Method, device and readable storage medium for determining corner reflector deployment scheme

Abstract

The application discloses a kind of corner reflector deployment scheme determination method, equipment and readable storage medium, the method comprises obtaining the environment parameter corresponding to the point to be deployed and the running trajectory of detector;According to the running trajectory, the distance straight line corresponding to the point to be deployed is determined, and the environment parameter is determined to be selected deployment point;Determine the first connecting line parallel to the running trajectory and the second connecting line parallel to the distance straight line in the connecting line corresponding to adjacent selected deployment point;The first connecting line with length greater than the direction effect distance and / or the second connecting line corresponding to the selected deployment point with length greater than the distance effect distance are target deployment point;According to the coordinates of the target deployment point, corner reflector deployment scheme is generated, so that the technical problem that the anti-interference ability of corner reflector is poor in the related art, leading to low monitoring accuracy is effectively solved, and the technical effect of accurately detecting the degree of building deformation is realized.

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

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

[0003] In related technologies, the corner reflector can be applied to the fields of safety monitoring of important buildings in cities, deformation monitoring of bridges, etc. For example, it is applied to synthetic aperture radar for deformation detection to monitor whether a building has deformed or to determine the deformation degree of the building.

[0004] However, in the traditional building deformation monitoring method, the corner reflector has poor anti-interference capability, resulting in low monitoring accuracy and failing to meet the three-dimensional deformation monitoring requirement. SUMMARY

[0005] The embodiments of the present application provide a method for determining a corner reflector deployment scheme, a device for determining a corner reflector deployment scheme, and a computer-readable storage medium, solve the technical problem that the corner reflector has poor anti-interference capability in related technologies, resulting in low monitoring accuracy and failing to meet the three-dimensional deformation monitoring requirement, and achieve the technical effect of accurately detecting the deformation degree of a building.

[0006] The embodiments of the present application provide a method for determining a corner reflector deployment scheme, which comprises:

[0007] Obtaining an environment parameter corresponding to a to-be-deployed point and a running track of a detector;

[0008] Determining a distance-wise straight line corresponding to the to-be-deployed point according to the running track, and determining a to-be-selected deployment point according to the environment parameter;

[0009] Determining a first connecting line parallel to the running track and a second connecting line parallel to the distance-wise straight line in a connecting line corresponding to adjacent to-be-selected deployment points;

[0010] Taking the to-be-selected deployment points corresponding to the first connecting line with a length greater than a direction effect distance and / or the second connecting line with a length greater than a distance-wise effect distance as target deployment points;

[0011] Generating a corner reflector deployment scheme according to the coordinates of the target deployment points.

[0012] Optionally, before the step of taking the first connecting line with a length greater than a direction effect distance, and / or the second connecting line with a length greater than a distance direction effect distance as a target deployment point, the method further comprises:

[0013] determining a direction resolution corresponding to the running track of the probe, and a distance direction resolution corresponding to the distance direction straight line;

[0014] obtaining a preset direction effect parameter and a distance direction effect parameter;

[0015] determining the direction effect distance according to the direction resolution and the direction effect parameter, and determining the distance direction effect distance according to the distance direction resolution and the distance direction effect parameter.

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

[0017] Optionally, the step of determining the candidate deployment point according to the environmental parameters comprises:

[0018] obtaining an incident signal cross section of the probe at the latitude and longitude coordinate;

[0019] determining a candidate deployment point with no obstacle in the incident signal cross section according to the optical image;

[0020] determining a signal interference value of the candidate deployment point based on the environmental parameters, and screening the candidate deployment point with a signal interference value meeting a preset deployment condition.

[0021] Optionally, the step of determining a signal interference value of the candidate deployment point based on the environmental parameters, and screening the candidate deployment point with a signal interference value meeting a preset deployment condition comprises:

[0022] obtaining a three-dimensional coordinate of the candidate deployment point, and calculating a radar coordinate corresponding to the candidate deployment point in combination with the three-dimensional coordinate and the latitude and longitude coordinate;

[0023] obtaining a radar map, and determining a background reflection intensity value at the radar coordinate;

[0024] when the background reflection intensity value is less than or equal to a first threshold value, the radio interference value is less than or equal to a second threshold value, the power transmission interference value is less than or equal to a third threshold value, and the satellite signal intensity value is greater than or equal to a fourth threshold value, determining the candidate deployment point as the target deployment point.

[0025] Optionally, the first line parallel to the running track and the second line parallel to the distance straight line in the line connecting the adjacent candidate deployment point positions corresponding to the target deployment point position are determined.

[0026] determining a line connecting the adjacent candidate deployment point positions;

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

[0028] when the first angle is less than a first preset angle, determining that the line is the first line;

[0029] when the second angle is less than a second preset angle, determining that the line is the second line.

[0030] Optionally, before the step of generating the corner reflector deployment scheme according to the coordinates of the target deployment point position, the method further comprises:

[0031] when the first angle is greater than the first preset angle and the second angle is greater than the second preset angle, determining that the candidate deployment point position is the target deployment point position.

[0032] Optionally, the step of generating the corner reflector deployment scheme according to the coordinates of the target deployment point position comprises:

[0033] determining unqualified deployment point positions whose lengths of the first lines are less than the direction effect distance or whose lengths of the second lines are less than the distance effect distance;

[0034] removing the unqualified deployment point positions, and generating the corner reflector deployment scheme according to the latitude and longitude coordinates of the screened target deployment point positions.

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

[0036] In addition, the present application also proposes a computer readable storage medium, which stores a corner reflector deployment scheme determination program, and the corner reflector deployment scheme determination program implements the steps of the corner reflector deployment scheme determination method as described above when executed by a processor.

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

[0038] 1、Since the environment parameters corresponding to the to-be-deployed point are acquired and the running track of the detector is acquired, a distance-direction straight line corresponding to the to-be-deployed point is determined according to the running track, and a to-be-deployed point is determined according to the environment parameters, a first connecting line parallel to the running track and a second connecting line parallel to the distance-direction straight line are determined in a connecting line corresponding to adjacent to-be-deployed points, the to-be-deployed point corresponding to the first connecting line with a length greater than a direction effect distance and / or the second connecting line with a length greater than a distance-direction effect distance is taken as a target deployment point, and an angle reflector deployment scheme is generated according to the coordinates of the target deployment point, so that the technical problem that the anti-interference capability of the angle reflector is poor in the related art, the monitoring precision is low, and the three-dimensional deformation monitoring requirement cannot be met is effectively solved, and the technical effect that the deformation degree of the building is accurately detected is achieved. BRIEF DESCRIPTION OF DRAWINGS

[0039] Figure 1 It is a flowchart of a method for determining an angle reflector deployment scheme according to an embodiment of the present application.

[0040] Figure 2 It is a flowchart of a method for determining an angle reflector deployment scheme according to an embodiment of the present application.

[0041] Figure 3 It is a flowchart of a method for determining an angle reflector deployment scheme according to an embodiment of the present application.

[0042] Figure 4 It is a schematic diagram of a hardware structure related to an angle reflector deployment scheme determination device according to an embodiment of the present application. DETAILED DESCRIPTION

[0043] In the related art, deformation detection is usually performed by using a synthetic aperture radar to monitor whether a building has deformed or to determine the deformation degree of the building, but the anti-interference capability of the angle reflector for reflecting a signal is poor, the monitoring precision is low, and the three-dimensional deformation monitoring requirement cannot be met. The main technical scheme adopted in the embodiments of the present application is that the running track of the detector and the environment parameters of the to-be-deployed point are acquired, a distance-direction straight line perpendicular to the running track is determined, the target deployment point meeting the deployment condition is selected according to the distance between adjacent to-be-deployed points, and the angle reflector deployment scheme is generated according to the coordinates of the target deployment point. Thus, the deformation degree of the building is accurately detected.

[0044] For a better understanding of the above technical solutions, the exemplary embodiments of the present application will be described in more detail below with reference to the accompanying drawings. Although the 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 so that the present application can be more thoroughly understood and the scope of the present application can be accurately conveyed to those skilled in the art.

[0045] Embodiment one

[0046] The embodiment one of the present application discloses a method for determining a corner reflector deployment scheme, referring to Figure 1 , the method for determining a corner reflector deployment scheme comprises:

[0047] Step S110, obtaining the environment parameters corresponding to the to-be-deployed point and the running trajectory of the probe;

[0048] In this embodiment, the to-be-deployed point can be pre-set according to the construction drawings or map of the construction site, and the environment parameters are the parameters required to meet the deployment conditions. The probe can be a radar, and the running trajectory is the projection of the probe trajectory on the earth's surface.

[0049] As an optional implementation, the environment parameters can be at least one of radio interference value, power transmission interference value, satellite signal strength value, latitude and longitude coordinates, and optical image.

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

[0051] In this embodiment, the distance straight line is perpendicular to the running trajectory on the horizontal plane, i.e. the distance straight line and the running trajectory form an orthogonal coordinate system on the horizontal plane. The to-be-selected deployment point is selected according to whether the environment parameters meet the pre-set deployment conditions.

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

[0053] Optionally, step S120 comprises:

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

[0055] Step S122, determining the to-be-deployed point where the incident signal cross section does not exist obstacles according to the optical image;

[0056] In step S123, a signal interference value of the to-be-deployed point is determined based on the environment parameter, and the to-be-deployed point position that meets the preset deployment condition is screened out as the to-be-selected deployment point position.

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

[0058] As an optional implementation, the latitude and longitude coordinates of the to-be-deployed point position are determined, the cross section of the incident signal of the probe at the latitude and longitude coordinates is obtained, and it is determined whether there is an obstacle between the to-be-deployed point position and the probe according to the obtained optical image, and the to-be-deployed point position without the obstacle is selected. The to-be-deployed point position without the obstacle is determined, the signal interference value is determined based on the environment parameter of the to-be-deployed point position, and the to-be-deployed point position that meets the preset deployment condition is screened out as the to-be-selected deployment point position.

[0059] For example, based on the obtained environment parameter, a corresponding weight value is determined for each environment parameter according to a preset calculation formula, and then the signal interference value is calculated.

[0060] For example, the obtained environment parameter is regarded as the signal interference value, and when each environment parameter meets the corresponding deployment condition, the to-be-deployed point position is determined as the to-be-selected deployment point position.

[0061] Optionally, step S123 includes:

[0062] In step S1231, the three-dimensional coordinates of the to-be-deployed point position are obtained, and the radar coordinates corresponding to the to-be-deployed point position are calculated in combination with the three-dimensional coordinates and the latitude and longitude coordinates.

[0063] In step S1232, a radar map is obtained, and the background reflection intensity value at the radar coordinates is determined.

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

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

[0066] In step S130, a first line parallel to the running track and a second line parallel to the distance-to-straight line are determined in a line between adjacent to-be-selected deployment points.

[0067] In step S140, the to-be-selected deployment points corresponding to the first line with a length greater than the directional effect distance and / or the second line with a length greater than the distance-to-direction effect distance are target deployment points.

[0068] In the embodiment, the line is a straight line between adjacent to-be-selected deployment points, and the directional effect distance and the distance-to-direction effect distance are minimum distances in two perpendicular directions that do not produce sidelobe effects. When the distance between to-be-selected deployment points is less than the directional effect distance or the distance-to-direction effect distance, sidelobe effects are produced when a corner reflector is deployed at the point.

[0069] As an optional implementation, a line between adjacent to-be-selected deployment points is determined, a line parallel to the running track is selected as a first line, a line parallel to the distance-to-straight line is selected as a second line, a first line with a length greater than the directional effect distance and a second line with a length greater than the distance-to-direction effect distance are determined, and to-be-selected deployment points at the end points of the first line and the second line are target deployment points.

[0070] For example, the line between point one and point two can be greater than the directional effect distance or the distance-to-direction effect distance, but the line between point two and point three can be less than the directional effect distance or the distance-to-direction effect distance, in which case point two should be determined as a target deployment point, and point three is not a target deployment point.

[0071] In step S150, a corner reflector deployment scheme is generated 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 line is less than the directional effect distance, or the length of the second line is less than the distance effect distance.

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

[0075] As an optional implementation, the unqualified deployment point where the length of the first line is less than the directional effect distance, or the length of the second line is less than the distance effect distance, is determined, wherein when the length of the line between a certain unqualified deployment point and point one is less than the directional effect distance or the distance effect distance, but the length of the line between the unqualified deployment point and point two is greater than the directional effect distance or the distance effect distance, the unqualified deployment point should be determined as a target deployment point. The unqualified deployment point is removed, and the corner reflector deployment scheme is generated according to the latitude and longitude coordinates of the screened target deployment point, wherein the scheme further includes the elevation angle of the corner reflector installation.

[0076] Optionally, the optical image at the target deployment point is analyzed, and a point that does not meet the installation condition is screened out as an unqualified point. For example, there is water leakage or other harsh conditions at the point.

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

[0078] Since the environment parameters corresponding to the to-be-deployed point and the running track of the probe are acquired, the distance direction straight line corresponding to the to-be-deployed point is determined according to the running track, the to-be-deployed point is determined according to the environment parameters, the first line parallel to the running track and the second line parallel to the distance direction straight line are determined in the line between the adjacent to-be-deployed points, the to-be-deployed point corresponding to the first line with a length greater than the directional effect distance and / or the second line with a length greater than the distance effect distance is determined as a target deployment point, and the corner reflector deployment scheme is generated according to the coordinates of the target deployment point, the technical problem that the anti-interference ability of the corner reflector is poor in the related art, the monitoring precision is low, and the three-dimensional deformation monitoring demand cannot be met is effectively solved, and the technical effect that the building deformation degree is accurately detected is achieved.

[0079] Embodiment two

[0080] Based on embodiment one, embodiment two 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 corresponding to the running track of the probe, and the distance direction resolution corresponding to the distance direction straight line.

[0082] obtaining a preset direction effect parameter and a distance direction effect parameter;

[0083] determining the direction effect distance according to the direction resolution and the direction effect parameter, and determining the distance direction effect distance according to the distance direction resolution and the distance direction effect parameter.

[0084] In the embodiment, the direction resolution is information obtained by the detector, resolution in the direction of the running track, and the distance direction resolution is information obtained by the detector, resolution in the direction of the distance direction. The direction effect parameter and the distance direction effect parameter are determined according to experimental data.

[0085] As an optional implementation, the direction resolution in the direction of the running track is determined, the distance direction resolution in the direction of the distance direction is determined, the obtained direction resolution and distance direction resolution are averaged respectively to obtain the direction resolution and distance direction resolution. The preset direction effect parameter and distance direction effect parameter are obtained. The direction effect distance is obtained by multiplying the direction resolution by the direction effect parameter. The distance direction effect distance is obtained by multiplying the distance direction resolution by the distance direction effect parameter.

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

[0087] Since the direction effect distance is determined according to the direction resolution and the direction effect parameter, and the distance direction effect distance is determined according to the distance direction resolution and the distance direction effect parameter, the technical problem of side lobe effect existing in the installation of corner reflectors in the related art is effectively solved, and the side lobe effect between corner reflectors is effectively and conveniently avoided.

[0088] Embodiment Three

[0089] Based on Embodiment One, Embodiment Three of the present application provides a method for determining a corner reflector deployment scheme, referring to Figure 3 , step S130 comprises:

[0090] Step S310, determining a line connecting adjacent candidate deployment points.

[0091] Step S320, determining a first included angle between the line and the running track, and a second included angle between the line and the distance direction straight line.

[0092] Step S330, when the first included angle is less than a first preset angle, determining that the line is the first line.

[0093] Step S340, when the second included angle is less than the second preset angle, determining that the line is the second line.

[0094] In the embodiment, when the included angle between the line connecting the candidate deployment point and the running track or the distance direction straight line is less than the preset angle, it is determined that the line is parallel to the running track or the distance direction straight line.

[0095] As an optional implementation, the line connecting the adjacent candidate deployment points is determined, the included angle between each line and the running track is determined as a first included angle, and the included angle between each line and the distance direction straight line is determined as a second included angle. When the first included angle is less than a first preset angle, it is determined that the line is a first line. When the second included angle is less than a second preset angle, it is determined that the line is a second 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, and vice versa.

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

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

[0099] Step S350, when the first included angle is greater than the first preset angle, and the second included angle is greater than the second preset angle, determining that the candidate deployment point is the target deployment point.

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

[0101] For example, if the line between the two candidate deployment points and other candidate deployment points does not exist the first line or the second line, it is determined that the two candidate deployment points corresponding to the line are target deployment points.

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

[0103] Optionally, the finally determined target deployment point does not exist any first line or second line with other target deployment points, or the length of the existing first line is greater than the direction effect distance, and the length of the existing second line is greater than the distance direction effect distance.

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

[0105] By determining the line connecting the adjacent candidate deployment points, determining the first angle between the line and the running track and the second angle between the line and the distance straight line, determining the line as the first line when the first angle is less than the first preset angle, and determining the line as the second line when the second angle is less than the second preset angle, the technical problem that the anti-interference ability of the corner reflector is poor in the related art, resulting in low monitoring accuracy and failing to meet the three-dimensional deformation monitoring requirement is effectively solved, and the technical effect of accurately detecting the building deformation degree is achieved.

[0106] The application also provides a corner reflector deployment scheme determination device. Figure 4 , Figure 4 The application also provides a corner reflector deployment scheme determination device.

[0107] As shown in Figure 4 , the corner reflector deployment scheme determination device can 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. The communication bus 1002 is used to realize the connection and communication between the components. The user interface 1003 can include a display screen, an input unit such as a keyboard, and an optional user interface 1003 can also include a standard wired interface, a wireless interface. The network interface 1004 can optionally include a standard wired interface, a wireless interface (such as a wireless fidelity (WIreless-FIdelity, WI-FI) interface). The memory 1005 can be a high-speed random access memory (RAM) memory, or a stable non-volatile memory (NVM), such as a magnetic disk memory. The memory 1005 can also be a storage device independent of the aforementioned processor 1001.

[0108] Those skilled in the art can understand that Figure 4 the structure shown in the above does not constitute a limitation on the corner reflector deployment scheme determination device, and can include more or fewer components than the figure, or combine certain components, or different component deployment.

[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 also can read the data in the memory 1005 to realize the corner reflector deployment scheme determination.

[0110] Optionally, as shown in Figure 4 The memory 1005 as a storage medium can include an operating system, a data storage module, a network communication module, a user interface module, and a corner reflector deployment scheme determination program.

[0111] Optionally, in Figure 4 The network interface 1004 is mainly used for data communication with other devices, and the user interface 1003 is mainly used for data interaction with the user; the processor 1001 and the memory 1005 in the corner reflector deployment scheme determination device can be arranged in the corner reflector deployment scheme determination device.

[0112] As shown in Figure 4 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 related step operations of the corner reflector deployment scheme determination method provided in the embodiments of the present application:

[0113] Obtain the environment parameters corresponding to the to-be-deployed point and the running track of the probe;

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

[0115] Determine the first connecting line parallel to the running track and the second connecting line parallel to the distance-to-straight line in the connecting line corresponding to the adjacent to-be-selected deployment point;

[0116] The to-be-selected deployment point corresponding to the first connecting line with a length greater than the direction effect distance, and / or the second connecting line with a length greater than the distance-to-effect distance is the target deployment point;

[0117] Generate a corner reflector deployment scheme according to the coordinates of the target deployment point.

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

[0119] Determine the direction resolution corresponding to the running track of the probe, and the distance-to-resolution corresponding to the distance-to-straight line;

[0120] Obtain the preset direction effect parameter and distance-to-effect parameter;

[0121] Determine the direction effect distance according to the direction resolution and the direction effect parameter, and determine the distance-to-effect distance according to the distance-to-resolution and the distance-to-effect parameter.

[0122] Optionally, the processor 1001 can invoke the determination program of the corner reflector deployment scheme stored in the memory 1005, and further perform the following operations: the environment parameters include at least one of radio interference value, power transmission interference value, satellite signal strength value, latitude and longitude coordinates, and optical image.

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

[0124] Obtain the incident signal section of the probe at the latitude and longitude coordinates;

[0125] Determine the to-be-deployed point of the incident signal section from the optical image without obstacles;

[0126] Determine the signal interference value of the to-be-deployed point based on the environment parameters, and screen the to-be-deployed point that meets the preset deployment condition.

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

[0128] Obtain the three-dimensional coordinates of the to-be-deployed point, and calculate the radar coordinates corresponding to the to-be-deployed point in combination with the three-dimensional coordinates and the latitude and longitude coordinates;

[0129] Obtain a radar map and determine the background reflection intensity value at the radar coordinates;

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

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

[0132] Determine the line between adjacent to-be-deployed points;

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

[0134] When the first angle is less than a first preset angle, determine that the line is the first line;

[0135] When the second angle is less than a second preset angle, determine that the line is the second line.

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

[0137] When the first included angle is greater than the first preset angle, and the second included angle is greater than the second preset angle, the candidate deployment point is determined as the target deployment point.

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

[0139] determine the unqualified deployment point whose first line length is less than the direction effect distance, or whose second line length is less than the distance effect distance;

[0140] remove the unqualified deployment point, and generate the corner reflector deployment scheme according to the latitude and longitude coordinates of the target deployment point after screening.

[0141] In addition, the embodiment of the present application also proposes a computer readable storage medium, and the computer readable storage medium stores the determination program of the corner reflector deployment scheme. When the determination program of the corner reflector deployment scheme is executed by the processor, the related steps of any embodiment of the determination method of the corner reflector deployment scheme are realized.

[0142] Those skilled in the art should understand that the embodiments of the present application can be provided as a method, a system, or a computer program product. Therefore, the present application can adopt a completely hardware embodiment, a completely software embodiment, or an embodiment combining software and hardware aspects. Moreover, the present application can adopt the form of a computer program product implemented on one or more computer usable storage media (including but not limited to disk storage, CD-ROM, optical storage, etc.) containing computer usable program codes.

[0143] The present application is described with reference to flowcharts and / or block diagrams of the method, device (system), and computer program product according to the embodiments of the present application. It should be understood that each flow and / or block in the flowcharts and / or block diagrams, and the combination of the flows and / or blocks can be realized by computer program instructions. These computer program instructions can be provided to a general-purpose computer, a special-purpose computer, an embedded processor, or other programmable data processing devices to produce a machine, so that the instructions executed by the computer or other programmable data processing devices produce a device for implementing the functions specified in the flowcharts and / or block diagrams. Figure 1 The functions specified in one flow or multiple flows and / or blocks Figure 1 The device for implementing the functions specified in one flow or multiple flows and / or blocks

[0144] These computer program instructions can also be stored in a computer- readable memory that can direct a computer or other programmable data processing apparatus to function in a particular manner, such that the instructions stored in the computer-readable memory produce an article of manufacture including instructions which implement the Figure 1 function specified in the flow or flows and / or blocks Figure 1 of the block or blocks.

[0145] The computer program instructions can also be loaded onto a computer or other programmable data processing apparatus to cause a series of operational steps to be performed on the computer or other programmable apparatus to produce a computer implemented process such that the instructions which execute on the computer or other programmable apparatus provide steps for implementing the Figure 1 function specified in the flow or flows and / or blocks Figure 1 of the block or blocks.

[0146] It is noted that any references made herein to an element or apparatus should be understood in the context of the present application as references to at least one element or apparatus. It is further noted that in the claims the word comprising does not exclude any other elements or steps not specified in a claim. The word "a" or "an" preceding an element does not exclude the presence of a plurality of such elements. The application can be implemented by means of hardware comprising several distinct elements, and by means of a suitably programmed computer. In a unitary claim, several of the devices, if any, can be

[0147] While the preferred embodiments of the application have been described, it should be apparent that further modifications and improvements can be made by those skilled in the art that still fall within the scope of the application. Accordingly, no limitation is implied by the description or drawings.

[0148] Obviously, numerous modifications and variations of the present application are possible in light of the above teachings. It is therefore to be understood that within the scope of the appended claims and their equivalents, the application can be practiced otherwise than as specifically described.

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 locations to be deployed and the operating trajectory of the detectors; The distance line corresponding to the point to be deployed is determined based on the running trajectory, and the candidate deployment point is determined based on the environmental parameters; Determine the lines connecting adjacent candidate deployment points; Determine the first angle between the connecting line and the running trajectory, and the second angle between the connecting line and the distance-directing line; When the first included angle is less than the first preset angle, the connecting line is determined to be the first connecting line parallel to the running trajectory; When the second included angle is less than the second preset angle, the connecting line is determined to be a second connecting line parallel to the distance direction line; Determine the directional resolution of the detector corresponding to the running trajectory, and the range resolution corresponding to the range line; Obtain the preset directional effect parameters and range effect parameters; The directional effect distance is determined based on the directional resolution and the directional effect parameters, and the range effect distance is determined based on the range directional resolution and the range effect parameters. The candidate 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 directional effect distance are designated as the target deployment points. A corner reflector deployment scheme is generated based on the coordinates of the target deployment point.

2. The method for determining the corner reflector deployment scheme as described in claim 1, characterized in that, The environmental parameters include at least one of the following: radio interference value, power transmission interference value, satellite signal strength value, latitude and longitude coordinates, and optical image.

3. The method for determining the corner reflector deployment scheme as described in claim 2, characterized in that, The step of determining the candidate deployment locations based on the environmental parameters includes: Obtain the incident signal cross section of the detector at the latitude and longitude coordinates; Based on the optical image, determine the deployment point where there are no obstacles in the incident signal cross section; Based on the environmental parameters, the signal interference value of the location to be deployed is determined, and the candidate deployment locations whose signal interference values ​​meet the preset deployment conditions are selected.

4. The method for determining the corner reflector deployment scheme as described in claim 3, characterized in that, The step of determining the signal interference value of the deployment point based on the environmental parameters and filtering the candidate deployment points whose signal interference values ​​meet the preset deployment conditions includes: Obtain 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 with the latitude and longitude coordinates. Obtain the radar map and determine the background reflection intensity value at the radar coordinates; 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 location to be deployed is determined as the candidate deployment location.

5. The method for determining the corner reflector deployment scheme as described in claim 1, characterized in that, Before the step of generating the corner reflector deployment scheme based on the coordinates of the target deployment point, the method further includes: When the first included angle is greater than the first preset angle and the second included angle is greater than the second preset angle, the candidate deployment point is determined as the target deployment point.

6. The method for determining the corner reflector deployment scheme as described in claim 1, characterized in that, The step of generating a corner reflector deployment scheme based on the coordinates of the target deployment point includes: Determine unqualified deployment points where the length of the first connecting line is less than the directional effect distance, or the length of the second connecting line is less than the distance directional effect distance; Remove the unqualified deployment points, and generate the corner reflector deployment scheme based on the latitude and longitude coordinates of the selected target deployment points.

7. A device for determining a corner reflector deployment scheme, characterized in that, The method includes a memory, a processor, and a program for determining a corner reflector deployment scheme stored in the memory and executable on the processor. When the processor executes the program for determining the corner reflector deployment scheme, it implements the steps of the method for determining a corner reflector deployment scheme as described in any one of claims 1 to 6.

8. A computer-readable storage medium, characterized in that, The computer-readable storage medium stores a program for determining a corner reflector deployment scheme, which, when executed by a processor, implements the steps of the method for determining a corner reflector deployment scheme as described in any one of claims 1 to 6.

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