CN113379844A - Large-range surface quality detection method for airplane - Google Patents

Large-range surface quality detection method for airplane Download PDF

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CN113379844A
CN113379844A CN202110570721.6A CN202110570721A CN113379844A CN 113379844 A CN113379844 A CN 113379844A CN 202110570721 A CN202110570721 A CN 202110570721A CN 113379844 A CN113379844 A CN 113379844A
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airplane
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CN113379844B (en
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韩利亚
周力
陈代鑫
蒋德成
缑建杰
蔡怀阳
陈俊佑
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Chengdu Aircraft Industrial Group Co Ltd
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    • G06T7/80Analysis of captured images to determine intrinsic or extrinsic camera parameters, i.e. camera calibration
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06TIMAGE DATA PROCESSING OR GENERATION, IN GENERAL
    • G06T17/00Three dimensional [3D] modelling, e.g. data description of 3D objects
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Abstract

The invention relates to the technical field of aeronautical manufacturing surface quality detection, in particular to a method for detecting the large-range surface quality of an airplane, which comprises the steps of building a system, moving a line laser, simultaneously calculating the lengths of visible laser lines of all cameras, carrying out real-time three-dimensional reconstruction on the laser lines according to the internal and external parameters of two cameras with the longest common visible laser line and a shot laser line image, converting the laser lines into a unified coordinate system, comparing the obtained three-dimensional data with a three-dimensional model of a measured object, finding out an area with data missing, moving the line laser to scan the area, and repeating the three-dimensional reconstruction steps until complete data is obtained. By the method, the problems of influence of the precision of the movement mechanism and poor overall precision can be effectively solved.

Description

Large-range surface quality detection method for airplane
Technical Field
The invention relates to the technical field of aeronautical manufacturing surface quality detection, in particular to a method for detecting the large-range surface quality of an airplane.
Background
The aerial parts and the whole airplane are large in size, and in order to detect the surface quality of the aerial parts or the whole airplane based on images, a movable image acquisition device or a fixed image acquisition device consisting of a large number of cameras is needed. The whole precision of the mobile image acquisition device is influenced by the precision of the movement mechanism.
The three-dimensional data of the same laser line can be reconstructed by shooting the same laser line by the double cameras, and the three-dimensional data of a profile can be generated by sweeping, namely the laser scanning three-dimensional measurement method. When the dual-camera is used for line laser three-dimensional measurement, the laser plane does not need to be calibrated, so that the position of the laser is not required to be accurate. Therefore, the fixed image acquisition device composed of a large number of cameras has better adaptability compared with the movable image acquisition device.
However, when a large area of a surface is scanned, for example, when an aircraft complete machine is scanned, due to the visual field limitation of a single camera, a large number of cameras need to be arranged to cover the whole area, and when the number of cameras is increased greatly, the bandwidth requirement of data transmission is also increased greatly, for example, for a gray scale camera with ten million pixel levels, the data volume of each picture is as high as 10MB, if the data is collected at the rate of 30 frames per second, the bandwidth is 300MB/s, a system formed by only 30 cameras needs the support of a ten-trillion network, and if the number of cameras is continuously increased, the bandwidth requirement is difficult to meet.
Disclosure of Invention
In order to solve the technical problems, the invention provides a method for detecting the large-scale surface quality of an airplane, which can effectively solve the problems of poor overall precision due to the influence of the precision of a motion mechanism and effectively reduce the requirement of the data transmission bandwidth of the whole system.
The invention is realized by adopting the following technical scheme:
a method for detecting the quality of a large-scale surface of an airplane is characterized by comprising the following steps: the method comprises the following steps:
step 1, building a large-range multi-camera surface quality detection system, wherein the large-range multi-camera surface quality detection system comprises a plurality of cameras with fixed positions, a set of visual fields of all the cameras can cover the surface of a detected object, and any point on the surface of the detected object is visible to at least two cameras;
step 2, sequencing the multiple cameras to ensure that a sufficiently large public view field exists between the cameras with adjacent serial numbers, and a sufficiently large public view field exists between the camera with the last serial number and the camera with the first serial number;
step 3, calibrating internal and external parameters of all cameras;
step 4, driving the line laser to move around the measured object by the moving mechanism, projecting laser to the surface of the measured object, and traversing the whole surface of the measured object;
step 5, in the moving process, all cameras simultaneously calculate the lengths of the visible laser lines, and two cameras with the longest common visible laser line perform real-time three-dimensional reconstruction on the laser line according to internal and external parameters and the shot laser line image, and convert the three-dimensional data into a unified coordinate system according to the internal and external parameters of all the cameras;
step 6, when the two cameras with the longest common visible laser lines change, the two cameras with the longest common visible laser lines are replaced by a new group of cameras for calculation, and the three-dimensional data are converted into a unified coordinate system in the same way;
and 7, comparing the obtained three-dimensional data with the three-dimensional model of the measured object, finding out the area with data missing, moving the line laser to scan the area, and repeating the three-dimensional reconstruction step until complete data is obtained.
In the step 5, the length of the visible laser line is calculated by all the cameras at the same time, specifically: setting a brightness threshold value for a camera i, carrying out binarization on an image to enable the pixel of the image position of a laser line to be 1, enabling the pixels at the other positions to be 0, and calculating the longest diameter L of the pixel connected domain of 1iAnd mixing LiAnd feeding back to the control system.
The longest diameter LiMeter (2)The calculation method specifically comprises the following steps: drawing a circumscribed rectangle of the connected domain, wherein four sides of the rectangle are tangent to the most prominent points in four directions of the connected domain, rotating the rectangle by taking the center of the rectangle as a rotation center, keeping the constraint of tangency of the four sides in the rotating process, continuously calculating the length of the long side of the rectangle in the rotating process, and the length of the longest long side of the rectangle is Li
The two cameras with the longest common visible laser line in the step 5 specifically refer to: to LiSorting, selecting the largest and next largest LiTwo corresponding cameras.
The real-time three-dimensional reconstruction of the laser line in the step 5 specifically includes:
step 5.1, aligning the base line of the camera according to the internal and external parameters of the camera, and performing the operation of aligning the base line of the camera
Figure BDA0003082570060000021
Of
Figure BDA0003082570060000022
Extracted, the coordinate system of camera i is multiplied by
Figure BDA0003082570060000023
Coordinate system multiplication of camera j
Figure BDA0003082570060000024
Wherein camera i and camera j are LiTwo cameras corresponding to the largest and the next largest,
Figure BDA0003082570060000025
converting the coordinate of the camera i and the camera j;
step 5.2, horizontally arranging the converted images of the cameras i and j left and right, wherein the corresponding point of one point P in the images of the cameras i and j in the three-dimensional space is positioned on the same horizontal line;
step 5.3, extracting the center line of the laser line in the image, and selecting a point P on the center line of the laser line in the image of the camera iiFinding the center line of the laser line in the image of the camera j by making a horizontal lineCorresponding point P ofj
Step 5.4, setting the world coordinate system coordinate of the point P as PWThe world coordinate system is established under the coordinate system of the camera 1, having
Figure BDA0003082570060000031
Simultaneous solvation of PWIn the same way, all points on the central line of the laser line can be reconstructed in three dimensions; wherein, KiIs an internal parameter matrix, K, of camera ijIs the internal parameter matrix of camera j.
The step 7 specifically includes: let three-dimensional data be P ═ P1,p2,p3,…,pnDispersing the three-dimensional model of the measured object into a point cloud form Q ═ Q1,q2,q3,…,qnWherein q isiIs piAnd setting a rotation and translation matrix T at the closest point in Q, decomposing the rotation and translation matrix T into a rotation matrix R and a translation matrix T, and solving R and T which enable the following objective function to be minimum:
Figure BDA0003082570060000032
converting P to PT=P·R+t,PTDeleting the point cloud with P in Q for the point cloud with P and Q alignedTThe distance between the points in the three-dimensional reconstruction method is smaller than a threshold value delta, the remaining points are missing areas, the positions of the points are displayed by coordinates of the points, the line laser is moved to the positions of the points, the areas are scanned, and the three-dimensional reconstruction step is repeated until complete data are obtained.
And the camera lens is provided with an optical filter with the same luminous frequency as the line laser.
The fact that a sufficiently large public view exists between cameras with adjacent serial numbers in the step 2 specifically means that: the size of the common field of view should exceed 1/3 for the single camera field of view, i.e., the region 1/3 within one camera field of view can be seen by its neighboring cameras; there is enough big public view between the camera of last serial number and the camera of first serial number, specifically: the ordering of the cameras is done in a loop back manner.
Compared with the prior art, the invention has the beneficial effects that:
1. the method is simple and reliable, and has high accuracy and good stability. The method is suitable for acquiring the three-dimensional data of the surface of a large-size measured object to carry out comprehensive detection, the overall measurement precision is independent of the precision of the motion mechanism, the method only depends on the precision of the calibration of the internal and external parameters of the camera, and the method has high precision stability. The requirement on the motion mechanism is low, an open-loop motion mechanism can be adopted, and the difficulty of system construction is low.
2. The form of a motion mechanism carrying the line laser is not required, a three-coordinate gantry mechanism and a six-degree-of-freedom robot can be adopted, the robot can also be held by hands, different motion modes can also be combined for use, and the usability of the system is enhanced;
3. the coordinate system of the measured data is determined by the fixed camera coordinate system, and the data in different measurement examples are located in the same fixed coordinate system, so that the difficulty of data processing is reduced.
4. The camera lens is fitted with a filter having the same frequency as the line laser light to ensure that only light from the laser enters the camera lens.
Drawings
The invention will be described in further detail with reference to the following description taken in conjunction with the accompanying drawings and detailed description, in which:
FIG. 1 is a schematic flow diagram of the present invention;
FIG. 2 is a schematic view of the structure of the detection system of the present invention.
Detailed Description
Example 1
As a basic implementation mode of the invention, referring to the attached figure 1 of the specification, the invention comprises a method for detecting the quality of a large-scale surface of an airplane, which comprises the following steps:
step 1, a large-range multi-camera surface quality detection system is built, the system comprises a plurality of cameras with fixed positions, the set of the vision fields of all the cameras can cover the surface of a measured object, and any point on the surface of the measured object is visible to at least two cameras.
And 2, sequencing the multiple cameras, wherein the serial numbers of the cameras are 1,2,3, … … i, i +1 and … … N in sequence, so that a sufficiently large public view is ensured between the cameras with adjacent serial numbers, and a sufficiently large public view is ensured between the camera with the last serial number and the camera with the first serial number.
And step 3, calibrating internal and external parameters of all cameras.
And 4, driving the line laser to move around the measured object by the moving mechanism, projecting the laser to the surface of the measured object, and traversing the whole surface of the measured object.
And 5, in the moving process, simultaneously calculating the lengths of the visible laser lines by all the cameras, carrying out real-time three-dimensional reconstruction on the laser lines by two cameras with the longest common visible laser line according to internal and external parameters and shot laser line images, and converting the three-dimensional data into a unified coordinate system according to the internal and external parameters of all the cameras.
And 6, when the two cameras with the longest common visible laser line change, replacing the two cameras with the longest common visible laser line by a new group of cameras for calculation, and converting the three-dimensional data into a unified coordinate system.
And 7, comparing the obtained three-dimensional data with the three-dimensional model of the measured object, finding out the area with data missing, moving the line laser to scan the area, and repeating the three-dimensional reconstruction step until complete data is obtained.
Example 2
As a best mode for implementing the invention, the invention comprises a method for detecting the quality of the wide-range surface of the airplane, which comprises the following steps:
step 1, building a large-range multi-camera surface quality detection system, referring to the attached figure 2 of the specification, wherein the system comprises a plurality of cameras with fixed positions and a line laser driven by a motion mechanism. The set of all camera fields of vision can cover the measured object surface, and just arbitrary point on measured object surface all is visible to two at least cameras. Each camera is respectively provided with a data line and a synchronous signal line which are connected with the control system, the data line is used for transmitting the shot pictures, and the synchronous line is used for transmitting the trigger signals, so that all the cameras can shoot synchronously. Each camera has a simple calculation function and can perform simple image processing. The camera lens is fitted with a filter having the same frequency as the line laser light to ensure that only light from the laser enters the camera lens.
And 2, sequencing the multiple cameras, wherein the serial numbers of the cameras are 1,2,3, … … i, i +1 and … … N in sequence, so that a large enough common view field is ensured between the cameras with adjacent serial numbers, and the size of the common view field is larger than 1/3 of the view field of a single camera, namely, a 1/3 area in the view field of one camera can be seen by the adjacent cameras. There is a sufficiently large common view between the cameras of the last sequence number and the cameras of the first sequence number, i.e. the sorting is done in a loop-back manner. Wherein the requirements of steps 1 and 2 can be surely fulfilled by increasing the number of cameras.
And step 3, calibrating internal and external parameters of all cameras. The internal parameters are the properties of the lens and the imaging element of the camera to form an internal parameter matrix KiThe external parameters are coordinate system conversion relations between the cameras, and the external parameters of two adjacent cameras are
Figure BDA0003082570060000051
And by changing over the chains
Figure BDA0003082570060000052
And (4) converting. Wherein the external parameters take the camera 1 as a reference, and the conversion relation from the coordinate system of other cameras to the coordinate system of the camera 1 is calculated, and sequentially
Figure BDA0003082570060000053
i is 1,2,3, …, N. The conversion relationship between the camera i and the camera j is
Figure BDA0003082570060000054
And 4, driving the line laser to move around the measured object by the moving mechanism, projecting the laser to the surface of the measured object, and traversing the whole surface of the measured object. The movement mechanism is mainly a gantry mechanism and a robot, and can also carry out supplementary scanning by holding a laser at the position which cannot be covered by the movement mechanism.
Step 5, in the motion process, all cameras simultaneously calculate the length of the visible laser linesThe degree is calculated by the following method: setting a brightness threshold value for a camera i, carrying out binarization on an image to enable the pixel of the image position of a laser line to be 1, enabling the pixels at the other positions to be 0, and calculating the longest diameter L of the pixel connected domain of 1iThe specific calculation mode is that drawing a circumscribed rectangle of the connected domain, respectively making four sides of the rectangle tangent with the most prominent points in four directions of the connected domain, rotating the rectangle by taking the center of the rectangle as a rotation center, keeping the constraint of tangency of the four sides in the rotation process, continuously calculating the length of the long side of the rectangle in the process, wherein the length of the longest long side of the rectangle is LiAnd mixing LiAnd feeding back to the control system.
To LiSorting, selecting the largest and next largest LiCorresponding two cameras i and j. And receiving images of the two cameras, and performing real-time three-dimensional reconstruction on the laser line according to internal and external parameters and the shot images. The concrete mode is as follows:
step 5.1, aligning the base line of the camera according to the internal and external parameters of the camera, and performing the operation of aligning the base line of the camera
Figure BDA0003082570060000061
Of
Figure BDA0003082570060000062
Extracted, the coordinate system of camera i is multiplied by
Figure BDA0003082570060000063
Coordinate system multiplication of camera j
Figure BDA0003082570060000064
Wherein camera i and camera j are LiTwo cameras corresponding to the largest and the next largest,
Figure BDA0003082570060000065
converting the coordinate of the camera i and the camera j;
step 5.2, horizontally arranging the converted images of the cameras i and j left and right, wherein the corresponding point of one point P in the images of the cameras i and j in the three-dimensional space is positioned on the same horizontal line;
step 5.3, extracting the center line of the laser line in the image, and selecting a point P on the center line of the laser line in the image of the camera iiFinding out the corresponding point P on the central line of the laser line in the image of the camera j by making a horizontal linej
Step 5.4, setting the world coordinate system coordinate of the point P as PWThe world coordinate system is established under the coordinate system of the camera 1, having
Figure BDA0003082570060000066
Simultaneous solvation of PWAnd points on the central line of the laser line can be completely reconstructed in three dimensions in the same way. Wherein, KiIs an internal parameter matrix, K, of camera ijIs the internal parameter matrix of camera j.
And 6, when the two cameras with the longest common visible laser line change, replacing the two cameras with the longest common visible laser line by a new group of cameras for calculation, and converting the three-dimensional data into a unified coordinate system.
Step 7, the obtained three-dimensional data P is set as { P ═ P1,p2,p3,…,pnRegistering the three-dimensional model of the measured object in a manner of dispersing the three-dimensional model of the measured object into a point cloud form Q (Q ═ Q)1,q2,q3,…,qnWherein q isiIs piAnd setting a rotation and translation matrix T at the closest point in Q, decomposing the rotation and translation matrix T into a rotation matrix R and a translation matrix T, and solving R and T which enable the following objective function to be minimum:
Figure BDA0003082570060000067
converting P to PT=P·R+t,PTDeleting the point cloud with P in Q for the point cloud with P and Q alignedTThe distance between the points in the three-dimensional reconstruction method is smaller than a threshold value delta, the remaining points are missing areas, the positions of the points are displayed by coordinates of the points, the line laser is moved to the positions of the points, the areas are scanned, and the three-dimensional reconstruction step is repeated until complete data are obtained.
In summary, after reading the present disclosure, those skilled in the art should make various other modifications without creative efforts according to the technical solutions and concepts of the present disclosure, which are within the protection scope of the present disclosure.

Claims (8)

1. A method for detecting the quality of a large-scale surface of an airplane is characterized by comprising the following steps: the method comprises the following steps:
step 1, building a large-range multi-camera surface quality detection system, wherein the large-range multi-camera surface quality detection system comprises a plurality of cameras with fixed positions, a set of visual fields of all the cameras can cover the surface of a detected object, and any point on the surface of the detected object is visible to at least two cameras;
step 2, sequencing the multiple cameras to ensure that a sufficiently large public view field exists between the cameras with adjacent serial numbers, and a sufficiently large public view field exists between the camera with the last serial number and the camera with the first serial number;
step 3, calibrating internal and external parameters of all cameras;
step 4, driving the line laser to move around the measured object by the moving mechanism, projecting laser to the surface of the measured object, and traversing the whole surface of the measured object;
step 5, in the moving process, all cameras simultaneously calculate the lengths of the visible laser lines, and two cameras with the longest common visible laser line perform real-time three-dimensional reconstruction on the laser line according to internal and external parameters and the shot laser line image, and convert the three-dimensional data into a unified coordinate system according to the internal and external parameters of all the cameras;
step 6, when the two cameras with the longest common visible laser lines change, the two cameras with the longest common visible laser lines are replaced by a new group of cameras for calculation, and the three-dimensional data are converted into a unified coordinate system in the same way;
and 7, comparing the obtained three-dimensional data with the three-dimensional model of the measured object, finding out the area with data missing, moving the line laser to scan the area, and repeating the three-dimensional reconstruction step until complete data is obtained.
2. According to the claimsThe method for detecting the quality of the large-range surface of the airplane in the calculation 1 is characterized by comprising the following steps: in the step 5, the length of the visible laser line is calculated by all the cameras at the same time, specifically: setting a brightness threshold value for a camera i, carrying out binarization on an image to enable the pixel of the image position of a laser line to be 1, enabling the pixels at the other positions to be 0, and calculating the longest diameter L of the pixel connected domain of 1iAnd mixing LiAnd feeding back to the control system.
3. The method for detecting the quality of the large-scale surface of the airplane as claimed in claim 2, wherein the method comprises the following steps: the longest diameter LiThe calculating method specifically further comprises: drawing a circumscribed rectangle of the connected domain, wherein four sides of the rectangle are tangent to the most prominent points in four directions of the connected domain, rotating the rectangle by taking the center of the rectangle as a rotation center, keeping the constraint of tangency of the four sides in the rotating process, continuously calculating the length of the long side of the rectangle in the rotating process, and the length of the longest long side of the rectangle is Li
4. The method for detecting the quality of the large-scale surface of the airplane as claimed in claim 2 or 3, wherein the method comprises the following steps: the two cameras with the longest common visible laser line in the step 5 specifically refer to: to LiSorting, selecting the largest and next largest LiTwo corresponding cameras.
5. The method for detecting the quality of the large-scale surface of the airplane as claimed in claim 1, wherein the method comprises the following steps: the real-time three-dimensional reconstruction of the laser line in the step 5 specifically includes:
step 5.1, aligning the base line of the camera according to the internal and external parameters of the camera, and performing the operation of aligning the base line of the camera
Figure FDA0003082570050000021
Of
Figure FDA0003082570050000022
Extracted, the coordinate system of camera i is multiplied by
Figure FDA0003082570050000023
Coordinate system multiplication of camera j
Figure FDA0003082570050000024
Wherein camera i and camera j are LiTwo cameras corresponding to the largest and the next largest,
Figure FDA0003082570050000025
converting the coordinate of the camera i and the camera j;
step 5.2, horizontally arranging the converted images of the cameras i and j left and right, wherein the corresponding point of one point P in the images of the cameras i and j in the three-dimensional space is positioned on the same horizontal line;
step 5.3, extracting the center line of the laser line in the image, and selecting a point P on the center line of the laser line in the image of the camera iiFinding out the corresponding point P on the central line of the laser line in the image of the camera j by making a horizontal linej
Step 5.4, setting the world coordinate system coordinate of the point P as PWThe world coordinate system is established under the coordinate system of the camera 1 and has Pi=KiT1 iPw,Pj=KjT1 jPwSimultaneous resolution of PWIn the same way, all points on the central line of the laser line can be reconstructed in three dimensions; wherein, KiIs an internal parameter matrix, K, of camera ijIs the internal parameter matrix of camera j.
6. The method for detecting the quality of the large-scale surface of the airplane as claimed in claim 1, wherein the method comprises the following steps: the step 7 specifically includes: let three-dimensional data be P ═ P1,p2,p3,…,pnDispersing the three-dimensional model of the measured object into a point cloud form Q ═ Q1,q2,q3,…,qnWherein q isiIs piAt the closest point in Q, a rotation and translation matrix T is set and decomposed into a rotation matrix R and a translation matrix T, and the sum of R and T which minimizes the following objective function is solvedt:
Figure FDA0003082570050000026
Converting P to PT=P·R+t,PTDeleting the point cloud with P in Q for the point cloud with P and Q alignedTThe distance between the points in the three-dimensional reconstruction method is smaller than a threshold value delta, the remaining points are missing areas, the positions of the points are displayed by coordinates of the points, the line laser is moved to the positions of the points, the areas are scanned, and the three-dimensional reconstruction step is repeated until complete data are obtained.
7. The method for detecting the quality of the large-scale surface of the airplane as claimed in claim 1, wherein the method comprises the following steps: and the camera lens is provided with an optical filter with the same luminous frequency as the line laser.
8. The method for detecting the quality of the large-scale surface of the airplane as claimed in claim 1, wherein the method comprises the following steps: the fact that a sufficiently large public view exists between cameras with adjacent serial numbers in the step 2 specifically means that: the size of the common field of view should exceed 1/3 for the single camera field of view, i.e., the region 1/3 within one camera field of view can be seen by its neighboring cameras; there is enough big public view between the camera of last serial number and the camera of first serial number, specifically: the ordering of the cameras is done in a loop back manner.
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2023142608A1 (en) * 2022-01-26 2023-08-03 上海飞机制造有限公司 System and method for obtaining aircraft profile

Citations (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090168045A1 (en) * 2007-12-28 2009-07-02 Industrial Technology Research Institute Three-dimensional surround scanning device and method thereof
CN101551918A (en) * 2009-04-28 2009-10-07 浙江大学 Acquisition method of large scene based on line laser
CN106500628A (en) * 2016-10-19 2017-03-15 杭州思看科技有限公司 A kind of 3-D scanning method containing multiple different wave length laser instrument and scanner
CN106780712A (en) * 2016-10-28 2017-05-31 武汉市工程科学技术研究院 Joint laser scanning and the three-dimensional point cloud generation method of Image Matching
CN107121062A (en) * 2016-12-07 2017-09-01 苏州笛卡测试技术有限公司 A kind of robot three-dimensional scanning means and method
CN107578464A (en) * 2017-06-30 2018-01-12 长沙湘计海盾科技有限公司 A kind of conveyor belt workpieces measuring three-dimensional profile method based on line laser structured light
CN108020172A (en) * 2016-11-01 2018-05-11 中国科学院沈阳自动化研究所 A kind of aircraft surface workmanship detection method based on 3D data
CN108759714A (en) * 2018-05-22 2018-11-06 华中科技大学 A kind of multi-thread laser profile sensor coordinate system fusion and rotating axis calibration method
CN108828606A (en) * 2018-03-22 2018-11-16 中国科学院西安光学精密机械研究所 Laser radar and binocular visible light camera-based combined measurement method
CN109186491A (en) * 2018-09-30 2019-01-11 南京航空航天大学 Parallel multi-thread laser measurement system and measurement method based on homography matrix
CN109215108A (en) * 2017-06-30 2019-01-15 深圳先进技术研究院 Panorama three-dimensional reconstruction system and method based on laser scanning
CN109253706A (en) * 2018-08-24 2019-01-22 中国科学技术大学 A kind of tunnel 3 D measuring method based on digital picture
US10408606B1 (en) * 2018-09-24 2019-09-10 Faro Technologies, Inc. Quality inspection system and method of operation
CN110379013A (en) * 2019-06-17 2019-10-25 杭州电子科技大学 A kind of three-dimensional reconfiguration system based on multi-angle laser line scanning
CN110470238A (en) * 2019-07-02 2019-11-19 杭州非白三维科技有限公司 A kind of hand-held laser 3 d scanner, scan method and device
CN110487213A (en) * 2019-08-19 2019-11-22 杭州电子科技大学 Full view line laser structured light three-dimensional image forming apparatus and method based on spatial offset
CN111207695A (en) * 2020-01-14 2020-05-29 北京科技大学 Hot-rolled strip steel end three-dimensional contour measuring method based on double-line structured light
CN112361982A (en) * 2020-10-29 2021-02-12 山东省科学院激光研究所 Method and system for extracting three-dimensional data of large-breadth workpiece
CN112505065A (en) * 2020-12-28 2021-03-16 上海工程技术大学 Method for detecting surface defects of large part by indoor unmanned aerial vehicle
CN112525106A (en) * 2020-10-23 2021-03-19 清华大学 Three-phase machine cooperative laser-based 3D detection method and device

Patent Citations (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090168045A1 (en) * 2007-12-28 2009-07-02 Industrial Technology Research Institute Three-dimensional surround scanning device and method thereof
CN101551918A (en) * 2009-04-28 2009-10-07 浙江大学 Acquisition method of large scene based on line laser
CN106500628A (en) * 2016-10-19 2017-03-15 杭州思看科技有限公司 A kind of 3-D scanning method containing multiple different wave length laser instrument and scanner
CN106780712A (en) * 2016-10-28 2017-05-31 武汉市工程科学技术研究院 Joint laser scanning and the three-dimensional point cloud generation method of Image Matching
CN108020172A (en) * 2016-11-01 2018-05-11 中国科学院沈阳自动化研究所 A kind of aircraft surface workmanship detection method based on 3D data
CN107121062A (en) * 2016-12-07 2017-09-01 苏州笛卡测试技术有限公司 A kind of robot three-dimensional scanning means and method
CN109215108A (en) * 2017-06-30 2019-01-15 深圳先进技术研究院 Panorama three-dimensional reconstruction system and method based on laser scanning
CN107578464A (en) * 2017-06-30 2018-01-12 长沙湘计海盾科技有限公司 A kind of conveyor belt workpieces measuring three-dimensional profile method based on line laser structured light
CN108828606A (en) * 2018-03-22 2018-11-16 中国科学院西安光学精密机械研究所 Laser radar and binocular visible light camera-based combined measurement method
CN108759714A (en) * 2018-05-22 2018-11-06 华中科技大学 A kind of multi-thread laser profile sensor coordinate system fusion and rotating axis calibration method
CN109253706A (en) * 2018-08-24 2019-01-22 中国科学技术大学 A kind of tunnel 3 D measuring method based on digital picture
US10408606B1 (en) * 2018-09-24 2019-09-10 Faro Technologies, Inc. Quality inspection system and method of operation
CN109186491A (en) * 2018-09-30 2019-01-11 南京航空航天大学 Parallel multi-thread laser measurement system and measurement method based on homography matrix
CN110379013A (en) * 2019-06-17 2019-10-25 杭州电子科技大学 A kind of three-dimensional reconfiguration system based on multi-angle laser line scanning
CN110470238A (en) * 2019-07-02 2019-11-19 杭州非白三维科技有限公司 A kind of hand-held laser 3 d scanner, scan method and device
CN110487213A (en) * 2019-08-19 2019-11-22 杭州电子科技大学 Full view line laser structured light three-dimensional image forming apparatus and method based on spatial offset
CN111207695A (en) * 2020-01-14 2020-05-29 北京科技大学 Hot-rolled strip steel end three-dimensional contour measuring method based on double-line structured light
CN112525106A (en) * 2020-10-23 2021-03-19 清华大学 Three-phase machine cooperative laser-based 3D detection method and device
CN112361982A (en) * 2020-10-29 2021-02-12 山东省科学院激光研究所 Method and system for extracting three-dimensional data of large-breadth workpiece
CN112505065A (en) * 2020-12-28 2021-03-16 上海工程技术大学 Method for detecting surface defects of large part by indoor unmanned aerial vehicle

Non-Patent Citations (9)

* Cited by examiner, † Cited by third party
Title
IGOR JOVANˇCEVI´C等: "3D Point Cloud Analysis for Detection and Characterization of Defects on Airplane Exterior Surface", 《JOURNAL OF NONDESTRUCTIVE EVALUATION》 *
IGOR JOVANˇCEVI´C等: "3D Point Cloud Analysis for Detection and Characterization of Defects on Airplane Exterior Surface", 《JOURNAL OF NONDESTRUCTIVE EVALUATION》, vol. 36, no. 74, 17 October 2017 (2017-10-17), pages 1 - 17, XP036368940, DOI: 10.1007/s10921-017-0453-1 *
WEI HUANG AND RADOVAN KOVACEVIC: "A Laser-Based Vision System for Weld Quality Inspection", 《SENSORS》 *
WEI HUANG AND RADOVAN KOVACEVIC: "A Laser-Based Vision System for Weld Quality Inspection", 《SENSORS》, vol. 11, no. 1, 6 January 2011 (2011-01-06), pages 506 - 521 *
严成: "基于T-Scan的飞机蒙皮对缝测量与数据处理", 《中国优秀硕士学位论文全文数据库 工程科技Ⅱ辑》 *
严成: "基于T-Scan的飞机蒙皮对缝测量与数据处理", 《中国优秀硕士学位论文全文数据库 工程科技Ⅱ辑》, no. 3, 15 March 2018 (2018-03-15), pages 031 - 386 *
吴兴江: "基于激光的便携式飞机装配接缝质量检测仪及应用", 《计测技术》 *
吴兴江: "基于激光的便携式飞机装配接缝质量检测仪及应用", 《计测技术》, vol. 31, no. 5, 28 October 2011 (2011-10-28), pages 22 - 26 *
李康等: "基于无人机的大场景序列图像自动采集和三维建模", 《西北大学学报(自然科学版)》, vol. 47, no. 1, 28 February 2017 (2017-02-28), pages 30 - 37 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2023142608A1 (en) * 2022-01-26 2023-08-03 上海飞机制造有限公司 System and method for obtaining aircraft profile

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