WO2023273243A1 - Unmanned aerial vehicle surveying and mapping method and system based on millimeter wave radar - Google Patents

Unmanned aerial vehicle surveying and mapping method and system based on millimeter wave radar Download PDF

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Publication number
WO2023273243A1
WO2023273243A1 PCT/CN2021/141120 CN2021141120W WO2023273243A1 WO 2023273243 A1 WO2023273243 A1 WO 2023273243A1 CN 2021141120 W CN2021141120 W CN 2021141120W WO 2023273243 A1 WO2023273243 A1 WO 2023273243A1
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Prior art keywords
detection point
latitude
distance
longitude
uav
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PCT/CN2021/141120
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French (fr)
Chinese (zh)
Inventor
龚超
于巍巍
李俊桦
丁季明
欧昊一
沈黎玲
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上海为彪汽配制造有限公司
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Publication of WO2023273243A1 publication Critical patent/WO2023273243A1/en

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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/88Radar or analogous systems specially adapted for specific applications
    • G01S13/89Radar or analogous systems specially adapted for specific applications for mapping or imaging
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C7/00Tracing profiles
    • G01C7/02Tracing profiles of land surfaces
    • G01C7/04Tracing profiles of land surfaces involving a vehicle which moves along the profile to be traced

Definitions

  • the invention relates to the technical field of topographic surveying and mapping, in particular to a method and system for surveying and mapping of an unmanned aerial vehicle based on millimeter wave radar.
  • Topographic surveying and mapping is mainly to accurately measure the coordinates of the boundary points of the land parcel ownership boundary, and to accurately draw the location, area, ownership relationship, utilization status and other elements of the land parcel and its attachments on the drawings and record them in special Mapping work in the table book.
  • the RTK system includes a fixed measuring station and a mobile measuring station.
  • the fixed measuring station transmits its observation value and the coordinate information of the measuring station to the mobile measuring station through the data link.
  • the mobile measuring station not only receives the data from the fixed measuring station
  • the data also receives the GPS data sent by the satellite, combined with the calculation of the current coordinate data of the two stations on the mobile side; because the PTK system measurement must use GPS data, it is difficult for the mobile measurement station to receive GPS data when passing through densely populated houses or dense trees. PTK is difficult to fix, it is impossible to calculate the current coordinate data of the mobile survey station, it is difficult to complete the land survey work, and the scope of application is narrow.
  • the existing topographic surveying and mapping methods have the defects of low operation efficiency, narrow application range or low surveying and mapping accuracy.
  • the purpose of the present invention is to provide a method and system for UAV surveying and mapping based on millimeter-wave radar, so as to improve the operational efficiency of topographical survey, narrow application range and surveying and mapping accuracy.
  • the present invention provides a method for surveying and mapping of an unmanned aerial vehicle based on a millimeter wave radar, comprising the steps of:
  • the target area includes several detection points;
  • the positioning data of the positioning device carried on the drone calculate the altitude value and latitude and longitude value of the detection point
  • a topographic map of the target area is generated according to the altitude values and latitude and longitude values of all detection points.
  • the obtaining the relative distance and relative angle between the UAV and each detection point includes the steps of:
  • millimeter-wave radar After the millimeter-wave radar emits electromagnetic waves to scan the target area, acquire the electromagnetic wave transmitting and receiving state information of the millimeter-wave radar;
  • the relative distance and relative angle between the UAV and each detection point are calculated according to the electromagnetic wave receiving and receiving state information and the antenna installation distance.
  • the state information of electromagnetic wave transmission and reception includes the time difference and phase difference of electromagnetic wave transmission and reception; the relative distance and relative distance between the UAV and each detection point are calculated according to the state information of electromagnetic wave transmission and reception and the antenna installation distance.
  • Angular includes steps:
  • the relative distance between the unmanned aerial vehicle and each detection point is calculated by substituting the following formula (1);
  • the wavelength of the electromagnetic wave and the phase difference, the relative angle is calculated by substituting the following formula (2);
  • R represents the relative distance
  • represents the relative angle
  • c represents the speed of light
  • ⁇ T represents the time difference between transmitting and receiving the electromagnetic wave
  • represents the wavelength of the electromagnetic wave
  • represents the phase difference
  • L represents the antenna installation distance
  • the calculating the altitude value and the latitude and longitude value of the detection point according to the relative distance and relative angle, and the positioning data of the positioning device carried on the UAV includes the steps of:
  • the positioning data includes latitude and longitude information and altitude information of the drone;
  • the latitude and longitude information is substituted into the following formula (6) to calculate the latitude value of the detection point;
  • Jn sin ⁇ *S/(cos(Wn)*D) (7)
  • the altitude value of the detection point is calculated by substituting the following formula (8);
  • the R represents the relative distance
  • represents the relative angle
  • S represents the stroke distance
  • h represents the stroke height
  • represents the distance between the straight line where the relative distance is located and the straight line where the left and right directions are located.
  • W n represents the latitude value of the nth detection point
  • J n represents the longitude value of the nth detection point
  • H n represents the altitude value of the nth detection point.
  • the generating the topographic map of the target area according to the altitude values and latitude and longitude values of all detection points includes the steps of:
  • the present invention also provides a drone surveying and mapping system based on millimeter wave radar, including:
  • the control module is used to control several millimeter-wave radars installed at the bottom of the drone to emit electromagnetic waves to scan the target area;
  • An acquisition module configured to calculate the relative distance between the UAV and each detection point, and the relative angle between the UAV and each detection point in the height direction; the target area includes several detection points;
  • the processing module is used to calculate the altitude value and latitude and longitude value of the detection point according to the relative distance and relative angle, as well as the positioning data of the positioning device carried on the drone;
  • a generating module configured to generate a topographic map of the target area according to the altitude values and latitude and longitude values of all detection points.
  • the acquisition module includes:
  • the first acquisition sub-module is used to acquire the electromagnetic wave transmitting and receiving status information of the millimeter wave radar after the millimeter wave radar emits electromagnetic waves to scan the target area;
  • the calculation sub-module is used to calculate the relative distance and relative angle between the unmanned aerial vehicle and each detection point according to the state information of transmitting and receiving electromagnetic waves and the installation distance of the antenna.
  • the electromagnetic wave transceiving state information includes electromagnetic wave transceiving time difference and phase difference;
  • the calculation submodule includes:
  • the relative distance calculation unit is used to calculate the relative distance between the UAV and each detection point by substituting the following formula (1) according to the time difference between sending and receiving of the electromagnetic wave;
  • the relative angle calculation unit is used to calculate the relative angle by substituting the following formula (2) according to the antenna installation distance, the wavelength of the electromagnetic wave and the phase difference;
  • R represents the relative distance
  • represents the relative angle
  • c represents the speed of light
  • ⁇ T represents the time difference between transmitting and receiving the electromagnetic wave
  • represents the wavelength of the electromagnetic wave
  • represents the phase difference
  • L represents the antenna installation distance
  • processing module includes:
  • the second acquisition sub-module is used to acquire the positioning data measured by the positioning device;
  • the positioning data includes the longitude and latitude information and the altitude information of the drone;
  • the distance calculation sub-module is used to calculate the travel distance between the drone and the detection point in the left and right directions by substituting the following formula (4) according to the relative distance and the relative angle;
  • the height calculation sub-module is used to calculate the travel height in the height direction between the drone and the detection point by substituting the following formula (5) according to the relative distance and the relative angle;
  • the latitude calculation submodule is used to calculate the latitude value of the detection point by substituting the following formula (6) into the longitude and latitude information according to the travel distance;
  • the longitude calculation submodule is used to calculate the longitude value of the detection point according to the travel distance and the latitude and longitude information by substituting the following formula (7);
  • Jn sin ⁇ *S/(cos(Wn)*D) (7)
  • the altitude calculation submodule is used to calculate the altitude value of the detection point by substituting the following formula (8) according to the travel height and the altitude information;
  • the R represents the relative distance
  • represents the relative angle
  • S represents the stroke distance
  • h represents the stroke height
  • represents the distance between the straight line where the relative distance is located and the straight line where the left and right directions are located.
  • W n represents the latitude value of the nth detection point
  • J n represents the longitude value of the nth detection point
  • H n represents the altitude value of the nth detection point.
  • the generating module includes:
  • the comparison sub-module is used to compare several altitude values and latitude and longitude values of the current detection point, and if they do not match, delete the altitude value and the latitude and longitude value of the current detection point;
  • the operational efficiency of terrain surveying, narrow application range and surveying and mapping accuracy can be improved.
  • Fig. 1 is a flow chart of an embodiment of a method for unmanned aerial vehicle surveying and mapping based on millimeter-wave radar of the present invention
  • Fig. 2 is a flow chart of another embodiment of a method for surveying and mapping of an unmanned aerial vehicle based on a millimeter-wave radar in the present invention
  • Fig. 3 is a flow chart of another embodiment of a method for surveying and mapping of an unmanned aerial vehicle based on a millimeter-wave radar in the present invention
  • Fig. 4 is a schematic diagram of the relationship between detection points and electromagnetic waves sent and received by the drone in a millimeter-wave radar-based UAV surveying and mapping method according to the present invention.
  • a kind of UAV surveying and mapping method based on millimeter wave radar comprises:
  • S100 controls several millimeter-wave radars installed at the bottom of the UAV to emit electromagnetic waves to scan the target area, and calculates the relative distance between the UAV and each detection point, and the distance between the UAV and each detection point in the height direction The relative angle on the above; the target area includes several detection points;
  • the target area refers to the area detected by the drone flight, which can be a valley, a hilly area, or an urban area where the drone is allowed to fly.
  • the entire target area is composed of a boundary and an internal area, and the target area can be Discrete into several detection points.
  • Millimeter wave radar refers to the radar operating in the millimeter wave band, and its operating frequency is usually selected in the range of 30-300GHz.
  • the operating frequency band of the millimeter wave radar of the present invention is between 60-64 GHz and 76-81 GHz.
  • millimeter-wave radar sensors with operating frequency bands of 60-64GHz and 76-81GHz are arranged at the bottom of the drone, and electromagnetic waves are emitted by several millimeter-wave radars installed on the bottom of the drone to scan the entire target area to obtain detection Data
  • the processing end including the controller or processor installed on the UAV, and the server connected to the UAV for wireless communication
  • can obtain detection data from various millimeter-wave radars in a wireless or wired manner and then calculate the relative distance between the UAV and each detection point according to the detection data, and calculate the relative angle between the UAV and each detection point in the height direction according to the detection data.
  • S200 Calculate and obtain the altitude value and latitude and longitude value of the detection point according to the relative distance and relative angle, and the positioning data of the positioning device carried on the drone;
  • S300 generates a topographic map of the target area according to the altitude values and latitude and longitude values of all detection points.
  • the processing end calculates the altitude value and latitude and longitude value of each detection point according to the relative distance and relative angle obtained from the above calculation, as well as the positioning data of the positioning device mounted on the UAV. Finally, the processing end generates a topographic map of the target area based on the altitude values and latitude and longitude values of all detection points.
  • the present invention is applicable to fields such as geological exploration, infrastructure, civil engineering, patrol inspection, etc.
  • the present invention uses the form of unmanned aerial vehicles to detect and obtain the drawings required for surveying and mapping, and obtains surveying and mapping parameters (the altitude value and latitude and longitude value of each detection point in the target area) Fast speed and high work efficiency.
  • surveying and mapping parameters the altitude value and latitude and longitude value of each detection point in the target area
  • fast speed and high work efficiency since the use of drones for detection is not restricted by the terrain, compared with manual detection, it can be used for surveying and mapping under complex terrain, and has a wide range of applications.
  • the surveying and mapping detection angle of the drone becomes larger. 120°.
  • the processing end can calculate the altitude difference at every interval of 1 meter.
  • the present invention can arrange several millimeter-wave radars according to requirements, and re-judgment the altitude information and latitude and longitude values of the same location, that is, the same detection point, which can not only improve the terrain detection accuracy of the target area, but also increase the coverage of a single flight of the surveyed area.
  • a kind of UAV surveying and mapping method based on millimeter wave radar comprises:
  • S120 calculate and obtain the relative distance and relative angle between the UAV and each detection point according to the electromagnetic wave transceiving state information and the antenna installation distance;
  • S200 Calculate and obtain the altitude value and latitude and longitude value of the detection point according to the relative distance and relative angle, and the positioning data of the positioning device carried on the drone;
  • S300 generates a topographic map of the target area according to the altitude values and latitude and longitude values of all detection points.
  • the processing end controls the millimeter-wave radar to emit electromagnetic waves to scan the target area, it obtains the electromagnetic wave sending and receiving status information of the millimeter-wave radar from each millimeter-wave radar. Since the installation positions of the antennas (including electromagnetic wave transmitting antennas and electromagnetic wave receiving antennas) installed on each UAV are fixed, the processing end can obtain the installation distance between the antennas, that is, the antenna installation distance. In this way, the processing end can calculate the relative distance and relative angle between the UAV and each detection point according to the state information of electromagnetic wave transmission and reception and the installation distance of the antenna.
  • the present invention is applicable to fields such as geological exploration, infrastructure, civil engineering, patrol inspection, etc.
  • the present invention uses the form of unmanned aerial vehicles to detect and obtain the drawings required for surveying and mapping, and obtains surveying and mapping parameters (the altitude value and latitude and longitude value of each detection point in the target area) Fast speed and high work efficiency.
  • surveying and mapping parameters the altitude value and latitude and longitude value of each detection point in the target area
  • fast speed and high work efficiency since the use of drones for detection is not restricted by the terrain, compared with manual detection, it can be used for surveying and mapping under complex terrain, and has a wide range of applications.
  • the surveying and mapping detection angle of the drone becomes larger. 120°.
  • the processing end can calculate the altitude difference at every interval of 1 meter.
  • the present invention can arrange several millimeter-wave radars according to requirements, and re-judgment the altitude information and latitude and longitude values of the same location, that is, the same detection point, which can not only improve the terrain detection accuracy of the target area, but also increase the coverage of a single flight of the surveyed area.
  • a method for surveying and mapping of drones based on millimeter-wave radar includes:
  • the millimeter-wave radar after the millimeter-wave radar emits electromagnetic waves to scan the target area, acquire electromagnetic wave transmitting and receiving state information of the millimeter-wave radar;
  • the electromagnetic wave transmitting and receiving state information includes electromagnetic wave transmitting and receiving time difference and phase difference;
  • S121 calculates the relative distance between the unmanned aerial vehicle and each detection point by substituting the following formula (1) according to the time difference between the sending and receiving of the electromagnetic waves;
  • R represents the relative distance
  • represents the relative angle
  • c represents the speed of light
  • ⁇ T represents the time difference between transmitting and receiving the electromagnetic wave
  • represents the wavelength of the electromagnetic wave
  • represents the phase difference
  • L represents the antenna installation distance
  • the positioning data includes latitude and longitude information and altitude information of the drone;
  • Jn sin ⁇ *S/(cos(Wn)*D) (7)
  • the R represents the relative distance
  • represents the relative angle
  • S represents the stroke distance
  • h represents the stroke height
  • represents the distance between the straight line where the relative distance is located and the straight line where the left and right directions are located.
  • W n represents the latitude value of the nth detection point
  • J n represents the longitude value of the nth detection point
  • H n represents the altitude value of the nth detection point.
  • the millimeter-wave radar emits electromagnetic waves to scan the target area for detection. Since the bottom of the UAV can obtain several detection points at a time, the detection points A, B, C, ... as shown in Figure 4 below. Taking detection point A and detection point C as an example, refer to the above formula for conversion.
  • UAV unmanned aerial vehicle
  • UAV obtains the positioning data measured by positioning equipment such as Beidou, GPS, and Glonass systems in real time, that is, through real-time measurement of positioning equipment.
  • the latitude and longitude information and altitude information of the drone are recorded by the Flash memory installed in the drone at this time.
  • the processing end retrieves the latitude and longitude information and altitude information of the drone from the positioning device or Flash memory of the drone. According to the latitude and longitude information and altitude information of the UAV, the processing end can convert the latitude and longitude and altitude values of detection point A by referring to the above formula.
  • S310 compares several altitude values and latitude and longitude values of the current detection point, and deletes the altitude value and latitude and longitude value of the current detection point if they do not match;
  • S320 switch and compare the next detection point, until the acquisition of several altitude values and latitude and longitude values of all detection points in the target area match, draw and generate The topographic map.
  • the processing end records and integrates the data frame, that is, the latitude and longitude coordinates measured by the installation equipment installed on the UAV, that is, matches the altitude information of the terrain at each latitude and longitude according to the flight trajectory and scanning range of the UAV.
  • the longitude and latitude values of all detection points and the corresponding altitude information measured by the radar in real time are converted, and then according to the real-time 3D terrain mapping data of the target area where the track is located, that is, the latitude and longitude values of all detection points and the corresponding altitude information, generate Real-time 3D terrain map of the target area where the track is located.
  • the present invention arranges several millimeter-wave radars according to requirements, and conducts re-judgment and verification on the altitude information and latitude and longitude values of the same location, that is, the same detection point, which can not only improve the terrain detection accuracy of the target area, but also increase the coverage of a single flight of the surveyed area.
  • the present invention does not need to rely on manual field surveying and mapping to obtain the original data, which not only saves the manpower of manual surveying and mapping, but also relies on the distance calculation formula to accurately obtain the terrain data of the target area, which can effectively reduce the terrain measurement error of the target area, making the overall
  • the topographic measurements are more precise, resulting in more accurate and reliable topographic maps.
  • the present invention also provides a drone surveying and mapping system based on millimeter wave radar, including:
  • the control module is used to control several millimeter-wave radars installed at the bottom of the drone to emit electromagnetic waves to scan the target area;
  • An acquisition module configured to calculate the relative distance between the UAV and each detection point, and the relative angle between the UAV and each detection point in the height direction; the target area includes several detection points;
  • the processing module is used to calculate the altitude value and latitude and longitude value of the detection point according to the relative distance and relative angle, as well as the positioning data of the positioning device carried on the drone;
  • a generating module configured to generate a topographic map of the target area according to the altitude values and latitude and longitude values of all detection points.
  • this embodiment is a system embodiment corresponding to the above method embodiment.
  • this embodiment is a system embodiment corresponding to the above method embodiment.
  • the acquisition module includes:
  • the first acquisition sub-module is used to acquire the electromagnetic wave transmitting and receiving status information of the millimeter wave radar after the millimeter wave radar emits electromagnetic waves to scan the target area;
  • the calculation sub-module is used to calculate the relative distance and relative angle between the UAV and each detection point according to the state information of the electromagnetic wave transmission and reception and the installation distance of the antenna.
  • this embodiment is a system embodiment corresponding to the above method embodiment.
  • this embodiment is a system embodiment corresponding to the above method embodiment.
  • the electromagnetic wave transceiving state information includes electromagnetic wave transceiving time difference and phase difference;
  • the calculation submodule includes:
  • the relative distance calculation unit is used to calculate the relative distance between the UAV and each detection point by substituting the following formula (1) according to the time difference between sending and receiving of the electromagnetic wave;
  • the relative angle calculation unit is used to calculate the relative angle by substituting the following formula (2) according to the antenna installation distance, the wavelength of the electromagnetic wave and the phase difference;
  • R represents the relative distance
  • represents the relative angle
  • c represents the speed of light
  • ⁇ T represents the time difference between transmitting and receiving the electromagnetic wave
  • represents the wavelength of the electromagnetic wave
  • represents the phase difference
  • L represents the antenna installation distance
  • this embodiment is a system embodiment corresponding to the above method embodiment.
  • this embodiment is a system embodiment corresponding to the above method embodiment.
  • processing module includes:
  • the second acquisition sub-module is used to acquire the positioning data measured by the positioning device;
  • the positioning data includes the longitude and latitude information and the altitude information of the drone;
  • the distance calculation sub-module is used to calculate the travel distance between the drone and the detection point in the left and right directions by substituting the following formula (4) according to the relative distance and the relative angle;
  • the height calculation sub-module is used to calculate the travel height in the height direction between the drone and the detection point by substituting the following formula (5) according to the relative distance and the relative angle;
  • the latitude calculation submodule is used to calculate the latitude value of the detection point by substituting the following formula (6) into the longitude and latitude information according to the travel distance;
  • the longitude calculation submodule is used to calculate the longitude value of the detection point according to the travel distance and the latitude and longitude information by substituting the following formula (7);
  • Jn sin ⁇ *S/(cos(Wn)*D) (7)
  • the altitude calculation submodule is used to calculate the altitude value of the detection point by substituting the following formula (8) according to the travel height and the altitude information;
  • the R represents the relative distance
  • represents the relative angle
  • S represents the stroke distance
  • h represents the stroke height
  • represents the distance between the straight line where the relative distance is located and the straight line where the left and right directions are located.
  • W n represents the latitude value of the nth detection point
  • J n represents the longitude value of the nth detection point
  • H n represents the altitude value of the nth detection point.
  • this embodiment is a system embodiment corresponding to the above method embodiment.
  • this embodiment is a system embodiment corresponding to the above method embodiment.
  • the generating module includes:
  • the comparison sub-module is used to compare several altitude values and latitude and longitude values of the current detection point, and if they do not match, delete the altitude value and the latitude and longitude value of the current detection point;
  • this embodiment is a system embodiment corresponding to the above method embodiment.
  • this embodiment is a system embodiment corresponding to the above method embodiment.
  • the disclosed apparatus/terminal device and method may be implemented in other ways.
  • the device/terminal device embodiments described above are only illustrative.
  • the division of the modules or units is only a logical function division.
  • there may be other division methods for example, multiple Units or components may be combined or integrated into another system, or some features may be omitted, or not implemented.
  • the mutual coupling or direct coupling or communication connection shown or discussed may be through some interfaces, and the indirect coupling or communication connection of devices or units may be in electrical, mechanical or other forms.
  • the units described as separate components may or may not be physically separated, and the components displayed as units may or may not be physical units, that is, they may be located in one place, or may be distributed to multiple network units. Part or all of the units can be selected according to actual needs to achieve the purpose of the solution of this embodiment.
  • each functional unit in each embodiment of the present application may be integrated into one processing unit, each unit may exist separately physically, or two or more units may be integrated into one unit.
  • the above-mentioned integrated units can be implemented in the form of hardware or in the form of software functional units.

Abstract

An unmanned aerial vehicle surveying and mapping method and system based on a millimeter wave radar, the method comprising: controlling multiple millimeter wave radars mounted at the bottom part of an unmanned aerial vehicle to transmit electromagnetic waves so as to scan a target area, and calculating the relative distance between the unmanned aerial vehicle and each detection point as well as the relative included angle between the unmanned aerial vehicle and each detection point along the height direction, the target area comprising multiple detection points (S100); according to the relative distance, the relative included angle, and positioning data of a positioning device mounted on the unmanned aerial vehicle, calculating to obtain the altitude value and the latitude and longitude values of the detection points (S200); and generating a topographic map of the target area according to the altitude value and the latitude and longitude values of all detection points (S300). Said method improves operation efficiency of topography surveying, the narrow application range and the mapping precision.

Description

一种基于毫米波雷达的无人机测绘方法和系统A method and system for unmanned aerial vehicle surveying and mapping based on millimeter wave radar 技术领域technical field
本发明涉及地形测绘技术领域,尤指一种基于毫米波雷达的无人机测绘方法和系统。The invention relates to the technical field of topographic surveying and mapping, in particular to a method and system for surveying and mapping of an unmanned aerial vehicle based on millimeter wave radar.
背景技术Background technique
地形测绘主要是对地块权属界线的界址点坐标进行精确测定,并把地块及其附着物的位置、面积、权属关系和利用状况等要素准确地绘制在图纸上和记录在专门的表册中的测绘工作。Topographic surveying and mapping is mainly to accurately measure the coordinates of the boundary points of the land parcel ownership boundary, and to accurately draw the location, area, ownership relationship, utilization status and other elements of the land parcel and its attachments on the drawings and record them in special Mapping work in the table book.
传统的地形测绘一般采用人工跑点的作业方式先对地块进行测量,测量过程中使用到全站仪或RTK系统。利用全站仪进行测量时,需要不断的进行搬站定向,作业效率低下。利用RTK系统进行测量时,RTK系统包括固定测量站和移动测量站,固定测量站通过数据链将其观测值和测站坐标信息一起传送给移动测量站,移动测量站不但接收来自固定测量站的数据,还接收卫星发送的GPS数据,结合计算移动侧两站当前坐标数据;由于PTK系统测量必须使用到GPS数据,而移动测量站经过房屋密集或树木密集的地方时,难以接收到GPS数据,PTK难以固定,无法计算得到移动测量站的当前坐标数据,难以完成地块测量工作,适用范围窄。Traditional topographic surveying and mapping generally adopts the operation method of manually running points to measure the plot first, and a total station or RTK system is used in the measurement process. When using a total station for measurement, it is necessary to continuously move and orient the station, which leads to low operating efficiency. When the RTK system is used for measurement, the RTK system includes a fixed measuring station and a mobile measuring station. The fixed measuring station transmits its observation value and the coordinate information of the measuring station to the mobile measuring station through the data link. The mobile measuring station not only receives the data from the fixed measuring station The data also receives the GPS data sent by the satellite, combined with the calculation of the current coordinate data of the two stations on the mobile side; because the PTK system measurement must use GPS data, it is difficult for the mobile measurement station to receive GPS data when passing through densely populated houses or dense trees. PTK is difficult to fix, it is impossible to calculate the current coordinate data of the mobile survey station, it is difficult to complete the land survey work, and the scope of application is narrow.
因此,现有的地形测绘方法存在作业效率低下、适用范围窄或测绘精度低的缺陷。Therefore, the existing topographic surveying and mapping methods have the defects of low operation efficiency, narrow application range or low surveying and mapping accuracy.
发明内容Contents of the invention
本发明的目的是提供一种基于毫米波雷达的无人机测绘方法和系统,实现提高地形测量的作业效率、适用范围窄和测绘精度。The purpose of the present invention is to provide a method and system for UAV surveying and mapping based on millimeter-wave radar, so as to improve the operational efficiency of topographical survey, narrow application range and surveying and mapping accuracy.
本发明提供的技术方案如下:The technical scheme provided by the invention is as follows:
本发明提供一种基于毫米波雷达的无人机测绘方法,包括步骤:The present invention provides a method for surveying and mapping of an unmanned aerial vehicle based on a millimeter wave radar, comprising the steps of:
控制安装于无人机底部的若干个毫米波雷达发射电磁波以扫描目标区域,计算所述无人机与各探测点之间的相对距离,以及所述无人机与各探测点在高度方向上的相对夹角;所述目标区域包括若干个探测点;Control several millimeter-wave radars installed at the bottom of the UAV to emit electromagnetic waves to scan the target area, calculate the relative distance between the UAV and each detection point, and the distance between the UAV and each detection point in the height direction The relative angle; The target area includes several detection points;
根据所述相对距离和相对夹角,以及搭载在所述无人机上的定位设备的定位数据,计算得到所述探测点的海拔高度值和经纬度值;According to the relative distance and relative angle, and the positioning data of the positioning device carried on the drone, calculate the altitude value and latitude and longitude value of the detection point;
根据所有探测点的海拔高度值和经纬度值,生成所述目标区域的地形图。A topographic map of the target area is generated according to the altitude values and latitude and longitude values of all detection points.
进一步的,所述获取所述无人机与各探测点之间的相对距离和相对夹角包括步骤:Further, the obtaining the relative distance and relative angle between the UAV and each detection point includes the steps of:
在所述毫米波雷达发射电磁波扫描目标区域后,获取所述毫米波雷达的电磁波收发状态信息;After the millimeter-wave radar emits electromagnetic waves to scan the target area, acquire the electromagnetic wave transmitting and receiving state information of the millimeter-wave radar;
根据所述电磁波收发状态信息和天线安装间距,计算得到所述无人机与各探测点之间的相对距离和相对夹角。The relative distance and relative angle between the UAV and each detection point are calculated according to the electromagnetic wave receiving and receiving state information and the antenna installation distance.
进一步的,所述电磁波收发状态信息包括电磁波收发时间差和相位差;所述根据所述电磁波收发状态信息和天线安装间距,计算得到所述无人机与各探测点之间的相对距离和相对夹角包括步骤:Further, the state information of electromagnetic wave transmission and reception includes the time difference and phase difference of electromagnetic wave transmission and reception; the relative distance and relative distance between the UAV and each detection point are calculated according to the state information of electromagnetic wave transmission and reception and the antenna installation distance. Angular includes steps:
根据所述电磁波收发时间差,代入下列公式(1)计算得到所述无人机与各探测点之间的相对距离;According to the time difference of transmitting and receiving of the electromagnetic wave, the relative distance between the unmanned aerial vehicle and each detection point is calculated by substituting the following formula (1);
Figure PCTCN2021141120-appb-000001
Figure PCTCN2021141120-appb-000001
根据天线安装间距、所述电磁波波长和相位差,代入下列公式(2)计算得到所述相对夹角;According to the antenna installation distance, the wavelength of the electromagnetic wave and the phase difference, the relative angle is calculated by substituting the following formula (2);
Figure PCTCN2021141120-appb-000002
Figure PCTCN2021141120-appb-000002
其中,R表示所述相对距离,θ表示所述相对夹角,c表示光速,ΔT表示所述电磁波收发时间差,λ表示电磁波波长,ΔΦ表示相位差,L表示天线安装间距。Wherein, R represents the relative distance, θ represents the relative angle, c represents the speed of light, ΔT represents the time difference between transmitting and receiving the electromagnetic wave, λ represents the wavelength of the electromagnetic wave, ΔΦ represents the phase difference, and L represents the antenna installation distance.
进一步的,所述根据所述相对距离和相对夹角,以及搭载在所述无人机上的定位设备的定位数据,计算得到所述探测点的海拔高度值和经纬度值包括步骤:Further, the calculating the altitude value and the latitude and longitude value of the detection point according to the relative distance and relative angle, and the positioning data of the positioning device carried on the UAV includes the steps of:
获取所述定位设备测量得到的定位数据;所述定位数据包括所述无人机的经纬度信息和海拔高度信息;Acquiring positioning data measured by the positioning device; the positioning data includes latitude and longitude information and altitude information of the drone;
根据所述相对距离、相对夹角,代入下列公式(4)计算得到所述无人机与所述探测点之间在左右方向上的行程距离;According to the relative distance and the relative angle, the following formula (4) is substituted into the calculation to obtain the travel distance in the left and right direction between the drone and the detection point;
S=sinθ*R                                            (4);S=sinθ*R (4);
根据所述相对距离、相对夹角,代入下列公式(5)计算得到所述无人机与所述探测点之间在高度方向上的行程高度;According to the relative distance and the relative angle, the following formula (5) is substituted into the calculation to obtain the travel height in the height direction between the UAV and the detection point;
h=cosθ*R                                            (5);h=cosθ*R (5);
根据所述行程距离,经纬度信息,代入下列公式(6)计算得到所述探测点的纬度值;According to the travel distance, the latitude and longitude information is substituted into the following formula (6) to calculate the latitude value of the detection point;
W n=cosα*S/D                                         (6); W n =cosα*S/D (6);
根据所述行程距离,经纬度信息,代入下列公式(7)计算得到所述探测点的经度值;According to described travel distance, longitude and latitude information, substitute following formula (7) to calculate and obtain the longitude value of described detection point;
J n=sinα*S/(cos(Wn)*D)                                 (7); Jn = sinα*S/(cos(Wn)*D) (7);
根据所述行程高度和所述海拔高度信息,代入下列公式(8)计算得到所述探测点的海拔高度值;According to the stroke height and the altitude information, the altitude value of the detection point is calculated by substituting the following formula (8);
Figure PCTCN2021141120-appb-000003
Figure PCTCN2021141120-appb-000003
其中,所述R表示所述相对距离,θ表示所述相对夹角,S表示所述 行程距离,h表示所述行程高度,α表示所述相对距离所在直线与左右方向所在直线之间的夹角,W n表示第n个探测点的纬度值,J n表示第n个探测点的经度值,H n表示第n个探测点的海拔高度值。 Wherein, the R represents the relative distance, θ represents the relative angle, S represents the stroke distance, h represents the stroke height, and α represents the distance between the straight line where the relative distance is located and the straight line where the left and right directions are located. angle, W n represents the latitude value of the nth detection point, J n represents the longitude value of the nth detection point, H n represents the altitude value of the nth detection point.
进一步的,所述根据所有探测点的海拔高度值和经纬度值,生成所述目标区域的地形图包括步骤:Further, the generating the topographic map of the target area according to the altitude values and latitude and longitude values of all detection points includes the steps of:
比对当前探测点的若干个海拔高度值和经纬度值,若不匹配则删除所述当前探测点的海拔高度值和经纬度值;Comparing several altitude values and latitude and longitude values of the current detection point, if they do not match, deleting the altitude value and latitude and longitude value of the current detection point;
切换比对下一探测点,直至获取到所述目标区域中所有探测点的若干个海拔高度值和经纬度值匹配为止,根据各探测点分别对应的若干个海拔高度值和经纬度值,绘制生成所述地形图。Switch and compare the next detection point until several altitude values and longitude and latitude values of all detection points in the target area are obtained to match. topographical map.
本发明还提供一种基于毫米波雷达的无人机测绘系统,包括:The present invention also provides a drone surveying and mapping system based on millimeter wave radar, including:
控制模块,用于控制安装于无人机底部的若干个毫米波雷达发射电磁波以扫描目标区域;The control module is used to control several millimeter-wave radars installed at the bottom of the drone to emit electromagnetic waves to scan the target area;
获取模块,用于计算所述无人机与各探测点之间的相对距离,以及所述无人机与各探测点在高度方向上的相对夹角;所述目标区域包括若干个探测点;An acquisition module, configured to calculate the relative distance between the UAV and each detection point, and the relative angle between the UAV and each detection point in the height direction; the target area includes several detection points;
处理模块,用于根据所述相对距离和相对夹角,以及搭载在所述无人机上的定位设备的定位数据,计算得到所述探测点的海拔高度值和经纬度值;The processing module is used to calculate the altitude value and latitude and longitude value of the detection point according to the relative distance and relative angle, as well as the positioning data of the positioning device carried on the drone;
生成模块,用于根据所有探测点的海拔高度值和经纬度值,生成所述目标区域的地形图。A generating module, configured to generate a topographic map of the target area according to the altitude values and latitude and longitude values of all detection points.
进一步的,所述获取模块包括:Further, the acquisition module includes:
第一获取子模块,用于在所述毫米波雷达发射电磁波扫描目标区域后,获取所述毫米波雷达的电磁波收发状态信息;The first acquisition sub-module is used to acquire the electromagnetic wave transmitting and receiving status information of the millimeter wave radar after the millimeter wave radar emits electromagnetic waves to scan the target area;
计算子模块,用于根据所述电磁波收发状态信息和天线安装间距,计 算得到所述无人机与各探测点之间的相对距离和相对夹角。The calculation sub-module is used to calculate the relative distance and relative angle between the unmanned aerial vehicle and each detection point according to the state information of transmitting and receiving electromagnetic waves and the installation distance of the antenna.
进一步的,所述电磁波收发状态信息包括电磁波收发时间差和相位差;所述计算子模块包括:Further, the electromagnetic wave transceiving state information includes electromagnetic wave transceiving time difference and phase difference; the calculation submodule includes:
相对距离计算单元,用于根据所述电磁波收发时间差,代入下列公式(1)计算得到所述无人机与各探测点之间的相对距离;The relative distance calculation unit is used to calculate the relative distance between the UAV and each detection point by substituting the following formula (1) according to the time difference between sending and receiving of the electromagnetic wave;
Figure PCTCN2021141120-appb-000004
Figure PCTCN2021141120-appb-000004
相对夹角计算单元,用于根据天线安装间距、所述电磁波波长和相位差,代入下列公式(2)计算得到所述相对夹角;The relative angle calculation unit is used to calculate the relative angle by substituting the following formula (2) according to the antenna installation distance, the wavelength of the electromagnetic wave and the phase difference;
Figure PCTCN2021141120-appb-000005
Figure PCTCN2021141120-appb-000005
其中,R表示所述相对距离,θ表示所述相对夹角,c表示光速,ΔT表示所述电磁波收发时间差,λ表示电磁波波长,ΔΦ表示相位差,L表示天线安装间距。Wherein, R represents the relative distance, θ represents the relative angle, c represents the speed of light, ΔT represents the time difference between transmitting and receiving the electromagnetic wave, λ represents the wavelength of the electromagnetic wave, ΔΦ represents the phase difference, and L represents the antenna installation distance.
进一步的,所述处理模块包括:Further, the processing module includes:
第二获取子模块,用于获取所述定位设备测量得到的定位数据;所述定位数据包括所述无人机的经纬度信息和海拔高度信息;The second acquisition sub-module is used to acquire the positioning data measured by the positioning device; the positioning data includes the longitude and latitude information and the altitude information of the drone;
距离计算子模块,用于根据所述相对距离、相对夹角,代入下列公式(4)计算得到所述无人机与所述探测点之间在左右方向上的行程距离;The distance calculation sub-module is used to calculate the travel distance between the drone and the detection point in the left and right directions by substituting the following formula (4) according to the relative distance and the relative angle;
S=sinθ*R                                            (4);S=sinθ*R (4);
高度计算子模块,用于根据所述相对距离、相对夹角,代入下列公式(5)计算得到所述无人机与所述探测点之间在高度方向上的行程高度;The height calculation sub-module is used to calculate the travel height in the height direction between the drone and the detection point by substituting the following formula (5) according to the relative distance and the relative angle;
h=cosθ*R                                            (5);h=cosθ*R (5);
纬度计算子模块,用于根据所述行程距离,经纬度信息,代入下列公式(6)计算得到所述探测点的纬度值;The latitude calculation submodule is used to calculate the latitude value of the detection point by substituting the following formula (6) into the longitude and latitude information according to the travel distance;
W n=cosα*S/D                                         (6); W n =cosα*S/D (6);
经度计算子模块,用于根据所述行程距离,经纬度信息,代入下列公式(7)计算得到所述探测点的经度值;The longitude calculation submodule is used to calculate the longitude value of the detection point according to the travel distance and the latitude and longitude information by substituting the following formula (7);
J n=sinα*S/(cos(Wn)*D)                                  (7); Jn = sinα*S/(cos(Wn)*D) (7);
海拔计算子模块,用于根据所述行程高度和所述海拔高度信息,代入下列公式(8)计算得到所述探测点的海拔高度值;The altitude calculation submodule is used to calculate the altitude value of the detection point by substituting the following formula (8) according to the travel height and the altitude information;
Figure PCTCN2021141120-appb-000006
Figure PCTCN2021141120-appb-000006
其中,所述R表示所述相对距离,θ表示所述相对夹角,S表示所述行程距离,h表示所述行程高度,α表示所述相对距离所在直线与左右方向所在直线之间的夹角,W n表示第n个探测点的纬度值,J n表示第n个探测点的经度值,H n表示第n个探测点的海拔高度值。 Wherein, the R represents the relative distance, θ represents the relative angle, S represents the stroke distance, h represents the stroke height, and α represents the distance between the straight line where the relative distance is located and the straight line where the left and right directions are located. angle, W n represents the latitude value of the nth detection point, J n represents the longitude value of the nth detection point, H n represents the altitude value of the nth detection point.
进一步的,所述生成模块包括:Further, the generating module includes:
比对子模块,用于比对当前探测点的若干个海拔高度值和经纬度值,若不匹配则删除所述当前探测点的海拔高度值和经纬度值;The comparison sub-module is used to compare several altitude values and latitude and longitude values of the current detection point, and if they do not match, delete the altitude value and the latitude and longitude value of the current detection point;
生成子模块,用于切换比对下一探测点,直至获取到所述目标区域中所有探测点的若干个海拔高度值和经纬度值匹配为止,根据各探测点分别对应的若干个海拔高度值和经纬度值,绘制生成所述地形图。Generate a sub-module for switching and comparing the next detection point until the acquisition of several altitude values and latitude and longitude values of all detection points in the target area match, according to the several altitude values and latitude values corresponding to each detection point Longitude and latitude values, draw to generate the topographic map.
通过本发明提供的一种基于毫米波雷达的无人机测绘方法和系统,能够提高地形测量的作业效率、适用范围窄和测绘精度。Through the millimeter-wave radar-based UAV surveying and mapping method and system provided by the present invention, the operational efficiency of terrain surveying, narrow application range and surveying and mapping accuracy can be improved.
附图说明Description of drawings
下面将以明确易懂的方式,结合附图说明优选实施方式,对一种基于毫米波雷达的无人机测绘方法和系统的上述特性、技术特征、优点及其实现方式予以进一步说明。The preferred implementation will be described below in a clear and understandable manner with reference to the accompanying drawings, and the above-mentioned characteristics, technical features, advantages and implementation methods of a millimeter-wave radar-based UAV surveying and mapping method and system will be further described.
图1是本发明一种基于毫米波雷达的无人机测绘方法的一个实施例的流程 图;Fig. 1 is a flow chart of an embodiment of a method for unmanned aerial vehicle surveying and mapping based on millimeter-wave radar of the present invention;
图2是本发明一种基于毫米波雷达的无人机测绘方法的另一个实施例的流程图;Fig. 2 is a flow chart of another embodiment of a method for surveying and mapping of an unmanned aerial vehicle based on a millimeter-wave radar in the present invention;
图3是本发明一种基于毫米波雷达的无人机测绘方法的另一个实施例的流程图;Fig. 3 is a flow chart of another embodiment of a method for surveying and mapping of an unmanned aerial vehicle based on a millimeter-wave radar in the present invention;
图4是本发明一种基于毫米波雷达的无人机测绘方法的探测点与无人机收发电磁波之间关系的示意图。Fig. 4 is a schematic diagram of the relationship between detection points and electromagnetic waves sent and received by the drone in a millimeter-wave radar-based UAV surveying and mapping method according to the present invention.
具体实施方式detailed description
以下描述中,为了说明而不是为了限定,提出了诸如特定系统结构、技术之类的具体细节,以便透彻理解本申请实施例。然而,本领域的技术人员应当清楚,在没有这些具体细节的其他实施例中也可以实现本申请。在其他情况中,省略对众所周知的系统、装置、电路以及方法的详细说明,以免不必要的细节妨碍本申请的描述。In the following description, specific details such as specific system structures and technologies are presented for the purpose of illustration rather than limitation, so as to thoroughly understand the embodiments of the present application. However, it will be apparent to those skilled in the art that the present application may be practiced in other embodiments without these specific details. In other instances, detailed descriptions of well-known systems, devices, circuits, and methods are omitted so as not to obscure the description of the present application with unnecessary detail.
应当理解,当在本说明书和所附权利要求书中使用时,术语“包括”指示所述描述特征、整体、步骤、操作、元素和/或组件的存在,但并不排除一个或多个其他特征、整体、步骤、操作、元素、组件和/或集合的存在或添加。It should be understood that when used in this specification and the appended claims, the term "comprising" indicates the presence of described features, integers, steps, operations, elements and/or components, but does not exclude one or more other Presence or addition of characteristics, wholes, steps, operations, elements, components and/or collections.
为使图面简洁,各图中只示意性地表示出了与本发明相关的部分,它们并不代表其作为产品的实际结构。另外,以使图面简洁便于理解,在有些图中具有相同结构或功能的部件,仅示意性地绘示了其中的一个,或仅标出了其中的一个。在本文中,“一个”不仅表示“仅此一个”,也可以表示“多于一个”的情形。In order to make the drawing concise, each drawing only schematically shows the parts related to the present invention, and they do not represent the actual structure of the product. In addition, to make the drawings concise and easy to understand, in some drawings, only one of the components having the same structure or function is schematically shown, or only one of them is marked. Herein, "a" not only means "only one", but also means "more than one".
还应当进一步理解,在本申请说明书和所附权利要求书中使用的术语“和/或”是指相关联列出的项中的一个或多个的任何组合以及所有可能组合,并且包括这些组合。It should also be further understood that the term "and/or" used in the description of the present application and the appended claims refers to any combination and all possible combinations of one or more of the associated listed items, and includes these combinations .
另外,在本申请的描述中,术语“第一”、“第二”等仅用于区分描述,而不 能理解为指示或暗示相对重要性。In addition, in the description of the present application, the terms "first", "second", etc. are only used to distinguish descriptions, and cannot be understood as indicating or implying relative importance.
为了更清楚地说明本发明实施例或现有技术中的技术方案,下面将对照附图说明本发明的具体实施方式。显而易见地,下面描述中的附图仅仅是本发明的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其他的附图,并获得其他的实施方式。In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the specific implementation manners of the present invention will be described below with reference to the accompanying drawings. Obviously, the accompanying drawings in the following description are only some embodiments of the present invention, and those skilled in the art can obtain other accompanying drawings based on these drawings and obtain other implementations.
本发明的一个实施例,如图1所示,一种基于毫米波雷达的无人机测绘方法,包括:One embodiment of the present invention, as shown in Fig. 1, a kind of UAV surveying and mapping method based on millimeter wave radar, comprises:
S100控制安装于无人机底部的若干个毫米波雷达发射电磁波以扫描目标区域,计算所述无人机与各探测点之间的相对距离,以及所述无人机与各探测点在高度方向上的相对夹角;所述目标区域包括若干个探测点;S100 controls several millimeter-wave radars installed at the bottom of the UAV to emit electromagnetic waves to scan the target area, and calculates the relative distance between the UAV and each detection point, and the distance between the UAV and each detection point in the height direction The relative angle on the above; the target area includes several detection points;
具体的,目标区域是指无人机飞行探测的区域,可以是山谷、丘陵地段,也可以是城市地段等允许无人机飞行的地段,整个目标区域由边界和内部区域构成,可以将目标区域离散成若干个探测点。毫米波雷达指工作在毫米波波段的雷达,其工作频率通常选在30~300GHz范围内。本发明的毫米波雷达的工作频段在60~64GHz、76~81GHz之间。本发明首先在无人机底部布置若干颗工作频段为60~64GHz、76~81GHz的毫米波雷达传感器,通过这些无人机底部安装的若干个毫米波雷达发射电磁波以扫描整个目标区域以获取检测数据,然后,处理端(包括安装在无人机上的控制器或者处理器,以及与无人机进行无线通信连接的服务器)就能够通过无线或者有线的方式,从各个毫米波雷达处获取检测数据,进而根据检测数据计算得到无人机与各探测点之间的相对距离,并根据检测数据计算得到无人机与各探测点在高度方向上的相对夹角。Specifically, the target area refers to the area detected by the drone flight, which can be a valley, a hilly area, or an urban area where the drone is allowed to fly. The entire target area is composed of a boundary and an internal area, and the target area can be Discrete into several detection points. Millimeter wave radar refers to the radar operating in the millimeter wave band, and its operating frequency is usually selected in the range of 30-300GHz. The operating frequency band of the millimeter wave radar of the present invention is between 60-64 GHz and 76-81 GHz. In the present invention, several millimeter-wave radar sensors with operating frequency bands of 60-64GHz and 76-81GHz are arranged at the bottom of the drone, and electromagnetic waves are emitted by several millimeter-wave radars installed on the bottom of the drone to scan the entire target area to obtain detection Data, and then, the processing end (including the controller or processor installed on the UAV, and the server connected to the UAV for wireless communication) can obtain detection data from various millimeter-wave radars in a wireless or wired manner , and then calculate the relative distance between the UAV and each detection point according to the detection data, and calculate the relative angle between the UAV and each detection point in the height direction according to the detection data.
S200根据所述相对距离和相对夹角,以及搭载在所述无人机上的定位设备的定位数据,计算得到所述探测点的海拔高度值和经纬度值;S200 Calculate and obtain the altitude value and latitude and longitude value of the detection point according to the relative distance and relative angle, and the positioning data of the positioning device carried on the drone;
S300根据所有探测点的海拔高度值和经纬度值,生成所述目标区域 的地形图。S300 generates a topographic map of the target area according to the altitude values and latitude and longitude values of all detection points.
具体的,处理端根据上述计算得到的相对距离和相对夹角,以及搭载在无人机上的定位设备的定位数据,计算得到各个探测点的海拔高度值和经纬度值。最后,处理端根据所有探测点的海拔高度值和经纬度值,生成目标区域的地形图。Specifically, the processing end calculates the altitude value and latitude and longitude value of each detection point according to the relative distance and relative angle obtained from the above calculation, as well as the positioning data of the positioning device mounted on the UAV. Finally, the processing end generates a topographic map of the target area based on the altitude values and latitude and longitude values of all detection points.
本发明适用于如地质勘探、基建、土建、巡检等领域,本发明采用无人机进行探测的形式获取测绘所需图纸,获取测绘参数(目标区域各探测点的海拔高度值和经纬度值)速度快,作业效率高。而且,由于采用无人机进行探测不受地形限制,相对于人工探测而言,可在复杂地形下进行测绘,适用范围广。最后,由于无人机底部安装有若干个毫米波雷达,使得无人机的测绘探测角度变大,示例性的,无人机底部四周安装有毫米波雷达,使得无人机的测绘探测角度达到120°。根据雷达的多普勒效应,处理端可计算出每间隔1米的高度差。本发明可依需求布置若干颗毫米波雷达,对同一位置即同一探测点的海拔高度信息,经纬度值进行复判,不仅仅可以提高目标区域的地形探测精度,亦可增大单次飞行所覆盖的测绘面积。The present invention is applicable to fields such as geological exploration, infrastructure, civil engineering, patrol inspection, etc. The present invention uses the form of unmanned aerial vehicles to detect and obtain the drawings required for surveying and mapping, and obtains surveying and mapping parameters (the altitude value and latitude and longitude value of each detection point in the target area) Fast speed and high work efficiency. Moreover, since the use of drones for detection is not restricted by the terrain, compared with manual detection, it can be used for surveying and mapping under complex terrain, and has a wide range of applications. Finally, since several millimeter-wave radars are installed at the bottom of the drone, the surveying and mapping detection angle of the drone becomes larger. 120°. According to the Doppler effect of the radar, the processing end can calculate the altitude difference at every interval of 1 meter. The present invention can arrange several millimeter-wave radars according to requirements, and re-judgment the altitude information and latitude and longitude values of the same location, that is, the same detection point, which can not only improve the terrain detection accuracy of the target area, but also increase the coverage of a single flight of the surveyed area.
本发明的一个实施例,如图2所示,一种基于毫米波雷达的无人机测绘方法,包括:One embodiment of the present invention, as shown in Fig. 2, a kind of UAV surveying and mapping method based on millimeter wave radar, comprises:
S110在所述毫米波雷达发射电磁波扫描目标区域后,获取所述毫米波雷达的电磁波收发状态信息;S110, after the millimeter-wave radar emits electromagnetic waves to scan the target area, acquire electromagnetic wave sending and receiving status information of the millimeter-wave radar;
S120根据所述电磁波收发状态信息和天线安装间距,计算得到所述无人机与各探测点之间的相对距离和相对夹角;S120 calculate and obtain the relative distance and relative angle between the UAV and each detection point according to the electromagnetic wave transceiving state information and the antenna installation distance;
S200根据所述相对距离和相对夹角,以及搭载在所述无人机上的定位设备的定位数据,计算得到所述探测点的海拔高度值和经纬度值;S200 Calculate and obtain the altitude value and latitude and longitude value of the detection point according to the relative distance and relative angle, and the positioning data of the positioning device carried on the drone;
S300根据所有探测点的海拔高度值和经纬度值,生成所述目标区域 的地形图。S300 generates a topographic map of the target area according to the altitude values and latitude and longitude values of all detection points.
具体的,本实施例与上述实施例相同的部分参见上述实施例,在此不再一一赘述。处理端控制毫米波雷达发射电磁波扫描目标区域后,从各个毫米波雷达处获取毫米波雷达的电磁波收发状态信息。由于每个无人机上所安装的天线(包括电磁波发射天线,电磁波接收天线)的安装位置固定,因此,处理端可获取各个天线之间的安装间距即天线安装间距。这样,处理端就可以根据电磁波收发状态信息和天线安装间距,计算得到无人机与各探测点之间的相对距离和相对夹角。Specifically, for the parts that are the same as those in the foregoing embodiments, refer to the foregoing embodiments, and details are not repeated here. After the processing end controls the millimeter-wave radar to emit electromagnetic waves to scan the target area, it obtains the electromagnetic wave sending and receiving status information of the millimeter-wave radar from each millimeter-wave radar. Since the installation positions of the antennas (including electromagnetic wave transmitting antennas and electromagnetic wave receiving antennas) installed on each UAV are fixed, the processing end can obtain the installation distance between the antennas, that is, the antenna installation distance. In this way, the processing end can calculate the relative distance and relative angle between the UAV and each detection point according to the state information of electromagnetic wave transmission and reception and the installation distance of the antenna.
本发明适用于如地质勘探、基建、土建、巡检等领域,本发明采用无人机进行探测的形式获取测绘所需图纸,获取测绘参数(目标区域各探测点的海拔高度值和经纬度值)速度快,作业效率高。而且,由于采用无人机进行探测不受地形限制,相对于人工探测而言,可在复杂地形下进行测绘,适用范围广。最后,由于无人机底部安装有若干个毫米波雷达,使得无人机的测绘探测角度变大,示例性的,无人机底部四周安装有毫米波雷达,使得无人机的测绘探测角度达到120°。根据雷达的多普勒效应,处理端可计算出每间隔1米的高度差。本发明可依需求布置若干颗毫米波雷达,对同一位置即同一探测点的海拔高度信息,经纬度值进行复判,不仅仅可以提高目标区域的地形探测精度,亦可增大单次飞行所覆盖的测绘面积。The present invention is applicable to fields such as geological exploration, infrastructure, civil engineering, patrol inspection, etc. The present invention uses the form of unmanned aerial vehicles to detect and obtain the drawings required for surveying and mapping, and obtains surveying and mapping parameters (the altitude value and latitude and longitude value of each detection point in the target area) Fast speed and high work efficiency. Moreover, since the use of drones for detection is not restricted by the terrain, compared with manual detection, it can be used for surveying and mapping under complex terrain, and has a wide range of applications. Finally, since several millimeter-wave radars are installed at the bottom of the drone, the surveying and mapping detection angle of the drone becomes larger. 120°. According to the Doppler effect of the radar, the processing end can calculate the altitude difference at every interval of 1 meter. The present invention can arrange several millimeter-wave radars according to requirements, and re-judgment the altitude information and latitude and longitude values of the same location, that is, the same detection point, which can not only improve the terrain detection accuracy of the target area, but also increase the coverage of a single flight of the surveyed area.
本发明的一个实施例,如图3所示,一种基于毫米波雷达的无人机测绘方法,包括:In one embodiment of the present invention, as shown in Figure 3, a method for surveying and mapping of drones based on millimeter-wave radar includes:
S110在所述毫米波雷达发射电磁波扫描目标区域后,获取所述毫米波雷达的电磁波收发状态信息;电磁波收发状态信息包括电磁波收发时间差和相位差;S110, after the millimeter-wave radar emits electromagnetic waves to scan the target area, acquire electromagnetic wave transmitting and receiving state information of the millimeter-wave radar; the electromagnetic wave transmitting and receiving state information includes electromagnetic wave transmitting and receiving time difference and phase difference;
S121根据所述电磁波收发时间差,代入下列公式(1)计算得到所述 无人机与各探测点之间的相对距离;S121 calculates the relative distance between the unmanned aerial vehicle and each detection point by substituting the following formula (1) according to the time difference between the sending and receiving of the electromagnetic waves;
Figure PCTCN2021141120-appb-000007
Figure PCTCN2021141120-appb-000007
S122根据天线安装间距、所述电磁波波长和相位差,代入下列公式(2)计算得到所述相对夹角;S122 According to the antenna installation distance, the wavelength of the electromagnetic wave and the phase difference, substitute the following formula (2) to calculate the relative angle;
Figure PCTCN2021141120-appb-000008
Figure PCTCN2021141120-appb-000008
其中,R表示所述相对距离,θ表示所述相对夹角,c表示光速,ΔT表示所述电磁波收发时间差,λ表示电磁波波长,ΔΦ表示相位差,L表示天线安装间距;Wherein, R represents the relative distance, θ represents the relative angle, c represents the speed of light, ΔT represents the time difference between transmitting and receiving the electromagnetic wave, λ represents the wavelength of the electromagnetic wave, ΔΦ represents the phase difference, and L represents the antenna installation distance;
S210获取所述定位设备测量得到的定位数据;所述定位数据包括所述无人机的经纬度信息和海拔高度信息;S210 Acquire positioning data measured by the positioning device; the positioning data includes latitude and longitude information and altitude information of the drone;
S220根据所述相对距离、相对夹角,代入下列公式(4)计算得到所述无人机与所述探测点之间在左右方向上的行程距离;S220 According to the relative distance and the relative angle, substitute the following formula (4) to calculate the travel distance between the UAV and the detection point in the left and right directions;
S=sinθ*R                                             (4);S=sinθ*R (4);
S230根据所述相对距离、相对夹角,代入下列公式(5)计算得到所述无人机与所述探测点之间在高度方向上的行程高度;S230 According to the relative distance and the relative angle, substitute the following formula (5) to calculate the travel height in the height direction between the UAV and the detection point;
h=cosθ*R                                             (5);h=cosθ*R (5);
S240根据所述行程距离,经纬度信息,代入下列公式(6)计算得到所述探测点的纬度值;S240 according to the travel distance, latitude and longitude information, into the following formula (6) to calculate the latitude value of the detection point;
W n=cosα*S/D                                          (6); W n =cosα*S/D (6);
S250根据所述行程距离,经纬度信息,代入下列公式(7)计算得到所述探测点的经度值;S250 according to the travel distance, latitude and longitude information, into the following formula (7) to calculate the longitude value of the detection point;
J n=sinα*S/(cos(Wn)*D)                                 (7); Jn = sinα*S/(cos(Wn)*D) (7);
S260根据所述行程高度和所述海拔高度信息,代入下列公式(8)计 算得到所述探测点的海拔高度值;S260 according to described travel altitude and described altitude information, substitute following formula (8) to calculate the altitude value of described detection point;
Figure PCTCN2021141120-appb-000009
Figure PCTCN2021141120-appb-000009
其中,所述R表示所述相对距离,θ表示所述相对夹角,S表示所述行程距离,h表示所述行程高度,α表示所述相对距离所在直线与左右方向所在直线之间的夹角,W n表示第n个探测点的纬度值,J n表示第n个探测点的经度值,H n表示第n个探测点的海拔高度值。 Wherein, the R represents the relative distance, θ represents the relative angle, S represents the stroke distance, h represents the stroke height, and α represents the distance between the straight line where the relative distance is located and the straight line where the left and right directions are located. angle, W n represents the latitude value of the nth detection point, J n represents the longitude value of the nth detection point, H n represents the altitude value of the nth detection point.
具体的,通过毫米波雷达发射电磁波扫描目标区域进行探测,由于无人机底部一次可获得若干个探测点,如下示意图4所示的探测点A、B、C,……。以探测点A、探测点C为例进行参照上述公式进行换算,UAV(无人机)实时获得北斗、GPS、格洛纳斯系统等定位设备测量得到的定位数据,即通过定位设备实时测量获取无人机的经纬度信息和海拔高度信息,并由无人机内实现安装的Flash内存记录此时无人机的经纬度信息和海拔高度信息。Specifically, the millimeter-wave radar emits electromagnetic waves to scan the target area for detection. Since the bottom of the UAV can obtain several detection points at a time, the detection points A, B, C, ... as shown in Figure 4 below. Taking detection point A and detection point C as an example, refer to the above formula for conversion. UAV (unmanned aerial vehicle) obtains the positioning data measured by positioning equipment such as Beidou, GPS, and Glonass systems in real time, that is, through real-time measurement of positioning equipment. The latitude and longitude information and altitude information of the drone are recorded by the Flash memory installed in the drone at this time.
然后,处理端从无人机的定位设备或者Flash内存处,调取无人机的经纬度信息和海拔高度信息。处理端根据无人机的经纬度信息和海拔高度信息,参照上述公式可以换算出探测点A的经纬度和海拔高度值。Then, the processing end retrieves the latitude and longitude information and altitude information of the drone from the positioning device or Flash memory of the drone. According to the latitude and longitude information and altitude information of the UAV, the processing end can convert the latitude and longitude and altitude values of detection point A by referring to the above formula.
示例性的,假设定位设备检测到的无人机的经纬度信息为纬度每秒距离为30.8m、经度每秒距离为cos该纬度*30.8m。那么,那么,即A点纬度值W A=cosα*L/30.8m*1秒,A点经度值J A=sinα*L/(cosW A*30.8m)*1秒。而且,A点海拔高度H A=无人机飞行的海拔高度信息H-行程高度h,C点海拔高度信息H C=行程高度h。 Exemplarily, it is assumed that the longitude and latitude information of the drone detected by the positioning device is that the latitude distance per second is 30.8m, and the longitude distance per second is cos the latitude*30.8m. Then, then, the latitude value of point A W A =cosα*L/30.8m*1 second, the longitude value of point A J A =sinα*L/( cosWA *30.8m)*1 second. Moreover, the altitude H A of point A = the altitude information H of the UAV flight - the travel height h, and the altitude information H C of point C = the travel height h.
S310比对当前探测点的若干个海拔高度值和经纬度值,若不匹配则删除所述当前探测点的海拔高度值和经纬度值;S310 compares several altitude values and latitude and longitude values of the current detection point, and deletes the altitude value and latitude and longitude value of the current detection point if they do not match;
S320切换比对下一探测点,直至获取到所述目标区域中所有探测点的若干 个海拔高度值和经纬度值匹配为止,根据各探测点分别对应的若干个海拔高度值和经纬度值,绘制生成所述地形图。S320 switch and compare the next detection point, until the acquisition of several altitude values and latitude and longitude values of all detection points in the target area match, draw and generate The topographic map.
具体的,处理端将该数据帧即当前与无人机上安装的安装设备所测量得到的经纬度坐标进行记录整合,即依据无人机飞行轨迹及扫描范围,匹配各经纬度下,地形的高度信息。以此类推换算出雷达实时量测到的所有探测点经纬度值以及对应的海拔高度信息,进而根据航迹所在目标区域的实时3D地形测绘数据即所有探测点经纬度值以及对应的海拔高度信息,生成航迹所在目标区域的实时3D地形图。Specifically, the processing end records and integrates the data frame, that is, the latitude and longitude coordinates measured by the installation equipment installed on the UAV, that is, matches the altitude information of the terrain at each latitude and longitude according to the flight trajectory and scanning range of the UAV. By analogy, the longitude and latitude values of all detection points and the corresponding altitude information measured by the radar in real time are converted, and then according to the real-time 3D terrain mapping data of the target area where the track is located, that is, the latitude and longitude values of all detection points and the corresponding altitude information, generate Real-time 3D terrain map of the target area where the track is located.
本发明依需求布置若干颗毫米波雷达,对同一位置即同一探测点的海拔高度信息,经纬度值进行复判核实,不仅仅可以提高目标区域的地形探测精度,亦可增大单次飞行所覆盖的测绘面积。本发明无需依赖人工实地测绘对原始数据的获取,不仅可以节省了人工进行测绘的人力,而且依赖距离计算的公式可以准确获取目标区域的地形数据,可以有效降低目标区域的地形测量误差,使得整体的地形测量结果更加精准,生成更准确,可信的地形图。The present invention arranges several millimeter-wave radars according to requirements, and conducts re-judgment and verification on the altitude information and latitude and longitude values of the same location, that is, the same detection point, which can not only improve the terrain detection accuracy of the target area, but also increase the coverage of a single flight of the surveyed area. The present invention does not need to rely on manual field surveying and mapping to obtain the original data, which not only saves the manpower of manual surveying and mapping, but also relies on the distance calculation formula to accurately obtain the terrain data of the target area, which can effectively reduce the terrain measurement error of the target area, making the overall The topographic measurements are more precise, resulting in more accurate and reliable topographic maps.
本发明还提供一种基于毫米波雷达的无人机测绘系统,包括:The present invention also provides a drone surveying and mapping system based on millimeter wave radar, including:
控制模块,用于控制安装于无人机底部的若干个毫米波雷达发射电磁波以扫描目标区域;The control module is used to control several millimeter-wave radars installed at the bottom of the drone to emit electromagnetic waves to scan the target area;
获取模块,用于计算所述无人机与各探测点之间的相对距离,以及所述无人机与各探测点在高度方向上的相对夹角;所述目标区域包括若干个探测点;An acquisition module, configured to calculate the relative distance between the UAV and each detection point, and the relative angle between the UAV and each detection point in the height direction; the target area includes several detection points;
处理模块,用于根据所述相对距离和相对夹角,以及搭载在所述无人机上的定位设备的定位数据,计算得到所述探测点的海拔高度值和经纬度值;The processing module is used to calculate the altitude value and latitude and longitude value of the detection point according to the relative distance and relative angle, as well as the positioning data of the positioning device carried on the drone;
生成模块,用于根据所有探测点的海拔高度值和经纬度值,生成所述 目标区域的地形图。A generating module, configured to generate a topographic map of the target area according to the altitude values and latitude and longitude values of all detection points.
具体的,本实施例是上述方法实施例对应的系统实施例,具体效果参见上述方法实施例,在此不再一一赘述。Specifically, this embodiment is a system embodiment corresponding to the above method embodiment. For specific effects, refer to the above method embodiment, which will not be repeated here.
进一步的,所述获取模块包括:Further, the acquisition module includes:
第一获取子模块,用于在所述毫米波雷达发射电磁波扫描目标区域后,获取所述毫米波雷达的电磁波收发状态信息;The first acquisition sub-module is used to acquire the electromagnetic wave transmitting and receiving status information of the millimeter wave radar after the millimeter wave radar emits electromagnetic waves to scan the target area;
计算子模块,用于根据所述电磁波收发状态信息和天线安装间距,计算得到所述无人机与各探测点之间的相对距离和相对夹角。The calculation sub-module is used to calculate the relative distance and relative angle between the UAV and each detection point according to the state information of the electromagnetic wave transmission and reception and the installation distance of the antenna.
具体的,本实施例是上述方法实施例对应的系统实施例,具体效果参见上述方法实施例,在此不再一一赘述。Specifically, this embodiment is a system embodiment corresponding to the above method embodiment. For specific effects, refer to the above method embodiment, which will not be repeated here.
进一步的,所述电磁波收发状态信息包括电磁波收发时间差和相位差;所述计算子模块包括:Further, the electromagnetic wave transceiving state information includes electromagnetic wave transceiving time difference and phase difference; the calculation submodule includes:
相对距离计算单元,用于根据所述电磁波收发时间差,代入下列公式(1)计算得到所述无人机与各探测点之间的相对距离;The relative distance calculation unit is used to calculate the relative distance between the UAV and each detection point by substituting the following formula (1) according to the time difference between sending and receiving of the electromagnetic wave;
Figure PCTCN2021141120-appb-000010
Figure PCTCN2021141120-appb-000010
相对夹角计算单元,用于根据天线安装间距、所述电磁波波长和相位差,代入下列公式(2)计算得到所述相对夹角;The relative angle calculation unit is used to calculate the relative angle by substituting the following formula (2) according to the antenna installation distance, the wavelength of the electromagnetic wave and the phase difference;
Figure PCTCN2021141120-appb-000011
Figure PCTCN2021141120-appb-000011
其中,R表示所述相对距离,θ表示所述相对夹角,c表示光速,ΔT表示所述电磁波收发时间差,λ表示电磁波波长,ΔΦ表示相位差,L表示天线安装间距。Wherein, R represents the relative distance, θ represents the relative angle, c represents the speed of light, ΔT represents the time difference between transmitting and receiving the electromagnetic wave, λ represents the wavelength of the electromagnetic wave, ΔΦ represents the phase difference, and L represents the antenna installation distance.
具体的,本实施例是上述方法实施例对应的系统实施例,具体效果参见上述方法实施例,在此不再一一赘述。Specifically, this embodiment is a system embodiment corresponding to the above method embodiment. For specific effects, refer to the above method embodiment, which will not be repeated here.
进一步的,所述处理模块包括:Further, the processing module includes:
第二获取子模块,用于获取所述定位设备测量得到的定位数据;所述定位数据包括所述无人机的经纬度信息和海拔高度信息;The second acquisition sub-module is used to acquire the positioning data measured by the positioning device; the positioning data includes the longitude and latitude information and the altitude information of the drone;
距离计算子模块,用于根据所述相对距离、相对夹角,代入下列公式(4)计算得到所述无人机与所述探测点之间在左右方向上的行程距离;The distance calculation sub-module is used to calculate the travel distance between the drone and the detection point in the left and right directions by substituting the following formula (4) according to the relative distance and the relative angle;
S=sinθ*R                                            (4);S=sinθ*R (4);
高度计算子模块,用于根据所述相对距离、相对夹角,代入下列公式(5)计算得到所述无人机与所述探测点之间在高度方向上的行程高度;The height calculation sub-module is used to calculate the travel height in the height direction between the drone and the detection point by substituting the following formula (5) according to the relative distance and the relative angle;
h=cosθ*R                                             (5);h=cosθ*R (5);
纬度计算子模块,用于根据所述行程距离,经纬度信息,代入下列公式(6)计算得到所述探测点的纬度值;The latitude calculation submodule is used to calculate the latitude value of the detection point by substituting the following formula (6) into the longitude and latitude information according to the travel distance;
W n=cosα*S/D                                         (6); W n =cosα*S/D (6);
经度计算子模块,用于根据所述行程距离,经纬度信息,代入下列公式(7)计算得到所述探测点的经度值;The longitude calculation submodule is used to calculate the longitude value of the detection point according to the travel distance and the latitude and longitude information by substituting the following formula (7);
J n=sinα*S/(cos(Wn)*D)                                 (7); Jn = sinα*S/(cos(Wn)*D) (7);
海拔计算子模块,用于根据所述行程高度和所述海拔高度信息,代入下列公式(8)计算得到所述探测点的海拔高度值;The altitude calculation submodule is used to calculate the altitude value of the detection point by substituting the following formula (8) according to the travel height and the altitude information;
Figure PCTCN2021141120-appb-000012
Figure PCTCN2021141120-appb-000012
其中,所述R表示所述相对距离,θ表示所述相对夹角,S表示所述行程距离,h表示所述行程高度,α表示所述相对距离所在直线与左右方向所在直线之间的夹角,W n表示第n个探测点的纬度值,J n表示第n个探测点的经度值,H n表示第n个探测点的海拔高度值。 Wherein, the R represents the relative distance, θ represents the relative angle, S represents the stroke distance, h represents the stroke height, and α represents the distance between the straight line where the relative distance is located and the straight line where the left and right directions are located. angle, W n represents the latitude value of the nth detection point, J n represents the longitude value of the nth detection point, H n represents the altitude value of the nth detection point.
具体的,本实施例是上述方法实施例对应的系统实施例,具体效果参见上述方法实施例,在此不再一一赘述。Specifically, this embodiment is a system embodiment corresponding to the above method embodiment. For specific effects, refer to the above method embodiment, which will not be repeated here.
进一步的,所述生成模块包括:Further, the generating module includes:
比对子模块,用于比对当前探测点的若干个海拔高度值和经纬度值,若不匹配则删除所述当前探测点的海拔高度值和经纬度值;The comparison sub-module is used to compare several altitude values and latitude and longitude values of the current detection point, and if they do not match, delete the altitude value and the latitude and longitude value of the current detection point;
生成子模块,用于切换比对下一探测点,直至获取到所述目标区域中所有探测点的若干个海拔高度值和经纬度值匹配为止,根据各探测点分别对应的若干个海拔高度值和经纬度值,绘制生成所述地形图。Generate a sub-module for switching and comparing the next detection point until the acquisition of several altitude values and latitude and longitude values of all detection points in the target area match, according to the several altitude values and latitude values corresponding to each detection point Longitude and latitude values, draw to generate the topographic map.
具体的,本实施例是上述方法实施例对应的系统实施例,具体效果参见上述方法实施例,在此不再一一赘述。Specifically, this embodiment is a system embodiment corresponding to the above method embodiment. For specific effects, refer to the above method embodiment, which will not be repeated here.
所属领域的技术人员可以清楚地了解到,为了描述的方便和简洁,仅以上述各程序模块的划分进行举例说明,实际应用中,可以根据需要而将上述功能分配由不同的程序模块完成,即将所述装置的内部结构划分成不同的程序单元或模块,以完成以上描述的全部或者部分功能。实施例中的各程序模块可以集成在一个处理单元中,也可是各个单元单独物理存在,也可以两个或两个以上单元集成在一个处理单元中,上述集成的单元既可以采用硬件的形式实现,也可以采用软件程序单元的形式实现。另外,各程序模块的具体名称也只是为了便于相互区分,并不用于限制本申请的保护范围。Those skilled in the art can clearly understand that for the convenience and brevity of description, only the division of the above-mentioned program modules is used as an example for illustration. In practical applications, the above-mentioned functions can be allocated by different program modules according to needs. The internal structure of the device is divided into different program units or modules to complete all or part of the functions described above. Each program module in the embodiment can be integrated in one processing unit, or each unit can exist separately physically, or two or more units can be integrated in one processing unit, and the above-mentioned integrated units can be implemented in the form of hardware , can also be implemented in the form of software program units. In addition, the specific names of the program modules are only for the convenience of distinguishing each other, and are not used to limit the protection scope of the present application.
它们可以用计算装置可执行的程序代码来实现,从而,可以将它们存储在存储装置中由计算装置来执行,或者将它们分别制作成各个集成电路模块,或者将它们中的多个模块或步骤制作成单个集成电路模块来实现。这样,本发明不限制于任何特定的硬件和软件结合。They can be implemented with program codes executable by computing devices, and thus, they can be stored in storage devices and executed by computing devices, or they can be made into individual integrated circuit modules, or a plurality of modules or steps in them Made into a single integrated circuit module to achieve. As such, the present invention is not limited to any specific combination of hardware and software.
在上述实施例中,对各个实施例的描述都各有侧重,某个实施例中没有详细描述或记载的部分,可以参见其他实施例的相关描述。In the above-mentioned embodiments, the descriptions of each embodiment have their own emphases, and for parts that are not described or recorded in detail in a certain embodiment, reference may be made to relevant descriptions of other embodiments.
本领域普通技术人员可以意识到,结合本文中所公开的实施例描述的各示例的单元及算法步骤,能够以电子硬件、或者计算机软件和电子硬件的结合来实现。这些功能究竟以硬件还是软件来执行,取决于技术方案的特定应用和设计约束条件。专业技术人员可以对每个特定的应用来使用不 同方法来实现所描述的功能,但是这种实现不应认为超出本申请的范围。Those skilled in the art can appreciate that the units and algorithm steps of the examples described in conjunction with the embodiments disclosed herein can be implemented by electronic hardware, or a combination of computer software and electronic hardware. Whether these functions are implemented by hardware or software depends on the specific application and design constraints of the technical solution. Those skilled in the art may use different methods to implement the described functions for each specific application, but such implementation should not be regarded as exceeding the scope of the present application.
在本申请所提供的实施例中,应该理解到,所揭露的装置/终端设备和方法,可以通过其他的方式实现。例如,以上所描述的装置/终端设备实施例仅仅是示意性的,例如,所述模块或单元的划分,仅仅为一种逻辑功能划分,实际实现时可以有另外的划分方式,例如,多个单元或组件可以结合或者可以集成到另一个系统,或一些特征可以忽略,或不执行。另一点,所显示或讨论的相互之间的耦合或直接耦合或通讯连接可以是通过一些接口,装置或单元的间接耦合或通讯连接,可以是电性、机械或其他的形式。In the embodiments provided in this application, it should be understood that the disclosed apparatus/terminal device and method may be implemented in other ways. For example, the device/terminal device embodiments described above are only illustrative. For example, the division of the modules or units is only a logical function division. In actual implementation, there may be other division methods, for example, multiple Units or components may be combined or integrated into another system, or some features may be omitted, or not implemented. In another point, the mutual coupling or direct coupling or communication connection shown or discussed may be through some interfaces, and the indirect coupling or communication connection of devices or units may be in electrical, mechanical or other forms.
所述作为分离部件说明的单元可以是或者也可以不是物理上分开的,作为单元显示的部件可以是或者也可以不是物理单元,即可以位于一个地方,或者也可以分布到多个网络单元上。可以根据实际的需要选择其中的部分或者全部单元来实现本实施例方案的目的。The units described as separate components may or may not be physically separated, and the components displayed as units may or may not be physical units, that is, they may be located in one place, or may be distributed to multiple network units. Part or all of the units can be selected according to actual needs to achieve the purpose of the solution of this embodiment.
另外,在本申请各个实施例中的各功能单元可能集成在一个处理单元中,也可以是各个单元单独物理存在,也可以两个或两个以上单元集成在一个单元中。上述集成的单元既可以采用硬件的形式实现,也可以采用软件功能单元的形式实现。In addition, each functional unit in each embodiment of the present application may be integrated into one processing unit, each unit may exist separately physically, or two or more units may be integrated into one unit. The above-mentioned integrated units can be implemented in the form of hardware or in the form of software functional units.
应当说明的是,上述实施例均可根据需要自由组合。以上所述仅是本发明的优选实施方式,应当指出,对于本技术领域的普通技术人员来说,在不脱离本发明原理的前提下,还可以做出若干改进和润饰,这些改进和润饰也应视为本发明的保护范围。It should be noted that the above embodiments can be freely combined as required. The above is only a preferred embodiment of the present invention, it should be pointed out that, for those of ordinary skill in the art, without departing from the principle of the present invention, some improvements and modifications can also be made, and these improvements and modifications can also be made. It should be regarded as the protection scope of the present invention.

Claims (10)

  1. 一种基于毫米波雷达的无人机测绘方法,其特征在于,包括步骤:An unmanned aerial vehicle surveying and mapping method based on millimeter-wave radar, is characterized in that, comprises steps:
    控制安装于无人机底部的若干个毫米波雷达发射电磁波以扫描目标区域,计算所述无人机与各探测点之间的相对距离,以及所述无人机与各探测点在高度方向上的相对夹角;所述目标区域包括若干个探测点;Control several millimeter-wave radars installed at the bottom of the UAV to emit electromagnetic waves to scan the target area, calculate the relative distance between the UAV and each detection point, and the distance between the UAV and each detection point in the height direction The relative angle; The target area includes several detection points;
    根据所述相对距离和相对夹角,以及搭载在所述无人机上的定位设备的定位数据,计算得到所述探测点的海拔高度值和经纬度值;According to the relative distance and relative angle, and the positioning data of the positioning device carried on the drone, calculate the altitude value and latitude and longitude value of the detection point;
    根据所有探测点的海拔高度值和经纬度值,生成所述目标区域的地形图。A topographic map of the target area is generated according to the altitude values and latitude and longitude values of all detection points.
  2. 根据权利要求1所述的基于毫米波雷达的无人机测绘方法,其特征在于,所述获取所述无人机与各探测点之间的相对距离和相对夹角包括步骤:The UAV surveying and mapping method based on millimeter-wave radar according to claim 1, wherein said obtaining the relative distance and relative angle between said UAV and each detection point comprises the steps of:
    在所述毫米波雷达发射电磁波扫描目标区域后,获取所述毫米波雷达的电磁波收发状态信息;After the millimeter-wave radar emits electromagnetic waves to scan the target area, acquire the electromagnetic wave transmitting and receiving state information of the millimeter-wave radar;
    根据所述电磁波收发状态信息和天线安装间距,计算得到所述无人机与各探测点之间的相对距离和相对夹角。The relative distance and relative angle between the UAV and each detection point are calculated according to the electromagnetic wave receiving and receiving state information and the antenna installation distance.
  3. 根据权利要求2所述的基于毫米波雷达的无人机测绘方法,其特征在于,所述电磁波收发状态信息包括电磁波收发时间差和相位差;所述根据所述电磁波收发状态信息和天线安装间距,计算得到所述无人机与各探测点之间的相对距离和相对夹角包括步骤:The UAV surveying and mapping method based on millimeter-wave radar according to claim 2, wherein the electromagnetic wave receiving and receiving status information includes electromagnetic wave receiving and receiving time difference and phase difference; according to the electromagnetic wave receiving and receiving status information and the antenna installation distance, Calculating the relative distance and relative angle between the UAV and each detection point includes steps:
    根据所述电磁波收发时间差,代入下列公式(1)计算得到所述无人机与各探测点之间的相对距离;According to the time difference of transmitting and receiving of the electromagnetic wave, the relative distance between the unmanned aerial vehicle and each detection point is calculated by substituting the following formula (1);
    Figure PCTCN2021141120-appb-100001
    Figure PCTCN2021141120-appb-100001
    根据天线安装间距、所述电磁波波长和相位差,代入下列公式(2)计算得到所述相对夹角;According to the antenna installation distance, the wavelength of the electromagnetic wave and the phase difference, the relative angle is calculated by substituting the following formula (2);
    Figure PCTCN2021141120-appb-100002
    Figure PCTCN2021141120-appb-100002
    其中,R表示所述相对距离,θ表示所述相对夹角,c表示光速,ΔT表示所述电磁波收发时间差,λ表示电磁波波长,ΔΦ表示相位差,L表示天线安装间距。Wherein, R represents the relative distance, θ represents the relative angle, c represents the speed of light, ΔT represents the time difference between transmitting and receiving the electromagnetic wave, λ represents the wavelength of the electromagnetic wave, ΔΦ represents the phase difference, and L represents the antenna installation distance.
  4. 根据权利要求1所述的基于毫米波雷达的无人机测绘方法,其特征在于,所述根据所述相对距离和相对夹角,以及搭载在所述无人机上的定位设备的定位数据,计算得到所述探测点的海拔高度值和经纬度值包括步骤:The UAV surveying and mapping method based on millimeter-wave radar according to claim 1, wherein the calculation is based on the relative distance and relative angle, and the positioning data of the positioning device mounted on the UAV. Obtaining the altitude value and the latitude and longitude value of the detection point includes the steps of:
    获取所述定位设备测量得到的定位数据;所述定位数据包括所述无人机的经纬度信息和海拔高度信息;Acquiring positioning data measured by the positioning device; the positioning data includes latitude and longitude information and altitude information of the drone;
    根据所述相对距离、相对夹角,代入下列公式(4)计算得到所述无人机与所述探测点之间在左右方向上的行程距离;According to the relative distance and the relative angle, the following formula (4) is substituted into the calculation to obtain the travel distance in the left and right direction between the drone and the detection point;
    S=sinθ*R    (4);S=sinθ*R (4);
    根据所述相对距离、相对夹角,代入下列公式(5)计算得到所述无人机与所述探测点之间在高度方向上的行程高度;According to the relative distance and the relative angle, the following formula (5) is substituted into the calculation to obtain the travel height in the height direction between the UAV and the detection point;
    h=cosθ*R    (5);h=cosθ*R (5);
    根据所述行程距离,经纬度信息,代入下列公式(6)计算得到所述探测点的纬度值;According to the travel distance, the latitude and longitude information is substituted into the following formula (6) to calculate the latitude value of the detection point;
    W n=cosα*S/D    (6); W n =cosα*S/D (6);
    根据所述行程距离,经纬度信息,代入下列公式(7)计算得到所述探测点的经度值;According to described travel distance, longitude and latitude information, substitute following formula (7) to calculate and obtain the longitude value of described detection point;
    J n=sinα*S/(cos(Wn)*D)    (7); Jn = sinα*S/(cos(Wn)*D) (7);
    根据所述行程高度和所述海拔高度信息,代入下列公式(8)计算得到所述探测点的海拔高度值;According to the stroke height and the altitude information, the altitude value of the detection point is calculated by substituting the following formula (8);
    Figure PCTCN2021141120-appb-100003
    Figure PCTCN2021141120-appb-100003
    其中,所述R表示所述相对距离,θ表示所述相对夹角,S表示所述行程 距离,h表示所述行程高度,α表示所述相对距离所在直线与左右方向所在直线之间的夹角,W n表示第n个探测点的纬度值,J n表示第n个探测点的经度值,H n表示第n个探测点的海拔高度值。 Wherein, the R represents the relative distance, θ represents the relative angle, S represents the stroke distance, h represents the stroke height, and α represents the distance between the straight line where the relative distance is located and the straight line where the left and right directions are located. angle, W n represents the latitude value of the nth detection point, J n represents the longitude value of the nth detection point, H n represents the altitude value of the nth detection point.
  5. 根据权利要求1-4任一项所述的基于毫米波雷达的无人机测绘方法,其特征在于,所述根据所有探测点的海拔高度值和经纬度值,生成所述目标区域的地形图包括步骤:According to the millimeter-wave radar-based UAV surveying and mapping method according to any one of claims 1-4, it is characterized in that, according to the altitude values and latitude and longitude values of all detection points, generating the topographic map of the target area includes step:
    比对当前探测点的若干个海拔高度值和经纬度值,若不匹配则删除所述当前探测点的海拔高度值和经纬度值;Comparing several altitude values and latitude and longitude values of the current detection point, if they do not match, deleting the altitude value and latitude and longitude value of the current detection point;
    切换比对下一探测点,直至获取到所述目标区域中所有探测点的若干个海拔高度值和经纬度值匹配为止,根据各探测点分别对应的若干个海拔高度值和经纬度值,绘制生成所述地形图。Switch and compare the next detection point until several altitude values and longitude and latitude values of all detection points in the target area are obtained to match. topographical map.
  6. 一种基于毫米波雷达的无人机测绘系统,其特征在于,包括:An unmanned aerial vehicle surveying and mapping system based on millimeter-wave radar, is characterized in that, comprises:
    控制模块,用于控制安装于无人机底部的若干个毫米波雷达发射电磁波以扫描目标区域;The control module is used to control several millimeter-wave radars installed at the bottom of the drone to emit electromagnetic waves to scan the target area;
    获取模块,用于计算所述无人机与各探测点之间的相对距离,以及所述无人机与各探测点在高度方向上的相对夹角;所述目标区域包括若干个探测点;An acquisition module, configured to calculate the relative distance between the UAV and each detection point, and the relative angle between the UAV and each detection point in the height direction; the target area includes several detection points;
    处理模块,用于根据所述相对距离和相对夹角,以及搭载在所述无人机上的定位设备的定位数据,计算得到所述探测点的海拔高度值和经纬度值;The processing module is used to calculate the altitude value and latitude and longitude value of the detection point according to the relative distance and relative angle, as well as the positioning data of the positioning device carried on the drone;
    生成模块,用于根据所有探测点的海拔高度值和经纬度值,生成所述目标区域的地形图。A generating module, configured to generate a topographic map of the target area according to the altitude values and latitude and longitude values of all detection points.
  7. 根据权利要求6所述的基于毫米波雷达的无人机测绘系统,其特征在于,所述获取模块包括:The UAV surveying and mapping system based on millimeter-wave radar according to claim 6, wherein the acquisition module includes:
    第一获取子模块,用于在所述毫米波雷达发射电磁波扫描目标区域后,获取所述毫米波雷达的电磁波收发状态信息;The first acquisition sub-module is used to acquire the electromagnetic wave transmitting and receiving status information of the millimeter wave radar after the millimeter wave radar emits electromagnetic waves to scan the target area;
    计算子模块,用于根据所述电磁波收发状态信息和天线安装间距,计算得到所述无人机与各探测点之间的相对距离和相对夹角。The calculation sub-module is used to calculate the relative distance and relative angle between the UAV and each detection point according to the state information of the electromagnetic wave transmission and reception and the installation distance of the antenna.
  8. 根据权利要求7所述的基于毫米波雷达的无人机测绘系统,其特征在于,所述电磁波收发状态信息包括电磁波收发时间差和相位差;所述计算子模块包括:The UAV surveying and mapping system based on millimeter-wave radar according to claim 7, wherein the electromagnetic wave sending and receiving status information includes electromagnetic wave sending and receiving time difference and phase difference; the calculation submodule includes:
    相对距离计算单元,用于根据所述电磁波收发时间差,代入下列公式(1)计算得到所述无人机与各探测点之间的相对距离;The relative distance calculation unit is used to calculate the relative distance between the UAV and each detection point by substituting the following formula (1) according to the time difference between sending and receiving of the electromagnetic wave;
    Figure PCTCN2021141120-appb-100004
    Figure PCTCN2021141120-appb-100004
    相对夹角计算单元,用于根据天线安装间距、所述电磁波波长和相位差,代入下列公式(2)计算得到所述相对夹角;The relative angle calculation unit is used to calculate the relative angle by substituting the following formula (2) according to the antenna installation distance, the wavelength of the electromagnetic wave and the phase difference;
    Figure PCTCN2021141120-appb-100005
    Figure PCTCN2021141120-appb-100005
    其中,R表示所述相对距离,θ表示所述相对夹角,c表示光速,ΔT表示所述电磁波收发时间差,λ表示电磁波波长,ΔΦ表示相位差,L表示天线安装间距。Wherein, R represents the relative distance, θ represents the relative angle, c represents the speed of light, ΔT represents the time difference between transmitting and receiving the electromagnetic wave, λ represents the wavelength of the electromagnetic wave, ΔΦ represents the phase difference, and L represents the antenna installation distance.
  9. 根据权利要求6所述的基于毫米波雷达的无人机测绘系统,其特征在于,所述处理模块包括:The UAV surveying and mapping system based on millimeter-wave radar according to claim 6, wherein the processing module includes:
    第二获取子模块,用于获取所述定位设备测量得到的定位数据;所述定位数据包括所述无人机的经纬度信息和海拔高度信息;The second acquisition sub-module is used to acquire the positioning data measured by the positioning device; the positioning data includes the longitude and latitude information and the altitude information of the drone;
    距离计算子模块,用于根据所述相对距离、相对夹角,代入下列公式(4)计算得到所述无人机与所述探测点之间在左右方向上的行程距离;The distance calculation sub-module is used to calculate the travel distance between the drone and the detection point in the left and right directions by substituting the following formula (4) according to the relative distance and the relative angle;
    S=sinθ*R    (4);S=sinθ*R (4);
    高度计算子模块,用于根据所述相对距离、相对夹角,代入下列公式(5)计算得到所述无人机与所述探测点之间在高度方向上的行程高度;The height calculation sub-module is used to calculate the travel height in the height direction between the drone and the detection point by substituting the following formula (5) according to the relative distance and the relative angle;
    h=cosθ*R    (5);h=cosθ*R (5);
    纬度计算子模块,用于根据所述行程距离,经纬度信息,代入下列公式(6)计算得到所述探测点的纬度值;The latitude calculation submodule is used to calculate the latitude value of the detection point by substituting the following formula (6) into the longitude and latitude information according to the travel distance;
    W n=cosα*S/D    (6); W n =cosα*S/D (6);
    经度计算子模块,用于根据所述行程距离,经纬度信息,代入下列公式(7)计算得到所述探测点的经度值;The longitude calculation submodule is used to calculate the longitude value of the detection point according to the travel distance and the latitude and longitude information by substituting the following formula (7);
    J n=sinα*S/(cos(Wn)*D)    (7); Jn = sinα*S/(cos(Wn)*D) (7);
    海拔计算子模块,用于根据所述行程高度和所述海拔高度信息,代入下列公式(8)计算得到所述探测点的海拔高度值;The altitude calculation submodule is used to calculate the altitude value of the detection point by substituting the following formula (8) according to the travel height and the altitude information;
    Figure PCTCN2021141120-appb-100006
    Figure PCTCN2021141120-appb-100006
    其中,所述R表示所述相对距离,θ表示所述相对夹角,S表示所述行程距离,h表示所述行程高度,α表示所述相对距离所在直线与左右方向所在直线之间的夹角,W n表示第n个探测点的纬度值,J n表示第n个探测点的经度值,H n表示第n个探测点的海拔高度值。 Wherein, the R represents the relative distance, θ represents the relative angle, S represents the stroke distance, h represents the stroke height, and α represents the distance between the straight line where the relative distance is located and the straight line where the left and right directions are located. angle, W n represents the latitude value of the nth detection point, J n represents the longitude value of the nth detection point, H n represents the altitude value of the nth detection point.
  10. 根据权利要求6-9任一项所述的基于毫米波雷达的无人机测绘系统,其特征在于,所述生成模块包括:The UAV surveying and mapping system based on millimeter-wave radar according to any one of claims 6-9, wherein the generation module includes:
    比对子模块,用于比对当前探测点的若干个海拔高度值和经纬度值,若不匹配则删除所述当前探测点的海拔高度值和经纬度值;The comparison sub-module is used to compare several altitude values and latitude and longitude values of the current detection point, and if they do not match, delete the altitude value and the latitude and longitude value of the current detection point;
    生成子模块,用于切换比对下一探测点,直至获取到所述目标区域中所有探测点的若干个海拔高度值和经纬度值匹配为止,根据各探测点分别对应的若干个海拔高度值和经纬度值,绘制生成所述地形图。Generate a sub-module for switching and comparing the next detection point until the acquisition of several altitude values and latitude and longitude values of all detection points in the target area match, according to the several altitude values and latitude values corresponding to each detection point Longitude and latitude values, draw to generate the topographic map.
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