CN111457895A - Target size calculation and display method for photoelectric load of unmanned aerial vehicle - Google Patents

Target size calculation and display method for photoelectric load of unmanned aerial vehicle Download PDF

Info

Publication number
CN111457895A
CN111457895A CN202010245766.1A CN202010245766A CN111457895A CN 111457895 A CN111457895 A CN 111457895A CN 202010245766 A CN202010245766 A CN 202010245766A CN 111457895 A CN111457895 A CN 111457895A
Authority
CN
China
Prior art keywords
unmanned aerial
aerial vehicle
calculating
moment
target
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN202010245766.1A
Other languages
Chinese (zh)
Other versions
CN111457895B (en
Inventor
黄欣宇
陈文�
魏瀚
吴也
王浩
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rainbow UAV Technology Co Ltd
Original Assignee
Rainbow UAV Technology Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Rainbow UAV Technology Co Ltd filed Critical Rainbow UAV Technology Co Ltd
Priority to CN202010245766.1A priority Critical patent/CN111457895B/en
Publication of CN111457895A publication Critical patent/CN111457895A/en
Application granted granted Critical
Publication of CN111457895B publication Critical patent/CN111457895B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C11/00Photogrammetry or videogrammetry, e.g. stereogrammetry; Photographic surveying
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C11/00Photogrammetry or videogrammetry, e.g. stereogrammetry; Photographic surveying
    • G01C11/04Interpretation of pictures
    • G01C11/30Interpretation of pictures by triangulation
    • G01C11/34Aerial triangulation
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C3/00Measuring distances in line of sight; Optical rangefinders

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Multimedia (AREA)
  • Electromagnetism (AREA)
  • Length Measuring Devices By Optical Means (AREA)

Abstract

The invention discloses a target size calculation and display method for photoelectric loads of an unmanned aerial vehicle, which comprises the following steps: receiving real-time telemetering data transmitted by the unmanned aerial vehicle and the photoelectric load; calculating to obtain the horizontal distance between the unmanned aerial vehicle and the detection target at the moment k according to the real-time telemetering data; calculating to obtain the actual height covered by the pitching direction and the actual width covered by the azimuth direction of the photoelectric load image at the moment k; calculating to obtain the actual width and height of each pixel in the photoelectric load image at the moment k; calculating to obtain the actual width and height of the detection target; and superposing and displaying the actual width and height of the detection target on the photoelectric load image. The invention analyzes and processes the real-time telemetering data transmitted by the unmanned aerial vehicle and the photoelectric load to obtain the actual width and height of the detected target, provides the size information of the detected target for ground operators, and assists the operators in classifying, judging and predicting the behavior of the detected target.

Description

Target size calculation and display method for photoelectric load of unmanned aerial vehicle
Technical Field
The invention belongs to the technical field of unmanned aerial vehicle target measurement, and particularly relates to a target size calculation and display method for photoelectric loads of an unmanned aerial vehicle.
Background
In recent years, with the rapid development of unmanned aerial vehicle system technology, the application field of unmanned aerial vehicles is becoming more and more extensive, and from the application of unmanned aerial vehicles, photoelectric loads are the most reliable and effective application loads, and play a vital role in many fields such as target reconnaissance, regional inspection, target striking guidance, striking efficiency evaluation, cable and pipeline inspection, forest fire prevention and the like.
In the task execution process of the unmanned aerial vehicle, the photoelectric load is crucial to the mastering of target information, and the success or failure of a flight task can be influenced. The target size information is inherent state information of the target, and if the size information of the target can be mastered in real time, the method can effectively assist an operator in classifying, identifying and predicting the behavior of the target, and improve the success rate of the flight mission aiming at the target category. Therefore, a target size calculation method which is high in real-time performance and effective is found, and size information of the target is presented to an operator in real time, so that the urgent need of the photoelectric load application of the unmanned aerial vehicle is met.
Disclosure of Invention
The technical problem of the invention is solved: the method for calculating and displaying the target size of the photoelectric load of the unmanned aerial vehicle comprises the steps of analyzing and processing real-time telemetering data transmitted by the unmanned aerial vehicle and the photoelectric load to obtain the actual width and height size of a detected target, providing size information of the detected target for ground operators, and assisting the operators in classifying, judging and predicting behaviors of the detected target.
In order to solve the technical problem, the invention discloses a target size calculation and display method of a photoelectric load of an unmanned aerial vehicle, which comprises the following steps:
receiving real-time telemetering data transmitted by the unmanned aerial vehicle and the photoelectric load;
calculating to obtain a horizontal distance S (k) between the unmanned aerial vehicle and a detection target at the moment k according to the real-time telemetering data;
according to the horizontal distance S (k), calculating to obtain the actual height h (k) covered by the pitching direction of the photoelectric load image at the time k and the actual width w (k) covered by the azimuth direction of the photoelectric load image at the time k;
according to the actual height h (k) and the actual width w (k), calculating to obtain the actual width and height [ w (k) ] of each pixel in the photoelectric load image at the moment kp,hp];
Obtaining pixel value [ s ] of detected targetpx,spy]According to the actual width and height dimension [ wp,hp]And detecting a pixel value [ s ] of the targetpx,spy]Calculating to obtain the actual width and height dimensions [ s ] of the detected targetx,sy];
And superposing and displaying the actual width and height of the detection target on the photoelectric load image.
In the above method for calculating and displaying the size of the target of the photoelectric load of the unmanned aerial vehicle, the horizontal distance s (k) between the unmanned aerial vehicle and the detection target at the time k is calculated according to the real-time telemetering data, and the method includes:
judging whether the telemetering data carries laser ranging information or not;
if the telemetering data carries laser ranging information, calculating to obtain a horizontal distance S (k) between the unmanned aerial vehicle and the detection target at the moment k according to the slant distance between the unmanned aerial vehicle and the detection target;
and if the telemetering data does not carry laser ranging information, calculating to obtain a horizontal distance S (k) between the unmanned aerial vehicle and the detection target at the moment k according to the ground height of the unmanned aerial vehicle.
In the above method for calculating and displaying the target size of the photoelectric load of the unmanned aerial vehicle, according to the slant distance between the unmanned aerial vehicle and the detection target, the horizontal distance s (k) between the unmanned aerial vehicle and the detection target at the time k is obtained by calculation, and the method includes:
the telemetering data is analyzed to obtain the laser ranging information at the moment k, the pitch angle β (k) of the unmanned aerial vehicle at the moment k and the pitch angle of the photoelectric load at the moment k
Figure BDA0002433937310000023
Determining the slant distance L (k) between the unmanned aerial vehicle and the detection target at the moment k according to the laser ranging information at the moment k;
calculating to obtain the distance S (k) between the unmanned aerial vehicle and the detection target at the moment k through a trigonometric relation:
Figure BDA0002433937310000021
in the above method for calculating and displaying the target size of the photoelectric load of the unmanned aerial vehicle, according to the ground height of the unmanned aerial vehicle, calculating the horizontal distance s (k) between the unmanned aerial vehicle and the detection target at the time k, including:
the telemetering data is analyzed to obtain the altitude H of the unmanned aerial vehicle at the moment ka(k) K moment unmanned aerial vehicle takeoff field altitude Hg(k) Pitching angle β (k) of unmanned aerial vehicle at moment k and pitching angle of photoelectric load at moment k
Figure BDA0002433937310000022
Calculating to obtain the distance S (k) between the unmanned aerial vehicle and the detection target at the moment k through a trigonometric relation:
Figure BDA0002433937310000031
in the method for calculating and displaying the target size of the photoelectric load of the unmanned aerial vehicle, the actual height h (k) covered by the photoelectric load image in the pitching direction at the moment k is as follows:
Figure BDA0002433937310000032
where τ (k) represents the angle of view of the photoelectric load in the pitch direction at time k.
In the method for calculating and displaying the target size of the photoelectric load of the unmanned aerial vehicle, the actual width w (k) covered by the photoelectric load image at the moment k in the azimuth direction is as follows:
Figure BDA0002433937310000033
where σ (k) represents the azimuthal angle of view of the photoelectric load at time k.
In the method for calculating and displaying the target size of the photoelectric load of the unmanned aerial vehicle, the actual width and height [ w ] of each pixel in the photoelectric load image at the moment kp,hp]Comprises the following steps:
Figure BDA0002433937310000034
wherein [ wr,hr]Representing a fixed resolution of the photovoltaic charge image.
In the method for calculating and displaying the size of the target of the photoelectric load of the unmanned aerial vehicle, the actual width and height sizes s of the target are detectedx,sy]Comprises the following steps:
[sx,sy]=[spx,spy][wp,hp]T
in the above-mentioned target size of unmanned aerial vehicle photoelectric load calculates and shows the method, judge whether carry laser range finding information in the telemetering measurement data, include:
obtaining a distance measurement value irradiated by laser from the telemetering data;
if the distance measurement value is larger than 300, determining that laser distance measurement information is carried in the telemetering data and the telemetering data is in a laser distance measurement information state;
and if the ranging value is 0 or negative, determining that the ranging value is invalid, and determining that the telemetry data does not carry laser ranging information and is in a laser ranging information-free state.
In the method for calculating and displaying the target size of the photoelectric load of the unmanned aerial vehicle,
[wr,hr]=[1920,1080]。
the invention has the following advantages:
(1) the invention discloses a target size calculation and display method of an unmanned aerial vehicle photoelectric load, which is characterized in that real-time telemetering data transmitted by an unmanned aerial vehicle and the photoelectric load are analyzed and processed to obtain the actual width and height sizes of a detected target, the size information of the detected target is provided for ground operators, the operators are assisted to classify, judge and predict the detected target, and the success rate of flight tasks aiming at the target category is improved.
(2) The invention discloses a target size calculation and display method for a photoelectric load of an unmanned aerial vehicle, which can provide real-time target size information for a photoelectric load operator through software algorithm calculation and display without adding any hardware equipment, and has the advantages of simple operation and low cost.
Drawings
Fig. 1 is a flowchart illustrating steps of a method for calculating and displaying a target size of a photoelectric load of an unmanned aerial vehicle according to an embodiment of the present invention;
FIG. 2 is a schematic diagram of the actual height covered by the photoelectric load image at the moment k in the pitching direction in the embodiment of the invention;
fig. 3 is a schematic diagram of the actual width covered by the photoelectric load image azimuth at time k in the embodiment of the present invention.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the embodiments of the present invention will be described in detail with reference to the accompanying drawings.
As shown in fig. 1, in the embodiment of the present invention, a method for calculating and displaying a target size of a photoelectric load of an unmanned aerial vehicle includes:
and step 101, receiving real-time telemetering data transmitted by the unmanned aerial vehicle and the photoelectric load.
In this embodiment, real-time telemetry data of the drone and the photovoltaic load is received through the drone link system.
And step 102, calculating to obtain a horizontal distance S (k) between the unmanned aerial vehicle and the detection target at the moment k according to the real-time telemetering data.
In the embodiment, for the photoelectric load with the laser source, the laser ranging information state and the non-laser ranging information state are divided; for photoelectric loads without laser sources, there is only a laser ranging information-free state. The horizontal distance S (k) between the unmanned aerial vehicle and the detection target at the moment k can be calculated by selecting different methods through judging whether the telemetering data carries laser ranging information or not.
Preferably, for the case that the telemetry data carries laser ranging information, the slant distance between the unmanned aerial vehicle and the detection target is directly given through the laser ranging information, namely the laser return value, the horizontal distance S (k) between the unmanned aerial vehicle and the detection target at the moment k can be obtained through resolving according to the slant distance between the unmanned aerial vehicle and the detection target, and the telemetry data is resolved to obtain the laser ranging information at the moment k, the pitch angle β (k) of the unmanned aerial vehicle at the moment k and the pitch angle of the photoelectric load at the moment k
Figure BDA0002433937310000054
Determining the slant distance L (k) between the unmanned aerial vehicle and the detection target at the moment k according to the laser ranging information at the moment k, and calculating to obtain the distance S (k) between the unmanned aerial vehicle and the detection target at the moment k through a trigonometric relation:
Figure BDA0002433937310000051
preferably, for the case that the telemetry data does not carry laser ranging information, the horizontal distance s (k) between the unmanned aerial vehicle and the detection target at the time k is obtained by calculation according to the ground altitude of the unmanned aerial vehicle: the telemetering data is analyzed to obtain the altitude H of the unmanned aerial vehicle at the moment ka(k) K moment unmanned aerial vehicle takeoff field altitude Hg(k) Pitching angle β (k) of unmanned aerial vehicle at moment k and pitching angle of photoelectric load at moment k
Figure BDA0002433937310000052
Calculating to obtain the distance S (k) between the unmanned aerial vehicle and the detection target at the moment k through a trigonometric relation:
Figure BDA0002433937310000053
it should be noted that, when the horizontal distance is performed according to the ground height of the unmanned aerial vehicle, it needs to first determine whether the detection target is located at the center of the field of view of the photoelectric load, and if the detection target is not located at the center of the field of view of the photoelectric load, the center of the field of view of the photoelectric load needs to be adjusted to the detection target.
Preferably, whether the telemetry data carries the laser ranging information may be determined as follows:
extracting a distance measurement value irradiated by laser from the telemetering data; if the distance measurement value is larger than 300, determining that laser distance measurement information is carried in the telemetering data and the telemetering data is in a state with the laser distance measurement information, and directly using the distance measurement value as an inclined distance between the unmanned aerial vehicle and a detection target; and if the ranging value is 0 or negative, determining that the ranging value is invalid, and the telemetering data does not carry laser ranging information and is in a laser ranging information-free state.
And 103, calculating the actual height h (k) covered by the pitching direction of the photoelectric load image at the time k and the actual width w (k) covered by the azimuth direction of the photoelectric load image at the time k according to the horizontal distance S (k).
In this embodiment, the photovoltaic loads have different field angles at different focal lengths:
as shown in fig. 2, when the elevation angle of the photoelectric load at time k is τ (k), the elevation angle corresponding to the lowermost edge of the photoelectric load image at time k is τ (k)
Figure BDA0002433937310000061
The pitch angle corresponding to the uppermost edge of the photoelectric load image at the moment k is
Figure BDA0002433937310000062
The actual height h (k) covered by the pitching direction of the photoelectric load image at the moment k is:
Figure BDA0002433937310000063
as shown in fig. 3, when the azimuthal viewing angle of the photoelectric load at time k is σ (k), the actual width w (k) covered by the azimuthal viewing angle of the photoelectric load image at time k is:
Figure BDA0002433937310000064
step (ii) of104, calculating to obtain the actual width and height [ w (k) ] of each pixel in the photoelectric load image at the moment k according to the actual height h (k) and the actual width w (k)p,hp]。
In this embodiment, the photoelectric payload image typically has a fixed resolution wr,hr]Then the actual width and height dimension [ w ] of each pixel in the photoelectric load image at time kp,hp]Comprises the following steps:
Figure BDA0002433937310000065
step 105, obtaining the pixel value [ s ] of the detection targetpx,spy]According to the actual width and height dimension [ wp,hp]Detecting pixel values [ s ] of a target for summationpx,spy]Calculating to obtain the actual width and height dimensions [ s ] of the detected targetx,sy]。
In this embodiment, for a detected target with obvious image characteristics (especially for a detected target with a load capable of being tracked for a long time), the target recognition algorithm can automatically calculate the pixel value [ s ] of the detected targetpx,spy]. For the detection target with less obvious target image characteristics or special target shape and size, the pixel value [ s ] of the detection target can be obtained in a manual selection modepx,spy]。
According to the actual width and height dimension [ w ]p,hp]Detecting pixel values [ s ] of a target for summationpx,spy]Then, the actual width and height [ s ] of the detected target can be calculatedx,sy]:
[sx,sy]=[spx,spy][wp,hp]T
For example, when the resolution of the photovoltaic charge image is fixed [ w ]r,hr]=[1920,1080]In time, there are:
Figure BDA0002433937310000071
namely:
Figure BDA0002433937310000072
and 106, superposing and displaying the actual width and height of the detection target on the photoelectric load image.
Although the present invention has been described with reference to the preferred embodiments, it is not intended to limit the present invention, and those skilled in the art can make variations and modifications of the present invention without departing from the spirit and scope of the present invention by using the methods and technical contents disclosed above.
Those skilled in the art will appreciate that the invention may be practiced without these specific details.

Claims (10)

1. A target size calculation and display method for photoelectric loads of an unmanned aerial vehicle is characterized by comprising the following steps:
receiving real-time telemetering data transmitted by the unmanned aerial vehicle and the photoelectric load;
calculating to obtain a horizontal distance S (k) between the unmanned aerial vehicle and a detection target at the moment k according to the real-time telemetering data;
according to the horizontal distance S (k), calculating to obtain the actual height h (k) covered by the pitching direction of the photoelectric load image at the time k and the actual width w (k) covered by the azimuth direction of the photoelectric load image at the time k;
according to the actual height h (k) and the actual width w (k), calculating to obtain the actual width and height [ w (k) ] of each pixel in the photoelectric load image at the moment kp,hp];
Obtaining pixel value [ s ] of detected targetpx,spy]According to the actual width and height dimension [ wp,hp]And detecting a pixel value [ s ] of the targetpx,spy]Calculating to obtain the actual width and height dimensions [ s ] of the detected targetx,sy];
And superposing and displaying the actual width and height of the detection target on the photoelectric load image.
2. The method for calculating and displaying the target size of the photoelectric load of the unmanned aerial vehicle according to claim 1, wherein the step of calculating the horizontal distance s (k) between the unmanned aerial vehicle and the detected target at the time k according to the real-time telemetry data comprises the following steps:
judging whether the telemetering data carries laser ranging information or not;
if the telemetering data carries laser ranging information, calculating to obtain a horizontal distance S (k) between the unmanned aerial vehicle and the detection target at the moment k according to the slant distance between the unmanned aerial vehicle and the detection target;
and if the telemetering data does not carry laser ranging information, calculating to obtain a horizontal distance S (k) between the unmanned aerial vehicle and the detection target at the moment k according to the ground height of the unmanned aerial vehicle.
3. The method for calculating and displaying the target size of the photoelectric load of the unmanned aerial vehicle according to claim 2, wherein the step of calculating the horizontal distance s (k) between the unmanned aerial vehicle and the detection target at the time k according to the slant distance between the unmanned aerial vehicle and the detection target comprises:
the telemetering data is analyzed to obtain the laser ranging information at the moment k, the pitch angle β (k) of the unmanned aerial vehicle at the moment k and the pitch angle of the photoelectric load at the moment k
Figure FDA0002433937300000011
Determining the slant distance L (k) between the unmanned aerial vehicle and the detection target at the moment k according to the laser ranging information at the moment k;
calculating to obtain the distance S (k) between the unmanned aerial vehicle and the detection target at the moment k through a trigonometric relation:
Figure FDA0002433937300000021
4. the method for calculating and displaying the target size of the photoelectric load of the unmanned aerial vehicle according to claim 2, wherein the step of calculating the horizontal distance s (k) between the unmanned aerial vehicle and the detected target at the time k according to the ground height of the unmanned aerial vehicle comprises:
the telemetering data is analyzed to obtain the altitude H of the unmanned aerial vehicle at the moment ka(k) K moment unmanned aerial vehicle takeoff field altitude Hg(k) Pitching angle β (k) of unmanned aerial vehicle at moment k and pitching angle of photoelectric load at moment k
Figure FDA0002433937300000022
Calculating to obtain the distance S (k) between the unmanned aerial vehicle and the detection target at the moment k through a trigonometric relation:
Figure FDA0002433937300000023
5. the method for calculating and displaying the target size of the photoelectric load of the unmanned aerial vehicle according to claim 3 or 4, wherein the actual height h (k) covered by the pitching direction of the photoelectric load image at the time k is:
Figure FDA0002433937300000024
where τ (k) represents the angle of view of the photoelectric load in the pitch direction at time k.
6. The method for calculating and displaying the target size of the photoelectric load of the unmanned aerial vehicle according to claim 5, wherein the actual width w (k) covered by the photoelectric load image azimuth at the time k is:
Figure FDA0002433937300000025
where σ (k) represents the azimuthal angle of view of the photoelectric load at time k.
7. The method for calculating and displaying the target size of the photoelectric load of the unmanned aerial vehicle according to claim 6, wherein the actual width and height [ w ] of each pixel in the photoelectric load image at the time kp,hp]Comprises the following steps:
Figure FDA0002433937300000026
wherein [ wr,hr]Representing a fixed resolution of the photovoltaic charge image.
8. The method of claim 7, wherein the actual width and height of the target [ s ] is detectedx,sy]Comprises the following steps:
[sx,sy]=[spx,spy][wp,hp]T
9. the method for calculating and displaying the target size of the photoelectric load of the unmanned aerial vehicle according to claim 2, wherein judging whether the telemetry data carries laser ranging information comprises:
obtaining a distance measurement value irradiated by laser from the telemetering data;
if the distance measurement value is larger than 300, determining that laser distance measurement information is carried in the telemetering data and the telemetering data is in a laser distance measurement information state;
and if the ranging value is 0 or negative, determining that the ranging value is invalid, and determining that the telemetry data does not carry laser ranging information and is in a laser ranging information-free state.
10. The method for calculating and displaying the target size of the photoelectric load of the unmanned aerial vehicle according to claim 7,
[wr,hr]=[1920,1080]。
CN202010245766.1A 2020-03-31 2020-03-31 Target size calculation and display method for photoelectric load of unmanned aerial vehicle Active CN111457895B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202010245766.1A CN111457895B (en) 2020-03-31 2020-03-31 Target size calculation and display method for photoelectric load of unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010245766.1A CN111457895B (en) 2020-03-31 2020-03-31 Target size calculation and display method for photoelectric load of unmanned aerial vehicle

Publications (2)

Publication Number Publication Date
CN111457895A true CN111457895A (en) 2020-07-28
CN111457895B CN111457895B (en) 2022-04-22

Family

ID=71683485

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202010245766.1A Active CN111457895B (en) 2020-03-31 2020-03-31 Target size calculation and display method for photoelectric load of unmanned aerial vehicle

Country Status (1)

Country Link
CN (1) CN111457895B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114353667A (en) * 2021-12-15 2022-04-15 中国船舶重工集团公司第七0九研究所 Ground target measurement method based on AR and unmanned aerial vehicle monocular vision and application thereof

Citations (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000003543A1 (en) * 1998-07-10 2000-01-20 Recon/Optical, Inc. Autonomous electro-optical framing camera system, unmanned airborne vehicle
CN102156481A (en) * 2011-01-24 2011-08-17 广州嘉崎智能科技有限公司 Intelligent tracking control method and system for unmanned aircraft
US8020769B2 (en) * 2007-05-21 2011-09-20 Raytheon Company Handheld automatic target acquisition system
CN102914294A (en) * 2012-09-10 2013-02-06 中国南方电网有限责任公司超高压输电公司天生桥局 System and method for measuring unmanned aerial vehicle electrical line patrol on basis of images
CN103353297A (en) * 2013-06-03 2013-10-16 长春理工大学 Airborne photoelectric measurement apparatus of dimensions and spacing of electric transmission line and target, and method thereof
EP2818958A2 (en) * 2013-06-14 2014-12-31 Kabushiki Kaisha Topcon Flying vehicle guiding system and flying vehicle guiding method
CN104330076A (en) * 2014-08-13 2015-02-04 王涛 Novel automatic aero-triangulation software
US20150204974A1 (en) * 2014-01-20 2015-07-23 Venkateshwara PILLAY System for mapping and tracking ground targets
CN105187723A (en) * 2015-09-17 2015-12-23 深圳市十方联智科技有限公司 Shooting processing method for unmanned aerial vehicle
CN107121666A (en) * 2017-04-17 2017-09-01 南京航空航天大学 A kind of near space moving target localization method based on unmanned vehicle
WO2017147792A1 (en) * 2016-03-01 2017-09-08 SZ DJI Technology Co., Ltd. Methods and systems for target tracking
CN107390545A (en) * 2017-07-31 2017-11-24 彩虹无人机科技有限公司 A kind of simulation training system of unmanned plane and its load
CN206989931U (en) * 2017-06-01 2018-02-09 南京卓实电气有限责任公司 A kind of transmission line of electricity Range Measurement System
WO2018027339A1 (en) * 2016-08-06 2018-02-15 SZ DJI Technology Co., Ltd. Copyright notice
CN107703963A (en) * 2014-07-30 2018-02-16 深圳市大疆创新科技有限公司 Target tracking system and method
CN108248891A (en) * 2017-12-27 2018-07-06 彩虹无人机科技有限公司 A kind of calibration system and scaling method for unmanned plane semiclosed loop rudder face
CN108286959A (en) * 2017-12-14 2018-07-17 彩虹无人机科技有限公司 A kind of O-E Payload for UAV is detectd to be calculated and display methods according to region
WO2018144929A1 (en) * 2017-02-02 2018-08-09 Infatics, Inc. (DBA DroneDeploy) System and methods for improved aerial mapping with aerial vehicles
CN108415452A (en) * 2017-12-25 2018-08-17 彩虹无人机科技有限公司 A kind of hollow long endurance unmanned aircraft task grouping
CN108426567A (en) * 2018-03-22 2018-08-21 西安闻泰电子科技有限公司 Subject is apart from display methods, apparatus and system
CN108845335A (en) * 2018-05-07 2018-11-20 中国人民解放军国防科技大学 Unmanned aerial vehicle ground target positioning method based on image and navigation information
CN109269352A (en) * 2018-09-20 2019-01-25 北京机械设备研究所 A kind of unmanned plane tracking goal approach and system based on ground location
CN109597427A (en) * 2018-11-28 2019-04-09 彩虹无人机科技有限公司 It is a kind of that method and system for planning is attacked with chance based on the bomb of unmanned plane
WO2019083791A1 (en) * 2017-10-24 2019-05-02 Loveland Innovations, LLC Crisscross boustrophedonic flight patterns for uav scanning and imaging
CN209085612U (en) * 2018-12-21 2019-07-09 北京大学 A kind of field 3 D image acquring system
CN209160024U (en) * 2018-10-29 2019-07-26 深圳博士智能科技有限公司 A kind of intelligent opto-electrical load of industry unmanned plane
CN110068306A (en) * 2019-04-19 2019-07-30 弈酷高科技(深圳)有限公司 A kind of unmanned plane inspection photometry system and method
CN110458888A (en) * 2019-07-23 2019-11-15 深圳前海达闼云端智能科技有限公司 Distance measuring method, device, storage medium and electronic equipment based on image
CN110470304A (en) * 2019-08-19 2019-11-19 西安因诺航空科技有限公司 A kind of high-precision target positioning-speed-measuring method based on UAV electro-optical's platform
WO2019222798A1 (en) * 2018-05-22 2019-11-28 Acid Ip Pty Ltd Drone flight programming method and system
CN110807473A (en) * 2019-10-12 2020-02-18 浙江大华技术股份有限公司 Target detection method, device and computer storage medium
WO2020037492A1 (en) * 2018-08-21 2020-02-27 SZ DJI Technology Co., Ltd. Distance measuring method and device

Patent Citations (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000003543A1 (en) * 1998-07-10 2000-01-20 Recon/Optical, Inc. Autonomous electro-optical framing camera system, unmanned airborne vehicle
US8020769B2 (en) * 2007-05-21 2011-09-20 Raytheon Company Handheld automatic target acquisition system
CN102156481A (en) * 2011-01-24 2011-08-17 广州嘉崎智能科技有限公司 Intelligent tracking control method and system for unmanned aircraft
CN102914294A (en) * 2012-09-10 2013-02-06 中国南方电网有限责任公司超高压输电公司天生桥局 System and method for measuring unmanned aerial vehicle electrical line patrol on basis of images
CN103353297A (en) * 2013-06-03 2013-10-16 长春理工大学 Airborne photoelectric measurement apparatus of dimensions and spacing of electric transmission line and target, and method thereof
EP2818958A2 (en) * 2013-06-14 2014-12-31 Kabushiki Kaisha Topcon Flying vehicle guiding system and flying vehicle guiding method
US20150204974A1 (en) * 2014-01-20 2015-07-23 Venkateshwara PILLAY System for mapping and tracking ground targets
CN107703963A (en) * 2014-07-30 2018-02-16 深圳市大疆创新科技有限公司 Target tracking system and method
CN104330076A (en) * 2014-08-13 2015-02-04 王涛 Novel automatic aero-triangulation software
CN105187723A (en) * 2015-09-17 2015-12-23 深圳市十方联智科技有限公司 Shooting processing method for unmanned aerial vehicle
WO2017147792A1 (en) * 2016-03-01 2017-09-08 SZ DJI Technology Co., Ltd. Methods and systems for target tracking
WO2018027339A1 (en) * 2016-08-06 2018-02-15 SZ DJI Technology Co., Ltd. Copyright notice
WO2018144929A1 (en) * 2017-02-02 2018-08-09 Infatics, Inc. (DBA DroneDeploy) System and methods for improved aerial mapping with aerial vehicles
CN107121666A (en) * 2017-04-17 2017-09-01 南京航空航天大学 A kind of near space moving target localization method based on unmanned vehicle
CN206989931U (en) * 2017-06-01 2018-02-09 南京卓实电气有限责任公司 A kind of transmission line of electricity Range Measurement System
CN107390545A (en) * 2017-07-31 2017-11-24 彩虹无人机科技有限公司 A kind of simulation training system of unmanned plane and its load
WO2019083791A1 (en) * 2017-10-24 2019-05-02 Loveland Innovations, LLC Crisscross boustrophedonic flight patterns for uav scanning and imaging
CN108286959A (en) * 2017-12-14 2018-07-17 彩虹无人机科技有限公司 A kind of O-E Payload for UAV is detectd to be calculated and display methods according to region
CN108415452A (en) * 2017-12-25 2018-08-17 彩虹无人机科技有限公司 A kind of hollow long endurance unmanned aircraft task grouping
CN108248891A (en) * 2017-12-27 2018-07-06 彩虹无人机科技有限公司 A kind of calibration system and scaling method for unmanned plane semiclosed loop rudder face
CN108426567A (en) * 2018-03-22 2018-08-21 西安闻泰电子科技有限公司 Subject is apart from display methods, apparatus and system
CN108845335A (en) * 2018-05-07 2018-11-20 中国人民解放军国防科技大学 Unmanned aerial vehicle ground target positioning method based on image and navigation information
WO2019222798A1 (en) * 2018-05-22 2019-11-28 Acid Ip Pty Ltd Drone flight programming method and system
WO2020037492A1 (en) * 2018-08-21 2020-02-27 SZ DJI Technology Co., Ltd. Distance measuring method and device
CN109269352A (en) * 2018-09-20 2019-01-25 北京机械设备研究所 A kind of unmanned plane tracking goal approach and system based on ground location
CN209160024U (en) * 2018-10-29 2019-07-26 深圳博士智能科技有限公司 A kind of intelligent opto-electrical load of industry unmanned plane
CN109597427A (en) * 2018-11-28 2019-04-09 彩虹无人机科技有限公司 It is a kind of that method and system for planning is attacked with chance based on the bomb of unmanned plane
CN209085612U (en) * 2018-12-21 2019-07-09 北京大学 A kind of field 3 D image acquring system
CN110068306A (en) * 2019-04-19 2019-07-30 弈酷高科技(深圳)有限公司 A kind of unmanned plane inspection photometry system and method
CN110458888A (en) * 2019-07-23 2019-11-15 深圳前海达闼云端智能科技有限公司 Distance measuring method, device, storage medium and electronic equipment based on image
CN110470304A (en) * 2019-08-19 2019-11-19 西安因诺航空科技有限公司 A kind of high-precision target positioning-speed-measuring method based on UAV electro-optical's platform
CN110807473A (en) * 2019-10-12 2020-02-18 浙江大华技术股份有限公司 Target detection method, device and computer storage medium

Non-Patent Citations (4)

* Cited by examiner, † Cited by third party
Title
WEIDONG DENG等: ""Multiple target recognition of UAV based on image processing"", 《JOURNAL OF PHYSICS: CONFERENCE SERIES》 *
周辉: ""无人机输电线路巡检可见光拍摄方法研究"", 《中国新技术新产品》 *
皮祖成: ""面向对象的无人机任务设备通信接收软件设计"", 《软件》 *
许金凯等: ""高寒区机载电力巡线光电稳定吊舱系统设计及应用"", 《中国电机工程学报》 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114353667A (en) * 2021-12-15 2022-04-15 中国船舶重工集团公司第七0九研究所 Ground target measurement method based on AR and unmanned aerial vehicle monocular vision and application thereof

Also Published As

Publication number Publication date
CN111457895B (en) 2022-04-22

Similar Documents

Publication Publication Date Title
US11783568B2 (en) Object classification using extra-regional context
CN110084165B (en) Intelligent identification and early warning method for abnormal events in open scene of power field based on edge calculation
CN108303747B (en) Inspection apparatus and method of detecting a gun
CN105023278B (en) A kind of motion target tracking method and system based on optical flow method
CN112102646B (en) Parking lot entrance positioning method and device in parking positioning and vehicle-mounted terminal
CN110910350B (en) Nut loosening detection method for wind power tower cylinder
EP3049793B1 (en) Structural hot spot and critical location monitoring
CN110147748B (en) Mobile robot obstacle identification method based on road edge detection
CN110136186B (en) Detection target matching method for mobile robot target ranging
CN115100741B (en) Point cloud pedestrian distance risk detection method, system, equipment and medium
CN111457895B (en) Target size calculation and display method for photoelectric load of unmanned aerial vehicle
CN117369479B (en) Unmanned aerial vehicle obstacle early warning method and system based on oblique photogrammetry technology
CN117788693B (en) Stair modeling method and device based on point cloud data, legged robot and medium
CN114359865A (en) Obstacle detection method and related device
Katsamenis et al. Real time road defect monitoring from UAV visual data sources
CN117130010A (en) Obstacle sensing method and system for unmanned vehicle and unmanned vehicle
KR102377393B1 (en) Image analysis method and system for recognition of Heavy Equipment and Gas Pipe
CN114898054A (en) Visual positioning method and system
Rout et al. Improved Pothole Detection Using YOLOv7 and ESRGAN
CN108280819B (en) Double-load remote sensing image fusion method
CN111815560A (en) Photovoltaic power station fault detection method and device, portable detection equipment and storage medium
CN118314488B (en) Extra-high voltage transformer station space-earth multi-scale re-decision target detection method
CN114419080B (en) Curtain wall inspection system and method
Lexinoski et al. Recognition, location, and depth estimation of objects in electrical substations
Essa et al. Real time automated machinery threat detection and identification system for pipeline infrastructure protection

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant