CN102359787A - WSN/MINS high-precision and real-time combination navigation information fusion method - Google Patents

WSN/MINS high-precision and real-time combination navigation information fusion method Download PDF

Info

Publication number
CN102359787A
CN102359787A CN2011101976900A CN201110197690A CN102359787A CN 102359787 A CN102359787 A CN 102359787A CN 2011101976900 A CN2011101976900 A CN 2011101976900A CN 201110197690 A CN201110197690 A CN 201110197690A CN 102359787 A CN102359787 A CN 102359787A
Authority
CN
China
Prior art keywords
mins
wsn
navigation
navigation information
zone
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
CN2011101976900A
Other languages
Chinese (zh)
Other versions
CN102359787B (en
Inventor
陈熙源
徐元
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.)
Southeast University
Original Assignee
Southeast University
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 Southeast University filed Critical Southeast University
Priority to CN 201110197690 priority Critical patent/CN102359787B/en
Publication of CN102359787A publication Critical patent/CN102359787A/en
Application granted granted Critical
Publication of CN102359787B publication Critical patent/CN102359787B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Position Fixing By Use Of Radio Waves (AREA)

Abstract

The invention relates to a WSN/MINS high-precision and real-time combination navigation information fusion method, and belongs to the technical field of combined positioning under a complex environment. According to the method, a wireless positioning network is autonomously built under a closed and complex environment; a LS-SVM method is adopted to train a navigation error model of a MINS navigation system; when the MINS navigation system leaves the training area, the navigation system is compensated depending on the previous trained error model. In the prior art, the positioning precision of the conventional MINS navigation system generates the drift along with the time, and the effective training network can not be provided under the closed environment. With the present invention, the disadvantages and the problems of the conventional MINS navigation system in the prior art are overcome; the persistent high-precision and real-time navigation is provided; the method can be applicable for long-distance and high-precision target positioning and tracking in the indoor environment, the underground mine and other closed and complex environments.

Description

Integrated navigation information fusion method during a kind of WSN/MINS high-precision real
Technical field
The integrated navigation information fusion method belongs to combined orientation technology field under the complex environment when the present invention relates to a kind of WSN/MINS high-precision real.
Background technology
In recent years, the demand of unknown node precise position information has been promoted the development of placement technology, this trend will remain unchanged in the following a very long time.In existing locator meams, satellite navigation and inertial navigation are the most frequently used dual modes.Wherein (Global Positioning System GPS) is a kind of mode the most commonly used to GPS.Though GPS can pass through the continual and steady positional information of precision; The drawbacks limit of external environments such as but it is subject to electromagnetic interference (EMI), block influence its range of application; Particularly in some scenes airtight, circumstance complication such as indoor, underground passages; Gps signal is seriously blocked, and can't effectively work.Micro-inertial navigation system (MEMS inertial navigation system; MINS) have complete autonomous, movable information comprehensively, in short-term, high-precision advantage; Though can realize independent navigation, error accumulates in time, will cause navigation accuracy seriously to descend under the service condition during long the boat.In order to overcome the shortcoming that independent use MINS or GPS navigation equipment are produced, combine the advantage of the two, many scholars merge above-mentioned two kinds of navigate modes, have formed GPS/MINS integrated navigation technology.Though integrated navigation system can compensate GPS losing lock situation through MINS; But because the error of MINS accumulates in time; This compensation can only be the short-term compensation, in case system is under the situation of GPS losing lock for a long time, bearing accuracy is difficult to reach long-time steady state (SS).In order to obtain metastable bearing accuracy, many scholars are applied to some intelligent algorithms in the integrated navigation system, and this method can make navigational system keep long-time must stablizing, but its bearing accuracy has very big dependence to the selection of training space.Yet under environment such as indoor, underground passage, gps signal is very faint, is difficult to build suitable training space.
In recent years, (Wireless Sensors Network, WSN) characteristics with its low cost, low-power consumption and low system complexity show very big potentiality in the short distance positioning field to wireless sensor network.Adopt WSN to carry out the short distance location and become a research focus gradually.The WSN location needs two category nodes to accomplish the location jointly: anchor node and blind node.Wherein anchor node is the node of location aware, and blind node is the unknown node in position.Adopting location technology among the present WSN all is to accomplish through one or several wireless channel physical parameter of measuring between unknown node and the known node.In position fixing process, when needs obtained the positional information of blind node, blind node at first sent Location Request obtaining corresponding wireless channel physical parameter between itself and the anchor node to anchor node, and these parameter informations are converted into corresponding range information.Obtain after the corresponding range information, (estimate that like maximum likelihood (Maximum Likehood Estimate, MLE) etc.) calculates the relative position information of blind node and anchor node, its concrete steps are as shown in Figure 1 through some data fusion methods.Compare with the conventional positioning mode; Except characteristics with low cost, low-power consumption and low system complexity; WSN can also independently accomplish the establishment of network, and making to position in some scenes airtight, circumstance complication such as indoor, underground passages becomes possibility.
WSN is that the unknown node location under the closed environment provides possibility; But because the communication technology that WSN adopts is generally short-distance wireless communication technology (like ZigBee, WIFI etc.); Therefore if want to accomplish the target following location of long distance; Need a large amount of network nodes to accomplish jointly, this does not also meet the demand of WSN low cost, low-power consumption.Though MINS can accomplish independent navigation, broken away from not the shortcoming that bearing accuracy is drifted about in time.
Summary of the invention
In order to address the above problem; Integrated navigation information fusion method when the invention provides a kind of WSN/MINS high-precision real; Through under airtight complex environment, independently building the wireless location network, adopt the navigation error model training of least square support vector long-pending (LS-SVM method), when the MINS navigational system is left training space to the MINS navigational system; The error model of training compensates navigational system before relying on; Overcome the shortcoming that traditional MINS positioning precision of navigation system is drifted about in time, and the problem that effective training network can't be provided under closed environment, lasting high precision real-time navigation is provided.
The present invention adopts following technical scheme for solving its technical matters:
The integrated navigation information fusion method comprises the following steps: during a kind of WSN/MINS high-precision real
(1) integrated navigation system is divided into training space and adaptive equalization zone two parts; Described training space is the zone of building WSN, and described adaptive equalization zone is for having only the zone of MINS signal;
(2) at training space; Wireless location and MINS navigational system based on WSN are worked simultaneously; At first utilize the relative navigation information of measuring unknown node based on the wireless location technology of WSN, the absolute navigation information that obtains on relative navigation information and the micro-inertial navigation system is carried out data fusion through extended Kalman filter;
(3) adopting EKF to carry out data fusion; And when drawing optimum navigation information, wave filter is made the error model that control information feeds back to WSN and MINS respectively, to the WSN wireless location system; Error model can be revised the relative position and the speed of unknown node; And to the MINS system, the optimal estimation that position, velocity error and the wave filter that MINS self is estimated provides gives training through the LS-SVM intelligent algorithm, seeks the relation between the two;
(4) leave the zone of building WSN when unknown node and get into the adaptive equalization zone; In this zone; Integrated navigation system obtains the relative navigation information of measuring less than WSN; Can only rely on the MINS system to accomplish this a part of independent navigation, the error model that MINS is utilized in the training space training carries out error compensation to the absolute navigation information of measuring, and obtains optimum navigation information.
Beneficial effect of the present invention is following:
1, utilizes the relative navigation information of measuring based on the wireless location technology of WSN; Carry out data fusion with the absolute navigation information that obtains on the MINS through extended Kalman filter; The navigation information that obtains, the precision of information that obtains than above-mentioned any single air navigation aid is higher.
2, the MINS error model that is utilized in training space training carries out error compensation to the absolute navigation information of measuring, and obtains optimum navigation information, has avoided can't working because of the WSN navigation causing navigation error to descend, can't guarantee the problem of navigation accuracy fast.
3, can be used for indoorly, the length under the airtight complex environment such as underground mine is followed the tracks of apart from the high precision target localization.
Description of drawings
Fig. 1 is the node locating step based on WSN.
Fig. 2 is a training space integrated navigation model.
Fig. 3 is adaptive equalization zone integrated navigation model.
Embodiment
Below in conjunction with accompanying drawing the invention is explained further details.
Like Fig. 2 is training space integrated navigation model; At training space; Wireless location and MINS navigational system based on WSN are worked simultaneously; At first utilize the relative navigation information of measuring unknown node based on the wireless location technology of WSN, the absolute navigation information that obtains on relative navigation information and the micro-inertial navigation system is carried out data fusion through extended Kalman filter; Adopting EKF to carry out data fusion; And when drawing optimum navigation information, wave filter is made the error model that control information feeds back to WSN and MINS respectively, to the WSN wireless location system; Error model can be revised the relative position and the speed of unknown node; And to the MINS system, the optimal estimation that position, velocity error and the wave filter that MINS self is estimated provides gives training through the LS-SVM intelligent algorithm, seeks the relation between the two.Concerning the WSN wireless location system, error model can be revised the relative position and the speed of unknown node.And concerning the MINS system, the optimal estimation that position, velocity error and the wave filter that MINS self is estimated provides gives training, seeks the relation between the two.
When unknown node is left the zone of building WSN, then integrated navigation system gets into the adaptive equalization zone, and is as shown in Figure 3.In this zone, integrated navigation system obtains the relative navigation information of measuring less than WSN, can only rely on the MINS system to accomplish this a part of independent navigation.The error model that MINS is utilized in the training space training carries out error compensation to the absolute navigation information of measuring; Obtain optimum navigation information; Avoided causing navigation error to descend, can't guarantee the problem of navigation accuracy fast, had certain feasibility and perspective because of WSN navigates to work.

Claims (1)

1. integrated navigation information fusion method during a WSN/MINS high-precision real is characterized in that comprising the following steps:
(1) integrated navigation system is divided into training space and adaptive equalization zone two parts, described training space is the zone of building WSN, and described adaptive equalization zone is for having only the zone of MINS signal;
(2) at training space; Wireless location and MINS navigational system based on WSN are worked simultaneously; At first utilize the relative navigation information of measuring unknown node based on the wireless location technology of WSN, the absolute navigation information that obtains on relative navigation information and the micro-inertial navigation system is carried out data fusion through extended Kalman filter;
(3) adopting EKF to carry out data fusion; And when drawing optimum navigation information, wave filter is made the error model that control information feeds back to WSN and MINS respectively, to the WSN wireless location system; Error model can be revised the relative position and the speed of unknown node; And to the MINS system, the optimal estimation that position, velocity error and the wave filter that MINS self is estimated provides gives training through the LS-SVM intelligent algorithm, seeks the relation between the two;
(4) leave the zone of building WSN when unknown node and get into the adaptive equalization zone; In this zone; Integrated navigation system obtains the relative navigation information of measuring less than WSN; Can only rely on the MINS system to accomplish this a part of independent navigation, the error model that MINS is utilized in the training space training carries out error compensation to the absolute navigation information of measuring, and obtains optimum navigation information.
CN 201110197690 2011-07-15 2011-07-15 WSN/MINS high-precision and real-time combination navigation information fusion method Active CN102359787B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201110197690 CN102359787B (en) 2011-07-15 2011-07-15 WSN/MINS high-precision and real-time combination navigation information fusion method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201110197690 CN102359787B (en) 2011-07-15 2011-07-15 WSN/MINS high-precision and real-time combination navigation information fusion method

Publications (2)

Publication Number Publication Date
CN102359787A true CN102359787A (en) 2012-02-22
CN102359787B CN102359787B (en) 2013-07-03

Family

ID=45585151

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201110197690 Active CN102359787B (en) 2011-07-15 2011-07-15 WSN/MINS high-precision and real-time combination navigation information fusion method

Country Status (1)

Country Link
CN (1) CN102359787B (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102679977A (en) * 2012-06-20 2012-09-19 南京航空航天大学 Distributive navigation unit based on inertia network and information fusion method thereof
CN102682572A (en) * 2012-03-27 2012-09-19 南京邮电大学 Wireless sensor network positioning-based intelligent person nursing method
CN104374389A (en) * 2014-12-10 2015-02-25 济南大学 Indoor mobile robot oriented IMU/WSN (inertial measurement unit/wireless sensor network) integrated navigation method
CN105737833A (en) * 2016-05-13 2016-07-06 上海会志信息科技有限公司 Indoor navigation method and indoor navigation device
CN106840154A (en) * 2017-03-21 2017-06-13 江苏星月测绘科技股份有限公司 Underground space inertia measurement and wireless senser integrated positioning system and method
CN109459025A (en) * 2018-11-08 2019-03-12 中北大学 A kind of class brain air navigation aid based on light stream UWB combination
CN109655060A (en) * 2019-02-19 2019-04-19 济南大学 Based on the KF/FIR and LS-SVM INS/UWB Integrated Navigation Algorithm merged and system
CN109916401A (en) * 2019-04-17 2019-06-21 济南大学 Using the seamless tight integration navigation methods and systems of distribution of LS-SVM auxiliary EKF filtering method
CN110530362A (en) * 2019-09-05 2019-12-03 北京航空航天大学 A kind of fireman's indoor orientation method based on single reference mode/inertia combination

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101858980A (en) * 2010-05-18 2010-10-13 东南大学 Intelligent hypercompact combination navigation method of vehicle-mounted GPS software-based receiver
CN101867868A (en) * 2010-03-26 2010-10-20 东南大学 Combined navigation unit and implementing method thereof

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101867868A (en) * 2010-03-26 2010-10-20 东南大学 Combined navigation unit and implementing method thereof
CN101858980A (en) * 2010-05-18 2010-10-13 东南大学 Intelligent hypercompact combination navigation method of vehicle-mounted GPS software-based receiver

Non-Patent Citations (4)

* Cited by examiner, † Cited by third party
Title
李正强等: "信息融合技术在组合导航***的应用", 《飞行力学》, vol. 24, no. 1, 31 March 2006 (2006-03-31) *
滕继涛等: "GNSS/INU/DMAP组合导航定位技术在车辆导航中的应用", 《中国惯性技术学报》, vol. 11, no. 1, 28 February 2003 (2003-02-28) *
祝雪芬等: "卡尔曼/粒子滤波器在船用组合导航中的应用", 《舰船电子工程》, vol. 29, no. 4, 30 April 2009 (2009-04-30) *
郭涛等: "无线电辅助捷联惯性导航***的设计及工程实现", 《导航与控制》, vol. 9, no. 1, 28 February 2010 (2010-02-28) *

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102682572A (en) * 2012-03-27 2012-09-19 南京邮电大学 Wireless sensor network positioning-based intelligent person nursing method
CN102679977A (en) * 2012-06-20 2012-09-19 南京航空航天大学 Distributive navigation unit based on inertia network and information fusion method thereof
CN104374389A (en) * 2014-12-10 2015-02-25 济南大学 Indoor mobile robot oriented IMU/WSN (inertial measurement unit/wireless sensor network) integrated navigation method
CN104374389B (en) * 2014-12-10 2017-04-05 济南大学 A kind of IMU/WSN Combinated navigation methods towards indoor mobile robot
CN105737833A (en) * 2016-05-13 2016-07-06 上海会志信息科技有限公司 Indoor navigation method and indoor navigation device
CN106840154A (en) * 2017-03-21 2017-06-13 江苏星月测绘科技股份有限公司 Underground space inertia measurement and wireless senser integrated positioning system and method
CN109459025A (en) * 2018-11-08 2019-03-12 中北大学 A kind of class brain air navigation aid based on light stream UWB combination
CN109655060A (en) * 2019-02-19 2019-04-19 济南大学 Based on the KF/FIR and LS-SVM INS/UWB Integrated Navigation Algorithm merged and system
CN109655060B (en) * 2019-02-19 2021-07-06 济南大学 INS/UWB integrated navigation algorithm and system based on KF/FIR and LS-SVM fusion
CN109916401A (en) * 2019-04-17 2019-06-21 济南大学 Using the seamless tight integration navigation methods and systems of distribution of LS-SVM auxiliary EKF filtering method
CN109916401B (en) * 2019-04-17 2021-03-12 济南大学 Distributed seamless tight combination navigation method and system adopting LS-SVM assisted EKF filtering method
CN110530362A (en) * 2019-09-05 2019-12-03 北京航空航天大学 A kind of fireman's indoor orientation method based on single reference mode/inertia combination

Also Published As

Publication number Publication date
CN102359787B (en) 2013-07-03

Similar Documents

Publication Publication Date Title
CN102359787B (en) WSN/MINS high-precision and real-time combination navigation information fusion method
CN102494684B (en) Navigation information zero tight combination method based on WSN (Wireless Sensors Network)/MINS (Micro Inertial Navigation System)
CN103148855B (en) INS (inertial navigation system)-assisted wireless indoor mobile robot positioning method
Zhang et al. A combined GPS UWB and MARG locationing algorithm for indoor and outdoor mixed scenario
CN102636166B (en) Course angle-based WSN/INS integrated navigation system and method
CN102692223B (en) Control method of multilevel non-linear filters for wireless sensor network (WSN)/inertial navigation system (INS) combination navigation
CN102494685B (en) H infinity information fusion method for WSN (Wireless Sensors Network)/INS (Inertial Navigation System) high-precision real-time combination and navigation
US10289122B2 (en) Communication link accessibility aware navigation
CN103207634A (en) Data fusion system and method of differential GPS (Global Position System) and inertial navigation in intelligent vehicle
CN108303079B (en) Data smoothing method for underwater USBL reverse application
CN106123895B (en) Inertial navigation origin positioning method and system based on UWB ranging
CN111595348A (en) Master-slave mode cooperative positioning method of autonomous underwater vehicle combined navigation system
CN105066993A (en) LBL/MINS integrated navigation system and navigation information fusion method thereof
CN104316058A (en) Interacting multiple model adopted WSN-INS combined navigation method for mobile robot
CN113900061A (en) Navigation positioning system and method based on UWB wireless positioning and IMU fusion
KR101504063B1 (en) Moving bag
CN114838732B (en) Collaborative navigation method based on graph optimization under communication limited environment
CN104296741B (en) WSN/AHRS (Wireless Sensor Network/Attitude Heading Reference System) tight combination method adopting distance square and distance square change rate
CN111198567A (en) Multi-AGV collaborative dynamic tracking method and device
CN104374389A (en) Indoor mobile robot oriented IMU/WSN (inertial measurement unit/wireless sensor network) integrated navigation method
CN112556695B (en) Indoor positioning and three-dimensional modeling method, system, electronic equipment and storage medium
Liu et al. An indoor 3-D quadrotor localization algorithm based on WiFi RTT and MEMS sensors
Cao et al. Uwb based integrated communication and positioning system for multi-uavs close formation
Yuan et al. MIAKF: Motion inertia estimated adaptive Kalman filtering for underground mine tunnel positioning
CN110658515A (en) Multi-user IMU positioning and aligning method based on UWB single base station

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
EE01 Entry into force of recordation of patent licensing contract

Application publication date: 20120222

Assignee: Jiangsu Rothwell Electric Co., Ltd.

Assignor: Southeast University

Contract record no.: 2014320000094

Denomination of invention: A WSN/MINS high precision real-time integrated navigation information fusion method

Granted publication date: 20130703

License type: Exclusive License

Record date: 20140228

LICC Enforcement, change and cancellation of record of contracts on the licence for exploitation of a patent or utility model