validity of each stop line coordinate data is verified based on the existing aircraft position anchor point resource map.

3. The method for arranging multiple types of combined ground anchors according to claim 1, characterized in that: The image processing of the combined anchor arrangement diagram comprises: Marking the anchor requirement area and existing anchor points of the combined anchor arrangement diagram as shaded areas; Converting the marked combined anchor arrangement diagram into a picture; The shadow area is extracted from the image based on the HSV color space, and the shadow area is converted into a binary mask.

4. The method for arranging multiple types of combined ground anchors according to claim 1, characterized in that: The clustering algorithm includes: K-Means algorithm.

5. The method for arranging multiple types of combined ground anchors according to claim 1, characterized in that: The method of using a clustering algorithm to determine the minimum number of anchor arrangements and corresponding point information that meet the mooring requirements of each aircraft type based on the anchor demand area and the existing anchor point resources includes: Extracting overlapping areas based on the anchor demand area and the existing anchor point resources; Based on the overlapping area, a clustering algorithm is used to determine the minimum number of anchor arrangements and corresponding point information that meet the mooring requirements of each model.

6. The method for arranging multiple types of combined ground anchors according to claim 1, characterized in that: The corresponding machine model is marked at each stop line of the combined ground anchor arrangement diagram.

7. The method for arranging multiple types of combined ground anchors according to claim 1, characterized in that: The generating and outputting of a multi-model combined ground anchor layout diagram based on the number of ground anchor layouts and corresponding point information includes: Calculate the distance from each anchor point to the first stop line based on the minimum number of anchors arranged, the corresponding point information and the coordinate data of the first stop line; Generate a multi-model combined ground anchor layout diagram based on the minimum number of ground anchor layouts, the corresponding point information, and each of the distances; Output the multi-model combined ground anchor layout diagram.

8. A multi-model combined ground anchor arrangement device, characterized in that: include: Loading module: used to load the existing aircraft anchor point resource map, each stop line coordinate data and scale; Load the anchor layout diagram of the corresponding model based on the model information of the anchor to be combined; A superposition module, configured to superimpose each of the ground anchor arrangement diagrams and the existing ground anchor point resource diagram based on the scale and the coordinate data of each of the stop lines to obtain a combined ground anchor arrangement diagram; An image processing module is used to perform image processing on the combined ground anchor arrangement diagram to extract the ground anchor requirement area and the existing ground anchor points; An optimization module, configured to determine the minimum number of anchor arrangements and corresponding point information that meet the mooring requirements of each aircraft type by using a clustering algorithm based on the anchor demand area and the existing anchor point resources; A generation and output module is used to generate and output a multi-model combined ground anchor layout diagram based on the number of ground anchor layouts and corresponding point information.

9. An electronic device, characterized in that: The electronic device comprises: at least one processor; and, a memory communicatively connected to the at least one processor; wherein, The memory stores instructions that can be executed by the at least one processor, and the instructions are executed by the at least one processor so that the at least one processor can execute the multi-machine combination ground anchor deployment method described in any one of claims 1-7.

10. A non-transitory computer-readable storage medium, characterized in that: The non-transitory computer-readable storage medium stores computer instructions, and the computer instructions are used to enable a computer to execute the multi-type combined anchor deployment method described in any one of claims 1-7.

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