CN1195991C - Global-positioning satellite positioning system and global-positioning satellite positioning method - Google Patents
Global-positioning satellite positioning system and global-positioning satellite positioning method Download PDFInfo
- Publication number
- CN1195991C CN1195991C CNB001201751A CN00120175A CN1195991C CN 1195991 C CN1195991 C CN 1195991C CN B001201751 A CNB001201751 A CN B001201751A CN 00120175 A CN00120175 A CN 00120175A CN 1195991 C CN1195991 C CN 1195991C
- Authority
- CN
- China
- Prior art keywords
- data
- gps
- code
- navigation data
- polarity
- 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.)
- Expired - Fee Related
Links
Images
Landscapes
- Position Fixing By Use Of Radio Waves (AREA)
Abstract
The integral number of PN frames is limited because of the limit of the reversal data polarities which are not detected in the prior art, and thus, the sensibility can not be improved obviously. In addition, a terminal device obtains Doppler information from an external device frequently and even the terminal device arranged at one side has to communicate with the external device, which results in the problem of the consumption of communication cost. The present invention has a solution that using a relative peak position detection unit determines the starting of the demarcation points of the reversed polarities; all code blocks on the position corresponding to a plurality of PN frames of each bit formed into navigation data are summarized to form a C/A code; the C/A code and the C/A code generated inside the GPS terminal device are calculated to figure out a virtual distance. In the occasion where a receiving electric field detected by a receiving electric field strength detection unit is good, the position is calculated according to navigation data extracted from the GPS terminal device. In the occasion where a receiving electric field is not good, the position is calculated according to the virtual distance and navigation data received from the external device.
Description
Technical field
The present invention relates to GPS positioning system and GPS localization method, be used for reception and come from the Satellite GPS signal, thereby correctly detect receiving position.
Background technology
Around the earth many artificial satellites are arranged, the electric wave of the identical carrier frequency 1575.42GHZ of emission continuously from each satellite.This electric wave is received respectively to distribute to the different code pattern of each satellite by virtual noise code phases modulation back.As this virtual noise code known have can general public use the code pattern that changes by so-called C/A code regulation.In addition, when being used to locate, the user must be carried the navigation data that is made of information such as the modified value on satellite-orbit information and the satellite, ionospheric correction factors by the polarity reversal that makes the C/A code and be launched on above-mentioned electric wave.
Above-mentioned C/A code as shown in figure 13, be 1023 bits=1msec as the 1PN frame, the signal of the rule that 1 data bit is made up of the 20PN frame.That is, above-mentioned navigation data is 50BPS, the signal of 1000PN frame/second.
Figure 14 is a block scheme of representing for example to be documented in the GPS positioning system of the prior art in No. 5663734 instructions of United States Patent (USP), and 101 is land stations in the drawings, and it is equipped with GPS receiving antenna 102 and emitting antenna 103,104th, remote device.
This remote device 104 comprises: the frequency converter 106 that the RF from GPS receiving antenna 105 is become IF, simulating signal from this frequency converter 106 is transformed into the A/D transducer 107 of digital signal, storage is from the storer (digital rapid change storer) 108 of the output of this A/D transducer 107, and processing is from the digital signal processing circuit (hereinafter to be referred as the DSP circuit) 109 of the general programmable of the signal of this storer 108.
In addition, also have and be equipped with the program EPROM110 that links to each other with DSP circuit 109, frequency mixer 111, the modulator-demodular unit 118 that the microprocessor 114 of power regulator 112, address write circuit 113, microprocessor 114, RAM (storer) 115, EEPROM116 and transmit receive antenna 117 links to each other.
The following describes the operation of said system.
Utilize DSP circuit 109 to carry out calculating between cut section, DSP circuit 109 uses the fast Fourier transform (FFT) algorithm.Whereby can be by promptly finishing coherent detection many times between the standard signal that generates in inside and the received signal, come the very fast calculating of carrying out between cut section.Fast fourier transformation algorithm is surveyed the time of occurrence of each gps signal simultaneously concurrently, thereby has accelerated calculation procedure.
In case DSP circuit 109 has been finished the calculating between each target satellite cut section, just this information is sent to microprocessor 114 through interconnective bus 122.
Then, microprocessor 114 utilizes modulator-demodular unit 118 being used to calculate the interval censored data of cutting apart of determining the final position, and sends land station 101 to through data link 119.
Except partition data, also can send to land station to expression from the storer 108 initial data of collecting simultaneously to timing characteristic by communication line 119 emission data time institute elapsed times.This timing characteristic can improve the ability of the land station 101 that carries out computing.Here it is can calculate the reason of gps satellite position in the moment of data aggregation whereby.
Though modulator-demodular unit 118 sends and receives by data communication circuit 119 information of carrying out, also utilize another to send for this purpose and receive electric wire 117.Modulator-demodular unit 118 comprises receiver and transmitter, and both can alternately be used in combination on transmission/reception antennas 117.Same land station 101 also can use other antenna 103 in order to send/receive data ring information, thereby can receive gps signal continuously through GPS receiving antenna 10 in land station 101.
In DSP circuit 109, carry out position calculation in case of necessity between reach below the several seconds and expect, but this decides by being stored in the data volume in the storer 108 and the speed of DSP circuit 109 or several DSP circuit.
As mentioned above, storer 108 is caught corresponding long interior record of time, by utilizing the fast convolution method to handle big like this blocks of data effectively the ability of handling the low signal of incoming level (signal when for example seriously blocking the level decline that makes reception because of fixed buildings, trees etc.) is improved.
For whole ordering territory of visual gps satellite all is to utilize data computation that same intermediate conversion crosses.Change rapidly at signal amplitude under the state of (for example obstacle in city etc.), this will give play to the performance also higher than the GPS receiver of Continuous Tracking formula.
The signal Processing of carrying out with above-mentioned DSP circuit 109 is described below with reference to Figure 13.The purpose of this processing is that the waveform that relative interior produces is determined regularly characteristic of received waveform, in order further to improve sensitivity, and will be to above-mentioned waveform through in the time of 100ms to 1S, handling usually for a long time.
The random sample (PN frame) that the GPS letter (C/A code) that receives is repeated to sort by 1023 chips=1msec is formed and continuous PN frame is added up mutually.For example because at 1 second time memory at 1000 PN frames, the institute so that the 1st frame sequential ground be added in mutually on the 2nd frame, the generation the result be added on the 3rd frame.Shown in following Figure 15 (A)～(E), carry out addition like that in turn.The result obtains the signal of the duration of 1PN frame=1023 chips, just can determine two the relative timing characteristic of phasetophases territories (pseudo range) of promptly sorting in proper order if this order phase place and benchmark of this locality compared in proper order.
Existing GPS positioning system is by above-mentioned formation.Be called the signal Processing before the correlation computations that receives the standby integration of gps signal in order to realize high sensitivity, but in this process, be subjected to the influence that storage effect that the polarity reversal because of navigation data causes reduces.In order to prevent this influence, above-mentioned standby integration carries out at 5～10PN frame.
Be included in the content difference of the phase place of the C/A code in the GPS received signal, the possibility that on each bit boundaries of navigation data, exists phase polarity to put upside down along with navigation data.For this reason, because in such processing, the polarity of C/A code is along with navigation data changes, so exist when utilizing the polarity integration (cumulative addition) of C/A code, signal content disappears mutually mutually, the shortcoming that signal to noise ratio (S/N ratio) (S/N) can not be improved.
That is, can not detect the separation of navigation data polarity reversal.
Therefore the integration number is limited in theory, the problem that exists signal to noise ratio (S/N ratio) fully not improve.
In addition, remote device as end device is being carried out position finding (hereinafter to be referred as the location) when handling, at every turn all from land station's acquired information, calculate the pseudo range of each visible satellite, according to this pseudo range the result is sent to server, owing to communication between essential all the time when locating and the server, therefore there is the problem that spends communication fee in the sense terminals device.
Summary of the invention
The present invention proposes in order to address the above problem, purpose provides GPS positioning system and the GPS localization method with high s/n ratio, also can carry out in the signal to noise ratio (S/N ratio) condition of severe even the invention has the advantages that with the communication of external device (ED), and try hard to cut down communication fee, even in the room, buildings blocks and down also can stablize reception.
According to the present invention, a kind of GPS positioning system at first is provided, comprise an external system, be used for obtaining navigation data from a gps signal, with a GPS terminal, be used to use navigation data to calculate from described external system, it is characterized in that, described GPS terminal comprises: a data acquiring portion is used for obtaining the data with polarity from a gps signal; A data processing section is used for changing this polarity based on the navigation data that obtains from described external system, and corresponding each part corresponding to a C/A code length calculate corresponding to the described data at identical chip position place add up and; A correlation computations part, be used to calculate relevant between the result of described processing and the C/A code, and pseudo range calculating section, be used for according to the correlation peak location that partly obtains from described correlation computations, calculate this GPS terminal and corresponding to the pseudo range between the satellite of described C/A code.
The GPS positioning system is in specified level when following at correlation peak, above-mentioned data block split position displacement can also be sent into the unit of above-mentioned stack sum unit.
The unit of the split position of above-mentioned mobile data piece is moved further data block in time, so that make correlation peak reach maximum, the unit that calculates above-mentioned pseudo range also can be according to the relevant peaks position calculation pseudo range that calculates.
Whether good above-mentioned GPS end device be equipped with reception from the Satellite GPS signal and detect to receive electric field electric field detecting unit, can the unit that above-mentioned data block is cut apart in turn received under the good situation of electric field, cut apart the gps data of doppler correction according to the navigation data that extracts from the gps signal of above-mentioned reception, cut apart the gps data that Doppler revises according to the navigation data that receives from external device (ED) receiving under the electric field condition of poor.
The GPS positioning system can have the navigation data calculating location that extracts according to the gps signal from above-mentioned reception under the good situation of electric field receiving, and is receiving under the electric field unfavorable condition according to the navigation data of accepting from the said external device and the position calculation unit of above-mentioned pseudo range calculating location.
The GPS positioning system can be the position calculation unit of the navigation data calculating location that receives according to the pseudo range that is calculated by the GPS end device with by external device (ED).
The unit that moves the split position of above-mentioned data block is in the split position that specified level can detect above-mentioned data block when following at correlation peak, also can only move the position that predetermined amount detects relevant peaks.
The amount of movement of the split position of above-mentioned data block is with very big before and after the beginning, and the amount of movement that diminishes then finishes.
Above-mentioned Doppler's amending unit can carry out Doppler's correction to the C/A code that is included in the gps signal that receives by the doppler information of the navigation data that obtains from external device (ED) or GPS end device itself.
The doppler correction of C/A code be revised and then be carried out to above-mentioned Doppler's amending unit also can by the gps signal that receives being carried out Doppler.
Whether excellent reception electric field detecting unit also can utilize the electric field level of detection that correlation computations length of an interval degree is changed to detect the reception electric field.
Whether excellent reception electric field detecting unit also can change addition length of an interval degree according to the state that receives electric field to detect the reception electric field.
The second, according to the present invention, provide a kind of GPS terminal, it is characterized in that comprise: a data acquiring portion is used for obtaining the data with polarity from a gps signal; A data processing section is used for changing this polarity based on the navigation data that obtains from this gps signal, and for calculate corresponding to each part of a C/A code length corresponding to the described data at identical chip position place add up and; A correlation computations part, be used to calculate relevant between the result of described processing and the C/A code, and pseudo range calculating section, be used for according to the correlation peak location that partly obtains from described correlation computations, calculate this GPS terminal and corresponding to the pseudo range between the satellite of described C/A code.
According to the present invention, a kind of GPS localization method is provided, it is characterized in that described method comprises: a first step is used for obtaining the data with polarity from a gps signal; One second step is used for changing this polarity based on navigation data, and for the time should in each part of a C/A code length calculate corresponding to the described data at identical chip position place add up and; A third step is used to calculate relevant between the result of described second step and this C/A code; One the 4th step is used for the correlation peak location of a correlation peak detection that obtains according to from described correlation computations; One the 5th step is used for according to described correlation peak location, detects a GPS terminal and corresponding to the pseudo range between the satellite of described C/A code.
Description of drawings
Fig. 1 is the block scheme that the user mode summary of 1 GPS positioning system and GPS localization method is described according to the embodiment of the present invention.
Fig. 2 is the block scheme of the concrete formation of table end device shown in Figure 1;
Fig. 3 is the more detailed block scheme of the end device of presentation graphs 2.
Fig. 4 is the procedure chart of explanation home server operation.
Fig. 5 is the flow diagram of explanation in the CPU26 of GPS positioning system.
Fig. 6 is the flow diagram of the CPU27 of explanation in the CPS positioning system.
Fig. 7 is the flow diagram of the CPU28 of explanation in the GPS positioning system.
Fig. 8 is the data plot of expression gps signal (C/A code signal).
Fig. 9 is the figure of explanation gps signal (C/A code signal) structure.
Figure 10 is the method key diagram that explanation detects navigation data polarity reversal separation.
Figure 11 is the block scheme that explanation detects the method for navigation data polarity reversal separation.
Figure 12 is the further explanatory drawings about the processing of the correlated results (correlation peak data) between 2 addition results and the C/A code.
Figure 13 is the key diagram of C/A code.
Figure 14 is the block scheme that expression GPS positioning system of the prior art constitutes.
Figure 15 is the key diagram that the C/A code in the prior art the GPS positioning system detects mode.
Embodiment
The following describes one embodiment of the present invention.
Fig. 1 is the block scheme of mode of operation summary of the GPS positioning system of explanation embodiments of the present invention 1, in Fig. 1, the 1st, target satellite, the 2nd, be equipped with and be arranged on reception from the receiving antenna in the good environment of the ken of the gps signal of target satellite 13 and as the home server that from the gps signal that receives, extracts the external device (ED) of navigation data and doppler data, the 4th, by end device wireless or that wire communication medium 5 are connected with home server 2, these end device 4 equipments effectively receive the receiving antenna 6 from the gps signal of satellite 1.
Description operation summarily below.
At first, when above-mentioned home server 2 receives gps signal at the receiving antenna 3 under being arranged on the good environment of the ken, judge S/N than whether good after (step ST1) carry out doppler data and calculate (step ST2), carry out GPS navigation data computation (step ST3).
Then, end device 4 detects the electric field intensity (step ST4) that receives by receiving antenna 6, judges the electric field that receives whether good (step ST5), as for being, then at end device one side extraction navigation data and doppler data (step ST6).If, then extract necessary navigation data and doppler data (step 7) from home server 2 for not.And, determine between the memory block and computation interval according to above-mentioned detected received electric field strength, the gps signal that receives is stored in (step ST8) in the storer.
Then the gps signal that receives is carried out Doppler and revise (step ST9), these data are divided into the bit length of navigation data, calculate correlation by correlation peak location detecting device (step ST10) and reach maximum that according to what calculate, and with these data as pseudo range.Navigation data according to this pseudo range and above-mentioned extraction carries out position calculation (step ST14).
As mentioned above, whether good according to this embodiment 1 by judging the reception electric field, can constitute the structure of only under the received field unfavorable condition, carrying out communication, so can reduce communication fee significantly with home server 2.
Fig. 2 is the block scheme that is illustrated in the concrete formation of the end device 4 shown in above-mentioned Fig. 1, the 7th, receiving circuit, 8 and 9 is mould/transformation of variables circuit (hereinafter to be referred as A/D), the 11st, the received electric field strength detecting unit, the 12nd, storer (DRAM), the 13rd, calculation processing unit, the 14th, and home server 2 between carry out data by electric wave and send to receive the antenna that is arranged on the wireless device 15, the 16th, be connected the modulator-demodular unit (or TA) on the wireless device 15, the 17th, be configured in the output circuit between modulator-demodular unit 16 and the bus 18.
Above-mentioned receiving circuit 7 has: the down converter 20 that links to each other with 24 with bandpass filter 19 respectively at output terminal, reference oscillator 21, synthesizer mixer 22 is the frequency divider 23 of the output frequency frequency division clock signal of this synthesizer mixer 22, I/Q transducer 25.Aforementioned calculation processing unit 13 has: continuous respectively CPU26, CPU27, the CPU28 on bus 18, be connected the storer (RAM) 29 on the bus 18, be connected the DSP30 on the CPU27, last config memory (ROM) 26a～28a respectively of each CPU26～CPU28.
Fig. 3 is the pie graph that is described in more detail Fig. 2, the same label of all parts identical with Fig. 2, and the repetitive description thereof will be omitted.Home server 2 has GPS benchmark receiving element 31, extracts the navigation data extracting unit 32 that is included in the navigation data in the gps data, doppler information computing unit 33, signal synthesis unit 36, signal emission receiving element 37.
Each unit from above-mentioned navigation data extracting unit 43 to position computing unit 57 separately is not provided with independently, and the function of these unit is carried out by the calculation processing unit 13 with CPU26～CPU28 and DSP30.In addition, illustrated embodiment is to show 3 CPU for brief description, in fact can only finish with 1 CPU.
The following describes operation.
Fig. 4 is the procedure chart of the operation of explanation home server 2.In home server 2, at first receive gps signal (step ST16) by GPS benchmark receiving element 31, then calculate doppler data by doppler information computing unit 33, (step ST17), extract GPS navigation data (step ST18) by navigation data extracting unit 32 simultaneously, synthetic by signal synthesis unit 6 then.When terminal 4 has request of data, just above-mentioned doppler data and navigation data are sent to end device 4 one sides (step ST19) from signal transmission/receiving element 37.
Fig. 5～Fig. 7 is the procedure chart of the operation of explanation in each CPU of GPS positioning system.In end device 4 one sides, at first in CPU26 one side, receive gps signal (step ST21) by antenna 6, after the gps signal that the vibration frequency of receive frequency translation circuit 20 by the reference oscillator 21 supplied with through synthetic frequency mixer 22 receives this is transformed into assigned frequency, by I/Q converter unit 25 I/Q conversion (step ST22) is carried out in the output of this receive frequency circuit 20, take out I signal and Q signal, carry out the A/D conversion by A/ D translation circuit 8,9.
In addition, by received electric field strength detecting unit 11 detections received electric field strength at this moment, select electric field level 1 (ultraweak), electric field level 2 (faint), electric field level 3 (normally) (step ST23～step ST25), the electric field level of corresponding these selections, by between the memory block and the interval determining unit 41 of correlation computations determine τ 1 between memory blocks, τ 2 between the memory block, τ 3 between the memory block (step ST26～step ST28), in the memory block S of interval (time) storer of determining 12, bring in constant renewal in the gps signal (step ST29) of storage by above-mentioned A/ D translation circuit 8,9.
Navigation data extracting unit 43 extracts navigation data after reading the content of memory block S.Always in the signal of the data cell 43 of navigating, extract doppler information by doppler information extracting unit 45, from signal, extract doppler information by Data Receiving unit 48 again, and be stored among the D of memory block from home server 2.Doppler's amending unit 46 reads the data (step ST30) of memory block D, and the data of memory block S are carried out being stored in (step ST31) among the H of memory block after Doppler revises.
Then read the content (step ST32) of the memory block L of store electricity field strength in the CPU27 side, as electric field level is 3, then read the data (step ST32b) of the memory block V that stores from the navigation data of navigation data extracting unit 43, in addition, as electric field level is 1 or 2 (ultraweak or faint), then the memory block V reading of data (step ST32a) from storing from the navigation data of home server by transmission/receiving element 48 and navigation data extracting unit 49.τ 1 between corresponding more above-mentioned specified memory, between the memory block between τ 2 and memory block the interval of τ 3 read gps signal and read the navigation data (step ST33) of regulation from memory block V from memory block H.Correlation peak location detecting unit 52 forms data block by the navigation data from the regulation of memory block V to cutting apart the back from the gps signal of memory block H by the bit length of this navigation data, each corresponding chip addition with 20 PN frames of (being in each bit of navigation data) in each data block, get the long-pending of these summed result bit corresponding with navigation data, τ 1 between all memory blocks, τ 2 between the memory block, summation forms the C/A code to these products in the interval of τ 3 between the memory block, carries out the correlation computations (step ST34) of this C/A code and the C/A code that is taken place by C/A code generating unit 51 then in above-mentioned all intervals.To describe afterwards about this processing.
Then, mobile navigation data in time so that make correlation peak reach maximum, the correlation peak location by same repeatedly correlation computations acquisition as the separation of the polarity reversal of navigation data and pseudo range (step ST36, S37).
Export the self-position result of calculation of carrying out subsequently according to navigation data and pseudo range.
In the CPU28 side, read the content (step ST41) of memory block L, whether judge electric field level at (step ST42) more than 3, if yes, then cut-off switch 47, and it is not linked to each other with home server 2, thereby can reading of data (step ST43).If NO, then connect switch 47, carry out data read (step ST44) from home server 2, navigation data is stored among the VS of memory block, doppler information is stored in by doppler information extracting unit 45 among the interval memory block D of respective electric field level (step ST45).
As mentioned above, according to this embodiment 1, judge whether the reception electric field is good, can constitute the structure that only when the reception electric field is bad, could carry out communication with home server, so can reduce communication fee significantly, simultaneously by the correlation peak location detecting unit, the regular C/A code that will be made of a plurality of chips is by the summation that adds up of the value of each cycle and same chip position, the increase and decrease separation of this summed result that adds up as the data starting position of suing for peace, because have the structure that to carry out the summation of C/A code, so can eliminate when carrying out data integrate (summation adds up) with the technology in the prior art, because of disappearing mutually mutually, signal content overcome the shortcoming that sensitivity (S/N) can not fully improve, thereby can determine to detect the C/A code and the pseudo range of being buried, obtain highly sensitive GPS positioning system by noise.
Embodiment with regard to correlation peak location detecting unit 52 is described in detail below.
In this embodiment, the regular C/A code that constitutes by a plurality of chips in any position the data block by 1 bit long of navigation data cut apart.With the summation that adds up of the value of the same chip position of the PN frame in each data block, the navigation data of accepting according to the navigation data that detects or from home server is with the result and the combinations of polarities addition of this summation that adds up, carry out correlation computations with this addition result and C/A code, the correlation peak location that obtains as the data starting position of suing for peace.
Each PN frame data when Fig. 8 shows navigation data length for the M bit and the relation of chip data.
At this, navigation data bit 1 is made up of the 20PN frame as shown in the figure, and 1 PN frame is made up of 1023 chips.Doppler revises the 1PN frame (C/A code=PN code) of the gps signal of back storage and is made up of 1023 chips.
Each PN frame of gps signal is made up of 1023 chips, for the digitizing of A/D transducer the time, according to the loyal transmission information of sampling theory, and is necessary with the frequency sample more than several times.Sampled data in memory block S and storer V is made up of the sample number more than the chip several times for this reason.
For example 1023 chips are used as the individual sampled value of 1023 * 2i (for example i=1,2 and 3) and are stored).
In the following description, for simplicity, according to standard declaration C/A shape sign indicating number chip units.
In Fig. 5, the doppler information (Doppler frequency of each satellite moves) that the CPU26 basis obtains from storer etc. carries out Doppler to each satellite and revises (step ST30, step ST31).These values are stored among the H of memory block, for being undertaken for the corrected signal of Doppler by the CPU27 of Fig. 5, the regular C/A code that will be made of a plurality of chips is divided into the data block of 1 bit long of navigation data at an arbitrary position, begin in turn with sampling location (=1023 * 2i of PN frame (=1023 chip) unit from the beginning position of each data block each dispersion, i=1,2,3), a length addition once to 1 bit (=20 frames ,=20 * 1023 chips) of navigation data.Can obtain 1023 * 2i summing value so altogether
The gps data of storage is the data of these PN frames repetitions and the continuous rule that occurs.And make the phase inversion of C/A code according to the polarity of each bit of navigation data (quite 20ms).The first head part of the bit of the navigation data when the first head part the during phase inversion of C/A code changes with navigation data is consistent.
Graph of a relation when navigation data length shown in Figure 9 is the M bit.In the drawings, d (ij, k) sample data of i chip of j PN frame of k bit of expression navigation data.With this data storage with stipulated time quite in the storer of (being that navigation data is M part bit in the present embodiment).It is which chip from gps signal that the data of storage can not be distinguished.Figure 10 is the key diagram that is stored in the data processing in the storer.Cut apart gps signal (C/A code) according to outside or inner navigation data, then the navigation data of cutting apart the composition bit is stored in the storer.The C/A code chip of navigation data M part bit that will read from arbitrary portion is stored in and adds up to 1023 * 20 * M chip storer.
Figure 10 with 20 * M capable * 1023 row the ranks forms show the data of input store at this moment.Chip data below first row the 1023rd row of these data are data of the 2nd row the 1st row.The following data of same the 2nd row the 1023rd row are data of the 3rd row the 1st row.Repeat this and arrange capable 1023 row up to 20 * M.
When utilization was cut apart arbitrarily gps signal (navigation data) from the outside or inner navigation data that obtains, this first head part was inconsistent usually with the first head part (the first head part of the true navigation data that exists in gps signal) that is stored in the gps signal phase inversion in the storer.
This correlation peak location detecting unit makes two above-mentioned first head part very consistent by the following method.
Below just Figure 11 be specifically described.
At first, in Figure 10, utilize the data computation following formula of the ranks of 20 row, 1023 row of cutting apart according to navigation data bit Dk:
S
1(D
1)＝d(1，1，1)+d(2，1，1)+d(3，1，1)+……+d(20，1，1)
S
2(D
1)＝d(1，2，1)+d(2，2，1)+d(3，2，1)+……+d(20，2，1)
S
3(D
1)＝d(1，3，1)+d(2，3，1)+d(3，3，1)+……+d(20，3，1)
S
1(D
1)＝d(1，i，1)+d(2，i，1)+d(3，i，1)+……+d(20，i，1)
S
1023(D
1)＝d(1，1023，1)+d(2，1023，1)+……+d(20，1023，1)
Then get S respectively
1(D
1), S
2(D
1) ... S
i(D
1) ... S
1023(D
1) and data bit D
1(=-1 or+1) long-pending;
Obtain D
1* S
1(D
1), D
1* S
2(D
1) ... D
1* S
i(D
1) ... D
1* S
1023(D
1).
Utilize following formula to calculate the data of cutting apart by navigation data bit again;
S
1(D
2)＝d(1，1，2)+d(2，1，2)+d(3，1，2)+……+d(20，1，2)
S
2(D
2)＝d(1，2，2)+d(2，2，2)+d(3，2，2)+……+d(20，2，2)
S
3(D
2)＝d(1，3，2)+d(2，3，2)+d(3，3，2)+……+d(20，3，2)
S
i(D
2)＝d(1，i，2)+d(2，i，2)+d(3，i，2)+……+d(20，i，2)
S
1023(D
2)＝d(1，1023，2)+d(2，1023，2)+……+d(20，1023，2)
Then get S respectively
1(D
2), S
2(D
2) ... S
i(D
2) ... S
1023(D
2) and data bit D
2(=-1 or+1) long-pending;
Obtain D
2* S
1(D
2), D
2* S
2(D
2) ... D
2* S
i(D
2) ... D
2* S
1023(D
2).
Equally, calculate by navigation data D with following formula
MThe data of cutting apart:
S
1(D
M)＝d(1，1，M)+d(2，1，M)+d(3，1，M)+……+d(20，1，M)
S
2(D
M)＝d(1，2，M)+d(2，2，M)+d(3，2，M)+……+d(20，2，M)
S
3(D
M)＝d(1，3，M)+d(2，3，M)+d(3，3，M)+……+d(20，3，M)
S
i(D
M)＝d(1，i，M)+d(2，i，M)+d(3，i，M)+……+d(20，i，M)
S
1023(D
M)＝d(1，1023，M)+d(2，1023，M)+……+d(20，1023，M)
Get S more respectively
1(D
M), S
2(D
M) ... S
i(D
M) ... S
1023(D
M) and data bit D
M(=-1 or+1) long-pending;
Obtain D
M* S
1(D
M), D
M* S
2(D
M) ..., D
M* S
i(D
M) ..., D
M* S
1023(D
M).
Then, calculating is following various:
C
1＝D
1×S
1(D
1)+D
2×S
1(D
2)+……D
M×S
1(D
M)
C
2＝D
1×S
2(D
1)+D
2×S
2(D
2)+……D
M×S
2(D
M)
C
3＝D
1×S
3(D
1)+D
2×S
3(D
2)+……D
M×S
3(D
M)
C
4＝D
1×S
4(D
1)+D
2×S
4(D
2)+……D
M×S
4(D
M)
C
1023＝D
1×S
1023(D
1)+D
2×S
1023(D
2)+……+D
M×S
1023(D
M)
Carry out by 1023 data C at this
1, C
2, C
3, C
4, C
10231023 correlation computations (step ST34) of the data group of forming and the C/A code that produces in inside.
The precision of correlation computations value, the increase of choosing along with sampled point and increasing.Figure 12 illustrates to improving relevant peaks positional precision method and choose the example of quite getting 2 sampled points at 1 bit, wherein (a) is the situation that real peak value is in sampled point central authorities, (b) being the situation that real peak value departs from sampled point a little, (c) is the real peak value situation consistent with sampled point.According to X
PPeak X is obtained in=p2/ (p1+p2) τ/2
P(local location that departs from sampled point), τ is the length of a suitable bit in the formula.
Judge that then correlation peak is whether more than setting (step ST51).If step ST51 judged result is for being, then as the fine setting pattern.
Promptly make on one side the mobile small quantity of navigation data (split position of data block)+Δ n chip, on one side-Δ n chip obtains the receipts sword point (step ST52) that this peak value becomes bigger.
If what step 53 was obtained is convergence point, then obtain above-mentioned relevant peaks position X
P, this peak value maximum position (pseudo range) is stored (step ST54) corresponding to the satellite numbering.
If step ST53 is that then small quantity+Δ n chip is not moved on the limit, the fine setting of navigation data position is repeated on-Δ n chip limit, repeats if be converged in the setting, then to obtain above-mentioned correlation peak location X till the convergence in step ST53
P, and this peak value maximum position (pseudo range) stored (step ST54) corresponding to satellite numbering.
In addition, judged result as above-mentioned step ST51 is not, then the limit makes and detects navigation data that correlation peak location uses and move per 1 piece of data in turn and reach more than the specified level up to correlation peak, repeats step ST34, and step ST57 is till step ST51 judged result is when being.In this repetitive cycling process, surpass the value of having stipulated as this moving range in step ST56, whether then verify the doppler correction value in step ST58 normal.Revise the doppler correction value if the doppler correction value in setting, reads once more and verifies in step ST59, repeat step ST34 and ST54.Surpass setting as doppler correction value in step ST58 at last, then think and can not detect the satellite numbering on this satellite, detection is wound up the case to store, and asks the pseudo range (step ST60) of other satellite then.
Above-mentioned steps ST34, step ST51～step ST59 are the processing for correlation peak location is obviously carried out.
As mentioned above, according to present embodiment, the continuous PN frame that to be made up of many bits and the C/A code of rule are divided into the data block of 1 bit length of navigation data at an arbitrary position, then to the summation that adds up of the value of the same chip position of the PN value in each data block of cutting apart, this summed result that adds up is sued for peace in conjunction with polarity according to the navigation data of GPS end device detection or from the navigation data that home server obtains then, carry out correlation computations with this summed result and C/A code.By the relevant peaks position that obtains as data and starting position, can not can be subjected to the navigation data change in polarity influence ground, efficiently to the summation that adds up of C/A code, even in for example tunnel, in the sensitive low place of the medium reception of buildings, also can receive the C/A code reliably.
If the structure of the GPS positioning system of the present invention of above explanation can be carried on mobile telephone, show the position of detecting by the GPS positioning system with the map datum read from storer, even then can obtain the mobile telephone that the precision that also can effectively use is high and have navigation feature in the low place of tunnel, the medium receiving sensitivity of buildings.
As mentioned above, according to the present invention, when detecting electric field intensity, because could obtain the formation of data when having only a little less than electric field intensity by external device (ED) and means of communication, so with often compare with the prior art that external device (ED) carries out communication, have the effect that can reduce communication cost significantly.
In addition, because formation of the present invention can go up the C/A code of continuous PN frame of being made up of many chips and rule at an arbitrary position, cut apart by navigation data bit length, then to the summation that adds up of the same chip position value of each C/A code of cutting apart, according to the navigation data that itself detects or from the navigation data that home server obtains the result that this adds up summation is carried out the polarity summation operation, carry out correlation computations with this summed result and C/A code, the relevant peaks position that obtains as the data starting position of suing for peace, so can not be subjected to the influence of navigation data change in polarity, the result is, can detect reliably by the C/A code of noise takeover, can also improve S/N.
Therefore, be applicable to mobile telephone, promptly in buildings, the low place of the first-class sensitivity of the railway platform of subway also has the effect that can receive the C/A code really.Can change the interval formation of summation according to the state that receives electric field owing to have,, just have the effect that can receive the C/A code reliablely so interosculate with the premises.
As other embodiment, can certainly utilize FFT to calculate or IFFT calculating carrying out supercomputing.
As other embodiment, also can replace above-mentioned correlation computations with the consistent number or the consistent degree of the C/A code of reception with the C/A code that itself produces.
Claims (11)
1. a GPS localization method is characterized in that, described method comprises:
A first step is used for obtaining the data with polarity from a gps signal;
One second step is used for changing this polarity based on navigation data, and for calculate corresponding to each part of a C/A code length corresponding to the described data at identical chip position place add up and;
A third step is used to calculate relevant between the result of described second step and this C/A code;
One the 4th step is used for the correlation peak location of a correlation peak detection that obtains according to from described correlation computations;
One the 5th step is used for according to described correlation peak location, detects a GPS terminal and corresponding to the pseudo range between the satellite of described C/A code.
2. the described GPS localization method of claim 1, it is characterized in that, described the 4th step comprises that further one is used for the displacement of described navigation data, and if do not obtain the correlation peak of a hope, then change the step of this polarity according to the navigation data after the described displacement.
3. the described GPS localization method of claim 2 is characterized in that, described displacement is according to the maximized direction of correlation peak is carried out.
4. the described GPS localization method of claim 2 is characterized in that, the value of described displacement is a predetermined value.
5. the described GPS localization method of claim 2 is characterized in that, the value of described displacement is changed to a little value from a big value.
6. the described GPS localization method of claim 1 is characterized in that, described the 4th step also comprises the step that a use is revised at Doppler of this gps signal execution from the doppler information of this gps signal acquisition.
7. the described GPS localization method of claim 6 is characterized in that, carries out Doppler at the described data with polarity that obtain and revise from this gps signal.
8. the described GPS localization method of claim 1 is characterized in that, response receives this gps signal, detects the intensity of an electric field that receives.
9. a GPS terminal is characterized in that, comprising:
A data acquiring portion is used for obtaining the data with polarity from a gps signal;
A data processing section is used for changing this polarity based on the navigation data that obtains from this gps signal, and for calculate corresponding to each part of a C/A code length corresponding to the described data at identical chip position place add up and;
A correlation computations part is used to calculate relevant between the result of described processing and the C/A code, and
A pseudo range calculating section is used for according to the correlation peak location that partly obtains from described correlation computations, calculates this GPS terminal and corresponding to the pseudo range between the satellite of described C/A code.
10. a GPS positioning system comprises an external system, is used for obtaining navigation data and a GPS terminal from a gps signal, is used to use the navigation data from described external system to calculate, it is characterized in that,
Described GPS terminal comprises:
A data acquiring portion is used for obtaining the data with polarity from a gps signal;
A data processing section is used for changing this polarity based on the navigation data that obtains from described external system, and corresponding each part corresponding to a C/A code length calculate corresponding to the described data at identical chip position place add up and;
A correlation computations part is used to calculate relevant between the result of described processing and the C/A code, and
A pseudo range calculating section is used for according to the correlation peak location that partly obtains from described correlation computations, calculates this GPS terminal and corresponding to the pseudo range between the satellite of described C/A code.
11. the described GPS positioning system of claim 10, it is characterized in that, when the correlation peak that correlation computations obtained of described correlation computations part does not reach the correlation peak of a hope, described data processing section is shifted to described navigation data, and changes this polarity according to the navigation data after the described displacement.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB001201751A CN1195991C (en) | 2000-05-24 | 2000-05-24 | Global-positioning satellite positioning system and global-positioning satellite positioning method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB001201751A CN1195991C (en) | 2000-05-24 | 2000-05-24 | Global-positioning satellite positioning system and global-positioning satellite positioning method |
Related Child Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNB2004100641187A Division CN100554995C (en) | 2000-05-24 | 2000-05-24 | GPS terminal, GPS positioning system and GPS localization method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1325029A CN1325029A (en) | 2001-12-05 |
| CN1195991C true CN1195991C (en) | 2005-04-06 |
Family
ID=4588153
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNB001201751A Expired - Fee Related CN1195991C (en) | 2000-05-24 | 2000-05-24 | Global-positioning satellite positioning system and global-positioning satellite positioning method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN1195991C (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI231105B (en) | 2003-11-06 | 2005-04-11 | Prolific Technology Inc | Global positioning satellite and correlating circuit thereof |
| CN1987515B (en) * | 2005-12-22 | 2010-12-29 | 凹凸科技（中国）有限公司 | Method and system for realizing GPS positioning under weak signal environment |
-
2000
- 2000-05-24 CN CNB001201751A patent/CN1195991C/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| CN1325029A (en) | 2001-12-05 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN1255689C (en) | Positioning method of global positioning system and receiving apparatus of global positioning system | |
| JP6437491B2 (en) | Method and apparatus for using assistance data for a satellite position system | |
| CN1264024C (en) | Method for improving signal acquisition in a global positioning system receiver | |
| US6825805B2 (en) | Search procedure for position determination system | |
| JP3528670B2 (en) | GPS receiver | |
| CN1261769C (en) | Method and appts. for satellite positioning system (SPS) time measurement | |
| US6965760B1 (en) | Satellite-based location system employing dynamic integration techniques | |
| JP5048649B2 (en) | Method and configuration for positioning using satellite | |
| US20110294516A1 (en) | Method and apparatus for determining location | |
| JP2008515351A (en) | Method for locating a mobile terminal in a cellular radio system | |
| CN1752769A (en) | Positioning system, positioning apparatus, positioning information providing apparatus and positioning method | |
| CN103069299B (en) | Portable communication terminals and methods for cooperative positioning support during poor satellite coverage | |
| CN1786732A (en) | Positioning signal reception device and control method of positioning signal reception device | |
| JP3270407B2 (en) | GPS positioning method, GPS terminal and GPS positioning system | |
| CN1195991C (en) | Global-positioning satellite positioning system and global-positioning satellite positioning method | |
| CN1788211A (en) | A method for the location of mobile terminals | |
| CN1591039A (en) | GPS terminal, GPS positioning system and GPS positioning method | |
| CN1501616A (en) | Code reuse apparatus in cdma wireless communication system using beamforming by antenna array and code reuse method therefor | |
| CN102265173B (en) | Event location determination | |
| US10989786B2 (en) | Outdoor localization using hotspot labels | |
| JP3390753B2 (en) | GPS positioning method, GPS terminal and GPS positioning system | |
| JP4293120B2 (en) | Satellite assignment method, program, and positioning device | |
| JPH10282205A (en) | Gps receiver | |
| CN107094287B (en) | Indoor pedestrian positioning system and method based on WIFI and magnetic field two-stage search | |
| JP5556332B2 (en) | Receiver |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C06 | Publication | ||
| PB01 | Publication | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20050406 Termination date: 20140524 |