CN106197412A - The pinpoint method of micro-inertial navigation is carried out based on accelerometer, gyroscope - Google Patents

The pinpoint method of micro-inertial navigation is carried out based on accelerometer, gyroscope Download PDF

Info

Publication number
CN106197412A
CN106197412A CN201610510837.XA CN201610510837A CN106197412A CN 106197412 A CN106197412 A CN 106197412A CN 201610510837 A CN201610510837 A CN 201610510837A CN 106197412 A CN106197412 A CN 106197412A
Authority
CN
China
Prior art keywords
acceleration
accelerometer
patrol officer
gyroscope
travel
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201610510837.XA
Other languages
Chinese (zh)
Inventor
张天承
王春生
关鹏
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.)
BEIJING HAYDEN ZHONGKE TECHNOLOGY Co Ltd
Original Assignee
BEIJING HAYDEN ZHONGKE TECHNOLOGY 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 BEIJING HAYDEN ZHONGKE TECHNOLOGY Co Ltd filed Critical BEIJING HAYDEN ZHONGKE TECHNOLOGY Co Ltd
Priority to CN201610510837.XA priority Critical patent/CN106197412A/en
Publication of CN106197412A publication Critical patent/CN106197412A/en
Pending legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/10Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
    • G01C21/12Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation

Abstract

The present invention proposes and a kind of carries out the pinpoint method of micro-inertial navigation based on accelerometer, gyroscope, including: utilize the acceleration of patrol officer described in accelerometer measures, according to described acceleration, the traveling of described patrol officer carried out disconnected step;Acceleration maximum according to the step in described patrol officer's traveling process and acceleration minima material calculation;Obtain the gyro data of vertical direction, calculate the deflection of the traveling of described patrol officer according to the gyro data of described vertical direction, it is thus achieved that direct of travel;According to patrol officer from a upper location point to the direct of travel of estimation, the length of step-length of marching forward, form new location point, by that analogy, it is thus achieved that multiple location points of described patrol officer, orient and patrol and examine track.The present invention only by the gyroscope in mobile phone, accelerometer, can realize the location to personnel according to default step-length scheduling algorithm, and positioning precision is high and equipment is simple.

Description

The pinpoint method of micro-inertial navigation is carried out based on accelerometer, gyroscope
Technical field
The present invention relates to mobile terminal positioning technology field, carry out micro-particularly to one based on accelerometer, gyroscope The pinpoint method of inertial navigation.
Background technology
Existing personnel positioning mode many employings GPS/ big-dipper satellite location mode, once in the position that signal of communication is the best Putting, above-mentioned location mode just cannot realize, and is limited by personnel region, has certain limitation.
Summary of the invention
The purpose of the present invention is intended at least solve one of described technological deficiency.
To this end, it is an object of the invention to propose a kind of based on accelerometer, that gyroscope carries out micro-inertial navigation is pinpoint Method, only by the gyroscope in mobile phone, accelerometer, can realize the location to personnel according to default step-length scheduling algorithm, fixed Position precision is high and equipment is simple.
To achieve these goals, embodiments of the invention provide one to carry out micro-inertial navigation based on accelerometer, gyroscope Pinpoint method, comprises the steps:
Utilize accelerometer, the movement track of gyroscope measuring and calculating patrol officer patrolling and examining in hand-held set, comprise the steps:
Step S1, utilizes the acceleration of patrol officer described in accelerometer measures, patrols and examines described according to described acceleration The traveling of personnel carries out disconnected step;
Step S2, according to acceleration maximum and the acceleration minima meter of the step in described patrol officer's traveling process Calculate step-length;
Step S3, obtains the gyro data of vertical direction, calculates described according to the gyro data of described vertical direction The deflection of the traveling of patrol officer, it is thus achieved that direct of travel;
Step S4, to the estimation of personnel's travel track in units of a step, the disconnected step obtained according to step S1, to each step According to step S3 obtain patrol officer from a upper location point to estimation direct of travel, the length of step S2 of marching forward estimating step length Degree, forms new location point, by that analogy, it is thus achieved that multiple location points of described patrol officer, orients and patrol and examine track.
Further, described in patrol and examine hand-held set and be positioned at the low back of described patrol officer so that described in patrol and examine hand-held set Movement locus consistent with the movement locus at described patrol officer's low back position.
Further, in described step S1, when described acceleration meets following condition, it is judged that described patrol officer steps One step:
(1) when the acceleration hits of back is more than setting value;
(2) it is more than the square mean number of previous step acceleration when the acceleration maximum of back;
(3) current acceleration positive going zeror crossing.
Further, in described step S2, described step-length L is
L=(amax-amin)0.25,
Wherein, amax is acceleration maximum in a step, and amin is acceleration minima in a step.
Further, in described step S3, described deflection is Anew=A+ ω * Δ t,
Wherein, A is former direct of travel, and ω is new gyroscope sample magnitude, and Δ t is that new sampled value is apart from a upper sampled value Time, Anew is new direct of travel.
Further, in described step S4, described patrol officer's location point is:
(x, y) new=(x+L*cosA, y+L*sinA),
Wherein, (x, y) is personnel's coordinate, and L is step-length, and A is direct of travel.
According to embodiments of the present invention carry out the pinpoint method of micro-inertial navigation based on accelerometer, gyroscope, utilize used Leading location uses the sensors such as accelerometer, the gyroscope of patrolling and examining in hand-held set to calculate the movement track of personnel.By obtaining respectively Take disconnected step, step-length and the direct of travel of patrol officer, extrapolate the new location point of personnel, and so on obtain multiple location points Constitute and patrol and examine track.The present invention is without satellite-signal location such as the GPS/ Big Dippeves, only by the gyroscope in mobile phone, accelerometer, Can realize the location to personnel according to default step-length scheduling algorithm, positioning precision is high and equipment is simple.
Aspect and advantage that the present invention adds will part be given in the following description, and part will become from the following description Obtain substantially, or recognized by the practice of the present invention.
Accompanying drawing explanation
Above-mentioned and/or the additional aspect of the present invention and advantage are from combining the accompanying drawings below description to embodiment and will become Substantially with easy to understand, wherein:
Fig. 1 is to carry out the pinpoint method of micro-inertial navigation according to the embodiment of the present invention based on accelerometer, gyroscope Flow chart.
Detailed description of the invention
Embodiments of the invention are described below in detail, and the example of embodiment is shown in the drawings, the most identical Or similar label represents same or similar element or has the element of same or like function.Retouch below with reference to accompanying drawing The embodiment stated is exemplary, it is intended to is used for explaining the present invention, and is not considered as limiting the invention.
As it is shown in figure 1, the embodiment of the present invention carry out the pinpoint method of micro-inertial navigation based on accelerometer, gyroscope, Utilize accelerometer, the movement track of gyroscope measuring and calculating patrol officer patrolling and examining in hand-held set, comprise the steps:
Step S1, utilizes the acceleration of accelerometer measures patrol officer, enters the traveling of patrol officer according to acceleration The disconnected step of row.
In one embodiment of the invention, patrol and examine hand-held set and be positioned at the low back of patrol officer, so that patrolling and examining hands The movement locus holding machine is consistent with the movement locus at patrol officer's low back position.
Human body, during advancing, can produce at vertical direction when single foot lands and the most significantly impact.When acceleration is full When being enough to lower condition, it is judged that patrol officer steps a step:
(1) when the acceleration hits of back is more than setting value, wherein, setting value can be that 0.05 times of gravity accelerates Degree;
(2) it is more than the square mean number of previous step acceleration when the acceleration maximum of back;
(3) current acceleration positive going zeror crossing.
Step S2, acceleration maximum and acceleration minima according to the step in patrol officer's traveling process calculate step Long.Wherein, in traveling process, the severe degree of human body acceleration and the step-length existence function relation of single step, material calculation L is:
L=(amax-amin)0.25,
Wherein, amax is acceleration maximum in a step, and amin is acceleration minima in a step.
Step S3, when wearing hand-held set by regulation requirement, hand-held set and health keep vertical direction substantially, obtain vertically side To gyro data, calculate the deflection of the traveling of patrol officer according to the gyro data of vertical direction, it is thus achieved that traveling side To.
Deflection is Anew=A+ ω * Δ t,
Wherein, A is former direct of travel, and ω is new gyroscope sample magnitude, and Δ t is that new sampled value is apart from a upper sampled value Time, Anew is new direct of travel.
Step S4, to the estimation of personnel's travel track in units of a step, the disconnected step obtained according to step S1, to each step According to step S3 obtain patrol officer from a upper location point to estimation direct of travel, the length of step S2 of marching forward estimating step length Degree, forms new location point, by that analogy, it is thus achieved that multiple location points of patrol officer, orients and patrol and examine track.
Patrol officer's location point is:
(x, y) new=(x+L*cosA, y+L*sinA),
Wherein, (x, y) is personnel's coordinate, and L is step-length, and A is direct of travel.
According to embodiments of the present invention carry out the pinpoint method of micro-inertial navigation based on accelerometer, gyroscope, utilize used Leading location uses the sensors such as accelerometer, the gyroscope of patrolling and examining in hand-held set to calculate the movement track of personnel.By obtaining respectively Take disconnected step, step-length and the direct of travel of patrol officer, extrapolate the new location point of personnel, and so on obtain multiple location points Constitute and patrol and examine track.The present invention is without satellite-signal location such as the GPS/ Big Dippeves, only by the gyroscope in mobile phone, accelerometer, Can realize the location to personnel according to default step-length scheduling algorithm, positioning precision is high and equipment is simple.
In the description of this specification, reference term " embodiment ", " some embodiments ", " example ", " specifically show Example " or the description of " some examples " etc. means to combine this embodiment or example describes specific features, structure, material or spy Point is contained at least one embodiment or the example of the present invention.In this manual, to the schematic representation of above-mentioned term not Necessarily refer to identical embodiment or example.And, the specific features of description, structure, material or feature can be any One or more embodiments or example in combine in an appropriate manner.
Although above it has been shown and described that embodiments of the invention, it is to be understood that above-described embodiment is example Property, it is impossible to be interpreted as limitation of the present invention, those of ordinary skill in the art is without departing from the principle of the present invention and objective In the case of above-described embodiment can be changed within the scope of the invention, revise, replace and modification.The scope of the present invention Extremely it is equal to by claims and limits.

Claims (6)

1. one kind carries out the pinpoint method of micro-inertial navigation based on accelerometer, gyroscope, it is characterised in that utilization is patrolled and examined hand-held Accelerometer in machine, the movement track of gyroscope measuring and calculating patrol officer, comprise the steps:
Step S1, utilizes the acceleration of patrol officer described in accelerometer measures, according to described acceleration to described patrol officer Traveling carry out disconnected step;
Step S2, acceleration maximum and acceleration minima according to the step in described patrol officer's traveling process calculate step Long;
Step S3, obtains the gyro data of vertical direction, patrols and examines according to the gyro data calculating of described vertical direction The deflection of the traveling of personnel, it is thus achieved that direct of travel;
Step S4, to the estimation of personnel's travel track in units of a step, the disconnected step obtained according to step S1, to each step according to Step S3 obtain patrol officer from a upper location point to estimation direct of travel, the length of step S2 of marching forward estimating step length, Form new location point, by that analogy, it is thus achieved that multiple location points of described patrol officer, orient and patrol and examine track.
2. carrying out the pinpoint method of micro-inertial navigation based on accelerometer, gyroscope as claimed in claim 1, its feature exists In, described in patrol and examine hand-held set and be positioned at the low back of described patrol officer so that described in patrol and examine the movement locus of hand-held set with The movement locus at described patrol officer's low back position is consistent.
3. carrying out the pinpoint method of micro-inertial navigation based on accelerometer, gyroscope as claimed in claim 1, its feature exists In, in described step S1, when described acceleration meets following condition, it is judged that described patrol officer steps a step:
(1) when the acceleration hits of back is more than setting value;
(2) it is more than the square mean number of previous step acceleration when the acceleration maximum of back;
(3) current acceleration positive going zeror crossing.
4. carrying out the pinpoint method of micro-inertial navigation based on accelerometer, gyroscope as claimed in claim 1, its feature exists In, in described step S2, described step-length L is
L=(amax-amin)0.25,
Wherein, amax is acceleration maximum in a step, and amin is acceleration minima in a step.
5. carrying out the pinpoint method of micro-inertial navigation based on accelerometer, gyroscope as claimed in claim 1, its feature exists In, in described step S3, described deflection is Anew=A+ ω * Δ t,
Wherein, A is former direct of travel, and ω is new gyroscope sample magnitude, Δ t be new sampled value apart from a upper sampled value time Between, Anew is new direct of travel.
6. carrying out the pinpoint method of micro-inertial navigation based on accelerometer, gyroscope as claimed in claim 1, its feature exists In, in described step S4, described patrol officer's location point is:
(x, y) new=(x+L*cosA, y+L*sinA),
Wherein, (x, y) is personnel's coordinate, and L is step-length, and A is direct of travel.
CN201610510837.XA 2016-06-30 2016-06-30 The pinpoint method of micro-inertial navigation is carried out based on accelerometer, gyroscope Pending CN106197412A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610510837.XA CN106197412A (en) 2016-06-30 2016-06-30 The pinpoint method of micro-inertial navigation is carried out based on accelerometer, gyroscope

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610510837.XA CN106197412A (en) 2016-06-30 2016-06-30 The pinpoint method of micro-inertial navigation is carried out based on accelerometer, gyroscope

Publications (1)

Publication Number Publication Date
CN106197412A true CN106197412A (en) 2016-12-07

Family

ID=57464546

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610510837.XA Pending CN106197412A (en) 2016-06-30 2016-06-30 The pinpoint method of micro-inertial navigation is carried out based on accelerometer, gyroscope

Country Status (1)

Country Link
CN (1) CN106197412A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115661971A (en) * 2022-12-27 2023-01-31 长江空间信息技术工程有限公司(武汉) Intelligent inspection method and device, computing equipment and storage medium

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102087109A (en) * 2009-12-04 2011-06-08 财团法人资讯工业策进会 System, device and method for estimating position
CN103616034A (en) * 2013-12-10 2014-03-05 山东省计算中心 Network pedometer based on Bluetooth and step calculation method
CN104101341A (en) * 2013-04-02 2014-10-15 广州三星通信技术研究有限公司 Method for positioning between mobile terminals and mobile terminal using the same
CN104713568A (en) * 2015-03-31 2015-06-17 上海帝仪科技有限公司 Gait recognition method and corresponding pedometer
CN104978775A (en) * 2014-04-04 2015-10-14 江苏中科泛联物联网科技股份有限公司 Inspection method and inspection system based on multi-sensor intelligent terminal
CN105241454A (en) * 2015-10-23 2016-01-13 中国兵器工业集团第二一四研究所苏州研发中心 System and method for pedestrian navigation based on multiple sensors

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102087109A (en) * 2009-12-04 2011-06-08 财团法人资讯工业策进会 System, device and method for estimating position
CN104101341A (en) * 2013-04-02 2014-10-15 广州三星通信技术研究有限公司 Method for positioning between mobile terminals and mobile terminal using the same
CN103616034A (en) * 2013-12-10 2014-03-05 山东省计算中心 Network pedometer based on Bluetooth and step calculation method
CN104978775A (en) * 2014-04-04 2015-10-14 江苏中科泛联物联网科技股份有限公司 Inspection method and inspection system based on multi-sensor intelligent terminal
CN104713568A (en) * 2015-03-31 2015-06-17 上海帝仪科技有限公司 Gait recognition method and corresponding pedometer
CN105241454A (en) * 2015-10-23 2016-01-13 中国兵器工业集团第二一四研究所苏州研发中心 System and method for pedestrian navigation based on multiple sensors

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115661971A (en) * 2022-12-27 2023-01-31 长江空间信息技术工程有限公司(武汉) Intelligent inspection method and device, computing equipment and storage medium

Similar Documents

Publication Publication Date Title
CN103940425B (en) A kind of magnetic inertia combines Strapdown inertial measurement method
CN110146077A (en) Pose of mobile robot angle calculation method
CN106595652B (en) Alignment methods between the backtracking formula of vehicle kinematics constraint auxiliary is advanced
CN109682377A (en) A kind of Attitude estimation method based on the decline of dynamic step length gradient
JP2016502069A5 (en)
CN107192387A (en) A kind of combined positioning method based on Unscented kalman filtering
CN107289930A (en) Pure inertia automobile navigation method based on MEMS Inertial Measurement Units
CN110764506B (en) Course angle fusion method and device of mobile robot and mobile robot
CN104864874B (en) A kind of inexpensive single gyro dead reckoning navigation method and system
CN112334736A (en) Method for calibrating a magnetometer of an object
CN106197376B (en) Car body obliqueness measurement method based on uniaxial MEMS inertial sensor
JP6645481B2 (en) Activity record data processing device, activity record data processing method, and activity record data processing program
JP6686985B2 (en) Trajectory estimation device, trajectory estimation method, and trajectory estimation program
CN111307114B (en) Water surface ship horizontal attitude measurement method based on motion reference unit
CN106197412A (en) The pinpoint method of micro-inertial navigation is carried out based on accelerometer, gyroscope
CN106986007B (en) Flight instruments and flying method
CN109752023B (en) Method for quickly estimating motion state of target
CN104699987B (en) A kind of arm inertia-type motion capture data fusion method
WO2012046508A1 (en) Travel track sensing device
CN105352528B (en) A kind of ins error online compensation method applied to ballistic missile
CN105203112B (en) A kind of martian atmosphere approach section accompanying flying beacon auxiliary navigation method
CN205403801U (en) Multisensor information fusion's on -vehicle DR system
CN110030992B (en) Air flyer high-speed rotation angle movement measuring method based on magnetometer
CN108510550A (en) A kind of binocular camera automatic calibration method and device
US10209069B2 (en) Offset calculation circuit and azimuth sensor using the same

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
EE01 Entry into force of recordation of patent licensing contract
EE01 Entry into force of recordation of patent licensing contract

Application publication date: 20161207

Assignee: Dongying Huada Electronic Technology Co., Ltd.

Assignor: BEIJING HAYDEN ZHONGKE TECHNOLOGY CO., LTD.

Contract record no.: 2017990000036

Denomination of invention: The pinpoint method of micro-inertial navigation is carried out based on accelerometer, gyroscope

License type: Common License

Record date: 20170125

RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20161207