CN109901139A - Laser radar scaling method, device, equipment and storage medium - Google Patents

Laser radar scaling method, device, equipment and storage medium Download PDF

Info

Publication number
CN109901139A
CN109901139A CN201811623241.6A CN201811623241A CN109901139A CN 109901139 A CN109901139 A CN 109901139A CN 201811623241 A CN201811623241 A CN 201811623241A CN 109901139 A CN109901139 A CN 109901139A
Authority
CN
China
Prior art keywords
laser radar
data
point cloud
cloud data
calibration
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN201811623241.6A
Other languages
Chinese (zh)
Other versions
CN109901139B (en
Inventor
冯荻
雷宇苍
杜杭肯
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.)
Wenyuan Zhixing Co Ltd
Original Assignee
Wenyuan Zhixing 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 Wenyuan Zhixing Co Ltd filed Critical Wenyuan Zhixing Co Ltd
Priority to CN201811623241.6A priority Critical patent/CN109901139B/en
Publication of CN109901139A publication Critical patent/CN109901139A/en
Application granted granted Critical
Publication of CN109901139B publication Critical patent/CN109901139B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02ATECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
    • Y02A90/00Technologies having an indirect contribution to adaptation to climate change
    • Y02A90/10Information and communication technologies [ICT] supporting adaptation to climate change, e.g. for weather forecasting or climate simulation

Landscapes

  • Navigation (AREA)
  • Optical Radar Systems And Details Thereof (AREA)

Abstract

The present invention relates to a kind of laser radar scaling method, device, equipment and storage medium, terminal obtains the point cloud data and high data of laser radar to be calibrated in preset calibration scene;And obtain the corresponding map datum of calibration scene;And then according to the point cloud data of laser radar to be calibrated, high data and map datum, position transformational relation is obtained by calibration algorithm;And then according to above-mentioned position transformational relation, the calibration result of laser radar is determined.In the application, terminal is according to the point cloud data of laser radar to be calibrated, high data and map datum, obtain the position transformational relation of laser radar and inertial navigation system automatically by calibration algorithm, and then calibration result is determined according to position transformational relation, so that the calibration result for obtaining laser radar is automatically obtained by calibration algorithm, the process that hand dipping obtains the calibration result of laser radar is avoided, and then improves the calibration efficiency of laser radar.

Description

Laser radar scaling method, device, equipment and storage medium
Technical field
The present invention relates to field of computer technology, more particularly to a kind of laser radar scaling method, device, equipment and Storage medium.
Background technique
With the development of unmanned technology, the location information of vehicle periphery is usually obtained using onboard sensor, into And the information detected according to sensor, the vehicle of automatic Pilot is planned, decision or control.
In general, onboard sensor will use multiple sensors to obtain the location information of vehicle periphery.But multiple sensings It has a certain difference, is needed by by multiple sensors between relative pose (including relative position and direction) between device Relative pose is demarcated, so that the location information of the collected vehicle periphery of multiple sensors is unified to the same coordinate system Under, and then according to the location information under the same coordinate system, Vehicular automatic driving is planned, decision or control.It is above-mentioned The process of calibration refers to obtaining the process of the relative position between multiple sensors.Existing laser radar scaling method is usual Physical measurement obtains the relative position of laser radar and other sensors by hand, and matching is marked depending on the relative position, To realize the relative pose between laser radar and other sensors.
Using the above method, laser radar is demarcated by manual physical measurement, especially for high-volume laser Low efficiency is demarcated in the calibration of radar.
Summary of the invention
Based on this, it is necessary to aiming at the problem that laser radar demarcates low efficiency, provide a kind of laser radar scaling method, dress It sets, equipment and storage medium.
In a first aspect, a kind of laser radar scaling method, which comprises
In preset calibration scene, the point cloud data and high data of laser radar to be calibrated are obtained;Institute Stating in calibration scene has target object of reference;
Obtain the corresponding map datum of the calibration scene;
According to the point cloud data of the laser radar to be calibrated, the high data and the map datum, The position transformational relation of the laser radar and the inertial navigation system is obtained by calibration algorithm;The calibration algorithm is used for After the point cloud data and the map datum are carried out coordinate system matching, matching result and high data are converted For the data under same coordinate system;
According to the position transformational relation, the calibration result of laser radar is determined.
It is described in preset calibration scene in one of the embodiments, obtain the point cloud number of laser radar to be calibrated According to and high data, comprising:
According to data collecting rule, in preset calibration scene, the multiframe point cloud of laser radar to be calibrated is obtained respectively The multiframe high data of data and inertial navigation system.
The point cloud data according to the laser radar to be calibrated, the inertial navigation in one of the embodiments, System data and the map datum are turned by the position that calibration algorithm obtains the laser radar and the inertial navigation system Change relationship, comprising:
The multiframe point cloud data is matched under the corresponding coordinate system of the map datum, multiframe point map cloud number is obtained According to;
The multiframe point map cloud data are converted under the corresponding coordinate system of the multiframe high data Point cloud data obtains the position transformational relation of the laser radar and the inertial navigation system.
It is described in one of the embodiments, that the multiframe point cloud data is matched to the corresponding coordinate of the map datum Under system, multiframe map point cloud data is obtained, comprising:
The point cloud data is matched under the corresponding coordinate system of the map datum by cloud algorithm, obtains point map Cloud data;Described cloud algorithm includes ICP algorithm, and/or, NDT algorithm.
It is described in one of the embodiments, that the multiframe point map cloud data are converted into multiframe inertial navigation system Point cloud data under the corresponding coordinate system of data of uniting, the position conversion for obtaining the laser radar and the inertial navigation system are closed System, comprising:
According to the multiframe inertial navigation data and the multiple relative pose equations of multiframe point map cloud data list; Wherein, the high data in a frame map point cloud data and same frame constitutes one group of data, every group of data corresponding one A relative pose equation;
According to each relative pose equation and the corresponding one group of data of the relative pose equation, the opposite position is calculated Position conversion parameter in appearance equation, to obtain multiple position conversion parameters;
The position transformational relation is determined according to multiple position conversion parameters and multiple relative pose equations.
It is described in one of the embodiments, to determine institute according to multiple position conversion parameters and multiple relative pose equations Rheme sets transformational relation, comprising:
Multiple relative pose equations are added up using least square method, obtain target relative pose equation;
Multiple relative position conversion parameters are concluded by enumeration, obtains and obtains target position conversion parameter;
Target position conversion parameter is substituted into the target relative pose equation, obtains the position transformational relation.
It is described in one of the embodiments, that the calibration result of laser radar is determined according to the position transformational relation, packet It includes:
The position transformational relation is determined as to the calibration result of the laser radar;
Alternatively,
The position transformational relation is visualized, and the result after visualization is determined as to the mark of the laser radar Determine result.
The target object of reference is the letter so that the laser radar and inertial navigation system in one of the embodiments, After number by the target object of reference, reflected signal strength is greater than the object of reference of preset threshold.
The preset calibration scene is according to the laser radar, the inertial navigation in one of the embodiments, The scene that the type of system and the type of the target object of reference determine.
Second aspect, a kind of laser radar caliberating device, described device include:
First obtains module, in preset calibration scene, obtaining the point cloud data of laser radar to be calibrated and being used to Property guidance system data;There is target object of reference in the calibration scene;
Second obtains module, for obtaining the corresponding map datum of the calibration scene;
Conversion module, for according to the point cloud data of the laser radar to be calibrated, the high data and The map datum is closed by the position conversion that the first calibration algorithm obtains the laser radar and the inertial navigation system System;After first calibration algorithm is used to the point cloud data and the map datum carrying out coordinate system matching, matching is tied Fruit and high data are converted to the data under same coordinate system;
Demarcating module, for determining the calibration result of laser radar according to the position transformational relation.
The third aspect, a kind of computer equipment, including memory and processor, the memory are stored with computer journey Sequence, the processor execute method and step described in above-mentioned laser radar scaling method.
Fourth aspect, a kind of computer readable storage medium are stored thereon with computer program, the computer program quilt Processor realizes method and step described in above-mentioned laser radar scaling method when executing.
Above-mentioned laser radar scaling method, device, equipment and storage medium, terminal obtain in preset calibration scene The point cloud data and high data of laser radar to be calibrated, wherein there is target object of reference in calibration scene;And it obtains Take the corresponding map datum of calibration scene;And then according to the point cloud data of laser radar to be calibrated, high data and Map datum, the position transformational relation of laser radar and inertial navigation system is obtained by calibration algorithm, and above-mentioned calibration algorithm is used After point cloud data and map datum are carried out coordinate system matching, matching result is converted to high data identical Data under coordinate system;And then according to position transformational relation, the calibration result of laser radar is determined.In the application, terminal according to Point cloud data, high data and the map datum of laser radar to be calibrated, obtain laser by calibration algorithm automatically The position transformational relation of radar and inertial navigation system, and then automatically determine according to position transformational relation the calibration knot of laser radar Fruit avoids the process that hand dipping obtains the calibration result of laser radar, and then improves the calibration efficiency of laser radar.
Detailed description of the invention
Fig. 1 is the schematic diagram for the laser radar Analysis environment that one embodiment provides;
Fig. 2 is the flow diagram of laser radar scaling method in one embodiment;
Fig. 3 is the flow diagram of laser radar scaling method in another embodiment;
Fig. 4 is the flow diagram of laser radar scaling method in another embodiment;
Fig. 5 is the flow diagram of laser radar scaling method in another embodiment;
Fig. 6 is the flow diagram of laser radar scaling method in another embodiment;
Fig. 7 is the structural schematic diagram for the laser radar caliberating device that one embodiment provides;
Fig. 8 is the structural schematic diagram for the laser radar caliberating device that another embodiment provides;
Fig. 9 is the structural schematic diagram for the laser radar caliberating device that another embodiment provides;
Figure 10 is the internal structure chart for the calculating knot equipment that one embodiment provides.
Specific embodiment
With the development of unmanned technology, the location information of vehicle periphery is usually obtained using onboard sensor, into And the information detected according to sensor, automatic driving vehicle is planned, decision or control.In general, onboard sensor Multiple sensors be will use to obtain the location information of vehicle periphery.But relative pose (including the phase between multiple sensors To position and orientation) between have a certain difference, need by demarcating the relative pose of multiple sensors, so that more Under the location information unification to the same coordinate system of a collected vehicle periphery of sensor, and then according in the same coordinate system Lower location information is planned the vehicle of automatic Pilot, decision or control.The process of above-mentioned calibration refers to obtaining multiple The process of relative position between sensor.Laser radar scaling method, device, equipment and storage medium provided by the present application, The problem of aiming to solve the problem that calibration low efficiency.
It should be noted that the method for laser radar calibration provided by the embodiments of the present application, can be applied not only to nobody In the scene of driving, it can also be applied in the scene of robot navigation, the embodiment of the present application does not do specific application scenarios Limitation.
Laser radar scaling method provided in this embodiment, can be adapted in application environment as shown in Figure 1.Such as Fig. 1 Shown, laser radar 10 and inertial navigation system 20 may be mounted at any position of vehicle, pass through acquisition by calibration algorithm Relative position information between laser radar 10 and inertial navigation system 20, to determine the calibration result of laser radar.
It should be noted that laser radar scaling method provided by the embodiments of the present application, executing subject can be laser The device of Radar Calibration, the device can be implemented as laser radar mark by way of software, hardware or software and hardware combining Fixed computer equipment it is some or all of.
To keep the purposes, technical schemes and advantages of the embodiment of the present application clearer, below in conjunction with the embodiment of the present application In attached drawing, the technical scheme in the embodiment of the application is clearly and completely described, it is clear that described embodiment is Some embodiments of the present application, instead of all the embodiments.
Fig. 2 is the flow diagram of laser radar scaling method in one embodiment.What is involved is pass through mark for the present embodiment Determine the position transformational relation that algorithm obtains laser radar and inertial navigation system automatically, and then automatic according to the position transformational relation Determine the detailed process of the calibration result of laser radar.As shown in Fig. 2, method includes the following steps:
S101, in preset calibration scene, obtain the point cloud data and inertial navigation system number of laser radar to be calibrated According to;Demarcating has target object of reference in scene.
Specifically, target object of reference can be the object of reference for making laser radar form good point cloud imaging characteristic, target ginseng It can be an object of reference according to object, be also possible to multiple objects of reference, the embodiment of the present application is without limitation.For example, target is joined It can be a straight, continuous wall or road tooth according to object.Preset calibration scene can be comprising target object of reference, and can make The scene that inertial navigation system normally positions is obtained, can be the outdoor crossroad that roadside has continuous, straight metope;Roadside L shape route with continuous, straight metope;There is the outdoor crossroad neatly built in roadside;There is the L shape road neatly built in roadside Line;There are non-perpendicular crossing or the L shape route for the typical target that meets the requirements in roadside;There is the parking lot for the typical target that meets the requirements in roadside Or the combine scenes that any one of vacant lot or several scenes are formed.For example, it is one that preset calibration scene, which may include, Straight, continuous road tooth, and inertial navigation system can normal connecting global positioning system (Global Positioning System, GPS), the scene that inertial navigation system is normally positioned.Point cloud data can be laser radar signal irradiation When to body surface, the reflection signal of the information such as carrying orientation, distance for being reflected may include multiple points in point cloud data The strength information of location information and corresponding reflection laser radar signal.
In preset calibration scene, the process of the point cloud data of laser radar specifically is being obtained, can be by swashing Optical radar sends radar signal, the point cloud data of acquisition to target object of reference;It is also possible to through laser radar to target reference Object sends laser radar signal, after the reflection signal of acquisition, first carries out a cloud cluster operation to the reflection signal, it is flat to obtain space Equal point cloud data, and then noise reduction process, the point cloud data of acquisition are carried out to the point cloud data of space average;The embodiment of the present application It is without limitation.
S102, the corresponding map datum of calibration scene is obtained.
Specifically, the corresponding map datum of calibration scene can be high-precision map datum, which may include more The location information of a point and corresponding image information.In the corresponding map datum of specific acquisition calibration scene, can be By the corresponding map datum of calibration scene stored in server download server, be also possible to by camera or other Device obtains the corresponding map datum of calibration scene in real time, and the embodiment of the present application is without limitation.
S103, according to the point cloud data of laser radar to be calibrated, high data and map datum, pass through calibration The position transformational relation of algorithm acquisition laser radar and inertial navigation system;Calibration algorithm is used for point cloud data and map datum After carrying out coordinate system matching, matching result and high data are converted into the data under same coordinate system.
Specifically, after calibration algorithm can be used for point cloud data and map datum carrying out coordinate system matching, matching is tied Fruit and high data are converted to the data under same coordinate system, can be the point cloud number of laser radar to be calibrated According to the algorithm for being converted to the data under the corresponding coordinate system of high data, it can also be and turn high data The algorithm for turning to the data under the corresponding coordinate system of point cloud data of laser radar to be calibrated, can also be laser to be calibrated The point cloud data and high data of radar are transformed into the algorithm of the data under third party's coordinate system, the embodiment of the present application It is without limitation.Position transformational relation can be the corresponding coordinate system of laser radar to be calibrated, corresponding with inertial navigation system Coordinate system between transformational relation.
It on the basis of the above embodiments, can target reference in the point cloud data by establishing laser radar to be calibrated Transformational relation between the location information of target object of reference in the location information and high data of object, determining should Position transformational relation.The location information of target object of reference in the point cloud data for specifically establishing laser radar to be calibrated, When transformational relation between the location information of the target object of reference in high data, it can be and enumerate coordinate system and turn Equation is changed, determines position transformational relation;It is also possible to choose coordinates of targets conversion side by enumerating multiple coordinate transfer equations Journey determines position transformational relation;The embodiment of the present application is without limitation.
S104, according to position transformational relation, determine the calibration result of laser radar.
Specifically, the calibration result of laser radar can be relative position between laser radar and inertial navigation system.On On the basis of stating embodiment, specifically according to position transformational relation, during the calibration result for determining laser radar, true After having determined position transformational relation, it is alternatively possible to which position transformational relation to be determined as to the calibration result of laser radar;Alternatively, will Position transformational relation is visualized, and the result after visualization is determined as to the calibration result of laser radar;The application is implemented Example is without limitation.
Above-mentioned laser radar scaling method, terminal obtain the point cloud of laser radar to be calibrated in preset calibration scene Data and high data, wherein there is target object of reference in calibration scene;And obtain the corresponding map of calibration scene Data;And then according to the point cloud data of laser radar to be calibrated, high data and map datum, pass through calibration algorithm The position transformational relation of laser radar and inertial navigation system is obtained, above-mentioned calibration algorithm is used for point cloud data and map datum After carrying out coordinate system matching, matching result and high data are converted into the data under same coordinate system;And then root According to position transformational relation, the calibration result of laser radar is determined.In the present embodiment, terminal is according to the point cloud of laser radar to be calibrated Data, high data and map datum obtain laser radar and inertial navigation system by calibration algorithm automatically Position transformational relation, and then the calibration result of laser radar is automatically determined according to position transformational relation, it avoids hand dipping and obtains The process of the calibration result of laser radar is obtained, and then improves the calibration efficiency of laser radar.
Optionally, target object of reference is so that the signal of laser radar transmitting is by the way that after target object of reference, reflection signal is strong Degree is greater than the object of reference of preset threshold.
Specifically, target object of reference is so that the signal of laser radar transmitting is by the way that after target object of reference, reflection signal is strong Degree is greater than the object of reference of preset threshold.After preset threshold may be such that the signal of laser radar transmitting passes through target object of reference, The signal strength of the laser radar signal of reflection is greater than the minimum radar signal strength that laser radar can identify;Preset threshold is also It can be when target object of reference is multiple objects of reference, so that multiple reflection signals that laser radar is obtained by multiple objects of reference Between do not interfere with each other multiple objects of reference position setting.
Optionally, preset calibration scene is true according to the type of laser radar, inertial navigation system and target object of reference Fixed scene.
Specifically, preset calibration scene can be ambient enviroment and not cause significant signal interference to target object of reference Scene.In preset calibration scene, laser radar passes through the signal acquisition laser radar to be calibrated that target object of reference is reflected back Point cloud data.Inertial navigation system obtains the location information of the ambient enviroment in GPS signal, i.e., by connecting with GPS in real time When the corresponding location information of multiple points.For example, being the point for obtaining laser radar to be calibrated by laser signal according to laser radar Cloud data, since angle scatterer has good scattering properties, the corresponding target object of reference of laser radar to laser signal It can be angle scatterer;Inertial navigation system is to obtain high data according to reception GPS signal, therefore inertia is led Boat system needs spacious place, so that GPS signal is not by external environmental interference.In turn, can according to laser radar to be calibrated, The type of inertial navigation system and target object of reference, determining that preset calibration scene is is not pass through angle scatterer to laser radar The signal of return causes significant electromagnetic interference, and inertial navigation system is enabled accurately to receive the outdoor sports of GPS signal.
On the basis of the above embodiments, above-mentioned S101 " in preset calibration scene, obtains laser radar to be calibrated Point cloud data and high data;Demarcating has target object of reference in scene ", it can be divided by data collecting rule The multiframe point cloud data of laser radar to be calibrated and the multiframe high data of inertial navigation system are not obtained, it is above-mentioned S101 " in preset calibration scene, obtains the point cloud data and high data of laser radar to be calibrated;Calibration Field There is target object of reference in scape ", a kind of possible implementation includes: according to data collecting rule, in preset calibration scene It is interior, the multiframe point cloud data of laser radar to be calibrated and the multiframe inertial navigation system number of inertial navigation system are obtained respectively According to.
Specifically, data collecting rule can be expression by target object of reference, obtain the point cloud of laser radar to be calibrated Data, the point cloud data of acquisition multiframe laser radar to be calibrated that can be static, the acquisition multiframe for being also possible to movement wait marking Determine the point cloud data of laser radar, the embodiment of the present application is without limitation.Specifically according to data collecting rule, passing through mesh When mark object of reference obtains the point cloud data of multiframe laser radar to be calibrated respectively, it can be the carrier where laser radar, place When halted state, the point cloud data of multiframe laser radar to be calibrated is obtained;It is also possible to above-mentioned carrier in slow driving status When, obtain the point cloud data of multiframe laser radar to be calibrated;The embodiment of the present application is without limitation.Above-mentioned carrier can be certainly It is dynamic to drive vehicle, assist driving vehicle or robot, the embodiment of the present application without limitation.
Fig. 3 is the flow diagram of laser radar scaling method in another embodiment.What is involved is bases for the present embodiment The point cloud data and map datum of laser radar to be calibrated obtain map point cloud data, and then point cloud data and inertia according to the map Guidance system data obtains the detailed process of position transformational relation.As shown in figure 3, above-mentioned S103 is " according to laser radar to be calibrated Point cloud data, high data and map datum, pass through calibration algorithm and obtain laser radar and inertial navigation system Position transformational relation " a kind of possible implementation the following steps are included:
S201, multiframe point cloud data is matched under the corresponding coordinate system of map datum, obtains multiframe map point cloud data.
Specifically, map point cloud data can be to project the point cloud data of laser radar to be calibrated to map datum and correspond to Coordinate system under the point cloud data that obtains.Specifically multiframe point cloud data is matched under the corresponding coordinate system of map datum, is obtained During multiframe map point cloud data, the point cloud data of every frame laser radar to be calibrated can be matched to map datum respectively In, obtain multiframe map point cloud data;It is also possible to the point cloud number of multiframe laser radar to be calibrated that will be obtained in synchronization According to cumulative mean is carried out, so that the signal strength of each position adds up, and according to the frame of point cloud data under the synchronization Number, the point cloud data after obtaining averagely;Likewise, obtain it is multiple other when inscribe it is average after point cloud data, and then will be more Point cloud data after frame is average is matched under the corresponding coordinate system of map datum, obtains multiframe map point cloud data.
Optionally, point cloud data is matched under the corresponding coordinate system of map datum by cloud algorithm, obtains point map Cloud data;Point cloud algorithm includes ICP algorithm, and/or, NDT algorithm.
Specifically, iteration closest approach (Iterative Closest Point, ICP) algorithm can be a kind of surface fitting Algorithm, the algorithm are the point sets based on quaternary number to point set method for registering.It concentrates from measurement point and to determine that its is corresponding with regard near point After point set, the new point set with regard near point is calculated.It is iterated calculating with this method, until the target letter that residual sum of squares (RSS) is constituted Numerical value is constant, terminates iterative process.Normal distribution transform (Normal Distribution Transform, NDT) algorithm can be with Applied to the statistical model of three-dimensional point, standard optimization techniques can be used to determine optimal between two clouds Match, do not utilize the feature calculation and matching of corresponding points in registration process, match time is short.For example, can be by a cloud number Determine that it after the corresponding point set with regard near point, calculates new nearest point cloud data point set, and to upper in map datum according to concentrating The process of stating is iterated calculating, until the target function value that residual sum of squares (RSS) is constituted is constant, terminates iterative process, obtains map Point cloud data.
S202, multiframe point map cloud data are converted to point cloud under the corresponding coordinate system of multiframe high data Data obtain the position transformational relation of laser radar and inertial navigation system.
It specifically, on the basis of the above embodiments, can be same by synchronization after obtaining multiframe map point cloud data The point map cloud data of position acquisition are transformed under the corresponding coordinate system of corresponding high data.Specifically will be more Frame point map cloud data are converted to the point cloud data under the corresponding coordinate system of multiframe high data, obtain laser radar With the position transformational relation of inertial navigation system, it can be by enumerating coordinate system transfer equation, determine position transformational relation;? It can be by enumerating multiple coordinate transfer equations, choose coordinates of targets transfer equation, determine position transformational relation;The application is real It is without limitation to apply example.
Multiframe point cloud data is matched under the corresponding coordinate system of map datum by above-mentioned laser radar scaling method, terminal, Multiframe map point cloud data is obtained, and multiframe point map cloud data are converted into the corresponding coordinate of multiframe high data Point cloud data under system obtains the position transformational relation of laser radar and inertial navigation system.In the present embodiment, terminal pass through by Multiframe point cloud data is matched under the corresponding coordinate system of map datum, obtains multiframe map point cloud data, and by the multiframe map Point cloud data is converted to the point cloud data under the corresponding coordinate system of multiframe high data, and terminal is obtained automatically The position transformational relation of laser radar and inertial navigation system is taken, and then according to the position transformational relation, and then is turned according to position The relationship of changing determines the calibration result of laser radar, so that the calibration result for obtaining laser radar automatically obtains, avoids hand Work measurement obtains the process of the calibration result of laser radar, and then improves the calibration efficiency of laser radar.
On the basis of the above embodiments, terminal can point cloud data according to laser radar to be calibrated, inertial navigation system Data of uniting and map datum obtain the position transformational relation of laser radar and inertial navigation system by calibration algorithm.Lead to below Fig. 4 is crossed the detailed process how terminal obtains according to calibration algorithm position transformational relation automatically is described in detail.Above-mentioned S202 " will Multiframe point map cloud data are converted to the point cloud data under the corresponding coordinate system of multiframe high data, obtain laser thunder Up to the position transformational relation with inertial navigation system " a kind of possible implementation the following steps are included:
S301, according to multiframe high data and the multiple relative pose sides of multiframe point map cloud data list Journey;Wherein, the high data in a frame map point cloud data and same frame constitutes one group of data, and every group of data are corresponding One relative pose equation.
Specifically, relative pose equation can be according to inertial navigation system number in a frame map point cloud data and same frame According to acquisition coordinate transfer equation.High data constitutes one group of data in one frame map point cloud data and same frame, should One group of data can be the frame map point cloud data and a frame high data in the acquisition of synchronization same position, Constitute one group of data in same frame.Specifically arranged according to multiframe high data and multiframe map point cloud data During lifting multiple relative pose equations, each frame map point cloud data corresponds to a high data.Wherein Map point cloud data is different from the expression way of coordinate information in high data, can enumerate relative pose equation, Laser radar data and other sensors data are unified for a kind of expression way.
S302, according to the corresponding one group of data of each relative pose equation and relative pose equation, calculate relative pose Position conversion parameter in equation, to obtain multiple position conversion parameters.
Specifically, each relative pose equation has corresponded to chart portfolio point cloud data and high data, by this Group map point cloud data and high data substitute into its corresponding relative pose equation, and the relative pose side is calculated Position conversion parameter in journey.Wherein point map cloud data include multiframe map point cloud data, and high data includes Multiframe high data, multiframe map point cloud data distinguish corresponding multiframe inertial navigation system and form multiple groups number According to multi-group data is substituted into its corresponding relative pose equation respectively, passes through to calculate and obtains multiple position conversion parameters.
S303, position transformational relation is determined according to multiple position conversion parameters and multiple relative pose equations.
Specifically, on the basis of the above embodiments, after obtaining multiple position conversion parameters, can be joined according to multiple positions Number determines position transformational relation with its corresponding multiple relative pose equation, can be and first determines a target relative pose side Journey, then target position conversion parameter is obtained, and then position is determined according to target relative position equation and target position conversion parameter Transformational relation.
Optionally, above-mentioned S303 " determines that position is converted according to multiple position conversion parameters and multiple relative pose equations A kind of possible implementation method of relationship ", is included the steps that in embodiment as shown in Figure 5:
S401, multiple relative pose equations are added up using least square method, obtains target relative pose equation.
Specifically, the thinking that can use least square method, multiple relative pose equations is added up, to be reduced The error of opposite azimuth equation, the optimal function that data can be found by minimizing the quadratic sum of error match.The present embodiment In, multiple relative pose equations can be added up, to obtain the best relative pose equation minimized the error, as target Relative pose equation.
S402, multiple relative position conversion parameters are concluded by enumeration, obtains and obtains target position conversion Parameter.
Specifically, position conversion parameter may include multiple parameters, can first be determined in multiple parameters by enumeration Partial parameters other parameters are concluded further according to partial parameters, obtain target position conversion parameter.For example, position turns Changing parameter may include a, b, c, d, e, six parameters of f, it is first determined the specific value of tri- parameters of a, b, c, and then according to a, Tri- parameter values of b, c, the multiple d of exhaustion, the numerical value of e, f choose multiple d of exhaustion, and the numerical value of e, f meet the numerical value of preset requirement For d, the parameter value of e, f.And then according to a, b, c, d, e, six parameter values of f determine position conversion parameter.
S403, target position conversion parameter is substituted into the target relative pose equation, obtains the position transformational relation.
Above-mentioned laser radar scaling method, terminal is according to multiframe high data and multiframe map point cloud data Multiple relative pose equations are enumerated, and according to the corresponding one group of data of each relative pose equation and relative pose equation, meter The position conversion parameter in relative pose equation is calculated, to obtain multiple position conversion parameters, and then is converted and is joined according to multiple positions Several and multiple relative pose equations determine position transformational relation.In the present embodiment, terminal is by enumerating multiple relative pose sides Journey obtains multiple position conversion parameters, and then determines that position turns according to multiple relative pose equations and multiple position conversion parameters Relationship is changed, so that the calibration result for obtaining laser radar is automatically obtained by calibration algorithm, avoids hand dipping acquisition The process of the calibration result of laser radar, and then improve calibration efficiency.
Fig. 6 is the flow chart of laser radar scaling method in another embodiment, as shown in fig. 6, in above-described embodiment On the basis of, a kind of laser radar scaling method includes:
S501, the multiframe of laser radar to be calibrated is obtained in preset calibration scene according to data collecting rule respectively The multiframe high data of point cloud data and inertial navigation system.
S502, point cloud data is matched under the corresponding coordinate system of map datum by cloud algorithm, obtains point map cloud Data;Point cloud algorithm includes ICP algorithm, and/or, NDT algorithm.
S503, according to multiframe inertial navigation data and the multiple relative pose equations of multiframe point map cloud data list;Its In, the high data in a frame map point cloud data and same frame constitutes one group of data, and every group of data are one corresponding Relative pose equation.
S504, according to the corresponding one group of data of each relative pose equation and relative pose equation, calculate relative pose Position conversion parameter in equation, to obtain multiple position conversion parameters.
S505, multiple relative pose equations are added up using least square method, obtains target relative pose equation.
S506, multiple relative position conversion parameters are concluded by enumeration, obtains and obtains target position conversion Parameter.
S507, target position conversion parameter is substituted into target relative pose equation, obtains position transformational relation.
The technology of embodiment corresponding to the technical effect of laser radar scaling method and above-described embodiment in the present embodiment Effect is similar, and details are not described herein.
It should be understood that although each step in the flow chart of Fig. 2-6 is successively shown according to the instruction of arrow, These steps are not that the inevitable sequence according to arrow instruction successively executes.Unless expressly stating otherwise herein, these steps Execution there is no stringent sequences to limit, these steps can execute in other order.Moreover, at least one in Fig. 2-6 Part steps may include that perhaps these sub-steps of multiple stages or stage are not necessarily in synchronization to multiple sub-steps Completion is executed, but can be executed at different times, the execution sequence in these sub-steps or stage is also not necessarily successively It carries out, but can be at least part of the sub-step or stage of other steps or other steps in turn or alternately It executes.
Fig. 7 is the structural schematic diagram for the laser radar caliberating device that one embodiment provides.As shown in fig. 7, laser radar Caliberating device, comprising: first, which obtains module 10, second, obtains module 20, conversion module 30 and demarcating module 40, in which:
First obtains module 10, in preset calibration scene, obtain laser radar to be calibrated point cloud data and High data;There is target object of reference in the calibration scene;
Second obtains module 20, for obtaining the corresponding map datum of the calibration scene;
Conversion module 30, for the point cloud data according to the laser radar to be calibrated, the high data With the map datum, closed by the position conversion that the first calibration algorithm obtains the laser radar and the inertial navigation system System;After first calibration algorithm is used to the point cloud data and the map datum carrying out coordinate system matching, matching is tied Fruit and high data are converted to the data under same coordinate system;
Demarcating module 40, for determining the calibration result of laser radar according to the position transformational relation.
In one embodiment, the first acquisition module 10 is specifically used for according to data collecting rule, in preset Calibration Field In scape, the multiframe point cloud data of laser radar to be calibrated and the multiframe inertial navigation system number of inertial navigation system are obtained respectively According to.
Laser radar caliberating device provided by the embodiments of the present application, can execute above method embodiment, realization principle Similar with technical effect, details are not described herein.
Fig. 8 is the structural schematic diagram for the laser radar caliberating device that another embodiment provides, embodiment shown in Fig. 7 On the basis of, conversion module 30 includes: matching unit 301 and converting unit 302, in which:
Matching unit 301 is obtained for the multiframe point cloud data to be matched under the corresponding coordinate system of the map datum Obtain multiframe point map cloud data;
Converting unit 302, for the multiframe point map cloud data to be converted to the multiframe high data Point cloud data under corresponding coordinate system obtains the position transformational relation of the laser radar and the inertial navigation system.
In one embodiment, matching unit 301 is specifically used for that the point cloud data is matched to institute by point cloud algorithm It states under the corresponding coordinate system of map datum, obtains map point cloud data;Described cloud algorithm includes ICP algorithm, and/or, NDT is calculated Method.
Fig. 9 is the structural schematic diagram for the laser radar caliberating device that another embodiment provides, real shown in Fig. 7 or Fig. 8 On the basis of applying example, converting unit 302, comprising: it enumerates subelement 3021, conversion subunit 3022 and determines subelement 3023, Wherein:
Subelement 3021 is enumerated, for arranging according to the multiframe inertial navigation data and the multiframe map point cloud data Lift multiple relative pose equations;Wherein, the high data in a frame map point cloud data and same frame constitutes one group Data, the corresponding relative pose equation of every group of data;
Conversion subunit 3022, for one group corresponding according to each relative pose equation and the relative pose equation Data calculate the position conversion parameter in the relative pose equation, to obtain multiple position conversion parameters;
Subelement 3023 is determined, for determining institute's rheme according to multiple position conversion parameters and multiple relative pose equations Set transformational relation.
In one embodiment, determine that subelement 3023 is specifically used for multiple relative pose equations using least square method It adds up, obtains target relative pose equation;Multiple relative position conversion parameters are concluded by enumeration, are obtained Obtain target position conversion parameter;Target position conversion parameter is substituted into the target relative pose equation, obtains the position Transformational relation.
In one embodiment, the position transformational relation is determined as to the calibration result of the laser radar;Alternatively, will The position transformational relation is visualized, and the result after visualization is determined as to the calibration result of the laser radar.
In one embodiment, the target object of reference is so that the signal of laser radar transmitting passes through the target After object of reference, reflected signal strength is greater than the object of reference of preset threshold.
In one embodiment, the preset calibration scene is according to the laser radar, the inertial navigation system Type and the target object of reference type determine scene.
Laser radar caliberating device provided by the embodiments of the present application, can execute above method embodiment, realization principle Similar with technical effect, details are not described herein.
A kind of specific restriction about laser radar caliberating device may refer to above for laser radar scaling method Restriction, details are not described herein.Modules in above-mentioned laser radar caliberating device can be fully or partially through software, hardware And combinations thereof realize.Above-mentioned each module can be embedded in the form of hardware or independently of in the processor in computer equipment, It can be stored in a software form in the memory in computer equipment, execute the above modules pair in order to which processor calls The operation answered.
In one embodiment, a kind of computer equipment is provided, which can be terminal, internal structure Figure can be as shown in Figure 10.The computer equipment includes the processor connected by system bus, memory, network interface, shows Display screen and input unit.Wherein, the processor of the computer equipment is for providing calculating and control ability.The computer equipment Memory includes non-volatile memory medium, built-in storage.The non-volatile memory medium is stored with operating system and computer Program.The built-in storage provides environment for the operation of operating system and computer program in non-volatile memory medium.The meter The network interface for calculating machine equipment is used to communicate with external terminal by network connection.When the computer equipment is executed by processor To realize a kind of laser radar scaling method.The display screen of the computer equipment can be liquid crystal display or electric ink is aobvious Display screen, the input unit of the computer equipment can be the touch layer covered on display screen, be also possible to computer equipment shell Key, trace ball or the Trackpad of upper setting can also be external keyboard, Trackpad or mouse etc..
It will be understood by those skilled in the art that structure shown in Figure 10, only part relevant to disclosure scheme The block diagram of structure, does not constitute the restriction for the computer equipment being applied thereon to disclosure scheme, and specific computer is set Standby may include perhaps combining certain components or with different component layouts than more or fewer components as shown in the figure.
In one embodiment, a kind of computer equipment, including memory and processor are provided, is stored in memory Computer program, the processor perform the steps of when executing computer program
In preset calibration scene, the point cloud data and high data of laser radar to be calibrated are obtained;Institute Stating in calibration scene has target object of reference;
Obtain the corresponding map datum of the calibration scene;
According to the point cloud data of the laser radar to be calibrated, the high data and the map datum, The position transformational relation of the laser radar and the inertial navigation system is obtained by calibration algorithm;The calibration algorithm is used for After the point cloud data and the map datum are carried out coordinate system matching, matching result and high data are converted For the data under same coordinate system;
According to the position transformational relation, the calibration result of laser radar is determined.
In one embodiment, it also performs the steps of when processor executes computer program according to data collecting rule, In preset calibration scene, the multiframe point cloud data of laser radar to be calibrated and the multiframe of inertial navigation system are obtained respectively High data.
In one embodiment, it also performs the steps of when processor executes computer program by the multiframe point cloud number According to being matched under the corresponding coordinate system of the map datum, multiframe map point cloud data is obtained;By the multiframe point map cloud number According to the point cloud data be converted under the corresponding coordinate system of the multiframe high data, the laser radar and institute are obtained State the position transformational relation of inertial navigation system.
In one embodiment, it is also performed the steps of institute when processor executes computer program through cloud algorithm It states point cloud data to be matched under the corresponding coordinate system of the map datum, obtains map point cloud data;Described cloud algorithm include ICP algorithm, and/or, NDT algorithm.
In one embodiment, it also performs the steps of when processor executes computer program according to the multiframe inertia Navigation data and the multiple relative pose equations of multiframe point map cloud data list;Wherein, a frame map point cloud data with High data in same frame constitutes one group of data, the corresponding relative pose equation of every group of data;According to each Relative pose equation and the corresponding one group of data of the relative pose equation, the position calculated in the relative pose equation turn Parameter is changed, to obtain multiple position conversion parameters;Institute is determined according to multiple position conversion parameters and multiple relative pose equations Rheme sets transformational relation.
In one embodiment, it also performs the steps of when processor executes computer program by multiple relative pose sides Cheng Caiyong least square method adds up, and obtains target relative pose equation;Multiple relative positions are converted by enumeration Parameter is concluded, and is obtained and is obtained target position conversion parameter;Target position conversion parameter is substituted into the target relative pose Equation obtains the position transformational relation.
In one embodiment, it also performs the steps of to convert the position when processor executes computer program and close System is determined as the calibration result of the laser radar;Alternatively, the position transformational relation is visualized, and will be after visualization Result be determined as the calibration result of the laser radar.
In one embodiment, the target object of reference is so that the signal of laser radar transmitting passes through the target After object of reference, reflected signal strength is greater than the object of reference of preset threshold.
In one embodiment, the preset calibration scene is according to the laser radar, the inertial navigation system Type and the target object of reference type determine scene.
Computer equipment provided in this embodiment, implementing principle and technical effect are similar with above method embodiment, This is repeated no more.
In one embodiment, a kind of computer readable storage medium is provided, computer program is stored thereon with, is calculated Machine program performs the steps of when being executed by processor
In preset calibration scene, the point cloud data and high data of laser radar to be calibrated are obtained;Institute Stating in calibration scene has target object of reference;
Obtain the corresponding map datum of the calibration scene;
According to the point cloud data of the laser radar to be calibrated, the high data and the map datum, The position transformational relation of the laser radar and the inertial navigation system is obtained by calibration algorithm;The calibration algorithm is used for After the point cloud data and the map datum are carried out coordinate system matching, matching result and high data are converted For the data under same coordinate system;
According to the position transformational relation, the calibration result of laser radar is determined.
In one embodiment, it also performs the steps of to be acquired according to data when computer program is executed by processor and advise Then, in preset calibration scene, the multiframe point cloud data and inertial navigation system of laser radar to be calibrated are obtained respectively Multiframe high data.
In one embodiment, it is also performed the steps of when computer program is executed by processor by the multiframe point cloud Under Data Matching to the corresponding coordinate system of the map datum, multiframe map point cloud data is obtained;By the multiframe point map cloud Data are converted to the point cloud data under the corresponding coordinate system of the multiframe high data, obtain the laser radar and The position transformational relation of the inertial navigation system.
In one embodiment, also performing the steps of when computer program is executed by processor will by cloud algorithm The point cloud data is matched under the corresponding coordinate system of the map datum, obtains map point cloud data;Described cloud algorithm packet ICP algorithm is included, and/or, NDT algorithm.
In one embodiment, it is also performed the steps of when computer program is executed by processor used according to the multiframe Property navigation data and the multiple relative pose equations of multiframe point map cloud data list;Wherein, a frame map point cloud data One group of data, the corresponding relative pose equation of every group of data are constituted with the high data in same frame;According to every A relative pose equation and the corresponding one group of data of the relative pose equation, calculate the position in the relative pose equation Conversion parameter, to obtain multiple position conversion parameters;It is determined according to multiple position conversion parameters and multiple relative pose equations The position transformational relation.
In one embodiment, it is also performed the steps of when computer program is executed by processor by multiple relative poses Equation is added up using least square method, obtains target relative pose equation;Multiple relative positions are turned by enumeration It changes parameter to be concluded, obtains and obtain target position conversion parameter;Target position conversion parameter is substituted into the target with respect to position Appearance equation obtains the position transformational relation.
In one embodiment, it is also performed the steps of when computer program is executed by processor and converts the position Relationship is determined as the calibration result of the laser radar;Alternatively, the position transformational relation is visualized, and will visualization Result afterwards is determined as the calibration result of the laser radar.
In one embodiment, the target object of reference is so that the signal of laser radar transmitting passes through the target After object of reference, reflected signal strength is greater than the object of reference of preset threshold.
In one embodiment, the preset calibration scene is according to the laser radar, the inertial navigation system Type and the target object of reference type determine scene.
Those of ordinary skill in the art will appreciate that realizing all or part of the process in above-described embodiment method, being can be with Relevant hardware is instructed to complete by computer program, the computer program can be stored in a non-volatile computer In read/write memory medium, the computer program is when being executed, it may include such as the process of the embodiment of above-mentioned each method.Wherein, To any reference of memory, storage, database or other media used in each embodiment provided by the disclosure, Including non-volatile and/or volatile memory.Nonvolatile memory may include read-only memory (ROM), programming ROM (PROM), electrically programmable ROM (EPROM), electrically erasable ROM (EEPROM) or flash memory.Volatile memory may include Random access memory (RAM) or external cache.By way of illustration and not limitation, RAM is available in many forms, Such as static state RAM (SRAM), dynamic ram (DRAM), synchronous dram (SDRAM), double data rate sdram (DDRSDRAM), enhancing Type SDRAM (ESDRAM), synchronization link (Synchlink) DRAM (SLDRAM), memory bus (Rambus) direct RAM (RDRAM), direct memory bus dynamic ram (DRDRAM) and memory bus dynamic ram (RDRAM) etc..
Each technical characteristic of embodiment described above can be combined arbitrarily, for simplicity of description, not to above-mentioned reality It applies all possible combination of each technical characteristic in example to be all described, as long as however, the combination of these technical characteristics is not deposited In contradiction, all should be considered as described in this specification.
The embodiments described above only express several embodiments of the present invention, and the description thereof is more specific and detailed, but simultaneously It cannot therefore be construed as limiting the scope of the patent.It should be pointed out that coming for those of ordinary skill in the art It says, without departing from the inventive concept of the premise, various modifications and improvements can be made, these belong to protection of the invention Range.Therefore, the scope of protection of the patent of the invention shall be subject to the appended claims.

Claims (12)

1. a kind of laser radar scaling method, which is characterized in that the described method includes:
In preset calibration scene, the point cloud data and high data of laser radar to be calibrated are obtained;The mark Determine that there is target object of reference in scene;
Obtain the corresponding map datum of the calibration scene;
According to the point cloud data of the laser radar to be calibrated, the high data and the map datum, pass through Calibration algorithm obtains the position transformational relation of the laser radar and the inertial navigation system;The calibration algorithm is used for institute After stating point cloud data and map datum progress coordinate system matching, matching result and high data are converted into phase With the data under coordinate system;
According to the position transformational relation, the calibration result of laser radar is determined.
2. method according to claim 1, which is characterized in that it is described in preset calibration scene, obtain laser to be calibrated The point cloud data and high data of radar, comprising:
The multiframe point cloud data of laser radar to be calibrated is obtained respectively in preset calibration scene according to data collecting rule And the multiframe high data of inertial navigation system.
3. method according to claim 2, which is characterized in that the point cloud data according to the laser radar to be calibrated, The high data and the map datum obtain the laser radar and the inertial navigation by calibration algorithm The position transformational relation of system, comprising:
The multiframe point cloud data is matched under the corresponding coordinate system of the map datum, multiframe map point cloud data is obtained;
The multiframe point map cloud data are converted into the point cloud under the corresponding coordinate system of the multiframe high data Data obtain the position transformational relation of the laser radar and the inertial navigation system.
4. method according to claim 3, which is characterized in that described that the multiframe point cloud data is matched to the map number According under corresponding coordinate system, multiframe map point cloud data is obtained, comprising:
The point cloud data is matched under the corresponding coordinate system of the map datum by cloud algorithm, obtains point map cloud number According to;Described cloud algorithm includes ICP algorithm, and/or, NDT algorithm.
5. method according to claim 3, which is characterized in that it is described the multiframe point map cloud data are converted to it is described more Point cloud data under the corresponding coordinate system of frame high data, obtains the laser radar and the inertial navigation system Position transformational relation, comprising:
According to the multiframe inertial navigation data and the multiple relative pose equations of multiframe point map cloud data list;Its In, the high data in a frame map point cloud data and same frame constitutes one group of data, and every group of data are one corresponding Relative pose equation;
According to each relative pose equation and the corresponding one group of data of the relative pose equation, the relative pose side is calculated Position conversion parameter in journey, to obtain multiple position conversion parameters;
The position transformational relation is determined according to multiple position conversion parameters and multiple relative pose equations.
6. method according to claim 5, which is characterized in that described according to multiple position conversion parameters and multiple with respect to position Appearance equation determines the position transformational relation, comprising:
Multiple relative pose equations are added up using least square method, obtain target relative pose equation;
Multiple relative position conversion parameters are concluded by enumeration, obtains and obtains target position conversion parameter;
Target position conversion parameter is substituted into the target relative pose equation, obtains the position transformational relation.
7. any one of -6 the method according to claim 1, which is characterized in that it is described according to the position transformational relation, it determines The calibration result of laser radar, comprising:
The position transformational relation is determined as to the calibration result of the laser radar;
Alternatively,
The position transformational relation is visualized, and the result after visualization is determined as to the calibration knot of the laser radar Fruit.
8. any one of -6 the method according to claim 1, which is characterized in that the target object of reference is so that the laser thunder Up to transmitting signal by the target object of reference after, reflected signal strength be greater than preset threshold object of reference.
9. any one of -6 the method according to claim 1, which is characterized in that the preset calibration scene is to be swashed according to described The scene that the type of optical radar, the type of the inertial navigation system and the target object of reference determines.
10. a kind of laser radar caliberating device, which is characterized in that described device includes:
First obtains module, in preset calibration scene, the point cloud data and inertia for obtaining laser radar to be calibrated to be led Navigate system data;There is target object of reference in the calibration scene;
Second obtains module, for obtaining the corresponding map datum of the calibration scene;
Conversion module, for according to the point cloud data of the laser radar to be calibrated, the high data and described Map datum obtains the position transformational relation of the laser radar and the inertial navigation system by the first calibration algorithm;Institute After the first calibration algorithm is stated for the point cloud data and the map datum to be carried out coordinate system matching, by matching result and it is used to Property guidance system data is converted to the data under same coordinate system;
Demarcating module, for determining the calibration result of laser radar according to the position transformational relation.
11. a kind of computer equipment, including memory and processor, the memory are stored with computer program, feature exists In when the processor executes the computer program the step of any one of realization claim 1-9 the method.
12. a kind of computer readable storage medium, is stored thereon with computer program, which is characterized in that the computer program The step of method of any of claims 1-9 is realized when being executed by processor.
CN201811623241.6A 2018-12-28 2018-12-28 Laser radar calibration method, device, equipment and storage medium Active CN109901139B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201811623241.6A CN109901139B (en) 2018-12-28 2018-12-28 Laser radar calibration method, device, equipment and storage medium

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201811623241.6A CN109901139B (en) 2018-12-28 2018-12-28 Laser radar calibration method, device, equipment and storage medium

Publications (2)

Publication Number Publication Date
CN109901139A true CN109901139A (en) 2019-06-18
CN109901139B CN109901139B (en) 2023-07-04

Family

ID=66943512

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201811623241.6A Active CN109901139B (en) 2018-12-28 2018-12-28 Laser radar calibration method, device, equipment and storage medium

Country Status (1)

Country Link
CN (1) CN109901139B (en)

Cited By (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110686704A (en) * 2019-10-18 2020-01-14 深圳市镭神智能系统有限公司 Pose calibration method, system and medium for laser radar and combined inertial navigation
CN110837080A (en) * 2019-10-28 2020-02-25 武汉海云空间信息技术有限公司 Rapid calibration method of laser radar mobile measurement system
CN111060132A (en) * 2019-11-29 2020-04-24 苏州智加科技有限公司 Calibration method and device for travelling crane positioning coordinates
CN111161353A (en) * 2019-12-31 2020-05-15 深圳一清创新科技有限公司 Vehicle positioning method and device, readable storage medium and computer equipment
CN111390911A (en) * 2020-04-03 2020-07-10 东莞仕达通自动化有限公司 Manipulator position calibration system and calibration method
CN111427060A (en) * 2020-03-27 2020-07-17 深圳市镭神智能系统有限公司 Two-dimensional grid map construction method and system based on laser radar
CN111427026A (en) * 2020-02-21 2020-07-17 深圳市镭神智能系统有限公司 Laser radar calibration method and device, storage medium and self-moving equipment
CN111458721A (en) * 2020-03-31 2020-07-28 江苏集萃华科智能装备科技有限公司 Exposed garbage identification and positioning method, device and system
CN112034431A (en) * 2020-09-25 2020-12-04 新石器慧拓(北京)科技有限公司 Radar and RTK external reference calibration method and device
CN112068108A (en) * 2020-08-11 2020-12-11 南京航空航天大学 Laser radar external parameter calibration method based on total station
CN112146682A (en) * 2020-09-22 2020-12-29 福建牧月科技有限公司 Sensor calibration method and device for intelligent automobile, electronic equipment and medium
CN112285676A (en) * 2020-10-22 2021-01-29 知行汽车科技(苏州)有限公司 Laser radar and IMU external reference calibration method and device
CN112379353A (en) * 2020-11-10 2021-02-19 上海交通大学 Combined calibration method and system among multiple target laser radars
CN112414444A (en) * 2019-08-22 2021-02-26 阿里巴巴集团控股有限公司 Data calibration method, computer equipment and storage medium
WO2021057612A1 (en) * 2019-09-25 2021-04-01 华为技术有限公司 Sensor calibration method and apparatus
CN112684432A (en) * 2019-10-18 2021-04-20 北京万集科技股份有限公司 Laser radar calibration method, device, equipment and storage medium
CN112731358A (en) * 2021-01-08 2021-04-30 奥特酷智能科技(南京)有限公司 Multi-laser-radar external parameter online calibration method
CN112964291A (en) * 2021-04-02 2021-06-15 清华大学 Sensor calibration method and device, computer storage medium and terminal
CN112965047A (en) * 2021-02-01 2021-06-15 中国重汽集团济南动力有限公司 Vehicle multi-laser radar calibration method, system, terminal and storage medium
CN113484843A (en) * 2021-06-02 2021-10-08 福瑞泰克智能系统有限公司 Method and device for determining external parameters between laser radar and integrated navigation
CN113534110A (en) * 2021-06-24 2021-10-22 香港理工大学深圳研究院 Static calibration method for multi-laser radar system
CN113767264A (en) * 2020-03-05 2021-12-07 深圳市大疆创新科技有限公司 Parameter calibration method, device, system and storage medium
WO2021253193A1 (en) * 2020-06-15 2021-12-23 深圳市大疆创新科技有限公司 Calibration method and calibration apparatus for external parameters of multiple groups of laser radars, and computer storage medium
CN113848541A (en) * 2021-09-22 2021-12-28 深圳市镭神智能系统有限公司 Calibration method and device, unmanned aerial vehicle and computer readable storage medium
CN113870343A (en) * 2020-06-30 2021-12-31 长沙智能驾驶研究院有限公司 Relative pose calibration method and device, computer equipment and storage medium
CN113933820A (en) * 2021-12-16 2022-01-14 中智行科技有限公司 Laser radar external reference calibration method without calibration object
CN114413887A (en) * 2021-12-24 2022-04-29 北京理工大学前沿技术研究院 Method, equipment and medium for calibrating external parameters of sensor
WO2022261825A1 (en) * 2021-06-15 2022-12-22 华为技术有限公司 Calibration method and device for automatic driving vehicle
WO2023103290A1 (en) * 2021-12-09 2023-06-15 上海禾赛科技有限公司 Calibration method, calibration device, calibration system and readable storage medium

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6608913B1 (en) * 2000-07-17 2003-08-19 Inco Limited Self-contained mapping and positioning system utilizing point cloud data
CN104794743A (en) * 2015-04-27 2015-07-22 武汉海达数云技术有限公司 Color point cloud producing method of vehicle-mounted laser mobile measurement system
CN105719284A (en) * 2016-01-18 2016-06-29 腾讯科技(深圳)有限公司 Data processing method, device and terminal
CN107204037A (en) * 2016-03-17 2017-09-26 中国科学院光电研究院 3-dimensional image generation method based on main passive 3-D imaging system
CN107421507A (en) * 2017-04-28 2017-12-01 上海华测导航技术股份有限公司 Streetscape data acquisition measuring method
CN107463918A (en) * 2017-08-17 2017-12-12 武汉大学 Lane line extracting method based on laser point cloud and image data fusion
US9870624B1 (en) * 2017-01-13 2018-01-16 Otsaw Digital Pte. Ltd. Three-dimensional mapping of an environment
CN107688184A (en) * 2017-07-24 2018-02-13 宗晖(上海)机器人有限公司 A kind of localization method and system
CN107796370A (en) * 2016-08-30 2018-03-13 北京四维图新科技股份有限公司 For obtaining the method, apparatus and mobile mapping system of conversion parameter
CN108594245A (en) * 2018-07-04 2018-09-28 北京国泰星云科技有限公司 A kind of object movement monitoring system and method

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6608913B1 (en) * 2000-07-17 2003-08-19 Inco Limited Self-contained mapping and positioning system utilizing point cloud data
CN104794743A (en) * 2015-04-27 2015-07-22 武汉海达数云技术有限公司 Color point cloud producing method of vehicle-mounted laser mobile measurement system
CN105719284A (en) * 2016-01-18 2016-06-29 腾讯科技(深圳)有限公司 Data processing method, device and terminal
CN107204037A (en) * 2016-03-17 2017-09-26 中国科学院光电研究院 3-dimensional image generation method based on main passive 3-D imaging system
CN107796370A (en) * 2016-08-30 2018-03-13 北京四维图新科技股份有限公司 For obtaining the method, apparatus and mobile mapping system of conversion parameter
US9870624B1 (en) * 2017-01-13 2018-01-16 Otsaw Digital Pte. Ltd. Three-dimensional mapping of an environment
CN107421507A (en) * 2017-04-28 2017-12-01 上海华测导航技术股份有限公司 Streetscape data acquisition measuring method
CN107688184A (en) * 2017-07-24 2018-02-13 宗晖(上海)机器人有限公司 A kind of localization method and system
CN107463918A (en) * 2017-08-17 2017-12-12 武汉大学 Lane line extracting method based on laser point cloud and image data fusion
CN108594245A (en) * 2018-07-04 2018-09-28 北京国泰星云科技有限公司 A kind of object movement monitoring system and method

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
韩栋斌 等: "基于多对点云匹配的三维激光雷达外参数标定", 《激光与光电子学进展》, no. 02 *

Cited By (43)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112414444A (en) * 2019-08-22 2021-02-26 阿里巴巴集团控股有限公司 Data calibration method, computer equipment and storage medium
CN112414444B (en) * 2019-08-22 2023-05-30 阿里巴巴集团控股有限公司 Data calibration method, computer equipment and storage medium
WO2021057612A1 (en) * 2019-09-25 2021-04-01 华为技术有限公司 Sensor calibration method and apparatus
CN110686704A (en) * 2019-10-18 2020-01-14 深圳市镭神智能系统有限公司 Pose calibration method, system and medium for laser radar and combined inertial navigation
CN112684432B (en) * 2019-10-18 2024-04-16 武汉万集光电技术有限公司 Laser radar calibration method, device, equipment and storage medium
CN112684432A (en) * 2019-10-18 2021-04-20 北京万集科技股份有限公司 Laser radar calibration method, device, equipment and storage medium
CN110837080A (en) * 2019-10-28 2020-02-25 武汉海云空间信息技术有限公司 Rapid calibration method of laser radar mobile measurement system
CN110837080B (en) * 2019-10-28 2023-09-05 武汉海云空间信息技术有限公司 Rapid calibration method of laser radar mobile measurement system
CN111060132A (en) * 2019-11-29 2020-04-24 苏州智加科技有限公司 Calibration method and device for travelling crane positioning coordinates
CN111161353A (en) * 2019-12-31 2020-05-15 深圳一清创新科技有限公司 Vehicle positioning method and device, readable storage medium and computer equipment
CN111161353B (en) * 2019-12-31 2023-10-31 深圳一清创新科技有限公司 Vehicle positioning method, device, readable storage medium and computer equipment
CN111427026A (en) * 2020-02-21 2020-07-17 深圳市镭神智能系统有限公司 Laser radar calibration method and device, storage medium and self-moving equipment
CN113767264A (en) * 2020-03-05 2021-12-07 深圳市大疆创新科技有限公司 Parameter calibration method, device, system and storage medium
CN111427060A (en) * 2020-03-27 2020-07-17 深圳市镭神智能系统有限公司 Two-dimensional grid map construction method and system based on laser radar
CN111427060B (en) * 2020-03-27 2023-03-07 深圳市镭神智能系统有限公司 Two-dimensional grid map construction method and system based on laser radar
CN111458721A (en) * 2020-03-31 2020-07-28 江苏集萃华科智能装备科技有限公司 Exposed garbage identification and positioning method, device and system
CN111390911A (en) * 2020-04-03 2020-07-10 东莞仕达通自动化有限公司 Manipulator position calibration system and calibration method
CN114080547A (en) * 2020-06-15 2022-02-22 深圳市大疆创新科技有限公司 Calibration method and calibration device for multiple groups of laser radar external parameters and computer storage medium
WO2021253193A1 (en) * 2020-06-15 2021-12-23 深圳市大疆创新科技有限公司 Calibration method and calibration apparatus for external parameters of multiple groups of laser radars, and computer storage medium
CN113870343A (en) * 2020-06-30 2021-12-31 长沙智能驾驶研究院有限公司 Relative pose calibration method and device, computer equipment and storage medium
CN113870343B (en) * 2020-06-30 2024-05-28 长沙智能驾驶研究院有限公司 Relative pose calibration method, device, computer equipment and storage medium
CN112068108A (en) * 2020-08-11 2020-12-11 南京航空航天大学 Laser radar external parameter calibration method based on total station
CN112146682A (en) * 2020-09-22 2020-12-29 福建牧月科技有限公司 Sensor calibration method and device for intelligent automobile, electronic equipment and medium
CN112034431A (en) * 2020-09-25 2020-12-04 新石器慧拓(北京)科技有限公司 Radar and RTK external reference calibration method and device
CN112034431B (en) * 2020-09-25 2023-09-12 新石器慧通(北京)科技有限公司 External parameter calibration method and device for radar and RTK
CN112285676B (en) * 2020-10-22 2024-02-09 知行汽车科技(苏州)股份有限公司 Laser radar and IMU external parameter calibration method and device
CN112285676A (en) * 2020-10-22 2021-01-29 知行汽车科技(苏州)有限公司 Laser radar and IMU external reference calibration method and device
CN112379353A (en) * 2020-11-10 2021-02-19 上海交通大学 Combined calibration method and system among multiple target laser radars
CN112731358B (en) * 2021-01-08 2022-03-01 奥特酷智能科技(南京)有限公司 Multi-laser-radar external parameter online calibration method
CN112731358A (en) * 2021-01-08 2021-04-30 奥特酷智能科技(南京)有限公司 Multi-laser-radar external parameter online calibration method
CN112965047A (en) * 2021-02-01 2021-06-15 中国重汽集团济南动力有限公司 Vehicle multi-laser radar calibration method, system, terminal and storage medium
CN112965047B (en) * 2021-02-01 2023-03-14 中国重汽集团济南动力有限公司 Vehicle multi-laser radar calibration method, system, terminal and storage medium
CN112964291A (en) * 2021-04-02 2021-06-15 清华大学 Sensor calibration method and device, computer storage medium and terminal
CN113484843A (en) * 2021-06-02 2021-10-08 福瑞泰克智能系统有限公司 Method and device for determining external parameters between laser radar and integrated navigation
WO2022261825A1 (en) * 2021-06-15 2022-12-22 华为技术有限公司 Calibration method and device for automatic driving vehicle
CN113534110B (en) * 2021-06-24 2023-11-24 香港理工大学深圳研究院 Static calibration method for multi-laser radar system
CN113534110A (en) * 2021-06-24 2021-10-22 香港理工大学深圳研究院 Static calibration method for multi-laser radar system
CN113848541B (en) * 2021-09-22 2022-08-26 深圳市镭神智能系统有限公司 Calibration method and device, unmanned aerial vehicle and computer readable storage medium
CN113848541A (en) * 2021-09-22 2021-12-28 深圳市镭神智能系统有限公司 Calibration method and device, unmanned aerial vehicle and computer readable storage medium
WO2023103290A1 (en) * 2021-12-09 2023-06-15 上海禾赛科技有限公司 Calibration method, calibration device, calibration system and readable storage medium
CN113933820A (en) * 2021-12-16 2022-01-14 中智行科技有限公司 Laser radar external reference calibration method without calibration object
CN114413887A (en) * 2021-12-24 2022-04-29 北京理工大学前沿技术研究院 Method, equipment and medium for calibrating external parameters of sensor
CN114413887B (en) * 2021-12-24 2024-04-02 北京理工大学前沿技术研究院 Sensor external parameter calibration method, device and medium

Also Published As

Publication number Publication date
CN109901139B (en) 2023-07-04

Similar Documents

Publication Publication Date Title
CN109901139A (en) Laser radar scaling method, device, equipment and storage medium
CN111208492B (en) Vehicle-mounted laser radar external parameter calibration method and device, computer equipment and storage medium
CN109975773A (en) Millimetre-wave radar scaling method, device, equipment and storage medium
CN106969763B (en) Method and apparatus for determining yaw angle of unmanned vehicle
CN109901138A (en) Laser radar scaling method, device, equipment and storage medium
CN113870343B (en) Relative pose calibration method, device, computer equipment and storage medium
CN109085608A (en) Obstacles around the vehicle detection method and device
CN110930495A (en) Multi-unmanned aerial vehicle cooperation-based ICP point cloud map fusion method, system, device and storage medium
JP7404010B2 (en) Position estimation device and method
CN109900298A (en) A kind of vehicle location calibration method and system
CN110501712A (en) For determining the method, apparatus, equipment and medium of position and attitude data
CN108326845B (en) Robot positioning method, device and system based on binocular camera and laser radar
CN109946701A (en) A kind of cloud coordinate transformation method and device
CN108061555A (en) A kind of vehicle location error correction method and device
CN112146682B (en) Sensor calibration method and device for intelligent automobile, electronic equipment and medium
CN108734780A (en) Method, apparatus and equipment for generating map
CN110579754A (en) Method for determining external parameters of a lidar and other sensors of a vehicle
CN106060781A (en) Spatial location method based on fusion of BIM (Building Information Modeling) and Zigbee technology
CN104618137A (en) Method and device for realizing towing exploration control network
US11423573B2 (en) System and methods for calibrating cameras with a fixed focal point
CN114485698A (en) Intersection guide line generating method and system
CN115272452A (en) Target detection positioning method and device, unmanned aerial vehicle and storage medium
CN112762936B (en) Multi-source positioning information fusion method applied to long-endurance unmanned aerial vehicle load
CN115166702A (en) Automatic calibration method and device of laser radar to vehicle body coordinate system based on high-precision positioning information
CN112747752A (en) Vehicle positioning method, device, equipment and storage medium based on laser odometer

Legal Events

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