CN106291609A - A kind of RTK precision assessment method - Google Patents

A kind of RTK precision assessment method Download PDF

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Publication number
CN106291609A
CN106291609A CN201610613043.6A CN201610613043A CN106291609A CN 106291609 A CN106291609 A CN 106291609A CN 201610613043 A CN201610613043 A CN 201610613043A CN 106291609 A CN106291609 A CN 106291609A
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CN
China
Prior art keywords
rtk
board
bar
support bar
precision
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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
CN201610613043.6A
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Chinese (zh)
Inventor
杭义军
邢丽
吕印新
贾文峰
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Jiyi Robot (shanghai) Co Ltd
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Jiyi Robot (shanghai) 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.)
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Publication date
Application filed by Jiyi Robot (shanghai) Co Ltd filed Critical Jiyi Robot (shanghai) Co Ltd
Priority to CN201610613043.6A priority Critical patent/CN106291609A/en
Publication of CN106291609A publication Critical patent/CN106291609A/en
Pending legal-status Critical Current

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    • 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
    • G01S19/01Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/13Receivers
    • G01S19/23Testing, monitoring, correcting or calibrating of receiver elements
    • 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
    • G01S19/40Correcting position, velocity or attitude
    • G01S19/41Differential correction, e.g. DGPS [differential GPS]

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  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)

Abstract

The present invention relates to equipment precision evaluation areas, particularly relate to a kind of RTK precision assessment method.A kind of RTK Accuracy Estimation of the open design of the present invention, compared with traditional RTK performance test methods by three kinds of skimulated motion unit simulation straight lines, sine and three kinds of motion modes of circle, the method for proposition is the easiest and Performance Evaluation is closer to Practical Performance;The method proposed can make people compare positioning precision and the superiority getting information about RTK, can be with the service precision (service precision under especially random motion state) of accurate evaluation RTK board, there is provided design reference for user in the combination property that the design initial stage grasps RTK board comprehensively, type selecting specific aim and the product combination property of RTK board can be effectively improved.

Description

A kind of RTK precision assessment method
Technical field
The present invention relates to equipment precision evaluation areas, particularly relate to a kind of RTK precision assessment method.
Background technology
In recent years, along with unmanned plane and the agrotechnical development of precision, all the positioning precision of its navigation system is proposed Higher accuracy requirement, and RTK technology is more and more applied to unmanned plane with its high positioning precision and other are correlated with Field.And the manufacturer of RTK board and broad categories, there is price superior performance preferably such as Tian Bao, the serial board of Novatel, Also have domestic such as the serial board of the producer such as compass in ancient China, middle Haidah, for a user, the only property from the user's manual of businessman Energy index and price are set out and are difficult to select most suitable RTK board.
Meanwhile, RTK board concentrates in quasistatic product at the application majority of survey field, although RTK is for technology The most dynamically with static restriction, but the conventional RTK board in survey field accumulation uses and type selecting experience can not be complete Instructing the RTK board type selecting in unmanned plane field, the relative surveying instrument field of applying of its reason mainly unmanned plane has bigger Difference, the dynamic property of RTK is had higher requirement by it.
And the most preferably test the performance indications with relatively different RTK boards and become a problem demanding prompt solution, pass The method of testing of system typically can carry out the static state of RTK board, linear motion, circulatory motion, straight line sinusoidal motion, and finally assesses The performance of RTK board, these methods have two aspect problems, and first, these methods are required for a specific device, and this A little devices also need to design the precision property reaching certain, and general user can not design this for the type selecting of certain RTK board The system of sample, therefore, such method does not has practicality;It addition, the Three models of simulation can not be very in above-mentioned method of testing Reflect that well RTK serviceability in unmanned plane, especially forms of motion and motion are the most all occurring making of change at random By situation, therefore, such method is the most not accurate enough.
Summary of the invention
It is an object of the invention to provide a kind of RTK precision assessment method, in view of the above problems, it compensate for above-mentioned defect And provide the advantage that
A kind of RTK precision assessment method, it is characterised in that including:
By RTK antenna installation at supporting bar top, and it is connected with RTK board by holding wire;
With described support bar bottom as initial point and rock described support bar, record described RTK antenna real-time position information also Be converted to coordinate information;
Calculate positional information at the bottom of the bar of described support bar, and with described in positional information calculation at the bottom of the bar of described support bar The space orientation residual error of RTK board, and then assess the measuring accuracy of described RTK board.
Above-mentioned method, it is characterised in that described method also includes:
Measure bottom described support bar to the distance of described RTK antenna phase center, according to bottom described support bar to institute State the distance of RTK antenna phase center and described RTK antenna real-time position information calculates position at the bottom of the bar of described support bar Coordinate.
Above-mentioned method, it is characterised in that calculated positional information at the bottom of the bar of described support bar by method of least square.
Above-mentioned method, it is characterised in that described method also includes:
Described RTK antenna is connected with central processing unit by described RTK board, in will be described in the data inputting of collection Central processor calculates, and then assesses the measuring accuracy of described RTK board.
Above-mentioned method, it is characterised in that described RTK board is connected with described central processing unit by Serial Port Line.
Above-mentioned method, it is characterised in that gather the real-time location coordinates information more than or equal to RTK antenna described in 3 groups.
In sum, a kind of RTK Accuracy Estimation of the open design of the present invention, with traditional by three kinds of skimulated motions The RTK performance test methods of unit simulation straight line, sine and three kinds of motion modes of circle is compared, and the method for proposition is the easiest And Performance Evaluation is closer to Practical Performance;The method proposed can make people compare and get information about the positioning precision of RTK and superior Property, can set for user with the service precision (service precision under especially random motion state) of accurate evaluation RTK board The meter initial stage is grasped the combination property of RTK board comprehensively and provides design reference, can be effectively improved type selecting specific aim and the product of RTK board Product combination property.
Accompanying drawing explanation
With reference to appended accompanying drawing, more fully to describe embodiments of the invention.But, appended accompanying drawing be merely to illustrate and Illustrate, be not intended that limitation of the scope of the invention.
Fig. 1 is the flow chart of the present invention.
Detailed description of the invention
The present invention is further illustrated with specific embodiment below in conjunction with the accompanying drawings, but not as the present invention's Limit.
The present invention proposes a kind of novel RTK dynamic accuracy appraisal procedure, and the method has only to RTK antenna is arranged on one The mapping pole top of individual 2~5 meters long, then fixes bottom pole.By the way of pitch of the laps rocks mapping bar, RTK is defeated for record The real time position gone out, then utilizes least-squares algorithm to try to achieve position at the bottom of bar, and then asks for the location residual error of RTK test.Contrast Positional precision at the bottom of bar just can be with accurate quantification different RTK board under random motion dynamically uses environment with residual error size after matching Precision index, thus carry out Technical Reference before the design that the type selecting work of RTK board provides valuable for designer.
Concrete, as it is shown in figure 1, be first the equipment connection of RTK board accuracy test, select the mapping of 2~5 meters Bar, is fixed on RTK receiver antenna the top of mapping bar, is drawn respectively through deconcentrator by receiver signal by coaxial cable In RTK board 1 and the RTK board 2 needing test;
Measure distance l to RTK antenna phase center bottom mapping baro
Shake mapping bar, gathers the longitude and latitude high position information that exports in real time of RTK board, by serial ports connect two boards card with Computer, gathers the longitude and latitude high position information that the RTK board during mapping bar shake exports in real time, if the longitude and latitude of record is high every time Shown in coordinate such as formula (1), wherein n is the data amount check of surveying record.Shake process, for keeping mapping bar bottom position constant, is surveyed Examination personnel shake mapping bar, then the movement locus of mapping bar top antenna will be always on a hemisphere face, its movement velocity with The direction of motion surveys and draws the amplitude of bar along with tester shakes, speed is changing always;
[L(n)(n),h(n)] (1)
The RTK board longitude and latitude high position gathered is to the conversion of rectangular coordinate;
Utilize first group of position coordinates [L of record(1)(1),h(1)] as basis reference, the longitude and latitude height remaining put is sat Mark is transformed into [x under rectangular coordinate system(n),y(n),z(n)], shown in transformation process such as formula (2), wherein, R is earth radius.
x(n)=(L(n)-L(1))×(R+H(1))
y(n)=(λ(n)(1))×(R+H(1))×cos(L(1))
z(n)=(H(n)-H(1)) (2)
Method of least square is utilized to solve position at the bottom of surveying instrument bar, it is assumed that bottom pole in rectangular coordinate system defined above Rectangular coordinate be [x, y, z], then the aerial position rectangular coordinate [x of a certain location point after conversion(n),y(n),z(n)] with bar at the bottom of Shown in relation such as formula (3) between rectangular coordinate [x, y, z], wherein loFor bottom described mapping bar in RTK antenna phase The distance of the heart.Nonlinear System of Equations (3) is carried out first order Taylor expansion, then its first order Taylor in-1 iterative process of kth Shown in expansion such as formula (4).Formula (4) can obtain the expression formula as shown in formula (5) after arranging, whereinExpression such as formula (6) shown in.When the data gathered are counted and met n > 3, i.e. can utilize The calculating formula Δ X=(G of little square lawTG)-1GTB, and the primary iteration value [x preseto,yo,zo] and the minimum threshold of Δ X (condition that i.e. iteration terminates), is iterated being calculated the optimum position under rectangular coordinate system bottom mapping bar by formula (5) Put [x, y, z].
B=G Δ X
Position rectangular coordinate at the bottom of the bar solved is utilized to calculate the space orientation residual error of RTK board, the test of assessment RTK board Precision.
When the data gathered are counted n > > 3, during such as n >=1000 or more points, obtain through least-squares algorithm matching Bottom mapping bar, the optimal location [x, y, z] under rectangular coordinate system will be the most accurate.Therefore, it can obtain with this point for the centre of sphere Shown in the volumetric position error such as formula (7) of RTK board outgoing position.
RTK outgoing position position deviation in the case of random motion can be accurately obtained, by this by formula (7) The statistical analysis of position deviation sequence can effectively assess different RTK board positioning performance under random motion environment from contrast Good and bad.
In sum, a kind of RTK Accuracy Estimation of the open design of the present invention, with traditional by three kinds of skimulated motions The RTK performance test methods of unit simulation straight line, sine and three kinds of motion modes of circle is compared, and the method for proposition is the easiest And Performance Evaluation is closer to Practical Performance;The method proposed can make people compare and get information about the positioning precision of RTK and superior Property, can set for user with the service precision (service precision under especially random motion state) of accurate evaluation RTK board The meter initial stage is grasped the combination property of RTK board comprehensively and provides design reference, can be effectively improved type selecting specific aim and the product of RTK board Product combination property.
By explanation and accompanying drawing, give the exemplary embodiments of the ad hoc structure of detailed description of the invention, based on present invention essence God, also can make other conversion.Although foregoing invention proposes existing preferred embodiment, but, these contents are not intended as Limitation.
For a person skilled in the art, after reading described above, various changes and modifications will be apparent to undoubtedly. Therefore, appending claims should regard whole variations and modifications of true intention and the scope containing the present invention as.In power The scope of any and all equivalence and content in the range of profit claim, be all considered as still belonging to the intent and scope of the invention.

Claims (6)

1. a RTK precision assessment method, it is characterised in that including:
By RTK antenna installation at supporting bar top, and it is connected with RTK board by holding wire;
With described support bar bottom as initial point and rock described support bar, record described RTK antenna real-time position information and change For coordinate information;
Calculate positional information at the bottom of the bar of described support bar, and with RTK described in positional information calculation at the bottom of the bar of described support bar The space orientation residual error of board, and then assess the measuring accuracy of described RTK board.
Method the most according to claim 1, it is characterised in that described method also includes:
Measure the distance to described RTK antenna phase center bottom described support bar, according to extremely described RTK bottom described support bar The distance of antenna phase center and described RTK antenna real-time position information calculate position coordinates at the bottom of the bar of described support bar.
Method the most according to claim 2, it is characterised in that calculated the bar of described support bar by method of least square End positional information.
Method the most according to claim 1, it is characterised in that described method also includes:
Described RTK antenna is connected with central processing unit by described RTK board, with will centre described in the data inputting of collection Reason device calculates, and then assesses the measuring accuracy of described RTK board.
Method the most according to claim 4, it is characterised in that described RTK board is processed with described central authorities by Serial Port Line Device connects.
Method the most according to claim 1, it is characterised in that gather the real time position more than or equal to RTK antenna described in 3 groups Coordinate information.
CN201610613043.6A 2016-07-29 2016-07-29 A kind of RTK precision assessment method Pending CN106291609A (en)

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Cited By (5)

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Publication number Priority date Publication date Assignee Title
RU2716360C1 (en) * 2017-01-10 2020-03-11 Шанхай Хуацэ Навигейшн Текнолоджи Лтд Method of measuring tilt of measuring rtk receiver
CN111025342A (en) * 2019-12-13 2020-04-17 航天神舟飞行器有限公司 Method for testing performance and Align data precision of Beidou board card of unmanned aerial vehicle
CN111030880A (en) * 2018-10-10 2020-04-17 千寻位置网络有限公司 Network RTK positioning quality evaluation method and device and network RTK positioning system
CN111414004A (en) * 2020-03-03 2020-07-14 桂林电子科技大学 RTK (real time kinematic) positioning system for unmanned aerial vehicle formation
CN115164943A (en) * 2022-09-08 2022-10-11 国网瑞嘉(天津)智能机器人有限公司 Testing method and device for positioning equipment, electronic equipment and storage medium

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US5929807A (en) * 1997-03-07 1999-07-27 Trimble Navigation Limited Method and apparatus for precision location of GPS survey tilt pole
CN102706361A (en) * 2012-05-18 2012-10-03 中国人民解放军92537部队 Attitude precision estimation method of multiple high-accuracy inertial navigations system
CN103674067A (en) * 2013-12-19 2014-03-26 哈尔滨工程大学 Auto-collimation theodolite based transfer alignment verification method
CN104567919A (en) * 2013-10-12 2015-04-29 北京航天计量测试技术研究所 Device for calibrating dynamic measurement errors of photogrammetric system and application method thereof
CN104897169A (en) * 2015-02-03 2015-09-09 南京航空航天大学 Testing system and method for dynamic precision of micro attitude module

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5929807A (en) * 1997-03-07 1999-07-27 Trimble Navigation Limited Method and apparatus for precision location of GPS survey tilt pole
CN102706361A (en) * 2012-05-18 2012-10-03 中国人民解放军92537部队 Attitude precision estimation method of multiple high-accuracy inertial navigations system
CN104567919A (en) * 2013-10-12 2015-04-29 北京航天计量测试技术研究所 Device for calibrating dynamic measurement errors of photogrammetric system and application method thereof
CN103674067A (en) * 2013-12-19 2014-03-26 哈尔滨工程大学 Auto-collimation theodolite based transfer alignment verification method
CN104897169A (en) * 2015-02-03 2015-09-09 南京航空航天大学 Testing system and method for dynamic precision of micro attitude module

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2716360C1 (en) * 2017-01-10 2020-03-11 Шанхай Хуацэ Навигейшн Текнолоджи Лтд Method of measuring tilt of measuring rtk receiver
US10591295B2 (en) 2017-01-10 2020-03-17 Shanghai Huace Navigation Technology Ltd Tilt measurement method for RTK measuring receiver
CN111030880A (en) * 2018-10-10 2020-04-17 千寻位置网络有限公司 Network RTK positioning quality evaluation method and device and network RTK positioning system
CN111025342A (en) * 2019-12-13 2020-04-17 航天神舟飞行器有限公司 Method for testing performance and Align data precision of Beidou board card of unmanned aerial vehicle
CN111414004A (en) * 2020-03-03 2020-07-14 桂林电子科技大学 RTK (real time kinematic) positioning system for unmanned aerial vehicle formation
CN115164943A (en) * 2022-09-08 2022-10-11 国网瑞嘉(天津)智能机器人有限公司 Testing method and device for positioning equipment, electronic equipment and storage medium
CN115164943B (en) * 2022-09-08 2022-12-23 国网瑞嘉(天津)智能机器人有限公司 Testing method and device for positioning equipment, electronic equipment and storage medium

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