CN103278177A - Calibration method of inertial measurement unit based on camera network measurement - Google Patents

Calibration method of inertial measurement unit based on camera network measurement Download PDF

Info

Publication number
CN103278177A
CN103278177A CN2013101535983A CN201310153598A CN103278177A CN 103278177 A CN103278177 A CN 103278177A CN 2013101535983 A CN2013101535983 A CN 2013101535983A CN 201310153598 A CN201310153598 A CN 201310153598A CN 103278177 A CN103278177 A CN 103278177A
Authority
CN
China
Prior art keywords
imu
coordinate system
measurement
coordinate
carrier
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
CN2013101535983A
Other languages
Chinese (zh)
Other versions
CN103278177B (en
Inventor
张红良
张小虎
朱宪伟
于起峰
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.)
National University of Defense Technology
Original Assignee
National University of Defense Technology
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 National University of Defense Technology filed Critical National University of Defense Technology
Priority to CN201310153598.3A priority Critical patent/CN103278177B/en
Publication of CN103278177A publication Critical patent/CN103278177A/en
Application granted granted Critical
Publication of CN103278177B publication Critical patent/CN103278177B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Navigation (AREA)

Abstract

The invention provides a calibration method of an inertial measurement unit (IMU) based on camera network measurement. The method comprises: by construction of the camera measure network, establishing a videogrammetric coordinate system relative with local geographical coordinates, providing a cooperate sign on the surface of an IMU carrier, tracking and measuring the cooperate sign by a camera, calculating the position and the attitude of the IMU, further getting projections of gravitational acceleration and input excitation of rotation angle or angular velocity in an IMU carrier system, by comparison between the input excitation and outputs of an accelerometer and a gyroscope in the IMU, optimally calculating IMU calibration parameters and realizing IMU calibration. The camera network system is used to measure the IMU input excitations, and replaces a turntable which plays a role in input excitation measurement in calibration process of a conventional IMU, and the method can be taken as an IMU calibration method in the absence of the turntable. The method is low in cost and easy to arrange, and the method has advantages in on-site IMU calibration and IMU calibration of a low cost inertial navigation system.

Description

IMU scaling method based on shooting networking measurement
Technical field
The present invention relates to inertial navigation, technical field of computer vision, refer specifically to measure IMU using camera network(Inertial Measurement Unit, IMU)Acceleration and rotate input stimulus, demarcate IMU parameters method.
Background technology
Scaling method conventional current IMU is the scaling method using turntable as core, there is many drawbacks, can only be carried out as demarcation in accurate laboratory, and condition requires high, and calibration process is complicated, it is difficult to for inertial navigation system field calibration;Demarcation is costly, or even is several times as much as inexpensive inertia device(Such as MEMS IMU)Development and production cost.
That carries out at present is broadly divided into two classes based on the IMU scaling methods without turntable or low precision turntable:Mould observation demarcation method and system level scaling method.The research of this kind of IMU scaling methods also treats that further deeply, the application that can't be adapted to completely in the demand of field calibration and low precision IMU demarcation, real system is few.
Using video camera networking to target imaging, by analyzing target image characteristics, feature of interest, target motion or displacement are measured, with noncontact, high accuracy, many advantages such as dynamic measurement are convenient for, posture, position accurate measurement and the motion measurement of various objects is had been widely used for.
The correlative study for measuring demarcation IMU using video camera is extremely rare, search only at present to three pertinent literatures, one is the LED using optical tracking system tracking measurement on IMU such as Kim, the angular speed and acceleration of measurement IMU motions, optimal estimating IMU parameter;The two-way collimated laser beam of utilization of the propositions such as Ling Liangpianshi Harbin Institute of Technology Chen Jie spring generates instruction hot spot on screen, the position orientation relation that hot spot solves system of the world and carrier system is shot using CMOS high-speed cameras, IMU angular velocity of satellite motion and acceleration are calculated, for demarcating IMU parameters.Proposed by the present invention is a kind of newer method based on shooting networking measurement demarcation IMU.
The content of the invention
The present invention proposes a kind of based on shooting networking measurement demarcation IMU(IMU)Method, principle schematic is as shown in figure 1, build video camera measurement network, calibrating camera, set up with the related videographic measurment coordinate system of locality geographic coordinate system, in IMU(IMU)Carrier surface sets cooperation mark, cooperation mark is measured using Camera location, calculate the position and attitude for obtaining IMU, and then obtain the projection of acceleration of gravity and rotational angle or turning rate input excitation in IMU carriers system, by the output for contrasting this input stimulus and accelerometer and gyro in IMU, optimization calculates IMU calibrating parameters, realizes that IMU is demarcated.
The present invention realizes that IMU input stimulus are measured using video camera networking, realizes that IMU is demarcated, specifically comprising following committed step:
1) shooting networking measuring system is built.Multiple cameras is set up around IMU to be calibrated, number of cameras, layout and visual field are rationally set, it is ensured that each cooperation in calibration process on IMU carriers is flagged with least two video cameras can be while see, to meet shooting intersection measurement condition.Cooperation mark is laid in IMU carrier surfaces, cooperation mark is accurately known in the position of IMU carrier coordinate systems, indicated using being easy to extract in the picture with pinpoint visualization(Such as crosshair, to cornet mark or LED).Networking video camera is using synchronous triggering pattern, and to IMU synchronous acquisition images, the output of accelerometer and gyro also synchronizes collection in IMU, for calibrated and calculated.
2) photographic measurement system is demarcated.Utilize the demarcation such as plane target plank, plumb line, control point shooting networking measuring system relevant parameter(Including position orientation relation between camera intrinsic parameter, multiple cameras etc.), the videographic measurment coordinate system related to local geographic coordinate system is set up, local gravity direction, local level, earth rotation direction etc. can be characterized.
3) IMU acceleration excitation shooting networking measurement.IMU acceleration input is acceleration of gravity in a static condition, IMU static state is placed, IMU is imaged using networking video camera, extract the cooperation mark that IMU carrier surfaces are laid in image, binocular or the intersection of many mesh obtain coordinate representation of the cooperation mark in videographic measurment coordinate system, when measuring more than three not conllinear cooperation marks, it can calculate according to cooperation mark at the coordinate of IMU carriers system and obtain position of the IMU carrier coordinate systems with respect to videographic measurment coordinate system, posture relation.Due to gravity direction in the expression of videographic measurment coordinate system, it is known that the trivector that therefore can obtain gravity in IMU carrier coordinate systems is represented, i.e. measurement obtains IMU acceleration input stimulus.
4)IMU rotates excitation shooting networking measurement.IMU real-time synchronizations are imaged using networking video camera, the cooperation mark that dynamic tracking measurement IMU carrier surfaces are laid, binocular or the intersection of many mesh obtain coordinate representation of each imaging moment cooperation mark in videographic measurment coordinate system, when measuring more than three not conllinear cooperation marks at each moment, it can calculate and obtain position of the moment IMU carrier coordinate systems with respect to videographic measurment coordinate system, posture relation.Using not in the same time between the real-time attitude changes of IMU carriers obtain IMU rotational angle or angular speed.According to IMU carriers system and the real-time pose relation of videographic measurment coordinate system, obtain rotational angle or angular velocity vector that IMU carrier coordinate systems are represented, i.e. measurement and obtain IMU rotation input stimulus.
5)The optimization of IMU calibrating parameters is resolved.Optimization design IMU static placement location and rotation order, utilize step 3), many static positions of method 4) measurement IMU, the input stimulus repeatedly rotated.While measuring the excitation of IMU acceleration and rotating excitation input, the measurement output of accelerometer and gyro in synchronous acquisition IMU.Compare IMU input and output, according to IMU input/output models and measurement error rule, optimization calculates each calibrating parameters of IMU, realizes IMU demarcation.
The present invention can reach following technique effect:
Videographic measurment technology is applied to IMU and demarcates field there is provided the new approaches that IMU is demarcated by the present invention, has innovated IMU calibration modes.Using the input stimulus for imaging group network system measurement IMU, input stimulus measurement effect of the turntable in traditional IMU demarcation is instead of, therefore the present invention can be as a kind of IMU without turntable scaling method.Compared with high precision turntable, shooting networking measuring system cost of the invention is low, it is easy to lay, and the present invention has advantage in IMU field calibrations and low cost inertial navigation system IMU demarcation.
Brief description of the drawings
IMU calibration system schematic diagrames of the Fig. 1 based on shooting networking measurement,
Fig. 2 sets up videographic measurment IMU demarcation coordinate system schematic diagrames using plumb line and control point,
Fig. 3 IMU acceleration excitation shooting networking instrumentation plan,
Fig. 4 IMU rotate excitation shooting networking instrumentation plan.
Embodiment
1st, videographic measurment IMU demarcates the foundation of coordinate system
Videographic measurment IMU demarcation establishment of coordinate system is, by calibrating camera network, to set up and local geographic coordinate system(N systems)Related videographic measurment coordinate system(Hereinafter referred to as m systems), utilize the basic concepts such as video camera Representation Level benchmark, gravity direction.
As shown in Fig. 2 gravity direction is visualized using plumb line, for enhancing effect of visualization, catenary can be coated to color, work indicates or makees catenary using LED line lamp on catenary.Horizontal plane-gravity direction coordinate system can be set up using plumb line.If there is north orientation benchmark, the relation between control point and north orientation benchmark is determined using total powerstation etc., so as to local geographic coordinate system be visualized by plumb line and control point, for calibrating camera network.For MEMS IMU demarcation, the influence of general earth rotation can be neglected, then can set up horizontal plane-gravity direction coordinate system without north orientation benchmark and demarcate coordinate system for IMU.
Because videographic measurment IMU demarcates the X-axis of coordinate system, Y-axis in local level, Z axis is parallel with gravity direction.Gravity direction unit vector IMU demarcate coordinate system in coordinate be
Figure 1
, wherein gmFor local gravitational acceleration IMU demarcate coordinate system expression, g=| gm| it is the size of acceleration of gravity.
2nd, IMU acceleration excitation shooting networking measurement
Under static conditions, IMU acceleration is actuated to gravity.IMU static state is placed, then IMU measurements are met
Wherein
Figure BDA0000312042913
For IMU carrier coordinate systems(B systems)Between videographic measurment coordinate system(M systems)Pose transformation matrix, fbFor IMU specific force.
The combination demarcation of IMU accelerometers needs known specific force fb, it was found from formula (1), if the placing attitude for obtaining IMU can be measured, i.e. IMU carriers lie in the pose transformation matrix that videographic measurment coordinate system is built
Figure BDA0000312042914
, it is possible to measurement obtains fb
As shown in figure 3, laying more than 3 non-co- line feature points in IMU carrier surfaces, position coordinates of the characteristic point in IMU carrier coordinate systems is, it is known that set respectively
Figure BDA0000312042915
(j=1,2,3…), these characteristic points are obtained in videographic measurment coordinate system using video camera intersection measurement(That is IMU demarcates coordinate system)Coordinate, if be respectively
Figure BDA0000312042916
(j=1,2,3…)If, IMU carrier coordinate system origins ObPosition in videographic measurment coordinate system is
Figure BDA0000312042917
, then have
Figure 3
Utilize the coordinate representation of more than 3 non-co- line feature points
Figure BDA0000312042919
(j=1,2,3…), can be solved and obtained according to formula (2)
Figure BDA00003120429111
With
Figure BDA00003120429112
The method for building up of coordinate system is demarcated according to IMU, acceleration of gravity is expressed as videographic measurment coordinate system
Figure 4
Understood according to (1), (3), IMU specific force input is
Figure 5
I.e.
Figure 6
3rd, IMU rotates excitation shooting networking measurement
As shown in figure 4, IMU turns to position 2 from position 1, carrier coordinate system is from b1Change to b2.More than 3 non-colinear cooperation marks are laid in IMU carrier surfaces, the position coordinates of these cooperation marks of video camera intersection measurement is utilized.If during position 1, coordinate of the cooperation mark in videographic measurment coordinate system is
Figure BDA00003120429116
(j=1,2,3…), go to behind position 2, coordinate of the cooperation mark in videographic measurment coordinate system is
Figure BDA00003120429117
(j=1,2,3…).Coordinate of the cooperation mark in IMU carrier coordinate systems be(j=1,2,3…), it is known that then having
Figure 7
Wherein
Figure BDA00003120429120
Figure BDA00003120429121
Respectively carrier coordinate system b1、b2To videographic measurment coordinate system m pose transformation matrix,
Figure BDA00003120429122
Figure BDA00003120429123
Respectively carrier coordinate system b1、b2Position vector of the origin in videographic measurment coordinate system.
According to formula (5), known coordinate is utilized
Figure BDA00003120429124
(j=1,2,3…)The coordinate measured
Figure BDA00003120429125
Figure BDA00003120429126
(j=1,2,3…)Can be in the hope of
Figure BDA00003120429127
Figure BDA00003120429128
With
Figure BDA00003120429129
Figure BDA00003120429130
.Pose transformation matrix is before and after obtaining IMU rotation
Figure 8
Note
Figure 9
, then corresponding to quaternary number can be write as
Wherein μ be anglec of rotation vector, μ=| μ | be anglec of rotation size.Position 1 can obtain to the anglec of rotation vector μ of position 2 according to formula (7).
IMU continuous rotation is shot using high-speed camera, then the time of adjacent two interframe is very short, IMU rotational angle very littles, and the anglec of rotation vector μ of adjacent two interframe is approximately the expression μ in carrier systemb, momentary rotational angle speed can be approximately
ωb(t)=μb/τ               (8)
Wherein τ is the time interval between the adjacent two frames imaging of videographic measurment.After the rotation for undergoing a period of time T, anglec of rotation vector total IMU is
Figure 11
For MEMS IMU demarcation, the influence of rotational-angular velocity of the earth can not be considered, then gyro turning rate input
Figure BDA00003120429135
Meet
Figure 12
For high-precision IMU demarcation, the influence of rotational-angular velocity of the earth must also be considered, then
4th, IMU calibrating parameters are calculated
If IMU uses following single order input/output model:
Figure 14
Wherein, fbIt is the expression than force vector in IMU carrier coordinate system b systems,
Figure BDA00003120429139
It is input angular velocity vector in the expression of b systems, NaIt is the accelerometer pulse output of unit interval, NgIt is the gyro pulse output of unit interval, Ka、KgThe calibration factor and installation relation matrix of accelerometer and gyro, f are represented respectively0、ω0It is zero inclined, δ of gyro and accelerometerfAnd δωIt is noise section, is typically modeled as white noise.
According to methods described above, it is possible to use the specific force input (f of many positions of photographic measurement system measurement IMUb)k(k=1,2,…)The turning rate input repeatedly rotated
Figure BDA00003120429140
(k=1,2,…), exported according to the measurement of accelerometer and gyro, K obtained using the method Optimization Solution such as least square methoda、KgAnd f0、ω0, so as to realize that IMU calibrating parameters are resolved.
If IMU uses other input/output models, the output of the input stimulus and IMU accelerometers and gyro according to measurement is corresponded to, Optimization Solution model parameter realizes that IMU is demarcated.Calibrated and calculated uses suitable parameter optimization calculation method, suppresses correlated error, improves stated accuracy.

Claims (7)

1. the IMU scaling method based on shooting networking measurement, it is characterised in that build video camera measurement network, the videographic measurment coordinate system related to local geographic coordinate system is set up, in IMU(Inertial Measurement Unit, IMU)Carrier surface sets cooperation mark, cooperation mark is measured using Camera location, calculate the position and attitude for obtaining IMU, and then obtain the projection of acceleration of gravity and rotational angle or turning rate input excitation in IMU carriers system, by the output for contrasting this input stimulus and accelerometer and gyro in IMU, optimization calculates IMU calibrating parameters, realizes that IMU is demarcated
Specifically comprise the following steps:
1) shooting networking measuring system is built:Multiple cameras is set up around IMU to be calibrated, each cooperation in guarantee calibration process on IMU carriers is flagged with least two video cameras can be while see, cooperation mark is laid in IMU carrier surfaces, cooperation mark is accurately known in the position of IMU carrier coordinate systems, networking video camera is using synchronous triggering pattern, to IMU synchronous acquisition images, the output of accelerometer and gyro also synchronizes collection in IMU, for calibrated and calculated;
2) photographic measurement system is demarcated:Utilize plane target plank, plumb line, control point demarcation shooting networking measuring system relevant parameter, including the position orientation relation between camera intrinsic parameter, multiple cameras, the videographic measurment coordinate system related to local geographic coordinate system is set up, local gravity direction, local level, earth rotation direction is characterized;
3) IMU acceleration excitation shooting networking measurement:IMU static state is placed, IMU is imaged using networking video camera, extract the cooperation mark that IMU carrier surfaces are laid in image, binocular or the intersection of many mesh obtain coordinate representation of the cooperation mark in videographic measurment coordinate system, when measuring more than three not conllinear cooperation marks, according to cooperation mark IMU carriers system coordinate, calculating obtains position of the IMU carrier coordinate systems with respect to videographic measurment coordinate system, posture relation, known to expression of the gravity direction in videographic measurment coordinate system, the trivector that gravity be can obtain in IMU carrier coordinate systems is represented, i.e. measurement obtains IMU acceleration input stimulus;
4)IMU rotates excitation shooting networking measurement:IMU real-time synchronizations are imaged using networking video camera, the cooperation mark that dynamic tracking measurement IMU carrier surfaces are laid, binocular or the intersection of many mesh obtain coordinate representation of each imaging moment cooperation mark in videographic measurment coordinate system, when measuring more than three not conllinear cooperation marks at each moment, calculating obtains position of the moment IMU carrier coordinate systems with respect to videographic measurment coordinate system, posture relation, using not in the same time between the real-time attitude changes of IMU carriers obtain IMU rotational angle or angular speed, according to IMU carriers system and the real-time pose relation of videographic measurment coordinate system, obtain rotational angle or angular velocity vector that IMU carrier coordinate systems are represented, i.e. measurement obtains IMU rotation input stimulus;
5)The optimization of IMU calibrating parameters is resolved:Utilize step 3), many static positions of method 4) measurement IMU, the input stimulus repeatedly rotated, while measuring the excitation of IMU acceleration and rotating excitation input, the measurement output of accelerometer and gyro in synchronous acquisition IMU, compare IMU input and output, according to IMU input/output models and measurement error rule, optimization calculates each calibrating parameters of IMU, realizes IMU demarcation.
2. the IMU scaling method according to claim 1 based on shooting networking measurement, it is characterised in that the cooperation mark is using being easy to extract in the picture and pinpoint visualization mark, such as crosshair, to cornet mark or LED.
3. the IMU scaling method according to claim 1 based on shooting networking measurement, it is characterised in that the demarcation photographic measurement system, specifically setting up process is:Pass through calibrating camera network, set up the videographic measurment coordinate system m system related to locality geographic coordinate system n systems, utilize video camera Representation Level benchmark, gravity direction basic concept, gravity direction is visualized using plumb line, horizontal plane-gravity direction coordinate system is set up, if there is north orientation benchmark, the relation between control point and north orientation benchmark is determined using total powerstation, local geographic coordinate system is visualized by plumb line and control point, for calibrating camera network.
4. the IMU scaling method according to claim 1 based on shooting networking measurement, it is characterised in that the IMU acceleration excitation shooting networking is measured, and detailed process is:
IMU static state is placed, IMU acceleration is actuated to acceleration of gravity, and IMU measurements are met
Figure 15
Wherein
Figure FDA0000312042902
For the pose transformation matrix between IMU carrier coordinate system b systems and videographic measurment coordinate system m systems, fbFor IMU specific force, gmBe acceleration of gravity in videographic measurment coordinate system, i.e. IMU demarcates the expression of coordinate system;
More than 3 non-co- line feature points are laid in IMU carrier surfaces, position coordinates of the characteristic point in IMU carrier coordinate systems is, it is known that set respectively
Figure FDA0000312042903
(j=1,2,3…), coordinate of these characteristic points in videographic measurment coordinate system is obtained using video camera intersection measurement, if being respectively
Figure FDA0000312042904
(j=1,2,3…)If, IMU carrier coordinate system origins ObPosition in videographic measurment coordinate system is, then have
Figure 16
Utilize the coordinate representation of more than 3 non-co- line feature points
Figure FDA0000312042907
(j=1,2,3…), solution obtains
Figure FDA0000312042909
With
Figure FDA00003120429010
The method for building up of coordinate system, expression g of the acceleration of gravity in videographic measurment coordinate system are demarcated according to IMUm, it is known that the specific force input for obtaining IMU therefore can be measured
Figure 17
5. the IMU scaling method according to claim 1 based on shooting networking measurement, its feature is as follows:The IMU rotates excitation shooting networking measurement, and detailed process is:
IMU is turned into position 2 from position 1, carrier coordinate system is from b1Change to b2, more than 3 non-colinear cooperation marks are laid in IMU carrier surfaces, using the position coordinates of these cooperation marks of video camera intersection measurement, if during position 1, coordinate of the cooperation mark in videographic measurment coordinate system is(j=1,2,3…), go to behind position 2, coordinate of the cooperation mark in videographic measurment coordinate system is
Figure FDA00003120429013
(j=1,2,3…), coordinate of the cooperation mark in IMU carrier coordinate systems be
Figure FDA00003120429014
(j=1,2,3…), it is known that then having
Figure 18
Wherein
Figure FDA00003120429016
Respectively carrier coordinate system b1、b2To videographic measurment coordinate system m pose transformation matrix,
Figure FDA00003120429018
Figure FDA00003120429019
Respectively carrier coordinate system b1、b2Position vector of the origin in videographic measurment coordinate system;
Utilize known coordinate
Figure FDA00003120429020
(j=1,2,3…)The coordinate measured
Figure FDA00003120429021
Figure FDA00003120429022
(j=1,2,3…)Try to achieve
Figure FDA00003120429023
Figure FDA00003120429024
With
Figure FDA00003120429025
Figure FDA00003120429026
, pose transformation matrix is before and after IMU rotation
Figure 19
If
Figure FDA00003120429028
The anglec of rotation vector of corresponding position 1 to position 2 is μ, IMU continuous rotation is shot using high-speed camera, then the time of adjacent two interframe is very short, IMU rotational angle very littles, and the anglec of rotation vector μ of adjacent two interframe is approximately the expression μ in carrier systemb, momentary rotational angle speed is approximately
ωb(t)=μb/τ            (6)
Wherein τ is the time interval between the adjacent two frames imaging of videographic measurment, and after the rotation for undergoing a period of time T, anglec of rotation vector total IMU is
Figure 20
If not considering the influence of rotational-angular velocity of the earth, gyro turning rate input
Figure FDA00003120429030
Meet
Figure 21
If considering the influence of rotational-angular velocity of the earth,
Figure 22
6. the IMU scaling method according to claim 1 based on shooting networking measurement, it is characterised in that the IMU calibrating parameters optimization is resolved, and detailed process is:If IMU uses following single order input/output model:
Figure 23
Wherein, fbThe ratio force vector represented for b systems,
Figure FDA00003120429034
The input angular velocity vector represented for b systems, NaIt is the accelerometer pulse output of unit interval, NgIt is the gyro pulse output of unit interval, Ka、KgThe calibration factor and installation relation matrix of accelerometer and gyro, f are represented respectively0、ω0It is zero inclined, δ of gyro and accelerometerfAnd δωIt is noise section, the specific force for measuring many positions of IMU using photographic measurement system inputs (fb)k(k=1,2,…)The turning rate input repeatedly rotated
Figure FDA00003120429035
(k=1,2,…), exported according to the measurement of accelerometer and gyro, Optimization Solution obtains Ka、KgAnd f0、ω0, realize that IMU calibrating parameters are resolved.
7. the IMU scaling method according to claim 1 based on shooting networking measurement, characterized in that, IMU uses other input/output models, then the output of the input stimulus and IMU accelerometers and gyro according to measurement is corresponded to, Optimization Solution model parameter, realizes that IMU is demarcated.
CN201310153598.3A 2013-04-27 2013-04-27 Calibration method of inertial measurement unit based on camera network measurement Active CN103278177B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310153598.3A CN103278177B (en) 2013-04-27 2013-04-27 Calibration method of inertial measurement unit based on camera network measurement

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310153598.3A CN103278177B (en) 2013-04-27 2013-04-27 Calibration method of inertial measurement unit based on camera network measurement

Publications (2)

Publication Number Publication Date
CN103278177A true CN103278177A (en) 2013-09-04
CN103278177B CN103278177B (en) 2015-07-01

Family

ID=49060765

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310153598.3A Active CN103278177B (en) 2013-04-27 2013-04-27 Calibration method of inertial measurement unit based on camera network measurement

Country Status (1)

Country Link
CN (1) CN103278177B (en)

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104236469B (en) * 2014-10-15 2017-01-11 郑州辰维科技股份有限公司 Method for measuring displacement of aircraft static test by taking photos
US9970781B2 (en) 2015-03-03 2018-05-15 West Virginia University Apparatus for three-axis IMU calibration with a single-axis rate table
CN108269286A (en) * 2016-12-30 2018-07-10 中国空气动力研究与发展中心超高速空气动力研究所 Polyphaser pose correlating method based on combination dimensional mark
WO2019009676A1 (en) * 2017-07-07 2019-01-10 Samsung Electronics Co., Ltd. System and methods for device tracking
CN109631887A (en) * 2018-12-29 2019-04-16 重庆邮电大学 Inertial navigation high-precision locating method based on binocular, acceleration and gyroscope
CN110132309A (en) * 2019-06-05 2019-08-16 西京学院 A kind of rocker arm of coal mining machine inertia/visual combination determines appearance device normalization method
CN110160557A (en) * 2018-09-29 2019-08-23 中国煤炭科工集团太原研究院有限公司 A kind of development machine inertial navigation system two-dimensional position precision calibration method and system
CN111024117A (en) * 2019-11-21 2020-04-17 中国航空工业集团公司西安飞行自动控制研究所 Vision-based inertial navigation system rapid alignment system and alignment method
CN111383282A (en) * 2018-12-29 2020-07-07 杭州海康威视数字技术股份有限公司 Pose information determination method and device
CN111862242A (en) * 2020-07-29 2020-10-30 北京轻威科技有限责任公司 Calibration system and method for optical inertial hybrid motion capture device
CN112461125A (en) * 2020-10-29 2021-03-09 北京空间机电研究所 Optical measurement system and measurement method for position and attitude of closed floating air ball
CN113984090A (en) * 2021-10-25 2022-01-28 北京科技大学 Online calibration and compensation method and device for IMU (inertial measurement Unit) error of wheeled robot
CN114018291A (en) * 2021-11-08 2022-02-08 中国科学院空天信息创新研究院 Calibration method and device for parameters of inertial measurement unit
WO2022063221A1 (en) * 2020-09-24 2022-03-31 影石创新科技股份有限公司 Method for generating rotation direction of gyroscope and computer device
WO2022198590A1 (en) * 2021-03-25 2022-09-29 华为技术有限公司 Calibration method and apparatus, intelligent driving system, and vehicle

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101539397A (en) * 2009-04-17 2009-09-23 中国人民解放军国防科学技术大学 Method for measuring three-dimensional attitude of object on precision-optical basis
CN101655361A (en) * 2009-08-31 2010-02-24 中国人民解放军国防科学技术大学 Method for measuring attitude of unstable reference platform based on double camera
CN102162738A (en) * 2010-12-08 2011-08-24 中国科学院自动化研究所 Calibration method of camera and inertial sensor integrated positioning and attitude determining system
US20110301902A1 (en) * 2010-06-04 2011-12-08 Apple Inc. Inertial measurement unit calibration system

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101539397A (en) * 2009-04-17 2009-09-23 中国人民解放军国防科学技术大学 Method for measuring three-dimensional attitude of object on precision-optical basis
CN101655361A (en) * 2009-08-31 2010-02-24 中国人民解放军国防科学技术大学 Method for measuring attitude of unstable reference platform based on double camera
US20110301902A1 (en) * 2010-06-04 2011-12-08 Apple Inc. Inertial measurement unit calibration system
CN102162738A (en) * 2010-12-08 2011-08-24 中国科学院自动化研究所 Calibration method of camera and inertial sensor integrated positioning and attitude determining system

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
杨浩等: "摄像机和惯性测量单元的相对位姿标定方法", 《机器人 ROBOT》, vol. 33, no. 4, 31 July 2011 (2011-07-31), pages 419 - 426 *
陈杰春等: "MEMS惯性测量组合初始标定方法研究", 《南京理工大学学报(自然科学版)》, vol. 32, no. 3, 30 June 2008 (2008-06-30), pages 285 - 290 *
陈杰春等: "一种标定陀螺仪的新方法", 《哈尔滨工程大学学报》, vol. 28, no. 4, 30 April 2007 (2007-04-30), pages 407 - 412 *

Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104236469B (en) * 2014-10-15 2017-01-11 郑州辰维科技股份有限公司 Method for measuring displacement of aircraft static test by taking photos
US9970781B2 (en) 2015-03-03 2018-05-15 West Virginia University Apparatus for three-axis IMU calibration with a single-axis rate table
CN108269286A (en) * 2016-12-30 2018-07-10 中国空气动力研究与发展中心超高速空气动力研究所 Polyphaser pose correlating method based on combination dimensional mark
US10565724B2 (en) 2017-07-07 2020-02-18 Samsung Electronics Co., Ltd. System and methods for device tracking
WO2019009676A1 (en) * 2017-07-07 2019-01-10 Samsung Electronics Co., Ltd. System and methods for device tracking
CN110160557A (en) * 2018-09-29 2019-08-23 中国煤炭科工集团太原研究院有限公司 A kind of development machine inertial navigation system two-dimensional position precision calibration method and system
CN110160557B (en) * 2018-09-29 2024-03-12 中国煤炭科工集团太原研究院有限公司 Two-dimensional position precision calibration method and system for inertial navigation system of heading machine
CN109631887B (en) * 2018-12-29 2022-10-18 重庆邮电大学 Inertial navigation high-precision positioning method based on binocular, acceleration and gyroscope
CN111383282A (en) * 2018-12-29 2020-07-07 杭州海康威视数字技术股份有限公司 Pose information determination method and device
CN111383282B (en) * 2018-12-29 2023-12-01 杭州海康威视数字技术股份有限公司 Pose information determining method and device
CN109631887A (en) * 2018-12-29 2019-04-16 重庆邮电大学 Inertial navigation high-precision locating method based on binocular, acceleration and gyroscope
CN110132309A (en) * 2019-06-05 2019-08-16 西京学院 A kind of rocker arm of coal mining machine inertia/visual combination determines appearance device normalization method
CN110132309B (en) * 2019-06-05 2023-04-25 西京学院 Calibration method of rocker arm inertia/vision combined attitude determination device of coal mining machine
CN111024117B (en) * 2019-11-21 2023-03-14 中国航空工业集团公司西安飞行自动控制研究所 Vision-based inertial navigation system rapid alignment system and alignment method
CN111024117A (en) * 2019-11-21 2020-04-17 中国航空工业集团公司西安飞行自动控制研究所 Vision-based inertial navigation system rapid alignment system and alignment method
CN111862242B (en) * 2020-07-29 2023-11-03 北京轻威科技有限责任公司 Calibration system and method for optical inertial mixing motion capture device
CN111862242A (en) * 2020-07-29 2020-10-30 北京轻威科技有限责任公司 Calibration system and method for optical inertial hybrid motion capture device
WO2022063221A1 (en) * 2020-09-24 2022-03-31 影石创新科技股份有限公司 Method for generating rotation direction of gyroscope and computer device
CN112461125B (en) * 2020-10-29 2023-02-28 北京空间机电研究所 Optical measurement system and measurement method for position and attitude of closed floating air ball
CN112461125A (en) * 2020-10-29 2021-03-09 北京空间机电研究所 Optical measurement system and measurement method for position and attitude of closed floating air ball
WO2022198590A1 (en) * 2021-03-25 2022-09-29 华为技术有限公司 Calibration method and apparatus, intelligent driving system, and vehicle
CN113984090A (en) * 2021-10-25 2022-01-28 北京科技大学 Online calibration and compensation method and device for IMU (inertial measurement Unit) error of wheeled robot
CN113984090B (en) * 2021-10-25 2023-07-04 北京科技大学 Wheel type robot IMU error online calibration and compensation method and device
CN114018291A (en) * 2021-11-08 2022-02-08 中国科学院空天信息创新研究院 Calibration method and device for parameters of inertial measurement unit

Also Published As

Publication number Publication date
CN103278177B (en) 2015-07-01

Similar Documents

Publication Publication Date Title
CN103278177B (en) Calibration method of inertial measurement unit based on camera network measurement
CN104658012B (en) Motion capture method based on inertia and optical measurement fusion
CN107909614B (en) Positioning method of inspection robot in GPS failure environment
CN110617821B (en) Positioning method, positioning device and storage medium
CN104154928B (en) Installation error calibrating method applicable to built-in star sensor of inertial platform
CN108036785A (en) A kind of aircraft position and orientation estimation method based on direct method and inertial navigation fusion
CN110100151A (en) The system and method for global positioning system speed is used in vision inertia ranging
CN107144241B (en) A kind of binocular vision high-precision measuring method based on depth of field compensation
CN108235735A (en) Positioning method and device, electronic equipment and computer program product
CN109520476B (en) System and method for measuring dynamic pose of rear intersection based on inertial measurement unit
CN102175416B (en) Multi-camera dynamic calibration method for measuring model attitude angle in wind tunnel test
CN106708066A (en) Autonomous landing method of unmanned aerial vehicle based on vision/inertial navigation
CN109710724A (en) A kind of method and apparatus of building point cloud map
WO2013004033A1 (en) Precision measurement method and system for star sensor
CN103940442A (en) Location method and device adopting accelerating convergence algorithm
CN103322984B (en) Based on the range finding of video image, speed-measuring method and device
CN110095659B (en) Dynamic testing method for pointing accuracy of communication antenna of deep space exploration patrol device
EP4155873A1 (en) Multi-sensor handle controller hybrid tracking method and device
CN102222333A (en) Method and device of mobile augmented reality of underground engineering based on mixed registration
CN109631876A (en) A kind of inspection prober localization method based on one camera navigation image
CN106969721A (en) A kind of method for three-dimensional measurement and its measurement apparatus
CN107782309A (en) Noninertial system vision and double tops instrument multi tate CKF fusion attitude measurement methods
CN109855822A (en) A kind of high-speed rail bridge based on unmanned plane vertically moves degree of disturbing measurement method
CN105607760A (en) Micro-inertial sensor based track recovery method and system
CN109445599A (en) Interaction pen detection method and 3D interactive system

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant