CN205656314U - Multimode satellite positioning system - Google Patents

Multimode satellite positioning system Download PDF

Info

Publication number
CN205656314U
CN205656314U CN201620231237.5U CN201620231237U CN205656314U CN 205656314 U CN205656314 U CN 205656314U CN 201620231237 U CN201620231237 U CN 201620231237U CN 205656314 U CN205656314 U CN 205656314U
Authority
CN
China
Prior art keywords
module
low noise
acoustic wave
signal
surface acoustic
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
Application number
CN201620231237.5U
Other languages
Chinese (zh)
Inventor
刘建圻
闫荷花
张严林
邹才凤
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.)
Guangdong Mechanical and Electrical College
Original Assignee
Guangdong Mechanical and Electrical College
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 Guangdong Mechanical and Electrical College filed Critical Guangdong Mechanical and Electrical College
Priority to CN201620231237.5U priority Critical patent/CN205656314U/en
Application granted granted Critical
Publication of CN205656314U publication Critical patent/CN205656314U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Position Fixing By Use Of Radio Waves (AREA)

Abstract

The utility model discloses a multimode satellite positioning system, including being used for receiving the antenna of satellite positioning signal, to the received signal carry on the signal amplification low noise amplification module, be used for carrying out surface acoustic wave filter module that filtering handled and advancing line location's orientation module according to the satellite signal after handling the signal after enlargeing, orientation module and surface acoustic wave filter module are connected, surface acoustic wave filter module is connected with low noise amplification module, low noise amplification module is connected with orientation module. The utility model discloses multimode satellite positioning system's orientation module circuit is functional, supports big dipper satellite positioning system (BDS) and global satellite positioning system (GPS) simultaneously, can realize well the real -time location and tracking of vehicle.

Description

A kind of multi-mode satellite alignment system
Technical field
This utility model relates to the research field of satellite fix, particularly to a kind of multi-mode satellite alignment system.
Background technology
Global position system develops into now, although positioning precision is greatly improved, but car working application proposes the highest requirement to positional precision, improves positioning precision imperative to improve Consumer's Experience.The development of BDS is very swift and violent, in March, 2015, a new generation's big-dipper satellite successful launch, opens the new journey realizing the networking of the year two thousand twenty whole world, and Big Dipper development strides into into " 3.0 epoch ", and Beidou satellite navigation system carries out the rhythm of whole world networking and accelerating.Same, Galileo system the most progressively comes into operation, and satellite fix, from traditional GPS epoch, enters into multi-mode satellite location time and changes.Owing to multi-mode satellite alignment system to be got well more than single GPS at the aspect such as availability, anti-interference, making multimode rake receiver greatly exceed single GPS in cost performance, compatible multiple satellite fix pattern is the trend of vehicle positioning future development.
Utility model content
Main purpose of the present utility model is that the shortcoming overcoming prior art is with not enough, it is provided that a kind of multi-mode satellite alignment system.
In order to achieve the above object, the present invention is by the following technical solutions:
A kind of multi-mode satellite alignment system of the present utility model, including the antenna for receiving satellite positioning signal, the framing signal received is carried out the low noise amplification module of signal amplification, for the surface acoustic wave filtration module being filtered processing to the signal after amplifying and the locating module positioned according to the satellite-signal after processing, described locating module is connected with surface acoustic wave filtration module, described surface acoustic wave filtration module is connected with low noise amplification module, and described low noise amplification module is connected with locating module.
As preferred technical scheme, described locating module uses XN647-8 locating module.
As preferred technical scheme, described low noise amplification module uses XN114 low noise amplification chip.
As preferred technical scheme, described surface acoustic wave filtration module uses EFCH1575TDB1 surface acoustic wave filtering chip.
As preferred technical scheme, described antenna uses the antenna of compatible BDS/GPS.
As preferred technical scheme, the specification of described BDS/GPS antenna is 25mm × 25mm × 4mm.
As preferred technical scheme, also include that ADC transducer, described ADC transducer are connected with locating module, for the location information received being converted into the output of NMEA agreement.
This utility model compared with prior art, has the advantage that and beneficial effect:
1, the locating module circuit performance of multi-mode satellite alignment system of the present utility model is good, well vehicle can be realized real time location tracking.
2, the most compatible BDS and GPS of multi-mode satellite alignment system of the present utility model.
3, the antenna performance of multi-mode satellite alignment system of the present utility model is good, and the actual signal strength values height receiving satellite of complete machine, close to theoretical value.
Accompanying drawing explanation
Fig. 1 is the structured flowchart of this utility model multi-mode satellite alignment system;
Fig. 2 is this utility model multi-mode satellite locating module circuit theory diagrams;
Fig. 3 is this utility model low noise amplification and SAW filter circuit theory diagrams;
Fig. 4 (a)-Fig. 4 (d) is respectively antenna at 4 the orientation complete machines in outdoor outdoor occasion east, south, west, north actual reception satellite signal strength value schematic diagram.
Detailed description of the invention
Below in conjunction with embodiment and accompanying drawing, this utility model is described in further detail, but embodiment of the present utility model is not limited to this.
Embodiment
As shown in Figure 1, a kind of multi-mode satellite alignment system of the present embodiment, including the antenna for receiving satellite positioning signal, the framing signal received is carried out the low noise amplification module of signal amplification, for the surface acoustic wave filtration module being filtered processing to the signal after amplifying and the locating module positioned according to the satellite-signal after processing, described locating module is connected with surface acoustic wave filtration module, described surface acoustic wave filtration module is connected with low noise amplification module, and described low noise amplification module is connected with locating module.
XN647-8 is the monolithic GNSS satellite navigation receiver module of a high-performance, low cost, has the features such as low-power consumption, high sensitivity, small size, it is possible to parallel reception multimodal satellite navigation signal.XN647-8 uses highly integrated system schema, rf receiver unit, baseband processing unit, temperature compensating crystal oscillator (TCXO/0.5ppm), low pressure difference linear voltage regulator (LDO) and part passive device (resistance, electric capacity, inductance) are internally integrated it, it is only necessary to little external resource just can be integrated in the application scheme of mobile terminal and handheld device.
XN647-8 has stronger weak signal capture ability and shorter primary positioning time, the correlator signal parameter search engine of base band internal proprietary can quickly capture usable satellite, and weak signal can be received, small-signal can be tracked under rugged environment and position by advanced tracking engine.
According to XN647-8 chip operation instruction and circuit requirements, Design Orientation modular circuit schematic diagram is as shown in Figure 2.Its main feature: miniaturization multimode GNSS receiver module, supports multiple global position system;Highly sensitive, cold start-up sensitivity is-148dBm, and tracking sensitivity is-165dBm;The startup time is fast, and cold start-up needs 29s, thermal starting to have only to 1s;Positioning precision reaches 2.5m;Programming is convenient, supports outside SPI flash memory data record.
Described low noise amplification module uses XN114 low noise amplification chip;Described surface acoustic wave filtration module uses EFCH1575TDB1 surface acoustic wave filtering chip.
XN114 is a the low noise amplifier chip being applied to receiver.Being designed with BiCMOS technique, have the characteristic of high-gain low-noise, under conditions of gain is 18dB, noise coefficient has reached 0.8dB.This chip application, in receiver front end, can be effectively improved the receiving sensitivity of receiver, expands the range of application of receiver.XN114 can be operated under+1.8V~+3.3V supply voltage, consumes electric current only 5.5mA, consumes electric current in the shutdown mode less than 10uA.Encapsulation uses 6-pin LGA form, and size is 1.5mm 1.0mm 0.75mm.Recommended work condition: supply voltage: 1.8V~3.3V operating temperature :-40 DEG C~85 DEG C.According to circuit requirements and chip operation instruction, designing low noise amplification harmony table filter circuit, its circuit theory diagrams are as shown in Figure 3.
The antenna supporting BDS/GPS refers to by accepting satellite-signal, thus carries out the used antenna that positions or navigate.Civil signal mid frequency open for BDS be the open civil signal L1 mid frequency of 1561.098MHz, GPS be 1575.42MHz, signal, typically at about-166dBm, belongs to weak signal.BDS/GPS antenna has four important parameters: gain (Gain), standing wave (VSWR), noise coefficient (Noise figure), axle ratio (Axial ratio).
Support the antenna measurement instrument of BDS/GPS: Network Analyzer (HP8752A), measuring process is as follows: 1) use calibrating device that Network Analyzer is carried out single port correction;2) antenna to be measured is connected on Network Analyzer;3) reflection coefficient (S11) needed for measuring, the relevant parameter such as return loss (Return Loss).
The antenna specification of compatible BDS/GPS is 25mmX25mmX4mm, related data is obtained by measuring process, Fig. 4 (a)-Fig. 4 (d) is respectively antenna in 4 the orientation complete machines in outdoor outdoor occasion east, south, west, north actual reception satellite signal strength value, antenna performance is good as known in the figure, and complete machine actual reception satellite signal strength value is close to theoretical value.
Utilize seizure sensitivity and tracking sensitivity that the positioning performance of multi-mode satellite alignment system is tested.Positioning chip, by supporting that the antenna of BDS/GPS receives satellite system signal, through filtering and amplifying circuit, delivers to XN647-8 monolithic GNSS satellite navigation receiver module the satellite-signal received, and through ADC conversion and internal arithmetic, is converted into the output of NMEA agreement.
Above-described embodiment is this utility model preferably embodiment; but embodiment of the present utility model is also not restricted to the described embodiments; other any without departing from the change made under spirit of the present utility model and principle, modify, substitute, combine, simplify; all should be the substitute mode of equivalence, within being included in protection domain of the present utility model.

Claims (7)

1. a multi-mode satellite alignment system, it is characterised in that include the sky for receiving satellite positioning signal Line, carries out the low noise amplification module of signal amplification, for the letter after amplifying to the framing signal received Number it is filtered the surface acoustic wave filtration module that processes and according to determining that the satellite-signal after processing carries out positioning Position module, described locating module is connected with surface acoustic wave filtration module, and described surface acoustic wave filtration module is with low Noise amplification module connects, and described low noise amplification module is connected with locating module.
Multi-mode satellite alignment system the most according to claim 1, it is characterised in that described locating module Use XN647-8 locating module.
Multi-mode satellite alignment system the most according to claim 1, it is characterised in that described low noise is put Big module uses XN114 low noise amplification chip.
Multi-mode satellite alignment system the most according to claim 1, it is characterised in that described surface acoustic wave Filtration module uses EFCH1575TDB1 surface acoustic wave filtering chip.
Multi-mode satellite alignment system the most according to claim 1, it is characterised in that described antenna uses The antenna of compatible BDS/GPS.
Multi-mode satellite alignment system the most according to claim 5, it is characterised in that described BDS/GPS The specification of antenna is 25mm × 25mm × 4mm.
Multi-mode satellite alignment system the most according to claim 1, it is characterised in that also include ADC Transducer, described ADC transducer is connected with locating module, for the location information received being converted into NMEA agreement exports.
CN201620231237.5U 2016-03-24 2016-03-24 Multimode satellite positioning system Expired - Fee Related CN205656314U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620231237.5U CN205656314U (en) 2016-03-24 2016-03-24 Multimode satellite positioning system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620231237.5U CN205656314U (en) 2016-03-24 2016-03-24 Multimode satellite positioning system

Publications (1)

Publication Number Publication Date
CN205656314U true CN205656314U (en) 2016-10-19

Family

ID=57356192

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620231237.5U Expired - Fee Related CN205656314U (en) 2016-03-24 2016-03-24 Multimode satellite positioning system

Country Status (1)

Country Link
CN (1) CN205656314U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108459297A (en) * 2017-12-29 2018-08-28 北京日月九天科技有限公司 A kind of northern instrument of precisely finger that can quickly find direct north

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108459297A (en) * 2017-12-29 2018-08-28 北京日月九天科技有限公司 A kind of northern instrument of precisely finger that can quickly find direct north

Similar Documents

Publication Publication Date Title
CN103713295B (en) Veneer triantennary high accuracy positioning direction-finding receiver
US9574882B2 (en) Automotive OBD-II device generating navigational information
CN102156289B (en) Dual-mode positioning time-service type receiver for compass satellite and global positioning system (GPS) satellite
CN104407354B (en) A kind of Beidou satellite navigation system double frequency positioning and directing instrument
CN205643718U (en) GPSBD -2 high accuracy differential positioning device
CN102890278A (en) MIMU (Micro Inertial Measurement Unit) fully-integrated navigation system based on FPGA (Field Programmable Gate Array) Beidou
CN110366233B (en) Low-power-consumption positioning method and device for Internet of things
KR101047229B1 (en) Gps rf front end and related method of providing a position fix, storage medium and apparatus for the same
CN103308932B (en) Monolithic multimode navigation chip based on broadband radio frequency direct technology
CN205656314U (en) Multimode satellite positioning system
CN104698476A (en) GPS satellite navigation receiver based on three-level mixing structure
CN203881947U (en) Single-board three-antenna high-precision positioning and orientation receiver
CN216599595U (en) Multi-mode multi-frequency high-precision positioning and orientation receiver
CN215641851U (en) Multi-frequency-point GNSS positioning device
CN219349146U (en) Multimode multifrequency navigation module
CN212160096U (en) Automatic navigation, positioning and orientation system of agricultural machine
CN218675306U (en) Double-frequency multi-mode lane-level high-precision inertial positioning system circuit
CN207782883U (en) A kind of Big Dipper/GPS dual mode satellite orientation and communication mobile phones
CN206133005U (en) Compass navigation satellite system's receiving arrangement based on niosII
CN206339658U (en) A kind of GPS
US20150181527A1 (en) Drive control method of reception unit and positioning device
CN102033233A (en) Bluetooth technology-integrated global positioning system receiver
CN103675860A (en) Global satellite navigation system receiving device
CN104570034A (en) Composite precise positioning system and positioning method thereof
CN211741581U (en) Positioning module with ultra-low power consumption

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20161019

Termination date: 20210324