CN107894603A - A kind of method based on Low-cost GPS inertia combined navigation positioning and optimizing - Google Patents

A kind of method based on Low-cost GPS inertia combined navigation positioning and optimizing Download PDF

Info

Publication number
CN107894603A
CN107894603A CN201711392601.1A CN201711392601A CN107894603A CN 107894603 A CN107894603 A CN 107894603A CN 201711392601 A CN201711392601 A CN 201711392601A CN 107894603 A CN107894603 A CN 107894603A
Authority
CN
China
Prior art keywords
gps
points
distance
low
calculated
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
CN201711392601.1A
Other languages
Chinese (zh)
Inventor
李黎黎
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.)
Heilongjiang Huida Technology Development Co Ltd
Original Assignee
Heilongjiang Huida Technology Development 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 Heilongjiang Huida Technology Development Co Ltd filed Critical Heilongjiang Huida Technology Development Co Ltd
Priority to CN201711392601.1A priority Critical patent/CN107894603A/en
Publication of CN107894603A publication Critical patent/CN107894603A/en
Pending legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S19/00Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/38Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
    • G01S19/39Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/42Determining position
    • G01S19/45Determining position by combining measurements of signals from the satellite radio beacon positioning system with a supplementary measurement
    • G01S19/47Determining position by combining measurements of signals from the satellite radio beacon positioning system with a supplementary measurement the supplementary measurement being an inertial measurement, e.g. tightly coupled inertial
    • 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
    • G01C21/165Navigation; 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 combined with non-inertial navigation instruments

Abstract

The invention discloses a kind of method based on Low-cost GPS inertia combined navigation positioning and optimizing, comprise the steps of:A, the latitude and longitude coordinates and deflection of vehicle can be got in real time from GPS;B, the angle change of vehicle movement, i.e. the deflection change from A points to B points in the horizontal direction are calculated using gyroscope;C, distance is calculated using accelerometer, i.e., quadratic integral is carried out to acceleration, get A points to the distance of B points;D, according to A point coordinates and move distance, B point coordinates is extrapolated;E, an EKF blending algorithm is designed, step A and step D output result are input in EKF, merge out an optimal coordinate.The beneficial effects of the invention are as follows:In GPS no signals, a metastable coordinate points can also be got.There is very big improvement for the problem of GPS scatterplots.

Description

A kind of method based on Low-cost GPS inertia combined navigation positioning and optimizing
Technical field
The present invention relates to GPS technology field, specifically a kind of side based on Low-cost GPS inertia combined navigation positioning and optimizing Method.
Background technology
Existing vehicle-mounted intelligent monitoring product uses pure GPS location, and the GPS of low cost has problems with: During no signal, position error is very big or can not position.When having signal, it may appear that scatterplot situation, i.e., it is fixed when walking straight line The coordinate points of position out have greatly not on this straight line.
The content of the invention
It is an object of the invention to provide a kind of method based on Low-cost GPS inertia combined navigation positioning and optimizing, with solution The problem of being proposed in certainly above-mentioned background technology.
To achieve the above object, the present invention provides following technical scheme:
A kind of method based on Low-cost GPS inertia combined navigation positioning and optimizing, is comprised the steps of:
A, the latitude and longitude coordinates and deflection of vehicle can be got in real time from GPS;
B, the angle change of vehicle movement, i.e. the deflection change from A points to B points in the horizontal direction are calculated using gyroscope;
C, distance is calculated using accelerometer, i.e., quadratic integral is carried out to acceleration, get A points to the distance of B points;
D, according to A point coordinates and move distance, B point coordinates is extrapolated;
E, an EKF blending algorithm is designed, step A and step D output result are input in EKF, merges out one most preferably Coordinate.
One kind is based on Low-cost GPS inertia combined navigation alignment system, including GPS, gyroscope, accelerometer, DR boat position Calculate that module and extended Kalman filter, the extended Kalman filter connect GPS and DR dead-reckoning modules, DR respectively Dead-reckoning module is also respectively connected with gyroscope and accelerometer.
Compared with prior art, the beneficial effects of the invention are as follows:In GPS no signals, one can also be got relatively Stable coordinate points.There is very big improvement for the problem of GPS scatterplots.
Brief description of the drawings
Fig. 1 is the structured flowchart based on Low-cost GPS inertia combined navigation alignment system.
Fig. 2 is the schematic diagram of the embodiment of the present invention.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete Site preparation describes, it is clear that described embodiment is only part of the embodiment of the present invention, rather than whole embodiments.It is based on Embodiment in the present invention, those of ordinary skill in the art are obtained every other under the premise of creative work is not made Embodiment, belong to the scope of protection of the invention.
Fig. 1-2 is referred to, a kind of method based on Low-cost GPS inertia combined navigation positioning and optimizing, is comprised the steps of:
A, the latitude and longitude coordinates and deflection of vehicle can be got in real time from GPS;
B, the angle change of vehicle movement, i.e. the deflection change from A points to B points in the horizontal direction are calculated using gyroscope;
C, distance is calculated using accelerometer, i.e., quadratic integral is carried out to acceleration, get A points to the distance of B points;
D, according to A point coordinates and move distance, B point coordinates is extrapolated;
E, an EKF blending algorithm is designed, step A and step D output result are input in EKF, merges out one most preferably Coordinate.
One kind is based on Low-cost GPS inertia combined navigation alignment system, including GPS, gyroscope, accelerometer, DR boat position Calculate that module and extended Kalman filter, the extended Kalman filter connect GPS and DR dead-reckoning modules, DR respectively Dead-reckoning module is also respectively connected with gyroscope and accelerometer.
The present invention operation principle be:Tested in the complicated plot of an environment, A roads have tree, and B is blocked, and C exists In tunnel, D is more open.
As seen from the figure, at C, GPS is in the state of complete no signal, and the coordinate after optimizing is relatively stable; A, blocked at B, so scatterplot situation be present, and the coordinate after optimizing is than more uniform.
It is obvious to a person skilled in the art that the invention is not restricted to the details of above-mentioned one exemplary embodiment, Er Qie In the case of without departing substantially from spirit or essential attributes of the invention, the present invention can be realized in other specific forms.Therefore, no matter From the point of view of which point, embodiment all should be regarded as exemplary, and be nonrestrictive, the scope of the present invention is by appended power Profit requires rather than described above limits, it is intended that all in the implication and scope of the equivalency of claim by falling Change is included in the present invention.Any reference in claim should not be considered as to the involved claim of limitation.
Moreover, it will be appreciated that although the present specification is described in terms of embodiments, not each embodiment is only wrapped Containing an independent technical scheme, this narrating mode of specification is only that those skilled in the art should for clarity Using specification as an entirety, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art It is appreciated that other embodiment.

Claims (2)

  1. A kind of 1. method based on Low-cost GPS inertia combined navigation positioning and optimizing, it is characterised in that comprise the steps of:
    A, the latitude and longitude coordinates and deflection of vehicle can be got in real time from GPS;
    B, the angle change of vehicle movement, i.e. the deflection change from A points to B points in the horizontal direction are calculated using gyroscope;
    C, distance is calculated using accelerometer, i.e., quadratic integral is carried out to acceleration, get A points to the distance of B points;
    D, according to A point coordinates and move distance, B point coordinates is extrapolated;
    E, an EKF blending algorithm is designed, step A and step D output result are input in EKF, merges out one most preferably Coordinate.
  2. 2. one kind is based on Low-cost GPS inertia combined navigation alignment system, it is characterised in that including GPS, gyroscope, acceleration Meter, DR dead-reckoning modules and extended Kalman filter, the extended Kalman filter connect GPS and DR boats position and pushed away respectively Module is calculated, DR dead-reckoning modules are also respectively connected with gyroscope and accelerometer.
CN201711392601.1A 2017-12-21 2017-12-21 A kind of method based on Low-cost GPS inertia combined navigation positioning and optimizing Pending CN107894603A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711392601.1A CN107894603A (en) 2017-12-21 2017-12-21 A kind of method based on Low-cost GPS inertia combined navigation positioning and optimizing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711392601.1A CN107894603A (en) 2017-12-21 2017-12-21 A kind of method based on Low-cost GPS inertia combined navigation positioning and optimizing

Publications (1)

Publication Number Publication Date
CN107894603A true CN107894603A (en) 2018-04-10

Family

ID=61808456

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201711392601.1A Pending CN107894603A (en) 2017-12-21 2017-12-21 A kind of method based on Low-cost GPS inertia combined navigation positioning and optimizing

Country Status (1)

Country Link
CN (1) CN107894603A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108873780A (en) * 2018-07-04 2018-11-23 李艳华 A kind of preceding dress TPMS device for supporting automatic positioning function
CN109031373A (en) * 2018-06-08 2018-12-18 北京航天光华电子技术有限公司 A kind of Intelligent Mobile Robot navigation system and method

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101907714A (en) * 2010-06-25 2010-12-08 陶洋 GPS aided positioning system and method based on multi-sensor data fusion
CN102519463A (en) * 2011-12-13 2012-06-27 华南理工大学 Navigation method and device based on extended Kalman filter
CN104698485A (en) * 2015-01-09 2015-06-10 中国电子科技集团公司第三十八研究所 BD, GPS and MEMS based integrated navigation system and method

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101907714A (en) * 2010-06-25 2010-12-08 陶洋 GPS aided positioning system and method based on multi-sensor data fusion
CN102519463A (en) * 2011-12-13 2012-06-27 华南理工大学 Navigation method and device based on extended Kalman filter
CN104698485A (en) * 2015-01-09 2015-06-10 中国电子科技集团公司第三十八研究所 BD, GPS and MEMS based integrated navigation system and method

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109031373A (en) * 2018-06-08 2018-12-18 北京航天光华电子技术有限公司 A kind of Intelligent Mobile Robot navigation system and method
CN108873780A (en) * 2018-07-04 2018-11-23 李艳华 A kind of preceding dress TPMS device for supporting automatic positioning function

Similar Documents

Publication Publication Date Title
CN104501838B (en) SINS Initial Alignment Method
CN102636149A (en) Combined measurement device and method for dynamic deformation of flexible bodies
CN102436004A (en) Positioning system and method thereof
CN101476891A (en) Accurate navigation system and method for movable object
CN103117011B (en) Dynamic positioning simulation test platform and position control method
CN103557876A (en) Strapdown inertial navigation initial alignment method for antenna tracking and stabilizing platform
CN102565834A (en) Single-frequency GPS (Global Positioning System) direction-finding system and direction-finding and positioning method thereof
CN105865461A (en) Automobile positioning system and method based on multi-sensor fusion algorithm
CN109807911A (en) Based on GNSS, UWB, IMU, laser radar, code-disc the multi-environment joint positioning method of outdoor patrol robot
CN102506872B (en) Method for judging flight route deviation
CN106681336A (en) Unmanned-aerial-vehicle height measurement control system based on fault-tolerance processing and control method
CN106840211A (en) A kind of SINS Initial Alignment of Large Azimuth Misalignment On methods based on KF and STUPF combined filters
CN103335649A (en) Inertial navigation system polar navigation parameter calculating method
CN110346824A (en) A kind of automobile navigation method, system, device and readable storage medium storing program for executing
CN107894603A (en) A kind of method based on Low-cost GPS inertia combined navigation positioning and optimizing
CN103674059A (en) External measured speed information-based horizontal attitude error correction method for SINS (serial inertial navigation system)
KR20220052312A (en) Vehicle positioning method, apparatus and autonomous driving vehicle
RU2539140C1 (en) Integrated strapdown system of navigation of average accuracy for unmanned aerial vehicle
KR20240011201A (en) Vehicle positioning methods, devices, electronic devices and storage media
CN104216405B (en) The air navigation aid and equipment of field robot
CN202649469U (en) Positioning device for judging position of effective global satellite positioning system
CN106403999A (en) GNSS-based real-time compensation method for inertial navigation accelerometer drifting
CN110356862B (en) Anti-collision method and system for stacker-reclaimer based on GPS positioning
CN103471593B (en) A kind of inertial navigation system measuring error modification method based on GPS information
RU2539131C1 (en) Strapdown integrated navigation system of average accuracy for mobile onshore objects

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

Application publication date: 20180410