CN109521781A - Unmanned plane positioning system, unmanned plane and unmanned plane localization method - Google Patents

Unmanned plane positioning system, unmanned plane and unmanned plane localization method Download PDF

Info

Publication number
CN109521781A
CN109521781A CN201811279904.7A CN201811279904A CN109521781A CN 109521781 A CN109521781 A CN 109521781A CN 201811279904 A CN201811279904 A CN 201811279904A CN 109521781 A CN109521781 A CN 109521781A
Authority
CN
China
Prior art keywords
unmanned plane
vision
information
visual pattern
positioning system
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.)
Pending
Application number
CN201811279904.7A
Other languages
Chinese (zh)
Inventor
黄立
李波
刘寿宝
周忠芬
顾兴
刘华斌
王效杰
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.)
Universal Aircraft Technology (shenzhen) Co Ltd
Original Assignee
Universal Aircraft Technology (shenzhen) 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 Universal Aircraft Technology (shenzhen) Co Ltd filed Critical Universal Aircraft Technology (shenzhen) Co Ltd
Priority to CN201811279904.7A priority Critical patent/CN109521781A/en
Publication of CN109521781A publication Critical patent/CN109521781A/en
Pending legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/10Simultaneous control of position or course in three dimensions
    • G05D1/101Simultaneous control of position or course in three dimensions specially adapted for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

The invention discloses a kind of unmanned plane positioning system, unmanned plane and unmanned plane localization methods, comprising: the vision processing module with image acquisition unit, its relevant information for being used to obtain the visual pattern on vision map, and the position of unmanned plane is obtained according to the relevant information of the visual pattern, and the vertex of adjacent visual pattern is connected according to pre-defined rule, the junction on two vertex forms an angle point;The vision processing module determines the position coordinates and posture information of the unmanned plane.The present invention can position in insecure environment in gps or noninertia navigation system under conditions of realizes the high accuracy positioning and real-time navigation of unmanned plane, and only need to be constructed by machine vision by two dimensional code, bar code etc. the vision map that can be identified can achieve the purpose that in real time position and control unmanned plane during flying posture, it is simple and practical, simultaneously, also working efficiency can be improved according to contexture by self flight path.

Description

Unmanned plane positioning system, unmanned plane and unmanned plane localization method
Technical field
The present invention relates to positioning and navigation fields, and in particular to a kind of unmanned plane positioning system, unmanned plane and unmanned plane are fixed Position method.
Background technique
Currently, the positioning of the motion carriers such as unmanned plane and navigation can only rely on GPS and inertial navigation system, but used Property navigation system in, due to its sensor be easy by external environmental interference, cause positioning accuracy low;In GPS positioning system In system, due to the limitation of the factors such as landform, Fabricated structures, some areas GPS signal is weaker or without GPS signal, therefore this A little regions also can not realize independent navigation by GPS.
Summary of the invention
In view of the foregoing drawbacks, the present invention provides a kind of unmanned plane positioning system, unmanned plane and unmanned plane localization method, It constructs identifiable vision map by visual patterns such as two dimensional codes, even if thus positioning insecure environment or nothing in gps The high accuracy positioning and real-time navigation of unmanned plane are realized under conditions of inertial navigation system.
The technical solution that the present invention is proposed with regard to above-mentioned technical problem is as follows:
On the one hand, a kind of unmanned plane positioning system is provided comprising: the visual processes mould with image acquisition unit Block is used to obtain the relevant information of the visual pattern on vision map, and is obtained according to the relevant information of the visual pattern The location information of unmanned plane, and the vertex of adjacent visual pattern is connected according to pre-defined rule, the junction on two vertex forms one Angle point;
The vision processing module determines the position coordinates of the unmanned plane according to following equation (1)-(7);
H=[h1 h2 h3]=λ K [r1 r2t] (5);
Wherein, s is scale factor, and Z=0, H are homography matrix, and R is spin matrix, and T is translation matrix, and u, v are formed The pixel coordinate of angle point, XYZ are three-dimensional world coordinate;xc=0, yc=0, zc=0, three is image acquisition unit in image Coordinate in acquiring unit coordinate system, Xc, Yc, ZcFor coordinate of the image acquisition unit in three-dimensional world coordinate system.
Preferably, the vision processing module determines that the posture of the unmanned plane is believed also according to following equation (8)-(11) Breath;
θz=atan2 (r21, r11) (8);
Wherein, θx, θy, θzFor three axis rotation angles of image acquisition unit, R is spin matrix.
Preferably, the localizing environment is indoor environment or the insecure environment of global positioning system signal.
Preferably, the vision map has at least one visual pattern, and each visual pattern is identical more Side shape, and have the relevant information of the visual pattern in each visual pattern.
Preferably, the unmanned plane positioning system further include:
Path planning module, according to the vision of path feature and acquisition between beginning and end, Origin And Destination Cartographic information independently constructs the path of connection source and position;
And motion-control module, it is used to it is expected the desired locations of destination, the desired speed of desired course using target The flight attitude information generation of vector, the Desired Height of unmanned plane and unmanned plane entirety is guidanceed command, and is referred to according to the guidance Enable the flight attitude of the position for adjusting the unmanned plane and/or the control unmanned plane.
Preferably, the method in the path of the autonomous building connection source and terminal includes simulated annealing, artificial gesture Field method, fuzzy logic algorithm, tabu search algorithm, visual map space, Grid Method, ant group algorithm, neural network algorithm, heredity are calculated One or more of method.
On the other hand, a kind of unmanned thermomechanical components are also provided comprising: body and above-mentioned unmanned plane positioning system.
Preferably, the unmanned thermomechanical components further include:
Sample detection module comprising at least one monitoring sensor is used to acquire ring during unmanned plane during flying The monitoring information to obtain sample monitoring information, and is sent to the end at user by the sample in border, and analyzing it End is shown;
And object identification module, it is used to obtain and is attached to the object information of body surface to be monitored, and by the object Body information is sent to the terminal at user and shows.
On the other hand, a kind of localization method of unmanned plane is also provided comprising following steps:
S1, vision map is set in the environment;
S2, the visual pattern on the vision map is grabbed by the image acquisition unit of vision processing module, obtaining should The relevant information of visual pattern, and determine that the vertex of two visual patterns connection is formed by angle according to the relevant information of visual pattern The position coordinates of point, the position coordinates of the unmanned plane are determined according to following equation (1)-(7);
H=[h1 h2 h3]=λ K [r1 r2t] (5);
Wherein, s is scale factor, and Z=0, H are homography matrix, and R is spin matrix, and T is translation matrix, and u, v are formed The pixel coordinate of angle point, XYZ are three-dimensional world coordinate;xc=0, yc=0, zc=0, three is image acquisition unit in image Coordinate in acquiring unit coordinate system, Xc, Yc, ZcFor coordinate of the image acquisition unit in three-dimensional world coordinate system;
And the posture information of the unmanned plane is determined according to following equation (8)-(11);
θz=atan2 (r21, r11) (8);
Wherein, θx, θy, θzFor three axis rotation angles of image acquisition unit, R is spin matrix.
Preferably, further includes:
S3, path planning module are according to the characteristics of path between beginning and end, Origin And Destination and the vision of acquisition Cartographic information independently constructs the path of connection source and terminal;
And S4, motion-control module using the target expectation desired locations of destination, desired course desired speed vector, The flight attitude information generation of Desired Height and the unmanned plane entirety of unmanned plane is guidanceed command, and guidances command adjustment according to described The position of the unmanned plane and/or the flight attitude of the control unmanned plane.
The present invention can position in insecure environment in gps or noninertia navigation system under conditions of realizes the height of unmanned plane Precision positioning and real-time navigation, and only need to be constructed by machine vision by two dimensional code, bar code etc. and can identify visually Figure can reach the purpose of positioning in real time and control unmanned plane during flying posture, simple and practical, meanwhile, it can also be flown according to contexture by self Walking along the street line improves working efficiency.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of unmanned plane positioning system in embodiment one;
Fig. 2 a is the structural schematic diagram of unmanned plane, vision map in embodiment one;
Fig. 2 b is the schematic diagram of angle point in embodiment one;
Fig. 3 is the structural schematic diagram of unmanned plane in embodiment two;
Fig. 4 is the structural schematic diagram of unmanned plane and object to be monitored in embodiment two.
Specific embodiment
For a clearer understanding of the technical characteristics, objects and effects of the present invention, now control attached drawing is described in detail A specific embodiment of the invention.
Embodiment one:
As shown in Fig. 1-2 a, unmanned plane positioning system includes: in the present embodiment
Vision processing module 1 is used to obtain 21 information of visual pattern on visually Fig. 2, and according to the vision figure The relevant information of case 21 obtains position and the posture information of the unmanned plane 100;The vision map is set in localizing environment; Wherein, the localizing environment is indoor environment or the insecure environment of global positioning system (GPS) signal;Preferably, the view Feel that ground Fig. 2 has at least one visual pattern 21, and each 21 color of the visual pattern is identical, in the present embodiment, Mei Yisuo Stating visual pattern 21 is identical polygon (including regular polygon, such as square, diamond shape, equilateral triangle);Meanwhile as schemed Shown in 2b, has the visual pattern by modes such as two dimensional code, bar code, AprilTag, QR codes in each visual pattern Relevant information (the corresponding number of such as visual pattern, shape, size, apex coordinate), and different visual pattern 21 Vertex connected according to pre-defined rule, for example, a certain vertex of a visual pattern 21 is only correspondingly connected with adjacent, another vision figure The junction on a certain vertex of case 21, two vertex forms an angle point 22;
Specifically, the vision processing module 1 includes that image acquisition unit 11, position determination unit 12 and posture determine list Member 13;
Wherein, described image acquiring unit 11 (such as camera) is for grabbing the visual pattern 21, and passes through identification two The modes such as dimension code, bar code, AprilTag, QR code obtain the relevant information of the visual pattern,
The position determination unit 12 connects described image acquiring unit 11, for the relevant information according to visual pattern 21 Determine that the vertex of two visual patterns connection is formed by the position coordinates of angle point 22, such as two visual patterns connected according to vertex Number obtains the coordinate information for being formed by angle point 22, so that it is determined that at least one angle point 22 (preferably 4 or more angle points 22) Position coordinates;And the position coordinates of the unmanned plane are determined according to following equation (1)-(7):
H=[h1 h2 h3]=λ K [r1 r2t] (5);
Wherein, s is scale factor, and Z=0, H are homography matrix, and R is spin matrix, and T is translation matrix, and u, v are formed The pixel coordinate of angle point, XYZ are three-dimensional world coordinate (i.e. the practical flight coordinate of unmanned plane);xc=0, yc=0, zc=0, three Person is coordinate of the image acquisition unit in image acquisition unit coordinate system, Xc, Yc, ZcIt is image acquisition unit in three-dimensional generation Coordinate in boundary's coordinate system;
It is as a result, that can determine that unmanned plane is whole to exist obtaining image acquisition unit after the coordinate in three-dimensional world coordinate system Physical location in three-dimensional world coordinate system;
The posture determination unit 13 connects described image acquiring unit 11, for being determined according to following equation (8)-(11) The posture information of the unmanned plane:
θz=atan2 (r21, r11) (8);
Wherein, θx, θy, θzFor three axis rotation angles of image acquisition unit, R is spin matrix;
It can determine the flight attitude letter of unmanned plane entirety after the three axis rotation angles for obtaining image acquisition unit 11 as a result, Breath.
Therefore, it even if the positioning system in the present embodiment positions in insecure environment in gps, can also not completely depend on used Property navigation system realize high accuracy positioning and real-time navigation, and only need to be constructed by machine vision by two dimensional code, bar code etc. The vision map that can be identified can achieve the purpose that position and grasp unmanned plane during flying posture in real time, simple and practical.
In addition, the unmanned plane positioning system further include:
Path planning module 2, according to beginning and end (position where the i.e. described vision map), Origin And Destination it Between path the characteristics of (whether move) and obtain including barrier quantity, barrier vision map information independence building The path of connection source and position;Wherein, the method in the path of the autonomous building connection source and terminal includes simulated annealing Algorithm, Artificial Potential Field Method, fuzzy logic algorithm, tabu search algorithm, visual map space, Grid Method, ant group algorithm, neural network One or more of algorithm, genetic algorithm;
Motion-control module 3 is used to swear using the desired locations of target expectation destination, the desired speed of desired course Amount, the flight attitude information of the Desired Height of unmanned plane and unmanned plane entirety guidance command (institute by pid control algorithm generation State and guidance command including roll angle, pitch angle and yaw angle), and the position of the unmanned plane is adjusted according to described guidance command And/or the flight attitude of the control unmanned plane.
Embodiment two:
A kind of unmanned thermomechanical components are present embodiments provided, as shown in Figure 3-4 comprising: body 100 ' and embodiment one The unmanned plane positioning system;
Sample detection module 101 comprising at least one monitoring sensor is used to acquire during unmanned plane during flying Sample (such as atmospheric sample) in environment, and analyze it, to obtain sample monitoring information, and the monitoring information is sent out The terminal to user is sent to show, so that user carries out decision;The sample monitoring information includes PM value, temperature and pollution One or more of object content;
And object identification module 102, as shown in figure 4, it is used to obtain the object letter for being attached to body surface to be monitored Breath, and the object information is sent to the terminal at user and is shown;Specifically, the object information includes type, number One or more of amount, the place of production;The object information is contained in the figures such as two dimensional code, bar code, AprilTag, QR code, And it can be obtained by way of scanning by the object identification module 102.
Embodiment three:
A kind of localization method for the unmanned plane realized by unmanned plane positioning system described in embodiment one comprising as follows Step:
S1, the vision map is set in the environment;
S2, the visual pattern on the vision map is grabbed by the image acquisition unit of vision processing module, and according to The relevant information of the visual pattern obtains position and the posture information of the unmanned plane;
Specifically, the step of obtaining position and the posture information of the unmanned plane according to the relevant information of the visual pattern Include:
S21, grab the visual pattern by image acquisition unit (such as camera), and by identification two dimensional code, bar code, The modes such as AprilTag, QR code obtain the relevant information of the visual pattern;
S22, position determination unit determine that the vertex of two visual patterns connection is formed according to the relevant information of visual pattern Angle point position coordinates, and determine according to following equation (1)-(7) position coordinates of the unmanned plane:
H=[h1 h2 h3]=λ K [r1 r2t] (5);
Wherein, s is scale factor, and Z=0, H are homography matrix, and R is spin matrix, and T is translation matrix, and u, v are formed The pixel coordinate of angle point, XYZ are three-dimensional world coordinate (i.e. the practical flight coordinate of unmanned plane);xc=0, yc=0, zc=0, three Person is coordinate of the image acquisition unit in image acquisition unit coordinate system, Xc, Yc, ZcIt is image acquisition unit in three-dimensional generation Coordinate in boundary's coordinate system;
It is as a result, that can determine that unmanned plane is whole to exist obtaining image acquisition unit after the coordinate in three-dimensional world coordinate system Physical location in three-dimensional world coordinate system;
S23, the posture determination unit determine the posture information of the unmanned plane according to following equation (8)-(11):
θz=atan2 (r21, r11) (8);
Wherein, θx, θy, θzFor three axis rotation angles of image acquisition unit, R is spin matrix;
It can determine the flight attitude letter of unmanned plane entirety after the three axis rotation angles for obtaining image acquisition unit as a result, Breath;
The characteristics of S3, path planning module are according to path between beginning and end, Origin And Destination (including barrier number Amount, whether barrier move) and the path of vision map information independence building connection source and terminal that obtains;
And S4, motion-control module using the target expectation desired locations of destination, desired course desired speed vector, The flight attitude information of Desired Height and the unmanned plane entirety of unmanned plane is guidanceed command by pid control algorithm generation, and according to The flight attitude for guidanceing command the position for adjusting the unmanned plane and/or the control unmanned plane.
In conclusion the present invention can position in insecure environment in gps, inertial navigation system reality can also not completely depended on Existing high accuracy positioning and real-time navigation, and only need to be constructed by the view that machine vision can identify by two dimensional code, bar code etc. Feel map be can reach in real time positioning and control unmanned plane during flying posture purpose, it is simple and practical, meanwhile, can also basis starting Contexture by self optimal flight path in position increases the aerial residence time, improves working efficiency.
The foregoing is merely presently preferred embodiments of the present invention, is not intended to limit the invention, it is all in spirit of the invention and Within principle, any modification, equivalent replacement, improvement and so on be should all be included in the protection scope of the present invention.

Claims (10)

1. a kind of unmanned plane positioning system comprising: the vision processing module with image acquisition unit is used to obtain vision The relevant information of visual pattern on map, and according to the relevant information of the visual pattern obtain unmanned plane location information, And the vertex of adjacent visual pattern is connected according to pre-defined rule, the junction on two vertex forms an angle point;
It is characterized in that, the vision processing module determines the position coordinates of the unmanned plane according to following equation (1)-(7);
H=[h1 h2 h3]=λ K [r1 r2t] (5);
Wherein, s is scale factor, and Z=0, H are homography matrix, and R is spin matrix, and T is translation matrix, and u, v are the angle point to be formed Pixel coordinate, XYZ is three-dimensional world coordinate;xc=0, yc=0, zc=0, three is that image acquisition unit is obtained in image Coordinate in unit coordinate system, Xc, Yc, ZcFor coordinate of the image acquisition unit in three-dimensional world coordinate system.
2. unmanned plane positioning system as described in claim 1, which is characterized in that the vision processing module is also according to following public affairs Formula (8)-(11) determine the posture information of the unmanned plane;
θz=atan2 (r21, r11) (8);
Wherein, θx, θy, θzFor three axis rotation angles of image acquisition unit, R is spin matrix.
3. unmanned plane positioning system as described in claim 1, which is characterized in that the localizing environment is indoor environment or the whole world The insecure environment of positioning system signal.
4. unmanned plane positioning system as described in claim 1, which is characterized in that the vision map has at least one vision Pattern, each visual pattern are identical polygon, and with the visual pattern in each visual pattern Relevant information.
5. unmanned plane positioning system as described in claim 1, which is characterized in that the unmanned plane positioning system further include:
Path planning module, according to the vision map of path feature and acquisition between beginning and end, Origin And Destination The path of information independence building connection source and position;
And motion-control module, the desired speed vector of the desired locations, desired course that are used to that target to be utilized it is expected destination, The flight attitude information generation of Desired Height and the unmanned plane entirety of unmanned plane is guidanceed command, and guidances command adjustment according to described The position of the unmanned plane and/or the flight attitude of the control unmanned plane.
6. unmanned plane positioning system as claimed in claim 5, which is characterized in that the autonomous building connection source and terminal The method in path includes simulated annealing, Artificial Potential Field Method, fuzzy logic algorithm, tabu search algorithm, visual map space, grid One or more of lattice method, ant group algorithm, neural network algorithm, genetic algorithm.
7. a kind of unmanned thermomechanical components characterized by comprising body and unmanned plane as claimed in any one of claims 1 to 6 Positioning system.
8. unmanned thermomechanical components as claimed in claim 7, which is characterized in that the unmanned thermomechanical components further include:
Sample detection module comprising at least one monitoring sensor is used to acquire in environment during unmanned plane during flying Sample, and analyze it, to obtain sample monitoring information, and by the monitoring information be sent to the terminal at user into Row display;
And object identification module, it is used to obtain the object information for being attached to body surface to be monitored, and the object is believed The terminal being sent at user is ceased to show.
9. a kind of localization method of unmanned plane, which comprises the steps of:
S1, vision map is set in the environment;
S2, the visual pattern on the vision map is grabbed by the image acquisition unit of vision processing module, obtains the vision The relevant information of pattern, and determine that the vertex of two visual patterns connection is formed by angle point according to the relevant information of visual pattern Position coordinates, and determine according to following equation (1)-(7) position coordinates of the unmanned plane;
H=[h1 h2 h3]=λ K [r1 r2t] (5);
Wherein, s is scale factor, and Z=0, H are homography matrix, and R is spin matrix, and T is translation matrix, and u, v are the angle point to be formed Pixel coordinate, XYZ is three-dimensional world coordinate;xc=0, yc=0, Zc=0, three is that image acquisition unit is obtained in image Coordinate in unit coordinate system, Xc, Yc, ZcFor coordinate of the image acquisition unit in three-dimensional world coordinate system;
And the posture information of the unmanned plane is determined according to following equation (8)-(11);
θz=atan2 (r21, r11) (8);
Wherein, θx, θy, θzFor three axis rotation angles of image acquisition unit, R is spin matrix.
10. localization method as claimed in claim 9, which is characterized in that further include:
S3, path planning module are according to the characteristics of path between beginning and end, Origin And Destination and the vision map of acquisition The path of information independence building connection source and terminal;
And S4, motion-control module using the target expectation desired locations of destination, desired course desired speed vector, nobody The flight attitude information generation of Desired Height and the unmanned plane entirety of machine is guidanceed command, and is guidanceed command described in adjustment according to described The position of unmanned plane and/or the flight attitude of the control unmanned plane.
CN201811279904.7A 2018-10-30 2018-10-30 Unmanned plane positioning system, unmanned plane and unmanned plane localization method Pending CN109521781A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201811279904.7A CN109521781A (en) 2018-10-30 2018-10-30 Unmanned plane positioning system, unmanned plane and unmanned plane localization method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201811279904.7A CN109521781A (en) 2018-10-30 2018-10-30 Unmanned plane positioning system, unmanned plane and unmanned plane localization method

Publications (1)

Publication Number Publication Date
CN109521781A true CN109521781A (en) 2019-03-26

Family

ID=65772713

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201811279904.7A Pending CN109521781A (en) 2018-10-30 2018-10-30 Unmanned plane positioning system, unmanned plane and unmanned plane localization method

Country Status (1)

Country Link
CN (1) CN109521781A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110989645A (en) * 2019-12-02 2020-04-10 西安欧意特科技有限责任公司 Target space attitude processing method based on compound eye imaging principle
CN110989646A (en) * 2019-12-02 2020-04-10 西安欧意特科技有限责任公司 Compound eye imaging principle-based target space attitude processing system
CN111678503A (en) * 2020-06-15 2020-09-18 西安航空职业技术学院 Unmanned aerial vehicle aerial survey control point arrangement and identification method and system
CN112051596A (en) * 2020-07-29 2020-12-08 武汉威图传视科技有限公司 Indoor positioning method and device based on node coding
CN113467512A (en) * 2021-07-19 2021-10-01 宁波权智科技有限公司 Unmanned aerial vehicle flying method and device based on neural network
CN113625774A (en) * 2021-09-10 2021-11-09 天津大学 Multi-unmanned aerial vehicle cooperative positioning system and method for local map matching and end-to-end distance measurement
CN114176425A (en) * 2021-12-30 2022-03-15 黄文朔 Self-service barbecue oven
JP7227936B2 (en) 2020-03-31 2023-02-22 西武建設株式会社 Drone guidance method and device
TWI829005B (en) * 2021-08-12 2024-01-11 國立政治大學 High-altitude positioning center setting method and high-altitude positioning flight control method

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016065623A1 (en) * 2014-10-31 2016-05-06 SZ DJI Technology Co., Ltd. Systems and methods for surveillance with visual marker
CN106647814A (en) * 2016-12-01 2017-05-10 华中科技大学 System and method of unmanned aerial vehicle visual sense assistant position and flight control based on two-dimensional landmark identification
CN107038722A (en) * 2016-02-02 2017-08-11 深圳超多维光电子有限公司 A kind of equipment localization method and device
CN107633536A (en) * 2017-08-09 2018-01-26 武汉科技大学 A kind of camera calibration method and system based on two-dimensional planar template
CN108198216A (en) * 2017-12-12 2018-06-22 深圳市神州云海智能科技有限公司 A kind of robot and its position and orientation estimation method and device based on marker

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016065623A1 (en) * 2014-10-31 2016-05-06 SZ DJI Technology Co., Ltd. Systems and methods for surveillance with visual marker
CN106687878A (en) * 2014-10-31 2017-05-17 深圳市大疆创新科技有限公司 Systems and methods for surveillance with visual marker
CN107038722A (en) * 2016-02-02 2017-08-11 深圳超多维光电子有限公司 A kind of equipment localization method and device
CN106647814A (en) * 2016-12-01 2017-05-10 华中科技大学 System and method of unmanned aerial vehicle visual sense assistant position and flight control based on two-dimensional landmark identification
CN107633536A (en) * 2017-08-09 2018-01-26 武汉科技大学 A kind of camera calibration method and system based on two-dimensional planar template
CN108198216A (en) * 2017-12-12 2018-06-22 深圳市神州云海智能科技有限公司 A kind of robot and its position and orientation estimation method and device based on marker

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
GREGORY G.SLABAUGH: "Computing Euler angles from a rotation matrix", 《WWW.DOC88.COM/P-314986360419.HTML》 *
网友: "根据相机旋转矩阵求解三个轴的旋转角", 《HTTPS://WWW.CNBLOGS.COM/SINGLEX/P/ROTATEMATRIX2EULER.HTML》 *
舒娜: "摄像机标定方法的研究", 《中国优秀硕士学位论文全文数据库 信息科技辑》 *

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110989645A (en) * 2019-12-02 2020-04-10 西安欧意特科技有限责任公司 Target space attitude processing method based on compound eye imaging principle
CN110989646A (en) * 2019-12-02 2020-04-10 西安欧意特科技有限责任公司 Compound eye imaging principle-based target space attitude processing system
CN110989645B (en) * 2019-12-02 2023-05-12 西安欧意特科技有限责任公司 Target space attitude processing method based on compound eye imaging principle
JP7227936B2 (en) 2020-03-31 2023-02-22 西武建設株式会社 Drone guidance method and device
CN111678503A (en) * 2020-06-15 2020-09-18 西安航空职业技术学院 Unmanned aerial vehicle aerial survey control point arrangement and identification method and system
CN112051596A (en) * 2020-07-29 2020-12-08 武汉威图传视科技有限公司 Indoor positioning method and device based on node coding
CN113467512A (en) * 2021-07-19 2021-10-01 宁波权智科技有限公司 Unmanned aerial vehicle flying method and device based on neural network
TWI829005B (en) * 2021-08-12 2024-01-11 國立政治大學 High-altitude positioning center setting method and high-altitude positioning flight control method
CN113625774A (en) * 2021-09-10 2021-11-09 天津大学 Multi-unmanned aerial vehicle cooperative positioning system and method for local map matching and end-to-end distance measurement
CN114176425A (en) * 2021-12-30 2022-03-15 黄文朔 Self-service barbecue oven
CN114176425B (en) * 2021-12-30 2023-10-27 黄文朔 Self-help barbecue oven

Similar Documents

Publication Publication Date Title
CN109521781A (en) Unmanned plane positioning system, unmanned plane and unmanned plane localization method
CN110446159B (en) System and method for accurate positioning and autonomous navigation of indoor unmanned aerial vehicle
Cesetti et al. A vision-based guidance system for UAV navigation and safe landing using natural landmarks
CN108351653B (en) System and method for UAV flight control
CN108351649B (en) Method and apparatus for controlling a movable object
Krajník et al. A practical multirobot localization system
CN105928498B (en) Method, the geodetic mapping and survey system, storage medium of information about object are provided
CN111427360B (en) Map construction method based on landmark positioning, robot and robot navigation system
Celik et al. Monocular vision SLAM for indoor aerial vehicles
CN102116625B (en) GIS (geographic information system)-GPS (global position system) navigation method of inspection robot
CN109579843A (en) Multirobot co-located and fusion under a kind of vacant lot multi-angle of view build drawing method
CN111527463A (en) Method and system for multi-target tracking
Breitenmoser et al. A monocular vision-based system for 6D relative robot localization
US20240126294A1 (en) System and method for perceptive navigation of automated vehicles
CN107850902A (en) Camera configuration in loose impediment
CN109388150A (en) Multi-sensor environment map structuring
CN109885086A (en) A kind of unmanned plane vertical landing method based on the guidance of multiple polygonal shape mark
Bao et al. Vision-based horizon extraction for micro air vehicle flight control
CN105644785A (en) Unmanned aerial vehicle landing method based on optical flow method and horizon line detection
CN109839118A (en) Paths planning method, system, robot and computer readable storage medium
CN111275015A (en) Unmanned aerial vehicle-based power line inspection electric tower detection and identification method and system
JP2023041675A (en) Drone-work support system and drone-work support method
CN109483507A (en) A kind of indoor vision positioning method of multiple wheeled robot walkings
CN103697883A (en) Aircraft horizontal attitude determination method based on skyline imaging
CN114371725A (en) System suitable for automatic inspection of wind turbine generator

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
RJ01 Rejection of invention patent application after publication

Application publication date: 20190326

RJ01 Rejection of invention patent application after publication