CN106556395A - A kind of air navigation aid of the single camera vision system based on quaternary number - Google Patents

A kind of air navigation aid of the single camera vision system based on quaternary number Download PDF

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Publication number
CN106556395A
CN106556395A CN201611010993.6A CN201611010993A CN106556395A CN 106556395 A CN106556395 A CN 106556395A CN 201611010993 A CN201611010993 A CN 201611010993A CN 106556395 A CN106556395 A CN 106556395A
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directions
degree
point
turn
quaternary number
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鲍泓
仝小露
娄海涛
刘元盛
员娇娇
权潇
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Beijing Union University
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Beijing Union University
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/26Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 specially adapted for navigation in a road network

Abstract

The present invention discloses a kind of air navigation aid of the single camera vision system based on quaternary number, including:Step 1, constructing environment map:Step 2, preservation map datum and tracing point coordinate information;Step 3, loading map and track point coordinates calculate corner β according to yaw angle θ, and the direction of step 4, the angle beta obtained according to step 3 and corner sends a command to vehicle bottom control.Using technical scheme, the navigation of the single camera vision system based on quaternary number on the ROS platforms under linux system is realized, research cost is reduced.

Description

A kind of air navigation aid of the single camera vision system based on quaternary number
Technical field
The invention belongs to the unmanned cruiser independent navigation field of low speed, is related to a kind of merely using room in monocular cam room Outside fix and the method for navigation.
Background technology
The unmanned intelligent vehicle that China is researching and developing just, in the middle of like a raging fire carrying out, has attracted countless colleges and universities, section Grind the extensive concern of mechanism's research worker and automobile vendor.The working environment of low speed patrol intelligent vehicle patrol is zoo, dynamic In thing garden, vegetation is grown prosperity, and it is weaker that Jing part of detecting patrol section receives gps signal, it is impossible to is advanced according to GPS navigation vehicle.Cause This, carries out map structuring using sensor acquisition external information and navigation is particularly important.SLAM problems are in driving intelligent in recent years Car field is constantly subjected to the extensive concern of research worker.The sensor that it can utilize robot self-contained sets up the environment being incremented by Map, then realizes self poisoning by building map, without the need for any external reference systems (such as:GPS) and other sensors, With potential economic worth and being widely applied prospect.
For in the research of unmanned intelligent vehicle, map structuring and positioning are vehicle DAS (Driver Assistant System)s and unmanned The key technology in intelligent vehicle field.What the various algorithms for SLAM had developed at present is more and more ripe, mainly uses one Plant or multiple sensors information allows the robot to independently build figure positioning.Its method for solving is divided into the side based on Kalman filtering Method, the method optimized based on particle filter method and based on figure.Method based on figure optimization is as which is in extensive environment It is excellent to build figure performance, become at present the main method of research both at home and abroad.But at present for the research of this respect is only limited to determine Position and figure is built, be substantially the navigation of joint other sensors information for navigation feature, such as ultrasonic sensor, Laser Measuring Distance meter, radar, stereoscopic vision etc., for the use of multisensor increased Financial cost.
The content of the invention
For the problems referred to above that prior art is present, the present invention is proposed on a kind of ROS platforms under linux system Air navigation aid based on the single camera vision system of quaternary number.Firstly, it is necessary to realize the map structuring based on key frame, it is critical only that The trajectory coordinates information of the image center that preservation is built during figure;Secondly tracing point coordinate information is carried out according to certain rule Overstocked point screening;Then map and track point coordinate data are reloaded;Last calculating according to navigational portions algorithm of the present invention is worked as Previous frame coordinate points complete navigation feature to the traveling angle and route of the next position image center point coordinates.
For achieving the above object, the present invention is adopted the following technical scheme that:
A kind of air navigation aid of the single camera vision system based on quaternary number, comprises the following steps:
Step 1, constructing environment map, comprise the following steps:
1) carry out camera calibration;
2) photographic head is fixed to into right ahead;
3) input picture is transformed into into greyscale color space from RGB color;
4) feature extraction and matching is carried out to image;
5) map initialization;
6) closed loop detection and reorientation;
7) obtain Current camera pose, calculate quaternary number be transformed into 180 degree to 180 degree scope Eulerian angles ψ, θ,It is described ψ、θ、Respectively about the z axis, the anglec of rotation of Y-axis, X-axis, yaw angle θ are the angle of present frame;
Step 2, preservation map datum and tracing point coordinate information;
Step 3, loading map and track point coordinates calculate corner β according to yaw angle θ,
The direction of step 4, the angle beta obtained according to step 3 and corner, sends a command to vehicle bottom control.
Preferably, ψ, θ andScope is -90 degree to 90 degree, and correspondence solution formula is:
When θ scopes for -180 degree to+180 degree when, correspondence solution part formula is:
Preferably, the process that step 3 calculates corner β is:
If (dx, dy), (gx, gy) are respectively current point and will reach point coordinates, present frame angle is θ, if current point and Impact point line with x-axis angle isScope is 0 to 90 degree;β is corner, and bottom Body Control is from left to right 180 degree is arrived for 0;γ judges angle for middle decision-making level, and different target point has different values from current point position relationship.Current location When being divided into following four kinds of different situations with aiming spot relative position relation:
When the direction of motion is E to F, i.e., as (dx>gx&&dy<When gy):
If 0=<θ<=90 i.e. L1 directions when, then left-hand rotation β=| θ |+90- α, if -180=<θ<- 90 i.e. L4 directions when, then Right-hand rotation β=| θ | -90+ α, if -90=<θ<0 i.e. L2 and L3 directions when, then judge γ=90- α-| θ |, if γ>0 i.e. L2 directions are then Left-hand rotation β=γ, otherwise i.e. then turn right β=- γ in L3 directions;
When the direction of motion is that F ' arrives E ', i.e., as (dx<gx&&dy>When gy):
If 0=<θ<=90 i.e. L1 directions when, then right-hand rotation β=90- | θ |+α, if -180=<θ<=-90 i.e. L4 directions when, Then left-hand rotation β=180- | θ |+90- α, if 90<θ<=180 i.e. L2 and L3 directions when, then judge γ=90- α-(180- | θ |), if γ>0 i.e. L3 directions when then turn left that otherwise i.e. then turn right β=γ β=- γ in L2 directions;
When direction of motion P is to Q, i.e., as (dx<gx&&dy<When gy):
If -90=<θ<=0 i.e. L1 directions when, then right-hand rotation β=90+ | θ |-α, if 90=<θ<=180 i.e. L4 directions when, then Left-hand rotation β=| θ | -90+ α, if 0<θ<90 i.e. L2 and L3 directions when, then judge γ=90- α-| θ |, if γ>0 i.e. L2 directions when then Right-hand rotation β=γ is otherwise that L3 directions are then turned left β=- γ;
When the direction of motion is that Q ' arrives P ', i.e., as (dx>gx&&dy>When gy):
If -90=<θ<=0 i.e. L1 directions when, then left-hand rotation β=90- | θ |+α, if 90=<θ<=180 i.e. L4 directions when, then Right-hand rotation β=180- | θ |+90- α, if -180=<θ<- 90 i.e. L2 and L3 directions when, then judge γ=90+ α-| θ |, if γ>0 is Then turning left during L2 directions, otherwise i.e. then turn right β=γ β=- γ in L3 directions;
The present invention is as using above technical scheme, which has advantages below:1st, the present invention utilizes monocular vision SLAM systems System calculates image center pose coordinate during figure is built as driving trace point coordinates.2nd, the present invention proposes that a kind of utilization builds figure Image center pose after rear monocular track point coordinates and reorientation calculates vehicle using quaternary number and the conversion of Eulerian angles Angle data is navigated, and the method is not used any other external sensor, is completed navigation using photographic head merely, is reduced Research cost, has potential using value.
Description of the drawings
Fig. 1 is method flow diagram involved in the present invention;
Fig. 2 is the chessboard figure that Zhang Zhengyou standardizitions are used;
Fig. 3 is FAST Corner Detection schematic diagrams;
Fig. 4 is the closed loop overhaul flow chart based on bag of words;
Fig. 5 is yaw angle calculation flow chart;
Fig. 6 is the corresponding Eulerian angles broken line graph of each frame;
Fig. 7 is corner direction calculating schematic diagram;
Fig. 8 is the navigation path result figure under unencryption map;
Fig. 9 is Fig. 8 trajector deviation analysis charts;
Figure 10 is the navigation path result figure under encryption map;
Figure 11 is Figure 10 trajector deviation analysis charts;
The GPS track comparison diagram that Figure 12 is built under figure and navigation for image;
Table 1 turns Eulerian angles value result for different quaternary numbers;
Table 2 is corner decision table.
Specific embodiment
The invention will be further described with reference to the accompanying drawings and examples.
The flow chart of the method for the invention is as shown in figure 1, comprise the following steps:
Step 1, map structuring
Step 1.1, camera calibration
Camera calibration method adopts Zhang Zhengyou camera calibration methods:If Fig. 2 lineaments are 7 black and white for taking advantage of that 7 length of sides are 0.02m Alternate grid.7 plane chessboard, hand-held chessboard is taken advantage of to obtain 30 multiple checkerboard images at various orientations camera alignment 7, i.e., The intrinsic parameter and distortion parameter of camera can be calculated.
Ultimate principle is as follows:
Wherein, Intrinsic Matrixes of the k for camera, [X Y 1]TFor the homogeneous coordinates put on plane chessboard, [u v 1]TPosition chess Homogeneous coordinates of the spot projection to corresponding point on the plane of delineation, [r on disk1 r2 r3] and t be the rotation under camera coordinates system respectively Turn and translation vector, k [r1 r2T] for homography matrix H.According to matrix solving method, when picture number is more than or equal to 3, k can To obtain unique solution.
Photographic head is fixed on right ahead by step 1.2, it is ensured that during map structuring and when navigating, position and direction are protected Hold constant.
Input picture is transformed into greyscale color space, conversion formula from RGB color by step 1.3:Gray=R* 0.299+G*0.587+B*0.114;
Step 1.4, carries out feature extraction and matching to image
Feature extraction and matching adopts ORB (Oriented Brief) method, detects initially with FAST-12 algorithms Characteristic point is as shown in Figure 3:
Gray values of the I (x) for any point on circumference, gray scales of the I (p) for the center of circle, εdFor the threshold value of gray value differences, if greatly Then think that p is a characteristic point in threshold value.
Then it is sub to calculate the description of a characteristic point using BRIEF algorithms:Select around characteristic point after smoothed image One Patch, by a kind of selected method picking out 256 points pair in this Patch.Then for each point Compare its brightness value to (p, q), if I (p)>I (q) then this to generate one in two-value string value be 1, if I (p) <I (q), then the value corresponded in two-value string is -1, is otherwise 0.All 256 points pair, between being all compared, then obtain one The binary string of individual 256 length, represents description using binary number string.
Step 1.5, map initialization
The map initialization of monocular SLAM is carried out, the first segment distance of dollying obtains two key frames, by key frame Between characteristic matching calculate Homography models or Fundamental models and obtain initialized cartographic model, The computational methods of Homography models are normalized DLT, and the computational methods of Fundamental matrix are normalized 8points.In visual odometry part, first to two width picture frame PK-2、PK-1Carry out feature extraction and Match somebody with somebody;Then trigonometric ratio PK-2、PK-1Feature, to new image PKFeature extraction and PK-1Characteristic matching;Finally by employing Camera pose is estimated in matching of the PnP algorithms from 3D to 2D, is optimized by Bundle Adjustment, can be excellent using figure Chemical industry tool g2o carries out map optimization.The model of PnP (Perspective-n-Point) problem is:
Attitudes of the R for camera, calibration matrixes of the C for camera, (u, v) is two-dimensional pixel coordinate, and (x, y, z) is three-dimensional coordinate Coordinate i.e. under world coordinate system.
Step 1.6, closed loop detection and reorientation
Present frame is converted into image bag of words, image data base is then retrieved, view data bag of words storehouse part is using classical DBoW2 bag of words storehouse model, by the similar scene for calculating the image that is input into and model in bag of words storehouse in monocular cam, be complete It is as shown in Figure 4 that key frame is searched in office's reorientation.The insertion standard of key frame is when the characteristic point cloud that new frame is detected is closed with reference When key frame characteristic point cloud gap is less than 90%, determines that present frame is key frame, preserve into map datum.It is special that we calculate ORB Seek peace each key frame map cloud point corresponding relation, RANSAC iterative calculation is then performed to each key frame, is calculated with PnP Method is found out the i.e. camera pose quaternary number in position of the camera in world coordinate system and is represented.Quaternary number is a scalar (w) and The combination of individual 3D vectors (x, y, z).The definition of quaternary number:
Q=[w x y z]T
|q|2=w2+x2+y2+z2=1
Step 1.7, obtains Current camera pose
The posture information of the Current camera that acquisition is calculated by PnP+RANSAC, that is, represent the quaternary of three dimensions rotation After number.Quaternary number is transformed into into Eulerian angles, ψ, θ,Respectively about the z axis, the anglec of rotation of Y-axis, X-axis, yaw angle θ are current The angle of frame.Generally ψ, θ of definition andScope is -90 degree to 90 degree, and correspondence solution formula is:
Eulerian angles turn quaternary number formula:
Driftage angle range can not uniquely represent current positional information when being -90 to 90 degree, it is therefore desirable to by yaw angle model Enclose expand to -180 degree is to 180 degree.When θ scopes for -180 degree to+180 degree when correspondence solution part formula it is as follows.It is only right For yaw angle is sought whole algorithm with reference to 1,2,3 its flow chart of formula as shown in figure 5, table 1 turns Eulerian angles for different quaternary numbers Value result, Fig. 6 are the Eulerian angles of correspondence each frame position when rotation takes two turns.
1 quaternary number of table turns the conversion output contrast (unit of Eulerian angles:Degree)
Present frame quaternary number True Eulerian angles θ This algorithm is exported
(0.0297,0.9994,0.0152,0.0046) -180 -180
(- 0.0275, -0.8640,0.0126,0.5025) -120 -120
(- 0.0214, -0.5709,0.0086,0.8207) -70 -70
(0.3214,0.117,0.3214,0.883) 0 0
(0.0049,0.5010, -0.0087,0.8654) 60 60
(0.0190,0.8360, -0.1951,0.5124) 120 120
(0.0348,0.9713, -0.2353, -0.0075) 180 180
Step 2, preserves map datum and tracing point coordinate information
By cloud data (three-dimensional coordinate, ORB Feature Descriptors in world coordinate system), key by the way of data flow Frame data (camera posture information) save as .bin formatted files, and the data that point coordinates information includes x and z directions are saved in In txt file.
Step 3, loading map and track point coordinates calculate corner
Step 3.1 loads the map built up, and execution resets bit function, calculates Current camera posture information with this.
Can be derived in the navigation algorithm based on camera tracing point according to the navigation algorithm based on GPS.Propose accordingly to be based on The navigation decision making algorithm of vision SLAM, as shown in Figure 7.Algorithm is divided into two parts:Choose pre- described point algorithm, calculate corner number of degrees β Algorithm.
Step 3.2 tracing point is encrypted, and is chosen pre- described point and is filtered pretreatment to pre- described point:Obtain by key frame approach Tracing point data division place can be than sparse, it is therefore desirable to carries out next step operation after being encrypted again.Using average The method of filtering is to sparse point encryption:
When choosing pre- described point, if current point is B points, according to search in the threshold value 0.35 before and after method a little, search Institute of the rope apart from all distances of B points in the range of 0.35 a little, is saved in array M [n]={ A, B, C, D ... }, then logarithm Group sorted from small to large sort (M, M+n) choose M [n] be pre- described point.For different map track datas has different Pre- described point selected threshold, needs carry out parameter selection according to actual map datum.For the non-starting point of closed path and terminal position Put:For the closed path of 200 tracing points:Initial piont mark 0, terminal label 199, after the point for searching is sorted most Big value chooses 0 point of label when being 199 be that next impact point is pre- described point, it is desirable to which 0 point to 199 dot spacings from great-than search threshold Value.
Step 3.3 calculates corner:Calculate corner number of degrees β algorithms:Propose two kinds of calculating corner algorithms.(if dx, dy), (gx, gy) is respectively current point and will reach point coordinates:
By angle, θ before Fig. 7 under the coordinate system of scope ± 180 °, if current point and impact point line with x-axis angle areScope is 0 to 90 degree;β is corner, and bottom Body Control is from left to right 0 to 180 degree;γ determines for centre Plan layer judges angle, and different target point has different values from current point position relationship.Corner decision table of the table 2 for correspondence Fig. 6, currently Position and aiming spot relative position relation are divided into four kinds of different situations shown in table.
2 corner decision table of table
When the direction of motion is E to F, i.e., as (dx>gx&&dy<When gy):
If 0=<θ<=90 i.e. L1 directions when, then left-hand rotation β=| θ |+90- α, if -180=<θ<- 90 i.e. L4 directions when, then Right-hand rotation β=| θ | -90+ α, if -90=<θ<0 i.e. L2 and L3 directions when, then judge γ=90- α-| θ |, if γ>0 i.e. L2 directions are then Left-hand rotation β=γ, otherwise i.e. then turn right β=- γ in L3 directions;
When the direction of motion is that F ' arrives E ', i.e., as (dx<gx&&dy>When gy):
If 0=<θ<=90 i.e. L1 directions when, then right-hand rotation β=90- | θ |+α, if -180=<θ<=-90 i.e. L4 directions when, Then left-hand rotation β=180- | θ |+90- α, if 90<θ<=180 i.e. L2 and L3 directions when, then judge γ=90- α-(180- | θ |), if γ>0 i.e. L3 directions when then turn left that otherwise i.e. then turn right β=γ β=- γ in L2 directions;
When direction of motion P is to Q, i.e., as (dx<gx&&dy<When gy):
If -90=<θ<=0 i.e. L1 directions when, then right-hand rotation β=90+ | θ |-α, if 90=<θ<=180 i.e. L4 directions when, then Left-hand rotation β=| θ | -90+ α, if 0<θ<90 i.e. L2 and L3 directions when, then judge γ=90- α-| θ |, if γ>0 i.e. L2 directions when then Right-hand rotation β=γ is otherwise that L3 directions are then turned left β=- γ;
When the direction of motion is that Q ' arrives P ', i.e., as (dx>gx&&dy>When gy):
If -90=<θ<=0 i.e. L1 directions when, then left-hand rotation β=90- | θ |+α, if 90=<θ<=180 i.e. L4 directions when, then Right-hand rotation β=180- | θ |+90- α, if -180=<θ<- 90 i.e. L2 and L3 directions when, then judge γ=90+ α-| θ |, if γ>0 is Then turning left during L2 directions, otherwise i.e. then turn right β=γ β=- γ in L3 directions;
Step 4, the angle beta obtained according to step 3 and the direction of corner, send a command to vehicle bottom control.
Conclusion:Fig. 8 is original camera trace information and independent navigation trace information, wherein it is not pass through to build figure track The data of encryption.Analysis finds that leading line and ground figure line are essentially coincided.The navigation path deviation data of concrete analysis Fig. 8 As shown in figure 9, maximum deviation is 0.029 about 0.1m, deviation is very little.Figure 10 is to build figure track and right through encryption The three circle navigation paths answered, Figure 11 is trajector deviation data, and trajector deviation maximum is 0.017, can be considered that route is essentially coincided. Figure 12 is during monocular vision builds figure while the gps data and the monocular vision under using said method of collection are navigated through The gps data trajectory diagram gathered in journey, is about 0.0013km at two track maximum deviations, and it is due to turning that deviation is larger herein The turning number of degrees at place are larger, and during self-navigation, turn inside diameter can be completely superposed where the turning number of degrees are little.
In sum, the present invention utilizes merely monocular cam, it is not necessary to any other external sensor, in less error In the range of realize navigation system based on monocular vision SLAM, reduce research and application cost, with potentially applying valency Value.

Claims (3)

1. a kind of air navigation aid of the single camera vision system based on quaternary number, it is characterised in that step includes:
Step 1, constructing environment map, comprise the following steps:
1) carry out camera calibration;
2) photographic head is fixed to into right ahead;
3) input picture is transformed into into greyscale color space from RGB color;
4) feature extraction and matching is carried out to image;
5) map initialization;
6) closed loop detection and reorientation;
7) obtain Current camera pose, calculate quaternary number be transformed into 180 degree to 180 degree scope Eulerian angles ψ, θ,The ψ, θ,Respectively about the z axis, the anglec of rotation of Y-axis, X-axis, yaw angle θ are the angle of present frame;
Step 2, preservation map datum and tracing point coordinate information;
Step 3, loading map and track point coordinates calculate corner β according to yaw angle θ,
The direction of step 4, the angle beta obtained according to step 3 and corner, sends a command to vehicle bottom control.
2. the air navigation aid of the single camera vision system based on quaternary number as claimed in claim 1, it is characterised in that ψ, θ andModel Enclose be -90 degree to 90 degree, correspondingly solution formula is:
When θ scopes for -180 degree to+180 degree when, correspondence solution part formula is:
3. the air navigation aid of the single camera vision system based on quaternary number as claimed in claim 2, it is characterised in that step 3 is counted Calculate corner β process be:
If (dx, dy), (gx, gy) are respectively current point and will reach point coordinates, if current point and impact point line and x-axis angle ForScope is 0 to 90 degree;β is corner, and bottom Body Control is from left to right 0 to 180 degree;γ is centre Decision-making level judges angle, and different target point has different values from current point position relationship.Current location and aiming spot are with respect to position When the relation of putting is divided into following four kinds of different situations:
When the direction of motion is E to F, i.e., as (dx>gx&&dy<When gy):
If 0=<θ<=90 i.e. L1 directions when, then left-hand rotation β=| θ |+90- α, if -180=<θ<- 90 i.e. L4 directions when, then turn right β =| θ | -90+ α, if -90=<θ<0 i.e. L2 and L3 directions when, then judge γ=90- α-| θ |, if γ>Then turn left β in 0 i.e. L2 directions =γ, otherwise i.e. then turn right β=- γ in L3 directions;
When the direction of motion is that F ' arrives E ', i.e., as (dx<gx&&dy>When gy):
If 0=<θ<=90 i.e. L1 directions when, then right-hand rotation β=90- | θ |+α, if -180=<θ<=-90 i.e. L4 directions when, then it is left Turn β=180- | θ |+90- α, if 90<θ<=180 i.e. L2 and L3 directions when, then judge γ=90- α-(180- | θ |), if γ>0 I.e. L3 directions when then turn left that otherwise i.e. then turn right β=γ β=- γ in L2 directions;
When direction of motion P is to Q, i.e., as (dx<gx&&dy<When gy):
If -90=<θ<=0 i.e. L1 directions when, then right-hand rotation β=90+ | θ |-α, if 90=<θ<=180 i.e. L4 directions when, then turn left β=| θ | -90+ α, if 0<θ<90 i.e. L2 and L3 directions when, then judge γ=90- α-| θ |, if γ>0 i.e. L2 directions when then turn right β =γ is otherwise that L3 directions are then turned left β=- γ;
When the direction of motion is that Q ' arrives P ', i.e., as (dx>gx&&dy>When gy):
If -90=<θ<=0 i.e. L1 directions when, then left-hand rotation β=90- | θ |+α, if 90=<θ<=180 i.e. L4 directions when, then turn right β=180- | θ |+90- α, if -180=<θ<- 90 i.e. L2 and L3 directions when, then judge γ=90+ α-| θ |, if γ>0 i.e. L2 side To when then turn left that otherwise i.e. then turn right β=γ β=- γ in L3 directions.
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CN107369181A (en) * 2017-06-13 2017-11-21 华南理工大学 Cloud data collection and processing method based on bi-processor architecture
CN107369181B (en) * 2017-06-13 2020-12-22 华南理工大学 Point cloud data acquisition and processing method based on dual-processor structure
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CN109900272B (en) * 2019-02-25 2021-07-13 浙江大学 Visual positioning and mapping method and device and electronic equipment
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CN111798574A (en) * 2020-06-11 2020-10-20 广州恒沙数字科技有限公司 Corner positioning method for three-dimensional field

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Application publication date: 20170405