CN101770033A - Fixing method of ambiguity network between CORS and system station - Google Patents

Fixing method of ambiguity network between CORS and system station Download PDF

Info

Publication number
CN101770033A
CN101770033A CN201010107336A CN201010107336A CN101770033A CN 101770033 A CN101770033 A CN 101770033A CN 201010107336 A CN201010107336 A CN 201010107336A CN 201010107336 A CN201010107336 A CN 201010107336A CN 101770033 A CN101770033 A CN 101770033A
Authority
CN
China
Prior art keywords
dtri
ambiguity
wide lane
delta
difference
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
CN201010107336A
Other languages
Chinese (zh)
Other versions
CN101770033B (en
Inventor
王庆
潘树国
沈雪峰
邓健
袁本银
柯福阳
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 201010107336 priority Critical patent/CN101770033B/en
Publication of CN101770033A publication Critical patent/CN101770033A/en
Application granted granted Critical
Publication of CN101770033B publication Critical patent/CN101770033B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Abstract

The invention discloses a fixing method of an ambiguity network between CORS system stations, which comprises the following steps: first, a wide-lane ambiguity float solution is worked out with the linear combination of carrier wave and pseudorange, the mean is solved through multi-epoch according to the long-wave features of wide-lane ambiguity, to determine the wide-lane ambiguity integer solution; and then the delay dry weight of a troposphere is estimated through a Neill model, L1 ambiguity is separated by the independent combination of an ionosphere, so as to determine L2 ambiguity; and finally accuracy test of ambiguity resolution is carried out. The method provided by the invention can fix the baseline ambiguity between CORSs in a short time, is quick, stable and easy to be implemented in projects.

Description

Integer ambiguity network fixing means between the CORS system station
Technical field
The present invention relates in the GNSS network differential positioning system baseline integer ambiguity network calculation method between reference station, relate in particular to integer ambiguity network fixing means between CORS (CORS) system station, belong to GNSS network differential positioning field.
Background technology
GNSS network differential location technology is the hot technology in present satnav field, be widely used in industries such as mapping and survey of territorial resources, with virtual reference station technology (VRS) is the network differential technology rise of representative, makes and sets up the recent tendency that reference station network type GPS service system becomes Current GPS technology application development.The VRS technology is as the GPS real-time dynamic positioning technology under many reference stations environment, be that collection Internet technology, wireless communication technique, computer networking technology and GPS technology are the network RTK location technology of one, also be wide, the most successful representative high-tech achievement of current application, the VRS technical system has been represented the conventional RTK developing direction of location technology of new generation afterwards.
The online of baseline integer ambiguity fixedly is the prerequisite that realizes the VRS technology between reference station.Growth along with parallax range between reference station, the systematic error correlativity weakens even disappears, systematic error residual error in two poor observed readings increases rapidly, cause being difficult to correctly determining integer ambiguity, make bearing accuracy descend, thereby the online of long baseline integer ambiguity fixedly is the important technological problems of restriction VRS/RTK real-time, reliability between reference station.The long baseline Ambiguity Solution Methods of domestic and international many scholar's centerings has been carried out many research work, mainly contain following certain methods: 1, Gao Xingwei has proposed single epoch of the integer ambiguity search procedure (Gao Xingwei between reference station, 2002), the main thought of this method is not understand system of equations, utilize directly that the survey station coordinate is known, blur level is searched for for these three conditions of the linear relationship between integer and the double frequency integer ambiguity, but its principle and imperfection, reliable be not so this method is used widely; 2, the Fast Carrier Phase Ambiguity Resolution of Zhou Letao is another kind of effectively long baseline blur level fixing means (Zhou Letao, 2006), and it resolves thinking and is to use parallel filtering and expands wave technology (Sun, 1999; Chen, 2000): earlier to the parallel Kalman filtering of carrying out of the irrelevant blur level of wide lane ambiguity and ionosphere, because the long wave characteristic in wide lane, must be found the solution earlier in the filtering, again with it as given value substitution ionosphere independent combination, make ionosphere independent combination wavelength expand 0.107m to by 0.006m, estimate to fix blur level and calculating parameter static solution by the estimation of component that zenith tropospheric delay is wet with to the integer of L1 blur level at last, but this method requires high for model parameter in the Kalman filtering.
Summary of the invention
The present invention is directed to the deficiency of prior art, proposed a kind of fast and be easy to that baseline integer ambiguity network calculation method is an integer ambiguity network fixing means between the CORS system station between the reference station of Project Realization, the technical scheme of this method is:
Integer ambiguity network fixing means between the CORS system station, it is characterized in that: at first utilize the linear combination of carrier wave and pseudorange to find the solution wide lane ambiguity floating-point and separate, long wave characteristic according to wide lane ambiguity, determine wide lane ambiguity integer solution, promptly wide lane integer ambiguity by finding the solution mean value many epoch; Estimate the dried wet component of tropospheric delay by the Neill model then, adopt the ionosphere independent combination to isolate the two difference of L1 carrier wave blur level, the two difference of definite then L2 carrier wave blur leveles; Carry out the verifying correctness of Carrier Phase Ambiguity Resolution at last.
Specifically can be according to the following steps:
(1) each reference station continuous acquisition observation data, and be real-time transmitted to central server, correspondence is added in the base station at each bar baseline two ends, has promptly imported L1, L2 carrier phase observation data, P1, information such as P2 pseudo range observed quantity.
(2) wide lane integer ambiguity fixes fast.Utilize the double frequency phase observed reading can eliminate ionospheric influence effectively, and by differential technique can cancellation receiver clock correction, the influence of satellite clock correction, weaken the influence (shorter baseline even can ignore) of track deviation and atmosphere delay deviation simultaneously to a great extent.Two kinds of methods of fixing main employing of wide lane integer ambiguity: a kind of is wide lane combination definition solving method, promptly directly finds the solution according to the definition of wide lane combination observation value, resolves the influence that the result mainly is subjected to atmosphere errors, is applicable to base length 30~50km; Another kind is dual-frequency P sign indicating number and phase observations value LINEAR COMBINATION METHOD, resolves the influence that the result mainly is subjected to the pseudorange precision, is applicable to that base length is 50~100km.Base length was selected calculation method during the present invention can use according to engineering, with fast fixing wide lane integer ambiguity.
1) wide lane combination definition solving method
According to the definition of the wide lane of double frequency combination observation value, can be expressed as wide lane ambiguity:
Figure GSA00000022077100021
In the formula,
Figure GSA00000022077100022
Be two poor operators; N wBe wide lane ambiguity;
Figure GSA00000022077100023
With
Figure GSA00000022077100024
Be respectively L 1, L 2The wave band carrier phase observation data; f 1, f 2Be L 1, L 2The frequency of wave band; λ w=c/ (f 1-f 2) be the wavelength of wide lane observed reading; ρ, O, T, I, M, ε are respectively and defend distance, orbit error, tropospheric delay, ionosphere delay, multipath effect and observation noise.
In CORS (CORS) network, satellite orbital error and Multi-Path Effects can be ignored, and defending distance can accurate Calculation obtain, so in following formula, Influenced by ionosphere and tropospheric two difference residual error.Because two differences tropospheres mainly are subjected to the influence of base length and satellite altitude angle size, promptly increase along with the increase of base length, reduce with the increase at satellite altitude angle, particularly the two difference of low clearance cornerdown star tropospheric delay sharply increase.Therefore, when base length within the specific limits, by setting satellite, consider wide lane wavelength X again by 10~20 ° of elevation angles w=86.2cm, ionosphere and tropospheric two difference residual error can be controlled within the half cycle the influence of wide lane ambiguity, utilize this method can determine single epoch
Figure GSA00000022077100026
Value.
2) dual-frequency P sign indicating number and phase observations value LINEAR COMBINATION METHOD
Because the GPS receiver that dual-frequency code is relevant not only can obtain carrier phase observation data, and can also obtain L1, the P sign indicating number pseudorange on the L2 frequency, so can adopt the LINEAR COMBINATION METHOD of dual-frequency P sign indicating number and phase observations value to find the solution wide lane ambiguity:
Figure GSA00000022077100027
P in the formula 1, P 2Be respectively L 1, L 2Wave band P sign indicating number pseudorange value.As can be seen, following formula has been eliminated the ionospheric convection layer and has been defended the distance influence for how much, ignores multipath effect, and following formula only is subjected to the influence of remaining two difference observation noises.Though the influence of pseudorange noise ratio carrier phase is much bigger, because the long wave characteristic of wide lane combination, the pseudorange noise is effectively suppressed.
Because the pseudorange The noise only utilizes list observed reading epoch to be difficult to correctly fixedly go out wide lane ambiguity according to following formula
Figure GSA00000022077100031
In the reference station network, sampling interval is very short, and in order to fix wide lane ambiguity exactly, the present invention is according to the accidental error characteristic of noise, and comprehensive many epoch, observation data was found the solution.
(3) the two difference of L1, L2 ambiguity resolution.After the wide lane ambiguity of two differences is determined, utilize and the irrelevant linear combination in ionosphere, adopt the Neill model to estimate the dried wet component of tropospheric delay simultaneously,, determine the two difference of L2 integer ambiguity then by 1 pair of poor integer ambiguity of the quick fixed L of sequential least square condition adjustment.And make full use of the topological relation of GNSS network differential positioning system base station net, check the accuracy of the two difference of L1, L2 blur level integer solutions, thereby improve the success ratio of two difference ambiguity resolution.
Adopt ionosphere independent linearity combination to determine
Figure GSA00000022077100032
Promptly
Figure GSA00000022077100033
= 1 λ w ( Δ ▿ ρ + Δ ▿ O + Δ ▿ T ) + f 2 f 1 + f 2 Δ ▿ N 1 - f 2 f 1 + f 2 Δ ▿ N 2
In the formula,
Figure GSA00000022077100035
Be two poor operators;
Figure GSA00000022077100036
Be no ionosphere delay combination observation value, ρ is station star distance, and O is an orbit error, and T is a tropospheric delay, takes narrow lane observed reading wavelength X into account n=c/ (f 1+ f 2) and according to wide lane ambiguity definition Δ ▿ N 2 = Δ ▿ N 1 - Δ ▿ N w , Have
Figure GSA00000022077100038
Because in the reference station network, satellite orbital error and Multi-Path Effects can be ignored, defending distance can accurate Calculation obtain,
Figure GSA00000022077100039
After accurately obtaining, determine in the following formula
Figure GSA000000220771000310
The main source that influences from tropospheric two difference residual errors.Because of tropospheric influence and satellite altitude angular dependence (-dance), introduce mapping function for this reason, it is expressed as zenith delay and about the product of the mapping function at satellite altitude angle, so can be with two difference blur leveles of L1 carrier wave
Figure GSA000000220771000311
As parameter to be estimated, zenith tropospheric delay ZD can obtain its initial value by the Neill model, is calculated as follows
Figure GSA000000220771000312
▿ MF ( θ p 1 ) - ▿ MF ( θ q 1 ) λ n . . . 0 ▿ MF ( θ p 2 ) - ▿ MF ( θ q 2 ) 0 λ n . . . . . . . . . . . . . . . . . . ▿ MF ( θ p k ) - ▿ ( θ q k ) 0 . . . λ n × ZD p ZD q Δ ▿ N 1 1 Δ ▿ N 1 2 . . . Δ ▿ N 1 k
In the formula, MF () is the troposphere mapping function; λ n, λ wIt is respectively the wavelength of narrow lane and wide lane observation;
Figure GSA00000022077100041
Be the combination of no ionosphere; Be wide lane ambiguity; f 1, f 2Frequency for L1 and L2;
Figure GSA00000022077100043
Be that two differences are defended distance; P, q are the reference station numbering; K+1 is the observation satellite number.
For resolving of following formula, the present invention adopts sequential adjustment to carry out the two difference of L1 carrier wave blur level
Figure GSA00000022077100044
Resolve the sequential adjustment calculation method.
Be located at t kHave m+1 satellite epoch, and n is arranged k* 1 observation vector L k, corresponding covariance matrix is Q k, weight matrix is
Figure GSA00000022077100045
At t K-1Obtain the model parameter vector estimated value epoch
Figure GSA00000022077100046
Corresponding covariance matrix is Q K-1, error equation is:
V k = A k X ^ k - L k
In the formula:
Figure GSA00000022077100048
Be n k* (m+2) design matrix;
Figure GSA00000022077100049
Be n k* 1 observing matrix;
X ^ k = ZD p ZD q Δ ▿ N 1 . . . T Be (m+2) * 1 state estimation vector;
It is as follows to resolve process:
P X ^ k = A k T P k A k + P X k - 1 ^ P L k = A k T P k L k + P L k - 1 X ^ k = P X ^ k - 1 P L k = P X ^ k - 1 ( A k T P k L k + P X k - 1 ^ X k - 1 ^ )
Initial value is P X ^ 1 = A 1 T P 1 A 1 , P L 1 = A 1 T P 1 L 1 ;
By above-mentioned sequential adjustment method, can determine the two difference of L1 blur level
Figure GSA000000220771000414
The two difference of L2 blur level: Δ ▿ N 2 = Δ ▿ N 1 - Δ ▿ N w ;
(4) network checks of blur level correctness.In view of the characteristics of reference station network, can pass through many baselines of reference station network combinatorial test blur level correctness.Inner network forming algorithm had substantial connection when this kind method of inspection calcaneus rete network differential system software was realized, the present invention adopts the Delaunay triangulation network as the base station network.
When adopting the Delaunay triangulation network, with triangle for resolving the unit substantially, article three, baseline is chosen identical reference satellite and is carried out two subtractive combinations, then for three baselines that resolve the unit in the network arbitrarily, all there is following relation (the unit Cel_ABC that resolves that constitutes with ABC is an example) in their corresponding blur level:
Δ ▿ N AB ij + Δ ▿ N BC ij + Δ ▿ N CA ij = 0
Advantage of the present invention and beneficial effect:
(1) the present invention can be used for the realization of the Network RTK of CORS system technology, the integer ambiguity between promptly can the real-time resolving reference station, thus prepare for generating dummy observation or correction.
(2) the present invention also is that baseline resolves the core algorithm of software afterwards.
Description of drawings
Fig. 1 is a baseline integer ambiguity network calculation method process flow diagram between reference station among the present invention;
Fig. 2 is a base station network diagram among the present invention;
Fig. 3 is an experiment base station network diagram among the present invention;
Fig. 4 is that wide lane combination definition solving method is found the solution wide lane ambiguity and separated figure as a result single epoch among the present invention;
Fig. 5 be among the present invention dual-frequency P sign indicating number and phase observations value LINEAR COMBINATION METHOD find the solution wide lane ambiguity single epoch of value and many epoch the mean value synoptic diagram;
Fig. 6 adopts the ionosphere independent combination to find the solution the two difference of L1 blur level synoptic diagram among the present invention.
Embodiment
Referring to Fig. 1, among the present invention between reference station baseline integer ambiguity network calculation method mainly undertaken by following flow process:
(1) each reference station continuous acquisition observation data, and be real-time transmitted to central server, correspondence is added in the base station at each bar baseline two ends, has promptly imported to comprise L1 L2 carrier phase observation data, P1, P2 pseudo range observed quantity information;
(2) select following two kinds of methods to resolve according to on-site actual situations and determine wide lane integer ambiguity:
When 1) base length is 30~50km, adopt wide lane combination definition solving method:
When 2) base length is 50~100km, adopt double frequency pseudorange P sign indicating number P1, P2 and phase observations value linear combination solving method:
(3) the two difference of L1, L2 ambiguity resolution
After the wide lane ambiguity of two differences is determined, utilize and the irrelevant linear combination in ionosphere, adopt the Neill model to estimate the dried wet component of tropospheric delay simultaneously,, determine the two difference of L2 integer ambiguity then by 1 pair of poor blur level of the quick fixed L of sequential least square condition adjustment;
(4) network checks of the two difference of L1, L2 blur level correctness:
When adopting the Delaunay triangulation network, with triangle for resolving the unit substantially, article three, baseline is chosen identical reference satellite and is carried out two subtractive combinations, then for three baselines that resolve the unit in the network arbitrarily, all there is following relation in their corresponding blur level, concern below satisfying that the two difference of L1, L2 blur leveles are correct
Δ ▿ N AB ij + Δ ▿ N BC ij + Δ ▿ N CA ij = 0
If the two difference of L1, L2 blur level satisfies following formula, then the search of the two difference of L1, L2 blur level finishes, and resolves end; Otherwise,, promptly, resolve again from resolving wide lane two difference blur level from (1).
Referring to Fig. 2, be the base station network, wherein alphabetical A-F represents base station, presses the network forming of Delaunay triangulation network network forming principle, sets up the CORS network, determines the triangle at place according to customer location, thereby carries out the network checks of the two difference of L1, L2 blur level correctness.
Use Jiangsu CORS data as example below.Experimental data is the observation data of three stations 30min on the 6th in (station, Jurong (BTJR), station, Yangzhou (BFYZ), Yang Zhongzhan (BTZF)) March in 2007 in the CORS of Jiangsu, Fig. 3 is three station topological relation figure, baseline BTJR-BFYZ (length 53353.895m) wherein, baseline BFYZ-BTZF (length 43668.153m), baseline BTZF-BTJR (length 70022.556m).The method that employing the present invention proposes is resolved its pair difference blur level, and end product is compared with the result that resolves who adopts high precision Bernese to resolve software.
The first step: fixing fast of wide lane ambiguity, adopt wide lane combination definition solving method and dual-frequency P sign indicating number and two kinds of methods of phase observations value LINEAR COMBINATION METHOD to find the solution wide lane ambiguity respectively, the PRN2 satellite that has just risen with baseline is example result such as Fig. 4, shown in Figure 5.
From Fig. 4, Fig. 5 as can be seen, wide lane combination definition solving method is separated error when very little single epoch at the satellite altitude angle bigger, along with the change at satellite altitude angle is big, resolves the result gradually near the correct round values of wide lane ambiguity.And in dual-frequency P sign indicating number and the phase observations value LINEAR COMBINATION METHOD single epoch of combination observation value all epoch separate and all on correct round values, fluctuate in next all left and right sides scope, variation with the satellite altitude angle is irrelevant, promptly adopt separate single epoch and can't fix wide lane ambiguity value, but after the method for totally averaging many epoch, wide lane ambiguity levels off to round values fast along with increasing of epoch, and wide lane ambiguity is fixed.
The present invention finds to adopt wide lane combination definition solving method in that base length is suitable during less than 50km through mass data test; In base length greater than 50km appropriate to the occasion employing dual-frequency P sign indicating number and phase observations value LINEAR COMBINATION METHOD.
Determining of second step: the L1 two difference blur level.The two difference of L1 carrier wave blur level restrains situation for convenience of explanation, and the blur level convergence situation of choosing No. 11 satellites of PRN shows that No. 28 satellites of PRN are as the reference satellite; Resolve the result according to Bernese, G28-G11CA 00:00:00...01:45:00 float=14.879 fixed=15.000 sigma=0.121num=421, then the two difference of the L1 carrier wave of PRN 11 blur level is 15.Resolve the result as shown in Figure 6.
As can be seen from Figure 6, when value that inferior little variance and minimum variance ratio>F distributes, the two difference of No. 11 satellites of PRN blur leveles are fixed, and the set time, it is consistent that result and Bernese resolve the result, satisfies CORS system related request fully about 180s.
The 3rd step: the network checks of blur level correctness.The present invention carries out the ambiguity resolution of aforesaid way to three baselines shown in Fig. 3, is example with No. 11 satellites of PRN, and the two difference of L1 blur leveles are as follows:
Baseline BTJR-BFYZ:15
Baseline BFYZ-BTZF:8
Baseline BTZF-BTJR:-23
Satisfy Δ ▿ N AB ij + Δ ▿ N BC ij + Δ ▿ N CA ij = 0 This test condition.

Claims (2)

1. integer ambiguity network fixing means between the CORS system station, it is characterized in that: at first utilize the linear combination of carrier wave and pseudorange to find the solution wide lane ambiguity floating-point and separate, long wave characteristic according to wide lane ambiguity, determine wide lane ambiguity integer solution, promptly wide lane integer ambiguity by finding the solution mean value many epoch; Estimate the dried wet component of tropospheric delay by the Neill model then, adopt the ionosphere independent combination to isolate the two difference of L1 carrier wave blur level, the two difference of definite then L2 carrier wave blur leveles; Carry out the verifying correctness of Carrier Phase Ambiguity Resolution at last.
2. according to integer ambiguity network fixing means between the described CORS system station of claim 1, specifically according to the following steps:
(1) each reference station continuous acquisition observation data, and be real-time transmitted to central server, correspondence is added in the base station at each bar baseline two ends, has promptly imported to comprise L1 L2 carrier phase observation data, P1, P2 pseudo range observed quantity information;
(2) select following two kinds of methods to resolve according to on-site actual situations and determine wide lane integer ambiguity:
When 1) base length is 30~50km, adopt wide lane combination definition solving method:
Definition according to the wide lane of double frequency combination observation value is expressed as wide lane ambiguity:
Figure FSA00000022077000011
In the formula,
Figure FSA00000022077000012
Be two poor operators; N wBe wide lane ambiguity;
Figure FSA00000022077000013
With
Figure FSA00000022077000014
Be respectively L 1, L 2The wave band carrier phase observation data; f 1, f 2Be L 1, L 2The frequency of wave band; λ w=c/ (f 1-f 2) be the wavelength of wide lane observed reading; ρ, O, T, I, M, ε are respectively and defend distance, orbit error, tropospheric delay, ionosphere delay, multipath effect and observation noise;
In CORS CORS network, satellite orbital error and Multi-Path Effects are ignored, and defending distance can accurate Calculation obtain, so in following formula,
Figure FSA00000022077000015
Influenced by ionosphere and tropospheric two difference residual error, because two differences troposphere mainly is subjected to the influence of base length and satellite altitude angle size, promptly increase along with the increase of base length, increase with the satellite altitude angle reduces, particularly the two difference of low clearance cornerdown star tropospheric delay sharply increase, therefore, when base length within the specific limits, by setting satellite, consider wide lane wavelength X again by 10~20 ° of elevation angles w=86.2cm, ionosphere and tropospheric two difference residual error can be controlled within the half cycle the influence of wide lane ambiguity, utilize this method can determine single epoch
Figure FSA00000022077000016
Value, the wide lane ambiguities of promptly two differences;
When 2) base length is 50~100km, adopt double frequency pseudorange P sign indicating number P1, P2 and phase observations value linear combination solving method:
Because the GPS receiver that dual-frequency code is relevant not only can obtain carrier phase observation data, and can also obtain L1, the P sign indicating number pseudorange on the L2 frequency, adopt the LINEAR COMBINATION METHOD of dual-frequency P sign indicating number and phase observations value to find the solution wide lane ambiguity:
Figure FSA00000022077000017
P in the formula 1, P 2Be respectively L 1, L 2Wave band P sign indicating number pseudorange value; According to the accidental error characteristic of noise, adopt comprehensive many epoch observation datas to find the solution;
(3) the two difference of L1, L2 ambiguity resolution
After the wide lane ambiguity of two differences is determined, utilize and the irrelevant linear combination in ionosphere, adopt the Neill model to estimate the dried wet component of tropospheric delay simultaneously,, determine the two difference of L2 integer ambiguity then by 1 pair of poor blur level of the quick fixed L of sequential least square condition adjustment;
Adopt ionosphere independent linearity combination to determine , promptly find the solution the two difference of L1 blur level:
Figure FSA00000022077000022
= 1 λ w ( Δ ▿ ρ + Δ ▿ O + Δ ▿ T ) + f 2 f 1 + f 2 Δ ▿ N 1 - f 2 f 1 + f 2 Δ ▿ N 2
In the formula, Be two poor operators; Be no ionosphere delay combination observation value, ρ is station star distance, and O is an orbit error, and T is a tropospheric delay, takes narrow lane observed reading wavelength X into account n=c/ (f 1+ f 2) and according to wide lane ambiguity definition
Figure FSA00000022077000026
Have
Figure FSA00000022077000027
Introduce mapping function, it is expressed as zenith delay and about the product of the mapping function at satellite altitude angle, with two difference blur leveles of L1
Figure FSA00000022077000028
As parameter to be estimated, zenith tropospheric delay ZD can obtain its initial value by the Neill model, is calculated as follows:
Figure FSA00000022077000029
▿ MF ( θ p 1 ) - ▿ MF ( θ q 1 ) λ n . . . 0 ▿ MF ( θ p 2 ) - ▿ MF ( θ q 2 ) 0 λ n . . . . . . . . . . . . . . . . . . ▿ MF ( θ p k ) - ▿ MF ( θ q k ) 0 . . . λ n × ZD p ZD q Δ ▿ N 1 1 Δ ▿ N 1 2 . . . Δ ▿ N 1 k
In the formula, MF () is the troposphere mapping function; λ n, λ wIt is respectively the wavelength of narrow lane and wide lane observation;
Figure FSA000000220770000211
Be the combination of no ionosphere;
Figure FSA000000220770000212
Be wide lane ambiguity; f 1, f 2Frequency for L1 and L2;
Figure FSA00000022077000031
Be that two differences are defended distance; P, q are the reference station numbering; K+1 is the observation satellite number;
Adopt sequential adjustment to carry out the two difference of L1 carrier wave blur level
Figure FSA00000022077000032
Resolve, the sequential adjustment calculation method is as follows:
Be located at t kHave m+1 satellite epoch, and n is arranged k* 1 observation vector L k, corresponding covariance matrix is Q k, weight matrix is
Figure FSA00000022077000033
At t K-1Obtain the model parameter vector estimated value epoch
Figure FSA00000022077000034
Corresponding covariance matrix is Q K-1, error equation is:
V k = A k - X ^ k - L k
In the formula:
Figure FSA00000022077000036
Be n k* (m+2) design matrix;
Figure FSA00000022077000037
Be n k* 1 observing matrix;
X ^ k = ZD p ZD q Δ ▿ N 1 . . . T Be (m+2) * 1 state estimation vector;
It is as follows to resolve process:
P X ^ k = A k T P k A k + P X k - 1 ^ P L k = A k T P k L k + P L k - 1 X ^ k = P X ^ k - 1 P L k = P X ^ k - 1 ( A k T P k L k + P X k - 1 ^ X k - 1 ^ )
Initial value is P X ^ 1 = A 1 T P 1 A 1 , P L 1 = A 1 T P 1 L 1 ;
By above-mentioned sequential adjustment method, can determine the two difference of L1 blur level
Figure FSA000000220770000312
The two difference of L2 blur level: Δ ▿ N 2 = Δ ▿ N 1 - Δ ▿ N w ;
(4) network checks of the two difference of L1, L2 blur level correctness:
When adopting the Delaunay triangulation network, with triangle for resolving the unit substantially, article three, baseline is chosen identical reference satellite and is carried out two subtractive combinations, then for three baselines that resolve the unit in the network arbitrarily, all there is following relation in their corresponding blur level, concerns below satisfying that the two difference of L1, L2 blur leveles are correct:
Δ ▿ N AB ij + Δ ▿ N BC ij + Δ ▿ N CA ij = 0 .
CN 201010107336 2010-02-08 2010-02-08 Fixing method of ambiguity network between CORS and system station Expired - Fee Related CN101770033B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201010107336 CN101770033B (en) 2010-02-08 2010-02-08 Fixing method of ambiguity network between CORS and system station

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201010107336 CN101770033B (en) 2010-02-08 2010-02-08 Fixing method of ambiguity network between CORS and system station

Publications (2)

Publication Number Publication Date
CN101770033A true CN101770033A (en) 2010-07-07
CN101770033B CN101770033B (en) 2013-04-03

Family

ID=42503012

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201010107336 Expired - Fee Related CN101770033B (en) 2010-02-08 2010-02-08 Fixing method of ambiguity network between CORS and system station

Country Status (1)

Country Link
CN (1) CN101770033B (en)

Cited By (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102298151A (en) * 2011-07-20 2011-12-28 东南大学 Error correction method in global navigation satellite system (GNSS) network differential positioning system
CN102426375A (en) * 2011-09-02 2012-04-25 东南大学 Phase integer ambiguity reliability checking method in GPS positioning technology
CN102650694A (en) * 2011-02-25 2012-08-29 中国人民解放军61081部队 Medium-long baseline ambiguity resolution method based on BeiDou four-frequency signal
CN103176188A (en) * 2013-03-19 2013-06-26 武汉大学 Single-epoch fixing method for enhancing PPP-RTK ambiguity of regional foundation
CN103605145A (en) * 2013-12-04 2014-02-26 上海华测导航技术有限公司 Method for achieving network real-time kinematic positioning based on GNSS multi-frequency data and CORS
CN104111467A (en) * 2014-07-21 2014-10-22 东南大学 Network real time kinematic (RTK) instant locating method based on big dipper tri-band wide-lane combination
CN104502935A (en) * 2014-12-29 2015-04-08 东南大学 Network RTK (real-time kinematic) ambiguity resolution method based on un-differential uncombined model
CN104635249A (en) * 2015-02-12 2015-05-20 东南大学 Quick fixing method for precise point positioning (PPP) ambiguity considering FCBs (Fractional Carrier Bias)
CN104898145A (en) * 2015-06-25 2015-09-09 和芯星通科技(北京)有限公司 Ambiguity fixing method and system based on semi-cycle ambiguity
CN105158783A (en) * 2015-08-21 2015-12-16 上海海积信息科技股份有限公司 Real-time dynamic differential positioning method and device thereof
CN105223598A (en) * 2015-09-28 2016-01-06 厦门理工学院 A kind of GNSS ambiguity of carrier phase simple epoch solution method
CN105372692A (en) * 2014-08-13 2016-03-02 北京和协导航科技有限公司 Quick integer ambiguity calculation method of Beidou attitude determination receiver
CN105549055A (en) * 2015-11-24 2016-05-04 航天恒星科技有限公司 Virtual observation data generation method and device
CN105842721A (en) * 2016-03-23 2016-08-10 中国电子科技集团公司第十研究所 Method for improving resolving success rate of medium and long baseline GPS integral cycle fuzziness
CN105911574A (en) * 2016-03-17 2016-08-31 孙红星 Reference station fuzziness verification method based on CORS known baseline component
CN106338738A (en) * 2015-11-13 2017-01-18 上海华测导航技术股份有限公司 Pierce point-based regional augmentation system real-time ionosphere modeling method
CN106970404A (en) * 2017-03-31 2017-07-21 东南大学 A kind of many redundant network RTK atmosphere errors interpolating methods based on Delaunay triangulation network
CN107121689A (en) * 2017-04-25 2017-09-01 武汉大学 GLONASS inter-frequency deviation single epoch method for quick estimating
CN107966718A (en) * 2017-11-23 2018-04-27 东华理工大学 A kind of improved searching for integer cycle method
WO2018126869A1 (en) * 2017-01-03 2018-07-12 华为技术有限公司 Positioning method and apparatus
CN108415049A (en) * 2018-04-19 2018-08-17 千寻位置网络有限公司 Improve the method that the wide lane ambiguity of network RTK double differences fixes accuracy
CN108508468A (en) * 2018-03-20 2018-09-07 安徽理工大学 Medium-long baselines single epoch Ambiguity Solution Methods, system, equipment, storage medium
CN108802781A (en) * 2018-05-03 2018-11-13 广州市中海达测绘仪器有限公司 The acquisition methods of integer ambiguity
CN109116394A (en) * 2018-09-10 2019-01-01 中国科学院国家授时中心 A kind of real-time dynamic positioning method suitable for different length baseline
CN109196381A (en) * 2016-03-18 2019-01-11 迪尔公司 Quick determination by auxiliary data to exact position
CN109521453A (en) * 2018-12-29 2019-03-26 广东电网有限责任公司 A kind of quick fixing means of CORS net long distance baselines fuzziness and device
CN110007320A (en) * 2017-04-12 2019-07-12 千寻位置网络有限公司 Network RTK calculation method
CN110109158A (en) * 2019-05-08 2019-08-09 广西壮族自治区基础地理信息中心 Subsequent supper-fast RTK location algorithm based on GPS, GLONASS and BDS multisystem
CN110161547A (en) * 2019-06-26 2019-08-23 哈尔滨工程大学 A kind of medium-long baselines Ambiguity Solution Methods of adaptive ionosphere estimation model
CN111103603A (en) * 2018-10-29 2020-05-05 千寻位置网络有限公司 Cloud positioning method and device based on CORS system, positioning system and cloud server
CN111323792A (en) * 2020-03-21 2020-06-23 哈尔滨工程大学 Ionized layer abnormal integrity monitoring method based on dual-frequency GBAS
CN112526569A (en) * 2021-02-18 2021-03-19 中国人民解放军国防科技大学 Multi-epoch step-by-step ambiguity solving method for inertial navigation auxiliary navigation relative positioning
CN114002724A (en) * 2021-12-30 2022-02-01 自然资源部第三大地测量队 Control point online real-time rapid analysis method and device based on CORS network

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7292183B2 (en) * 2005-06-08 2007-11-06 Trimble Navigation Limited GPS reference system providing synthetic reference phases for controlling accuracy of high integrity positions

Cited By (57)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102650694B (en) * 2011-02-25 2014-03-12 中国人民解放军61081部队 Medium-long baseline ambiguity resolution method based on BeiDou four-frequency signal
CN102650694A (en) * 2011-02-25 2012-08-29 中国人民解放军61081部队 Medium-long baseline ambiguity resolution method based on BeiDou four-frequency signal
CN102298151A (en) * 2011-07-20 2011-12-28 东南大学 Error correction method in global navigation satellite system (GNSS) network differential positioning system
CN102298151B (en) * 2011-07-20 2013-12-25 东南大学 Error correction method in global navigation satellite system (GNSS) network differential positioning system
CN102426375A (en) * 2011-09-02 2012-04-25 东南大学 Phase integer ambiguity reliability checking method in GPS positioning technology
CN103176188A (en) * 2013-03-19 2013-06-26 武汉大学 Single-epoch fixing method for enhancing PPP-RTK ambiguity of regional foundation
CN103176188B (en) * 2013-03-19 2014-09-17 武汉大学 Single-epoch fixing method for enhancing PPP-RTK ambiguity of regional foundation
CN103605145A (en) * 2013-12-04 2014-02-26 上海华测导航技术有限公司 Method for achieving network real-time kinematic positioning based on GNSS multi-frequency data and CORS
CN103605145B (en) * 2013-12-04 2017-02-08 北极星云空间技术股份有限公司 Method for achieving network real-time kinematic positioning based on GNSS multi-frequency data and CORS
CN104111467A (en) * 2014-07-21 2014-10-22 东南大学 Network real time kinematic (RTK) instant locating method based on big dipper tri-band wide-lane combination
CN104111467B (en) * 2014-07-21 2017-01-11 东南大学 Network real time kinematic (RTK) instant locating method based on big dipper tri-band wide-lane combination
CN105372692B (en) * 2014-08-13 2018-05-25 北京和协导航科技有限公司 A kind of Big Dipper surveys the quick integer ambiguity method of appearance receiver
CN105372692A (en) * 2014-08-13 2016-03-02 北京和协导航科技有限公司 Quick integer ambiguity calculation method of Beidou attitude determination receiver
CN104502935A (en) * 2014-12-29 2015-04-08 东南大学 Network RTK (real-time kinematic) ambiguity resolution method based on un-differential uncombined model
CN104635249A (en) * 2015-02-12 2015-05-20 东南大学 Quick fixing method for precise point positioning (PPP) ambiguity considering FCBs (Fractional Carrier Bias)
CN104635249B (en) * 2015-02-12 2017-05-03 东南大学 Quick fixing method for precise point positioning (PPP) ambiguity considering FCBs (Fractional Carrier Bias)
CN104898145B (en) * 2015-06-25 2017-05-31 和芯星通科技(北京)有限公司 A kind of fuzziness fixing means and system based on half cycle fuzziness
CN104898145A (en) * 2015-06-25 2015-09-09 和芯星通科技(北京)有限公司 Ambiguity fixing method and system based on semi-cycle ambiguity
CN105158783B (en) * 2015-08-21 2018-06-29 上海海积信息科技股份有限公司 A kind of real time dynamic differential localization method and its equipment
CN105158783A (en) * 2015-08-21 2015-12-16 上海海积信息科技股份有限公司 Real-time dynamic differential positioning method and device thereof
CN105223598A (en) * 2015-09-28 2016-01-06 厦门理工学院 A kind of GNSS ambiguity of carrier phase simple epoch solution method
CN105223598B (en) * 2015-09-28 2017-07-11 厦门理工学院 A kind of GNSS ambiguity of carrier phase simple epoch solution method
CN106338738A (en) * 2015-11-13 2017-01-18 上海华测导航技术股份有限公司 Pierce point-based regional augmentation system real-time ionosphere modeling method
CN106338738B (en) * 2015-11-13 2019-07-26 上海华测导航技术股份有限公司 Local Area Augmentation System real-time ionospheric modeling method based on point of puncture
CN105549055A (en) * 2015-11-24 2016-05-04 航天恒星科技有限公司 Virtual observation data generation method and device
CN105911574A (en) * 2016-03-17 2016-08-31 孙红星 Reference station fuzziness verification method based on CORS known baseline component
CN109196381B (en) * 2016-03-18 2023-10-20 迪尔公司 Rapid determination of accurate position by assistance data
CN109196381A (en) * 2016-03-18 2019-01-11 迪尔公司 Quick determination by auxiliary data to exact position
CN105842721A (en) * 2016-03-23 2016-08-10 中国电子科技集团公司第十研究所 Method for improving resolving success rate of medium and long baseline GPS integral cycle fuzziness
WO2018126869A1 (en) * 2017-01-03 2018-07-12 华为技术有限公司 Positioning method and apparatus
CN106970404B (en) * 2017-03-31 2020-07-17 东南大学 Multi-redundancy network RTK atmospheric error interpolation method based on Delaunay triangulation network
CN106970404A (en) * 2017-03-31 2017-07-21 东南大学 A kind of many redundant network RTK atmosphere errors interpolating methods based on Delaunay triangulation network
CN110007320B (en) * 2017-04-12 2022-12-20 千寻位置网络有限公司 Network RTK resolving method
CN110007320A (en) * 2017-04-12 2019-07-12 千寻位置网络有限公司 Network RTK calculation method
CN107121689B (en) * 2017-04-25 2019-07-09 武汉大学 GLONASS inter-frequency deviation single epoch method for quick estimating
CN107121689A (en) * 2017-04-25 2017-09-01 武汉大学 GLONASS inter-frequency deviation single epoch method for quick estimating
CN107966718B (en) * 2017-11-23 2021-04-20 东华理工大学 Improved integer ambiguity searching method
CN107966718A (en) * 2017-11-23 2018-04-27 东华理工大学 A kind of improved searching for integer cycle method
CN108508468A (en) * 2018-03-20 2018-09-07 安徽理工大学 Medium-long baselines single epoch Ambiguity Solution Methods, system, equipment, storage medium
CN108415049B (en) * 2018-04-19 2022-05-06 千寻位置网络有限公司 Method for improving network RTK double-difference wide lane ambiguity fixing accuracy
CN108415049A (en) * 2018-04-19 2018-08-17 千寻位置网络有限公司 Improve the method that the wide lane ambiguity of network RTK double differences fixes accuracy
CN108802781B (en) * 2018-05-03 2021-03-02 广州市中海达测绘仪器有限公司 Method for acquiring integer ambiguity
CN108802781A (en) * 2018-05-03 2018-11-13 广州市中海达测绘仪器有限公司 The acquisition methods of integer ambiguity
CN109116394A (en) * 2018-09-10 2019-01-01 中国科学院国家授时中心 A kind of real-time dynamic positioning method suitable for different length baseline
CN109116394B (en) * 2018-09-10 2020-08-07 中国科学院国家授时中心 Real-time dynamic positioning method suitable for baselines of different lengths
CN111103603B (en) * 2018-10-29 2023-01-06 千寻位置网络有限公司 Cloud positioning method and device based on CORS system, positioning system and cloud server
CN111103603A (en) * 2018-10-29 2020-05-05 千寻位置网络有限公司 Cloud positioning method and device based on CORS system, positioning system and cloud server
CN109521453B (en) * 2018-12-29 2022-01-25 广东电网有限责任公司 Method and device for rapidly fixing long-distance baseline ambiguity of CORS network
CN109521453A (en) * 2018-12-29 2019-03-26 广东电网有限责任公司 A kind of quick fixing means of CORS net long distance baselines fuzziness and device
CN110109158A (en) * 2019-05-08 2019-08-09 广西壮族自治区基础地理信息中心 Subsequent supper-fast RTK location algorithm based on GPS, GLONASS and BDS multisystem
CN110161547B (en) * 2019-06-26 2022-09-16 哈尔滨工程大学 Medium-long baseline ambiguity resolution method of adaptive ionosphere estimation model
CN110161547A (en) * 2019-06-26 2019-08-23 哈尔滨工程大学 A kind of medium-long baselines Ambiguity Solution Methods of adaptive ionosphere estimation model
CN111323792A (en) * 2020-03-21 2020-06-23 哈尔滨工程大学 Ionized layer abnormal integrity monitoring method based on dual-frequency GBAS
CN111323792B (en) * 2020-03-21 2023-11-17 哈尔滨工程大学 Ionosphere abnormal integrity monitoring method based on dual-frequency GBAS
CN112526569B (en) * 2021-02-18 2021-05-07 中国人民解放军国防科技大学 Multi-epoch step-by-step ambiguity solving method for inertial navigation auxiliary navigation relative positioning
CN112526569A (en) * 2021-02-18 2021-03-19 中国人民解放军国防科技大学 Multi-epoch step-by-step ambiguity solving method for inertial navigation auxiliary navigation relative positioning
CN114002724A (en) * 2021-12-30 2022-02-01 自然资源部第三大地测量队 Control point online real-time rapid analysis method and device based on CORS network

Also Published As

Publication number Publication date
CN101770033B (en) 2013-04-03

Similar Documents

Publication Publication Date Title
CN101770033B (en) Fixing method of ambiguity network between CORS and system station
US11002860B2 (en) GNSS-RTK-based positioning method
CN107193029B (en) Fuzziness fast determination method between the network RTK base station of Big Dipper three frequency signal
CN102998681B (en) A kind of high-frequency clock error estimation method of satellite navigation system
CN105223598B (en) A kind of GNSS ambiguity of carrier phase simple epoch solution method
CN102288978B (en) Continuous operational reference system (CORS) base station cycle slip detection and recovering method
CN101609140B (en) Compatible navigation receiver positioning system and positioning method thereof
CN101710179B (en) Global navigation satellite system (GNSS) triple-frequency motion-to-motion positioning method
CN109613585A (en) A kind of method of pair of real-time direction finding of antenna for base station ultra-short baseline GNSS double antenna
CN104714244A (en) Multi-system dynamic PPP resolving method based on robust self-adaption Kalman smoothing
CN105301617B (en) A kind of integer ambiguity validity check method in satellite navigation system
CN105158783A (en) Real-time dynamic differential positioning method and device thereof
CN106324629A (en) BDS_GPS_GLONASS precise point positioning integration method
CN101943749A (en) Method for positioning network RTK based on star-shaped virtual reference station
CN103576175A (en) Double-frequency multi-constellation GNSS integer ambiguity OTF solving method
CN104680008A (en) Multi-reference station-based network RTK (Real Time Kinematic) area atmospheric error modeling method
CN103941272A (en) GPS, GLONASS and BDS unified solution positioning method
CN104597465A (en) Method for improving convergence speed of combined precise point positioning of GPS (Global Position System) and GLONASS
CN105738926A (en) Method for calibrating phase inter-frequency bias between GLONASS system receiving machines
CN104316943B (en) A kind of pseudo-distance and Doppler combine differential position system and method
CN104375157A (en) Inertial navigation assisted Big Dipper single-frequency whole-cycle ambiguity calculation method under short baseline condition
CN105182388A (en) Rapidly convergent precise point positioning method
CN105510945A (en) PPP positioning method applied to satellite navigation landing outfield detection
CN106093967A (en) The ionosphere delay method for solving that a kind of pseudorange phase place is comprehensive
CN105044741A (en) Solution method of pseudo range phase comprehensive wide-area differential correction value

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: 20100707

Assignee: Nanjing Compass Navigation Technology Co., Ltd.

Assignor: Southeast University

Contract record no.: 2015320000041

Denomination of invention: Fixing method of ambiguity network between CORS and system station

Granted publication date: 20130403

License type: Exclusive License

Record date: 20150225

CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20130403

Termination date: 20160208

CF01 Termination of patent right due to non-payment of annual fee