CN110441805B - Long-baseline three-frequency ambiguity resolution method based on unequal measurement variance - Google Patents
Long-baseline three-frequency ambiguity resolution method based on unequal measurement variance Download PDFInfo
- Publication number
- CN110441805B CN110441805B CN201910828674.3A CN201910828674A CN110441805B CN 110441805 B CN110441805 B CN 110441805B CN 201910828674 A CN201910828674 A CN 201910828674A CN 110441805 B CN110441805 B CN 110441805B
- Authority
- CN
- China
- Prior art keywords
- ambiguity
- frequency
- equation
- pseudo
- calculated
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO 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
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
- G01S19/39—Determining 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
- G01S19/42—Determining position
- G01S19/43—Determining position using carrier phase measurements, e.g. kinematic positioning; using long or short baseline interferometry
- G01S19/44—Carrier phase ambiguity resolution; Floating ambiguity; LAMBDA [Least-squares AMBiguity Decorrelation Adjustment] method
Abstract
The invention provides a long-baseline three-frequency ambiguity resolution method based on unequal measurement variance, which solves the problem that when the combined coefficient is calculated by taking the minimum combined noise as an optimal target, the combined coefficient is not optimal and the combined noise is larger because the difference of pseudo-range noise of different frequency points is not considered in the conventional method. The invention considers the fact that pseudo-range noise of different frequency points is different, introduces the condition into the combination coefficient calculation, minimizes the combined noise, reduces the number of required epochs when using the ambiguity detection quantity of the second and third combinations of multi-epoch smoothing, reduces the requirement on data continuity, and has great significance for improving the success rate of fixing the three-frequency ambiguity and further finally improving the positioning accuracy.
Description
Technical Field
The invention relates to the technical field of high-precision data processing of satellite navigation systems, in particular to a three-frequency ambiguity resolution method under a long baseline condition.
Background
Ambiguity resolution is the basis for high-precision data processing of satellite navigation systems such as Precision Point Position (PPP), Real-time Kinematic (RTK), and the like. At present, a satellite navigation system represented by Beidou and GPS can broadcast three-frequency navigation signals, the three-frequency navigation signals bring information redundancy for ambiguity resolution, and the success rate of ambiguity resolution is improved.
Under the long baseline condition, because the spatial correlation of the ionosphere is weakened, and the ionosphere residual after double differences is larger, the pseudo-range observed quantity is generally added into an observation combination under the long baseline condition so as to meet the constraint of no geometry and no ionosphere. Due to the introduction of the pseudo range, the noise after combination is large, and therefore when the combination coefficient is constrained, the minimum noise after combination is taken as a constraint criterion on the basis of meeting the constraint of no geometry and no ionosphere. At present, when combined noise is calculated, pseudo range noise on three frequency points is generally assumed to be the same, but in an actual environment, the pseudo range noise of the three frequency points is obviously different because code loop parameters, front-end bandwidths, multipath effects and the like of a receiver at different frequency points are different. For the Beidou system, the pseudo range noise on B1I and B2I is significantly greater than B3I. For the GPS system, the pseudorange noise at L1 and L2 is significantly greater than the pseudorange noise at L5.
Therefore, at present, the combined noise calculated on the premise that the pseudo-range noise of the three frequency points is the same is not the actual combined noise, and the calculated combined coefficient is not the optimal combined coefficient, so that the difference of the pseudo-range measurement variance on different frequency points needs to be considered to determine the optimal combined coefficient.
Disclosure of Invention
Aiming at the defects in the prior art, the invention aims to provide a long-baseline three-frequency ambiguity resolution method based on unequal measurement variance. The method provided by the invention can reduce the combined noise and provide the fixed success rate of the ambiguity.
Under the long baseline condition, the calculation of the combined coefficient of the three-frequency ambiguity resolution generally takes the minimum noise after combination as the optimal target on the premise of meeting the constraint of no geometry and no ionosphere. In the traditional method, when the combined noise is calculated, the pseudo-range noise of three frequency points is assumed to be the same, and the fact that the pseudo-range noise on different frequency points is different due to different code loop bandwidths, front end bandwidths, multipath effects and the like of different frequency points is not considered, so that the calculated combined coefficient is not a real optimal coefficient, and the calculated combined noise is not the minimum. The invention can calculate the optimal combination coefficient by considering the fact that pseudo-range noises on different frequency points are different, reduce the combination noise and improve the fuzzy degree fixing success rate.
In order to achieve the technical purpose, the technical scheme of the invention is as follows:
a long-baseline three-frequency ambiguity resolution method based on unequal measurement variance comprises the following steps:
(1) the satellite navigation system broadcasts a three-frequency navigation signal, 3 frequency point pseudo ranges of the three-frequency navigation signal at the time t and carrier phases of three frequency points are given, and pseudo range noise of each frequency point is extracted;
(2) calculating pseudo-range noise standard deviation of each frequency point;
(3) given the carrier coefficients of the first combination, calculating the ambiguity of the first combination;
(4) given the carrier coefficients of the second combination, calculating the ambiguity of the second combination;
(5) given the carrier coefficients of the third combination, calculating the ambiguity of the third combination;
(6) and recovering the ambiguity of the three frequency points.
In the invention, the satellite navigation system is a global positioning system capable of broadcasting three-frequency navigation signals. The satellite navigation system can be a Global Positioning System (GPS), a Glonass satellite navigation system, a Beidou satellite navigation system and other satellite navigation systems capable of broadcasting three-frequency navigation signals.
In the step (1), pseudo range noise of each frequency point is extracted according to a formula (1):
MPind=ρind-(a0φ1+b0φ2+c0φ3) (1)
wherein, MPindWherein ind is 1,2,3, f is the three frequency points to be extracted1,f2,f3Pseudo-range noise at frequency points. RhoindWherein iD is 1,2,3, and f is the frequency of three frequencies respectively1,f2,f3And (4) frequency point pseudorange. Phi is a1,φ2,φ3Respectively three frequencies are respectively f1,f2,f3The frequency point is the carrier phase in meters. a is0,b0,c0Respectively three frequencies are respectively f1,f2,f3And (5) coefficients corresponding to the frequency points.
In the formula (1), a0,b0,c0Calculated from equation (2):
wherein f is1,f2,f3Frequencies of three frequency points, alpha, respectively0,β0For the introduced auxiliary coefficients, they are calculated together from equation (2).
In the step (2), the pseudo-range noise standard deviation of each frequency point is calculated according to a formula (3):
wherein the content of the first and second substances,indicating that the calculated three frequency points are respectively f1,f2,f3And pseudo range noise standard deviation of frequency points. MP (moving Picture experts group)indFor the three frequency points to be extracted are respectively f1,f2,f3The pseudo-range noise at the frequency point is calculated by the formula (1). N represents the number of epochs required to compute the pseudorange noise standard deviation, typically 50, and h and g represent the respective epochs.
Calculating the frequencies f according to the formula (4)1,f2Compared with the frequency of f3The amplification ratio of the pseudo-range noise standard deviation of the frequency point is as follows:
wherein the content of the first and second substances,for pseudo-range noise standard deviation, the calculation is performed by equation (3)
In step (3) of the present invention, the ambiguity of the first combination is calculated according to formula (5):
where c is the speed of light. (i, j, k) is the carrier coefficient of the first combination, and is (0, -1, 1). Lambda [ alpha ]ijkFor the first combined wavelength as shown in equation (5), calculated from equation (6):
(a1,b1,c1) As pseudo-range coefficients, calculated by equation (7):
wherein σρ3The pseudo-range noise standard deviation is calculated by formula (3). Lambda [ alpha ]1Representing frequency point f1Wavelength of carrier phase of c/f1。α1,β1For the introduced auxiliary coefficients, they are calculated together from equation (7).
In step (4) of the present invention, the ambiguity of the second combination is calculated according to formula (8):
wherein λ ismntFor the second combined wavelength, by formula(9) And (3) calculating:
(m, n, t) is the carrier coefficient of the second combination, which is (1, -1, 0); (i, j, k) is the carrier coefficient of the first combination, and is (0, -1, 1).
NijkCombined ambiguity for the first set of combinations, defined as Nijk=iN1+jN2+kN3,N1,N2,N3Respectively three frequency points f1,f2,f3Ambiguity of, NijkIs L calculated by the formula (5)1And taking the rounded value.
a2,b2,c2,d2Coefficients, which are respectively corresponding terms, are calculated by equation (10):
wherein alpha is2,β2For the introduced auxiliary coefficients, they are calculated together by equation (10);is the carrier phase variance in meters, taken to be 0.0009.
In step (5) of the present invention, the ambiguity of the third combination is calculated according to formula (11):
wherein λ isuvwFor the third combined wavelength, calculated by equation (12):
(u, v, w) is the carrier coefficient of the third combination, which is (0, 1, 0); (m, n, t) is the carrier coefficient of the second combination, which is (1, -1, 0); (i, j, k) is the carrier coefficient of the first combination, which is (0, -1, 1).
NmntCombined ambiguity for the second set of combinations, defined as Nmnt=mN1+nN2+tN3,NmntIs represented by the result L of equation (8)2Averaging over 10 epochs and rounding.
a3,b3,c3,d3,e3Coefficients, which are respectively corresponding terms, are calculated by equation (13):
α3,β3for the introduced auxiliary coefficients, they are calculated together from equation (13).
In step (6), the ambiguity of each frequency point is recovered according to a formula (14):
wherein N is1,N2,N3Respectively three frequencies of f1,f2,f3Ambiguity of frequency point, int (L)1) As a result of the single epoch rounding of equation (5),the result of rounding the result after averaging the results of 10 epochs for equation (8),the results of 200 epochs are averaged for equation (11) and rounded.
Compared with the prior art, the method has the following obvious advantages:
1. the invention considers the fact that the pseudo range noise of different frequency points is different, and applies the fact to the calculation process of the combination coefficient, thereby reducing the combination noise
2. The invention reduces the combination noise, thereby reducing the number of required epochs and reducing the requirement on data continuity when smoothing the ambiguity detection quantity of the second and third combinations by using multiple epochs.
Drawings
FIG. 1 is a block diagram of a three-frequency ambiguity resolution of the present invention under long baseline conditions.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention will be further described in detail with reference to the accompanying drawings.
Referring to fig. 1, the invention provides a long-baseline three-frequency ambiguity resolution method based on unequal measurement variance, aiming at satellite navigation systems such as a Global Positioning System (GPS), a glonass satellite navigation system and a Beidou satellite navigation system which can broadcast three-frequency navigation signals, and the method comprises the following steps:
(1) extracting pseudo range noise of each frequency point according to formula (1):
MPind=ρind-(a0φ1+b0φ2+c0φ3) (1)
wherein, MPindFor the three frequencies to be extracted are respectively f1,f2,f3Pseudo-range noise of frequency points, pindFor three frequencies respectively being f1,f2,f3The frequency point pseudorange, where ind is 1,2,3, represents the frequency point, phi1,φ2,φ3Respectively three frequencies are respectively f1,f2,f3Carrier phase with frequency point in meter0,b0,c0Respectively three frequencies are respectively f1,f2,f3And (5) coefficients corresponding to the frequency points.
a0,b0,c0Calculated from equation (2):
wherein f is1,f2,f3Frequencies of three frequency points, alpha, respectively0,β0For the introduced auxiliary coefficients, they are calculated together from equation (2).
(2) Calculating the pseudo-range noise standard deviation of each frequency point according to the formula (3):
wherein the content of the first and second substances,indicating that the calculated three frequency points are respectively f1,f2,f3And pseudo range noise standard deviation of frequency points. MP (moving Picture experts group)indFor the three frequency points to be extracted are respectively f1,f2,f3The pseudo-range noise at the frequency point is calculated by the formula (1). N represents the number of epochs required to compute the pseudorange noise standard deviation, typically 50, and h and g represent the respective epochs.
Calculating the frequencies f according to the formula (4)1,f2Compared with the frequency of f3The amplification ratio of the pseudo-range noise standard deviation of the frequency point is as follows:
wherein the content of the first and second substances,the pseudo-range noise standard deviation is calculated by formula (3).
(3) The ambiguity of the first combination is calculated according to equation (5):
where c is the speed of light and (i, j, k) is the carrier coefficient of the first combination, which is taken to be (0, -1, 1), respectively. Lambda [ alpha ]ijkFor the first combined wavelength, calculated by equation (6):
(a1,b1,c1) As pseudo-range coefficients, calculated by equation (7):
wherein σρ3Calculated as the pseudo-range noise standard deviation by equation (3), λ1Representing frequency point f1Wavelength of carrier phase of c/f1。α1,β1For the introduced auxiliary coefficients, they are calculated together from equation (7).
(4) Calculating the ambiguity of the second combination according to equation (8):
wherein λ ismntFor the second combined wavelength, calculated by equation (9):
(m, n, t) is the carrier coefficient of the second combination, which is (1, -1, 0). (i, j, k) is the carrier coefficient of the first combination, and is (0, -1, 1).
NijkCombined ambiguity for the first set of combinations, defined as Nijk=iN1+jN2+kN3,N1,N2,N3Respectively three frequencies of f1,f2,f3Ambiguity of frequency points, NijkHas a value of(5) Calculated L1And taking the rounded value.
a2,b2,c2,d2Coefficients, which are respectively corresponding terms, are calculated by equation (10):
wherein alpha is2,β2For the introduced auxiliary coefficients, they are calculated together by equation (10);is the carrier phase variance in meters, taken to be 0.0009.
(5) Calculating the third combined ambiguity according to equation (11):
wherein λ isuvwFor the third combined wavelength, calculated by equation (12):
(u, v, w) is the carrier coefficient of the third combination, which is (0, 1, 0); (m, n, t) is the carrier coefficient of the second combination, is (1, -1, 0), and (i, j, k) is the carrier coefficient of the first combination, and is (0, -1, 1). N is a radical ofmntCombined ambiguity for the second set of combinations, defined as Nmnt=mN1+nN2+tN3,NmntIs represented by the result L of equation (8)2Averaging over 10 epochs and rounding.
a3,b3,c3,d3,e3Coefficients, which are respectively corresponding terms, are calculated by equation (13):
wherein: alpha is alpha3,β3For the introduced auxiliary coefficients, they are calculated together from equation (13).
(6) And recovering the ambiguity of each frequency point according to the formula (14):
wherein N is1,N2,N3Respectively three frequencies of f1,f2,f3Ambiguity of frequency point, int (L)1) As a result of the single epoch rounding of equation (5),the result of rounding the result after averaging the results of 10 epochs for equation (8),the results of 200 epochs are averaged for equation (11) and rounded.
The invention solves the problem that when the minimum combined noise is used as the optimal target to calculate the combined coefficient, the combined coefficient is not optimal and the combined noise is larger because the difference of pseudo-range noise of different frequency points is not considered in the prior art. The invention considers the fact that pseudo-range noise of different frequency points is different, introduces the condition into the combination coefficient calculation, minimizes the combined noise, reduces the number of required epochs when using the ambiguity detection quantity of the second and third combinations of multi-epoch smoothing, reduces the requirement on data continuity, and has great significance for improving the success rate of fixing the three-frequency ambiguity and further finally improving the positioning accuracy.
The foregoing description of the preferred embodiments of the present invention has been included to describe the features of the invention in detail, and is not intended to limit the inventive concepts to the particular forms of the embodiments described, as other modifications and variations consistent with the principles of the present invention are also protected by the present patent. The subject matter of the present disclosure is defined by the claims, not by the detailed description of the embodiments.
Claims (5)
1. A long-baseline three-frequency ambiguity resolution method based on unequal measurement variance is characterized by comprising the following steps:
(1) the satellite navigation system broadcasts three-frequency navigation signals and provides three-frequency navigation signals at t moment and 3 frequency point pseudo ranges rho thereofindAnd three frequency points f1,f2,f3Carrier phase phi of1,φ2,φ3Extracting pseudo range noise MP of each frequency pointindWherein ind ═ 1,2, 3;
(2) calculating pseudo-range noise standard deviation of each frequency point;
calculating the pseudo-range noise standard deviation of each frequency point according to the formula (3):
wherein: n represents the number of epochs required for calculating the standard deviation of pseudo-range noise, and h and g respectively represent the h-th epoch and the g-th epoch;
calculating the frequencies f according to the formula (4)1,f2Compared with the frequency of f3The amplification ratio of the pseudo-range noise standard deviation of the frequency point is as follows:
(3) given the carrier coefficients of the first combination, calculating the ambiguity of the first combination;
the ambiguity of the first combination is calculated according to equation (5):
wherein c is the speed of light;
λijkis as followsA combined wavelength calculated by equation (6):
(i, j, k) is the carrier coefficient of the first combination, which is (0, -1, 1);
(a1,b1,c1) As pseudo-range coefficients, calculated by equation (7):
wherein the content of the first and second substances,calculating the pseudo-range noise standard deviation by a formula (3); lambda [ alpha ]1Representing frequency point f1Wavelength of carrier phase of c/f1;α1,β1The introduced auxiliary coefficient is calculated by formula (7);
(4) given the carrier coefficients of the second combination, calculating the ambiguity of the second combination;
calculating the ambiguity of the second combination according to equation (8):
wherein λ ismntFor the second combined wavelength, calculated by equation (9):
(m, n, t) is the carrier coefficient of the second combination, which is (1, -1, 0);
Nijkcombined ambiguity for the first set of combinations, defined as Nijk=iN1+jN2+kN3,N1,N2,N3Respectively three frequencies of f1,f2,f3Ambiguity of frequency points, NijkIs L calculated by the formula (5)1Taking the value after the rounding;
a2,b2,c2,d2coefficients, which are respectively corresponding terms, are calculated by equation (10):
wherein alpha is2,β2The introduced auxiliary coefficient is calculated by formula (10); sigmaφ23Taking the carrier phase variance in meters as 0.0009;
(5) given the carrier coefficients of the third combination, calculating the ambiguity of the third combination;
calculating the third combined ambiguity according to equation (11):
wherein λ isuvwFor the third combined wavelength, calculated by equation (12):
(u, v, w) is the carrier coefficient of the third combination, which is (0, 1, 0);
Nmntcombined ambiguity for the second set of combinations, defined as Nmnt=mN1+nN2+tN3,NmntIs represented by the result L of equation (8)2Averaging over 10 epochs and rounding to obtain the average value;
a3,b3,c3,d3,e3coefficients of the corresponding terms, respectively, expressed by the formula (1)3) And (3) calculating:
wherein alpha is3,β3The introduced auxiliary coefficient is calculated by formula (13);
(6) and recovering the ambiguity of the three frequency points.
2. The non-equal measurement variance-based long-baseline tri-band ambiguity resolution method of claim 1, wherein in step (1), the satellite navigation system is a global positioning system, a glonass satellite navigation system or a beidou satellite navigation system capable of broadcasting tri-band navigation signals.
3. The non-equal measurement variance-based long-baseline three-frequency ambiguity resolution method according to claim 1, wherein in step (1), the pseudo-range noise of each frequency point is extracted according to formula (1):
MPind=ρind-(a0φ1+b0φ2+c0φ3) (1)
wherein, MPindWherein ind is 1,2,3, and the three frequencies to be extracted are f1,f2,f3Pseudo-range noise of frequency points; rhoindFor three frequencies respectively being f1,f2,f3A frequency point pseudo range; phi is a1,φ2,φ3Respectively three frequencies are respectively f1,f2,f3The carrier phase of the frequency point in meters is taken as the unit; a is0,b0,c0Respectively three frequencies are respectively f1,f2,f3And (5) coefficients corresponding to the frequency points.
4. The non-equal measurement variance based long-baseline three-frequency ambiguity resolution method of claim 3, wherein in equation (1), a0,b0,c0Calculated from equation (2):
wherein f is1,f2,f3Frequencies of three frequency points, alpha, respectively0,β0Are all introduced auxiliary coefficients.
5. The non-equal measurement variance-based long-baseline three-frequency ambiguity resolution method according to claim 1, wherein in step (6), the ambiguity of each frequency point is restored according to formula (14):
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201910828674.3A CN110441805B (en) | 2019-09-03 | 2019-09-03 | Long-baseline three-frequency ambiguity resolution method based on unequal measurement variance |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201910828674.3A CN110441805B (en) | 2019-09-03 | 2019-09-03 | Long-baseline three-frequency ambiguity resolution method based on unequal measurement variance |
Publications (2)
Publication Number | Publication Date |
---|---|
CN110441805A CN110441805A (en) | 2019-11-12 |
CN110441805B true CN110441805B (en) | 2021-06-04 |
Family
ID=68438933
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201910828674.3A Active CN110441805B (en) | 2019-09-03 | 2019-09-03 | Long-baseline three-frequency ambiguity resolution method based on unequal measurement variance |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN110441805B (en) |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103837879A (en) * | 2012-11-27 | 2014-06-04 | 中国科学院光电研究院 | Method for realizing high-precision location based on Big Dipper system civil carrier phase combination |
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 |
CN105676250A (en) * | 2016-01-15 | 2016-06-15 | 北京航空航天大学 | GNSS-based single-epoch three-frequency ambiguity resolution method |
CN109001781A (en) * | 2018-08-01 | 2018-12-14 | 太原理工大学 | A kind of tri- frequency Ambiguity Solution Methods of BDS for taking ionosphere constraint into account |
-
2019
- 2019-09-03 CN CN201910828674.3A patent/CN110441805B/en active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103837879A (en) * | 2012-11-27 | 2014-06-04 | 中国科学院光电研究院 | Method for realizing high-precision location based on Big Dipper system civil carrier phase combination |
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 |
CN105676250A (en) * | 2016-01-15 | 2016-06-15 | 北京航空航天大学 | GNSS-based single-epoch three-frequency ambiguity resolution method |
CN109001781A (en) * | 2018-08-01 | 2018-12-14 | 太原理工大学 | A kind of tri- frequency Ambiguity Solution Methods of BDS for taking ionosphere constraint into account |
Non-Patent Citations (2)
Title |
---|
"A new unequal-weighted triple-frequency first order ionosphere correction algorithm and its application in COMPASS";WenXiang Liu et al.;《Science China(Physics,Mechanics & Astronomy)》;20120301;全文 * |
"北斗三频相位观测值线性组合模型及特性研究";张小红 等;《中国科学》;20151231;第45卷(第5期);全文 * |
Also Published As
Publication number | Publication date |
---|---|
CN110441805A (en) | 2019-11-12 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN100437142C (en) | Error separation method based on foundation strength system and foundation strength system | |
EP0609935B1 (en) | Method and apparatus for smoothing code measurements in a global positioning system receiver | |
US8593342B2 (en) | Utilizing SBAS signals to improve GNSS receiver performance | |
US7535414B2 (en) | Navigational positioning without timing information | |
US7924220B1 (en) | Method and apparatus for weak data frame sync in a positioning system | |
CN107728180B (en) | GNSS precision positioning method based on multi-dimensional particle filter deviation estimation | |
CN109581452A (en) | A kind of GNSS reference station ambiguity of carrier phase calculation method | |
US20070252754A1 (en) | System and method for advanced tight coupling of GPS and navigation based on dead reckoning | |
CN107728171B (en) | Particle filter based real-time tracking and precise estimation method for deviation between GNSS phase systems | |
US20200041658A1 (en) | Gnss receiver with a capability to resolve ambiguities using an uncombined formulation | |
CN110208836B (en) | GNSS high-adaptability cycle slip detection and restoration method based on Kalman filtering | |
US8184047B1 (en) | Method and apparatus for weak data bit sync in a positioning system | |
CN114924295A (en) | Carrier phase smoothing pseudorange positioning method, device and storage medium | |
CN110441800B (en) | Four-frequency cycle slip detection and restoration method based on linear combination optimization | |
CN110727000B (en) | Small cycle slip repairing method based on GNSS high sampling rate data | |
US10534087B1 (en) | Differential vector phase locked loop GPS reception method | |
CN116243591A (en) | Subnanosecond time service method integrating UTC (k) and Beidou broadcast ephemeris | |
CN111123322A (en) | Observed value real-time data preprocessing method, system, medium and equipment of satellite-borne GNSS receiver | |
CN110441805B (en) | Long-baseline three-frequency ambiguity resolution method based on unequal measurement variance | |
CN110441801B (en) | Three-frequency cycle slip detection and restoration method based on optimal fixed probability | |
US11513235B2 (en) | Global navigation satellite system (GNSS) signal tracking | |
Park et al. | Design of signal acquisition and tracking process based on multi-thread for real-time GNSS software receiver | |
JP6203608B2 (en) | GLONASS receiver | |
Pini et al. | Estimation of satellite-user ranges through GNSS code phase measurements | |
CN114152961A (en) | Cycle slip processing method and device of navigation system |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant |