Determination method and device of corner reflector deployment scheme and readable storage medium

Abstract

The invention discloses a corner reflector deployment scheme determination method and device, and a readable storage medium. The method comprises the steps of obtaining environment parameters corresponding to a point location to be deployed and a moving track of a detector; determining a distance direction straight line corresponding to the point to be deployed according to the moving trajectory, and determining a point location to be deployed according to the environmental parameters; determining a first connecting line parallel to the moving track and a second connecting line parallel to the distance direction straight line in connecting lines corresponding to the adjacent to-be-selected deployment point locations; taking the to-be-selected deployment point location corresponding to the first connection line with the length greater than the direction effect distance and / or the second connection line with the length greater than the distance direction effect distance as a target deployment point location; and a corner reflector deployment scheme is generated according to the coordinates of the target deployment point location, so that the technical problem of low monitoring precision caused by poor anti-interference capability of a corner reflector in related technologies is effectively solved, and the technical effect of accurately detecting the building deformation degree is further achieved.

Description

Technical Field

[0001] The present application relates to the field of radar detection, and in particular to a method for determining a corner reflector deployment scheme, a device for determining a corner reflector deployment scheme, and a computer-readable storage medium. Background Art

[0002] Radar corner reflectors are usually three-dimensional rigid structures composed of two or three mutually perpendicular metal planes. Due to the special geometric structure, radar electromagnetic waves irradiated on the corner reflector can produce multiple reflections inside it, and finally reflect the radar electromagnetic waves back along the incident direction. Therefore, the corner reflector has a strong radar scattering cross section and can be regarded as an echo enhancement device.

[0003] In related technologies, corner reflectors can be used in fields such as safety monitoring of important urban buildings and deformation monitoring of bridges. For example, they can be used in synthetic aperture radar for deformation detection to monitor whether the building has deformed or determine the degree of deformation of the building.

[0004] However, in traditional building deformation monitoring methods, corner reflectors have poor anti-interference capabilities, resulting in low monitoring accuracy and cannot meet the needs of three-dimensional deformation monitoring. Summary of the invention

[0005] The embodiments of the present application provide a method for determining a corner reflector deployment plan, a device for determining a corner reflector deployment plan, and a computer-readable storage medium, thereby solving the technical problem in the related art that the corner reflectors have poor anti-interference ability, resulting in low monitoring accuracy and unable to meet the three-dimensional deformation monitoring requirements, and achieves the technical effect of accurately detecting the degree of building deformation.

[0006] The embodiment of the present application provides a method for determining a corner reflector deployment scheme, and the method for determining a corner reflector deployment scheme includes:

[0007] Obtain the environmental parameters corresponding to the points to be deployed and the running trajectory of the detector;

[0008] Determine the distance straight line corresponding to the to-be-deployed point according to the running trajectory, and determine the to-be-selected deployment point according to the environmental parameters;

[0009] Determine, among the lines corresponding to the adjacent to-be-selected deployment points, a first line parallel to the running track and a second line parallel to the distance straight line;

[0010] The first connecting line having a length greater than the directional effect distance and / or the to-be-selected deployment point corresponding to the second connecting line having a length greater than the distance effect distance are used as target deployment points;

[0011] A corner reflector deployment plan is generated according to the coordinates of the target deployment points.

[0012] Optionally, before the step of taking the first link having a length greater than the directional effect distance and / or the candidate deployment point corresponding to the second link having a length greater than the distance directional effect distance as the target deployment point, the step further includes:

[0013] Determining the directional resolution of the detector corresponding to the running trajectory and the range resolution corresponding to the range straight line;

[0014] Obtain preset directional effect parameters and distance effect parameters;

[0015] The directional effect distance is determined according to the directional resolution and the directional effect parameter, and the distance effect distance is determined according to the distance resolution and the distance effect parameter.

[0016] Optionally, the environmental parameters include at least one of a radio interference value, a power transmission interference value, a satellite signal strength value, longitude and latitude coordinates, and an optical image.

[0017] Optionally, determining the to-be-selected deployment point according to the environmental parameters includes:

[0018] Acquire the incident signal cross section of the detector at the latitude and longitude coordinates;

[0019] Determine, according to the optical image, a point to be deployed where there are no obstacles in the incident signal cross section;

[0020] The signal interference value of the to-be-deployed point is determined based on the environmental parameter, and the to-be-selected deployment point whose signal interference value meets the preset deployment condition is screened.

[0021] Optionally, determining the signal interference value of the to-be-deployed point based on the environmental parameter, and screening the to-be-deployed point whose signal interference value meets a preset deployment condition includes:

[0022] Acquire the three-dimensional coordinates of the point to be deployed, and calculate the radar coordinates corresponding to the point to be deployed by combining the three-dimensional coordinates and the longitude and latitude coordinates;

[0023] Obtaining a radar map and determining a background reflection intensity value at the radar coordinates;

[0024] When the background reflection intensity value is less than or equal to a first threshold, the radio interference value is less than or equal to a second threshold, the power transmission interference value is less than or equal to a third threshold, and the satellite signal strength value is greater than or equal to a third threshold, the to-be-deployed point is determined to be the to-be-selected deployment point.

[0025] Optionally, the determining of the connecting lines corresponding to the adjacent to-be-selected deployment points, a first connecting line parallel to the running track and a second connecting line parallel to the distance straight line, comprises:

[0026] Determining a connection line between adjacent candidate deployment points;

[0027] Determine a first angle between the connecting line and the running track, and a second angle between the connecting line and the distance straight line;

[0028] When the first included angle is smaller than a first preset angle, determining the connecting line to be the first connecting line;

[0029] When the second included angle is smaller than the second preset angle, the connecting line is determined to be the second connecting line.

[0030] Optionally, before the step of generating a corner reflector deployment plan according to the coordinates of the target deployment point, the step further includes:

[0031] When the first angle is greater than the first preset angle, and the second angle is greater than the second preset angle, the to-be-selected deployment point is determined to be the target deployment point.

[0032] Optionally, generating a corner reflector deployment plan according to the coordinates of the target deployment point includes:

[0033] Determine an unqualified deployment point where the length of the first link is less than the directional effect distance, or the length of the second link is less than the distance effect distance;

[0034] The unqualified deployment points are removed, and the corner reflector deployment plan is generated according to the latitude and longitude coordinates of the screened target deployment points.

[0035] In addition, the present application also proposes a device for determining a corner reflector deployment scheme, which includes a memory, a processor, and a corner reflector deployment scheme determination program stored in the memory and executable on the processor, and when the processor executes the corner reflector deployment scheme determination program, it implements the steps of the corner reflector deployment scheme determination method as described above.

[0036] In addition, the present application also proposes a computer-readable storage medium, on which a program for determining a corner reflector deployment plan is stored. When the program for determining a corner reflector deployment plan is executed by a processor, the steps of the method for determining a corner reflector deployment plan as described above are implemented.

[0037] One or more technical solutions provided in the embodiments of the present application have at least the following technical effects or advantages:

[0038] 1. The environmental parameters corresponding to the points to be deployed and the running trajectory of the detector are obtained; the distance straight line corresponding to the points to be deployed is determined according to the running trajectory, and the selected deployment points are determined according to the environmental parameters; the first connecting line parallel to the running trajectory and the second connecting line parallel to the distance straight line are determined among the connecting lines corresponding to the adjacent selected deployment points; the selected deployment points corresponding to the first connecting line whose length is greater than the directional effect distance and / or the second connecting line whose length is greater than the distance effect distance are taken as target deployment points; the corner reflector deployment plan is generated according to the coordinates of the target deployment points. Therefore, the technical problem that the corner reflector has poor anti-interference ability in the related art, resulting in low monitoring accuracy and cannot meet the three-dimensional deformation monitoring requirements is effectively solved, thereby achieving the technical effect of accurately detecting the degree of building deformation. BRIEF DESCRIPTION OF THE DRAWINGS

[0039] Figure 1 This is a flow chart of Embodiment 1 of a method for determining a corner reflector deployment scheme of the present application;

[0040] Figure 2 This is a flow chart of Embodiment 2 of the method for determining the corner reflector deployment scheme of the present application;

[0041] Figure 3 This is a flow chart of Embodiment 3 of the method for determining the corner reflector deployment scheme of the present application;

[0042] Figure 4 This is a schematic diagram of the hardware structure involved in an embodiment of a device for determining a corner reflector deployment solution of the present application. DETAILED DESCRIPTION

[0043] In the related art, synthetic aperture radar is usually used for deformation detection to monitor whether a building has been deformed or to determine the degree of deformation of the building. However, the anti-interference ability of the corner reflector used to reflect the signal is poor, resulting in low monitoring accuracy and failure to meet the three-dimensional deformation monitoring requirements. The main technical solution adopted in the embodiment of the present application is: obtaining the running trajectory of the detector and the environmental parameters of the point to be deployed, and determining the distance straight line perpendicular to the running trajectory, screening out the target deployment points that meet the deployment conditions according to the distance between adjacent points to be deployed, and generating a corner reflector deployment plan according to the coordinates of the target deployment points. This achieves accurate detection of the degree of building deformation.

[0044] In order to better understand the above technical solution, exemplary embodiments of the present application will be described in more detail below with reference to the accompanying drawings. Although exemplary embodiments of the present application are shown in the accompanying drawings, it should be understood that the present application can be implemented in various forms and should not be limited by the embodiments described herein. On the contrary, these embodiments are provided in order to enable a more thorough understanding of the present application and to fully convey the scope of the present application to those skilled in the art.

[0045] Embodiment 1

[0046] Embodiment 1 of the present application discloses a method for determining a corner reflector deployment scheme, referring to Figure 1 , the method for determining the corner reflector deployment scheme includes:

[0047] Step S110, obtaining environmental parameters corresponding to the points to be deployed and the running trajectory of the detector;

[0048] In this embodiment, the points to be deployed can be pre-set according to the architectural drawings or maps of the construction site, and the environmental parameters are the parameters required to meet the deployment conditions. The detector can be a radar, and the running track is the projection of the detector's trajectory around the earth on the earth's surface.

[0049] As an optional implementation manner, the environmental parameter may be at least one of a radio interference value, a power transmission interference value, a satellite signal strength value, a latitude and longitude coordinates, and an optical image.

[0050] Step S120, determining the distance straight line corresponding to the to-be-deployed point according to the running trajectory, and determining the to-be-selected deployment point according to the environmental parameters;

[0051] In this embodiment, the distance straight line is perpendicular to the running track on the ground plane, that is, the distance straight line and the running track form a rectangular coordinate system on the ground plane. The deployment points to be selected are screened according to whether the environmental parameters meet the preset deployment conditions.

[0052] As an optional implementation, the projection of the running trajectory on the plane where the point to be deployed is located is determined, and a straight line on the plane that is perpendicular to the projection is used as the distance straight line.

[0053] Optionally, step S120 includes:

[0054] Step S121, obtaining the incident signal cross section of the detector at the latitude and longitude coordinates;

[0055] Step S122, determining, according to the optical image, a point to be deployed where no obstacle exists in the incident signal cross section;

[0056] Step S123, determining the signal interference value of the to-be-deployed point based on the environmental parameters, and screening the to-be-selected deployment points whose signal interference values ​​meet the preset deployment conditions.

[0057] In this embodiment, the detection signal emitted by the detector to a point can be regarded as a cone, the vertex of the cone is the detector, and the bottom surface is the plane where the point to be deployed is located.

[0058] As an optional implementation, determine the longitude and latitude coordinates of the point to be deployed, obtain the cross section of the incident signal of the detector at the longitude and latitude coordinates, determine whether there is an obstacle between the point to be deployed and the detector based on the acquired optical image, and select the point to be deployed without obstacles. Determine the point to be deployed without obstacles; determine the signal interference value based on the environmental parameters of the point to be deployed, and select the point to be deployed whose signal interference value meets the preset deployment conditions as the selected deployment point.

[0059] Exemplarily, based on the acquired environmental parameters, a corresponding weight value is determined for each environmental parameter according to a preset calculation formula, and then the signal interference value is calculated.

[0060] Exemplarily, the acquired environmental parameters are all regarded as signal interference values, and when each environmental parameter satisfies the corresponding deployment condition, the to-be-deployed point is determined as a to-be-selected deployment point.

[0061] Optionally, step S123 includes:

[0062] Step S1231, obtaining the three-dimensional coordinates of the point to be deployed, and calculating the radar coordinates corresponding to the point to be deployed by combining the three-dimensional coordinates and the longitude and latitude coordinates;

[0063] Step S1232, obtaining a radar map, and determining the background reflection intensity value at the radar coordinates;

[0064] Step S1233, when the background reflection intensity value is less than or equal to the first threshold, the radio interference value is less than or equal to the second threshold, the power transmission interference value is less than or equal to the third threshold, and the satellite signal strength value is greater than or equal to the third threshold, the to-be-deployed point is determined to be the to-be-selected deployment point.

[0065] As an optional implementation, collect laser point cloud data at the point to be deployed to establish a three-dimensional model of the point to be deployed; determine the three-dimensional coordinates of the point to be deployed in the three-dimensional model, and combine the three-dimensional coordinates and the longitude and latitude coordinates to infer the radar coordinates of the point to be deployed according to a preset algorithm; obtain the radar map corresponding to the detector, and determine the background reflection intensity value at the point to be deployed according to the radar data in the radar map; when the background reflection intensity value is less than or equal to the first threshold, the radio interference value is less than or equal to the second threshold, the power transmission interference value is less than or equal to the third threshold, and the satellite signal strength value is greater than or equal to the third threshold, determine that the point to be deployed is the selected deployment point. The first threshold, the second threshold, and the third threshold are predetermined.

[0066] Step S130, determining, among the lines corresponding to the adjacent to-be-selected deployment points, a first line parallel to the running track and a second line parallel to the distance straight line;

[0067] Step S140, taking the candidate deployment point corresponding to the first link whose length is greater than the directional effect distance and / or the second link whose length is greater than the distance effect distance as the target deployment point;

[0068] In this embodiment, the connecting line is a straight line between adjacent candidate deployment points, and the directional effect distance and the distance effect distance are the minimum distances in two perpendicular directions without generating a side lobe effect. When the distance between the candidate deployment points is less than the directional effect distance or the distance effect distance, deploying a corner reflector at this point will generate a side lobe effect.

[0069] As an optional implementation, determine the connecting lines between adjacent candidate deployment points, select the connecting line parallel to the running trajectory as the first connecting line; select the connecting line parallel to the distance straight line as the second connecting line; determine the first connecting line whose length is greater than the directional effect distance and the second connecting line whose length is greater than the distance effect distance; and use the candidate deployment points at the endpoints of the above-mentioned first connecting line and the second connecting line as the target deployment points.

[0070] For example, it may happen that the line connecting point one and point two is greater than the directional effect distance or the distance effect distance, but the line connecting point two and point three is less than the directional effect distance or the distance effect distance. At this time, point two should be determined as the target deployment point, while point three is not the target deployment point.

[0071] Step S150, generating a corner reflector deployment plan according to the coordinates of the target deployment point.

[0072] Optionally, step S150 includes:

[0073] Step S151, determining an unqualified deployment point where the length of the first link is less than the directional effect distance, or the length of the second link is less than the distance effect distance;

[0074] Step S152, removing the unqualified deployment points, and generating the corner reflector deployment plan according to the latitude and longitude coordinates of the screened target deployment points.

[0075] As an optional implementation, determine the unqualified deployment points where the length of the first connecting line is less than the directional effect distance, or the second connecting line is less than the distance effect distance, wherein when the connecting line between an unqualified deployment point and point one is less than the directional effect distance or the distance effect distance, but the length of the connecting line with point two is greater than the directional effect distance or the distance effect distance, it should be determined as a target deployment point. Remove the unqualified deployment points, and generate a corner reflector deployment plan based on the latitude and longitude coordinates of the screened target deployment points, wherein the plan also includes the elevation angle of the corner reflector installation.

[0076] Optionally, the optical images at the target deployment points are analyzed to screen out points that do not meet the installation conditions as unqualified points. For example, there is water leakage or other adverse conditions at the points.

[0077] The technical solutions in the above embodiments of the present application have at least the following technical effects or advantages:

[0078] The method adopts the following steps: obtaining the environmental parameters corresponding to the point to be deployed and the running trajectory of the detector; determining the distance straight line corresponding to the point to be deployed according to the running trajectory, and determining the selected deployment point according to the environmental parameters; determining the first line parallel to the running trajectory and the second line parallel to the distance straight line among the lines corresponding to the adjacent selected deployment points; taking the selected deployment point corresponding to the first line whose length is greater than the directional effect distance and / or the second line whose length is greater than the distance effect distance as the target deployment point; generating the corner reflector deployment plan according to the coordinates of the target deployment point. Therefore, the technical problem that the corner reflector has poor anti-interference ability, resulting in low monitoring accuracy and cannot meet the three-dimensional deformation monitoring requirements in the related technology is effectively solved, thereby achieving the technical effect of accurately detecting the degree of building deformation.

[0079] Embodiment 2

[0080] Based on the first embodiment, the second embodiment of the present application proposes a method for determining a corner reflector deployment scheme, referring to Figure 2 , before step S140, further comprising:

[0081] Step S210, determining the directional resolution of the detector corresponding to the running track, and the range resolution corresponding to the range straight line;

[0082] Step S220, obtaining preset directional effect parameters and distance effect parameters;

[0083] Step S230: determining the directional effect distance according to the directional resolution and the directional effect parameter, and determining the distance effect distance according to the distance resolution and the distance effect parameter.

[0084] In this embodiment, the directional resolution is the resolution of the information acquired by the detector in the direction of the running track, and the range resolution is the resolution of the information acquired by the detector in the range straight line direction. The directional effect parameter and the range effect parameter are determined based on experimental data.

[0085] As an optional implementation, the directional resolution of the detector in the direction of the running track is determined, and the range resolution in the range straight line direction is determined, and the obtained directional resolution and range resolution are averaged to obtain the directional resolution and the range resolution. The preset directional effect parameter and the range effect parameter are obtained; the directional resolution is multiplied by the directional effect parameter to obtain the directional effect distance; the range resolution is multiplied by the range effect parameter to obtain the range effect distance.

[0086] The technical solutions in the above embodiments of the present application have at least the following technical effects or advantages:

[0087] Since the directional effect distance is determined according to the directional resolution and the directional effect parameter, and the distance effect distance is determined according to the distance resolution and the distance effect parameter, the technical problem of the side lobe effect when the corner reflector is installed in the related technology is effectively solved, thereby achieving effective and convenient avoidance of the side lobe effect between corner reflectors.

[0088] Embodiment 3

[0089] Based on Example 1, Example 3 of the present application proposes a method for determining a corner reflector deployment scheme, referring to Figure 3 , step S130 includes:

[0090] Step S310, determining the connection lines between the adjacent candidate deployment points;

[0091] Step S320, determining a first angle between the connecting line and the running track, and a second angle between the connecting line and the distance straight line;

[0092] Step S330, when the first angle is less than a first preset angle, determining the connecting line to be the first connecting line;

[0093] Step S340: when the second included angle is smaller than the second preset angle, determining the connecting line as the second connecting line.

[0094] In this embodiment, when the angle between the connecting line between the candidate deployment points and the running trajectory or the distance straight line is less than a preset angle, it is also determined that the connecting line is parallel to the running trajectory or the distance straight line.

[0095] As an optional implementation, determine the connecting lines between adjacent to-be-selected deployment points, determine the angle between each connecting line and the running trajectory as the first angle; determine the angle between each connecting line and the distance straight line as the second angle; when the first angle is less than the first preset angle, determine the connecting line as the first connecting line; when the second angle is less than the second preset angle, determine the connecting line as the second connecting line.

[0096] For example, according to the resolution of the detector, when the resolution is smaller, that is, the detection accuracy is higher, the preset angle is smaller; otherwise, it is larger.

[0097] Exemplarily, the first preset angle is 30 degrees, and the second preset angle is 25 degrees.

[0098] Optionally, before step S150, the method further includes:

[0099] Step S350: When the first angle is greater than the first preset angle, and the second angle is greater than the second preset angle, determining the candidate deployment point as the target deployment point.

[0100] As an optional implementation, when the first angle is greater than the first preset angle and the second angle of the line is greater than the second preset angle, the two candidate deployment points corresponding to the line are determined to be target deployment points.

[0101] Exemplarily, if there is no first connection line or second connection line between the two candidate deployment points and other candidate deployment points, the two candidate deployment points corresponding to the connection line are determined to be target deployment points.

[0102] For example, if there is a first connection line or a second connection line between the two candidate deployment points and other candidate deployment points, it is necessary to re-determine whether the length of the first connection line or the second connection line is greater than the directional effect distance or the distance effect distance.

[0103] Optionally, the finally determined target deployment point does not have any first line or second line with other target deployment points, or the lengths of the existing first lines are greater than the directional effect distance; the lengths of the existing second lines are greater than the distance effect distance.

[0104] The technical solutions in the above embodiments of the present application have at least the following technical effects or advantages:

[0105] Since the method adopts the method of determining the connecting line between the adjacent selected deployment points, determining the first angle between the connecting line and the running track, and the second angle between the connecting line and the distance straight line, when the first angle is less than the first preset angle, determining the connecting line as the first connecting line, and when the second angle is less than the second preset angle, determining the connecting line as the second connecting line, the technical problem that the corner reflector in the related technology has poor anti-interference ability, resulting in low monitoring accuracy and cannot meet the three-dimensional deformation monitoring requirements is effectively solved, thereby achieving the technical effect of accurately detecting the degree of building deformation.

[0106] This application also proposes a device for determining a corner reflector deployment scheme, referring to Figure 4 , Figure 4 A schematic diagram of the device structure for determining a corner reflector deployment scheme for the hardware operating environment involved in an embodiment of the present application.

[0107] like Figure 4 As shown, the device for determining the corner reflector deployment scheme may include: a processor 1001, such as a central processing unit (CPU), a communication bus 1002, a user interface 1003, a network interface 1004, and a memory 1005. Among them, the communication bus 1002 is used to realize the connection and communication between these components. The user interface 1003 may include a display screen (Display), an input unit such as a keyboard (Keyboard), and the user interface 1003 may optionally include a standard wired interface and a wireless interface. The network interface 1004 may optionally include a standard wired interface and a wireless interface (such as a wireless fidelity (WIreless-FIdelity, WI-FI) interface). The memory 1005 may be a high-speed random access memory (Random Access Memory, RAM) memory, or a stable non-volatile memory (Non-Volatile Memory, NVM), such as a disk memory. The memory 1005 may optionally be a storage device independent of the aforementioned processor 1001.

[0108] Those skilled in the art will understand that Figure 4 The structure shown in the figure does not constitute a limitation on the device for determining the corner reflector deployment scheme, and may include more or less components than shown in the figure, or a combination of certain components, or a different deployment of components.

[0109] Optionally, the memory 1005 is electrically connected to the processor 1001, and the processor 1001 can be used to control the operation of the memory 1005, and can also read the data in the memory 1005 to determine the corner reflector deployment plan.

[0110] Alternatively, if Figure 4 As shown, the memory 1005 as a storage medium may include an operating system, a data storage module, a network communication module, a user interface module, and a program for determining a corner reflector deployment plan.

[0111] Optionally, in Figure 4 In the device for determining the corner reflector deployment plan shown, the network interface 1004 is mainly used for data communication with other devices; the user interface 1003 is mainly used for data interaction with the user; the processor 1001 and the memory 1005 in the device for determining the corner reflector deployment plan of the present application can be set in the device for determining the corner reflector deployment plan.

[0112] like Figure 4 As shown, the corner reflector deployment scheme determination device calls the corner reflector deployment scheme determination program stored in the memory 1005 through the processor 1001, and executes the relevant steps of the corner reflector deployment scheme determination method provided in the embodiment of the present application:

[0113] Obtain the environmental parameters corresponding to the points to be deployed and the running trajectory of the detector;

[0114] Determine the distance straight line corresponding to the to-be-deployed point according to the running trajectory, and determine the to-be-selected deployment point according to the environmental parameters;

[0115] Determine, among the lines corresponding to the adjacent to-be-selected deployment points, a first line parallel to the running track and a second line parallel to the distance straight line;

[0116] The first connecting line having a length greater than the directional effect distance and / or the to-be-selected deployment point corresponding to the second connecting line having a length greater than the distance effect distance are used as target deployment points;

[0117] A corner reflector deployment plan is generated according to the coordinates of the target deployment points.

[0118] Optionally, the processor 1001 may call a corner reflector deployment scheme determination program stored in the memory 1005, and further perform the following operations:

[0119] Determining the directional resolution of the detector corresponding to the running trajectory and the range resolution corresponding to the range straight line;

[0120] Obtain preset directional effect parameters and distance effect parameters;

[0121] The directional effect distance is determined according to the directional resolution and the directional effect parameter, and the distance effect distance is determined according to the distance resolution and the distance effect parameter.

[0122] Optionally, the processor 1001 can call a determination program for the corner reflector deployment plan stored in the memory 1005, and also perform the following operations: the environmental parameters include at least one of a radio interference value, a power transmission interference value, a satellite signal strength value, longitude and latitude coordinates, and an optical image.

[0123] Optionally, the processor 1001 may call a corner reflector deployment scheme determination program stored in the memory 1005, and further perform the following operations:

[0124] Acquire the incident signal cross section of the detector at the latitude and longitude coordinates;

[0125] Determine, according to the optical image, a point to be deployed where there are no obstacles in the incident signal cross section;

[0126] The signal interference value of the to-be-deployed point is determined based on the environmental parameter, and the to-be-selected deployment point whose signal interference value meets the preset deployment condition is screened.

[0127] Optionally, the processor 1001 may call a corner reflector deployment scheme determination program stored in the memory 1005, and further perform the following operations:

[0128] Acquire the three-dimensional coordinates of the point to be deployed, and calculate the radar coordinates corresponding to the point to be deployed by combining the three-dimensional coordinates and the longitude and latitude coordinates;

[0129] Obtaining a radar map and determining a background reflection intensity value at the radar coordinates;

[0130] When the background reflection intensity value is less than or equal to a first threshold, the radio interference value is less than or equal to a second threshold, the power transmission interference value is less than or equal to a third threshold, and the satellite signal strength value is greater than or equal to a third threshold, the to-be-deployed point is determined to be the to-be-selected deployment point.

[0131] Optionally, the processor 1001 may call a corner reflector deployment scheme determination program stored in the memory 1005, and further perform the following operations:

[0132] Determining a connection line between adjacent candidate deployment points;

[0133] Determine a first angle between the connecting line and the running track, and a second angle between the connecting line and the distance straight line;

[0134] When the first included angle is smaller than a first preset angle, determining the connecting line to be the first connecting line;

[0135] When the second included angle is smaller than the second preset angle, the connecting line is determined to be the second connecting line.

[0136] Optionally, the processor 1001 may call a corner reflector deployment scheme determination program stored in the memory 1005, and further perform the following operations:

[0137] When the first angle is greater than the first preset angle, and the second angle is greater than the second preset angle, the to-be-selected deployment point is determined to be the target deployment point.

[0138] Optionally, the processor 1001 may call a corner reflector deployment scheme determination program stored in the memory 1005, and further perform the following operations:

[0139] Determine an unqualified deployment point where the length of the first link is less than the directional effect distance, or the length of the second link is less than the distance effect distance;

[0140] The unqualified deployment points are removed, and the corner reflector deployment plan is generated according to the latitude and longitude coordinates of the screened target deployment points.

[0141] In addition, an embodiment of the present application also proposes a computer-readable storage medium, on which a program for determining a corner reflector deployment plan is stored. When the program for determining a corner reflector deployment plan is executed by a processor, the relevant steps of any embodiment of the method for determining a corner reflector deployment plan as described above are implemented.

[0142] Those skilled in the art will appreciate that the embodiments of the present application may be provided as methods, systems, or computer program products. Therefore, the present application may adopt the form of a complete hardware embodiment, a complete software embodiment, or an embodiment in combination with software and hardware. Moreover, the present application may adopt the form of a computer program product implemented in one or more computer-usable storage media (including but not limited to disk storage, CD-ROM, optical storage, etc.) that include computer-usable program code.

[0143] The present application is described with reference to the flowcharts and / or block diagrams of the methods, devices (systems), and computer program products according to the embodiments of the present application. It should be understood that each process and / or box in the flowchart and / or block diagram, as well as the combination of the processes and / or boxes in the flowchart and / or block diagram, can be implemented by computer program instructions. These computer program instructions can be provided to a processor of a general-purpose computer, a special-purpose computer, an embedded processor, or other programmable data processing device to generate a machine, so that the instructions executed by the processor of the computer or other programmable data processing device generate instructions for implementing the processes in the flowchart and / or block diagram. Figure 1 A process or multiple processes and / or boxes Figure 1 A device that provides the functions specified in a block or multiple blocks.

[0144] These computer program instructions may also be stored in a computer readable memory capable of directing a computer or other programmable data processing device to operate in a specific manner, so that the instructions stored in the computer readable memory produce an article of manufacture including an instruction device, which implements the process Figure 1 A process or multiple processes and / or boxes Figure 1 A function specified in one or more boxes.

[0145] These computer program instructions can also be loaded onto a computer or other programmable data processing device so that a series of operating steps are executed on the computer or other programmable device to produce a computer-implemented process, thereby providing instructions for implementing the process in the computer or other programmable device. Figure 1 A process or multiple processes and / or boxes Figure 1 The steps for the functions specified in one or more boxes.

[0146] It should be noted that in the claims, any reference signs placed between brackets shall not be construed as limiting the claims. The word "comprising" does not exclude the presence of components or steps not listed in the claims. The word "a" or "an" preceding a component does not exclude the presence of a plurality of such components. The present application may be implemented by means of hardware comprising several different components and by means of a suitably programmed computer. In a unit claim enumerating several means, several of these means may be embodied by the same item of hardware. The use of the words first, second, and third etc. does not indicate any order. These words may be interpreted as names.

[0147] Although the preferred embodiments of the present application have been described, those skilled in the art may make other changes and modifications to these embodiments once they have learned the basic creative concept. Therefore, the appended claims are intended to be interpreted as including the preferred embodiments and all changes and modifications falling within the scope of the present application.

[0148] Obviously, those skilled in the art can make various changes and modifications to the present application without departing from the spirit and scope of the present application. Thus, if these modifications and variations of the present application fall within the scope of the claims of the present application and their equivalents, the present application is also intended to include these modifications and variations.

Claims

1. A method for determining a corner reflector deployment scheme, characterized in that: The method for determining the corner reflector deployment scheme includes: Obtain the environmental parameters corresponding to the points to be deployed and the running trajectory of the detector; Determine the distance straight line corresponding to the to-be-deployed point according to the running trajectory, and determine the to-be-selected deployment point according to the environmental parameters; Determine, among the lines corresponding to the adjacent to-be-selected deployment points, a first line parallel to the running track and a second line parallel to the distance straight line; The first connecting line having a length greater than the directional effect distance and / or the to-be-selected deployment point corresponding to the second connecting line having a length greater than the distance effect distance are used as target deployment points; A corner reflector deployment plan is generated according to the coordinates of the target deployment points.

2. The method for determining a corner reflector deployment scheme according to claim 1, wherein: Before the step of taking the first link having a length greater than the directional effect distance and / or the candidate deployment point corresponding to the second link having a length greater than the distance effect distance as the target deployment point, the step further includes: Determining the directional resolution of the detector corresponding to the running trajectory and the range resolution corresponding to the range straight line; Obtain preset directional effect parameters and distance effect parameters; The directional effect distance is determined according to the directional resolution and the directional effect parameter, and the distance effect distance is determined according to the distance resolution and the distance effect parameter.

3. The method for determining a corner reflector deployment scheme according to claim 1, wherein: The environmental parameters include at least one of a radio interference value, a power transmission interference value, a satellite signal strength value, longitude and latitude coordinates, and an optical image.

4. The method for determining a corner reflector deployment scheme according to claim 3, wherein: The determining of the candidate deployment points according to the environmental parameters includes: Acquire the incident signal cross section of the detector at the latitude and longitude coordinates; Determine, according to the optical image, a point to be deployed where there are no obstacles in the incident signal cross section; The signal interference value of the to-be-deployed point is determined based on the environmental parameter, and the to-be-selected deployment point whose signal interference value meets the preset deployment condition is screened.

5. The method for determining a corner reflector deployment scheme according to claim 4, characterized in that: The determining the signal interference value of the to-be-deployed point based on the environmental parameter, and screening the to-be-deployed point whose signal interference value meets the preset deployment condition, includes: Acquire the three-dimensional coordinates of the point to be deployed, and calculate the radar coordinates corresponding to the point to be deployed by combining the three-dimensional coordinates and the longitude and latitude coordinates; Obtaining a radar map and determining a background reflection intensity value at the radar coordinates; When the background reflection intensity value is less than or equal to a first threshold, the radio interference value is less than or equal to a second threshold, the power transmission interference value is less than or equal to a third threshold, and the satellite signal strength value is greater than or equal to a third threshold, the to-be-deployed point is determined to be the to-be-selected deployment point.

6. The method for determining a corner reflector deployment scheme according to claim 1, wherein: The determining of the connecting lines corresponding to the adjacent candidate deployment points, a first connecting line parallel to the running track and a second connecting line parallel to the distance straight line, include: Determining a connection line between adjacent candidate deployment points; Determine a first angle between the connecting line and the running track, and a second angle between the connecting line and the distance straight line; When the first included angle is smaller than a first preset angle, determining the connecting line to be the first connecting line; When the second included angle is smaller than the second preset angle, the connecting line is determined to be the second connecting line.

7. The method for determining a corner reflector deployment scheme according to claim 6, wherein: Before the step of generating a corner reflector deployment plan according to the coordinates of the target deployment point, the method further includes: When the first angle is greater than the first preset angle, and the second angle is greater than the second preset angle, the to-be-selected deployment point is determined to be the target deployment point.

8. The method for determining a corner reflector deployment scheme according to claim 1, wherein: The generating of the corner reflector deployment scheme according to the coordinates of the target deployment point comprises: Determine an unqualified deployment point where the length of the first link is less than the directional effect distance, or the length of the second link is less than the distance effect distance; The unqualified deployment points are removed, and the corner reflector deployment plan is generated according to the latitude and longitude coordinates of the screened target deployment points.

9. A device for determining a corner reflector deployment scheme, characterized in that: The invention comprises a memory, a processor and a program for determining a corner reflector deployment scheme which is stored in the memory and can be run on the processor. When the processor executes the program for determining a corner reflector deployment scheme, the steps of the method for determining a corner reflector deployment scheme as described in any one of claims 1 to 8 are implemented.

10. A computer-readable storage medium, characterized in that: The computer-readable storage medium stores a program for determining a corner reflector deployment plan, and when the program for determining a corner reflector deployment plan is executed by a processor, the steps of the method for determining a corner reflector deployment plan as described in any one of claims 1 to 8 are implemented.

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