CN205879191U - Antenna gesture detection device - Google Patents

Antenna gesture detection device Download PDF

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Publication number
CN205879191U
CN205879191U CN201620673335.4U CN201620673335U CN205879191U CN 205879191 U CN205879191 U CN 205879191U CN 201620673335 U CN201620673335 U CN 201620673335U CN 205879191 U CN205879191 U CN 205879191U
Authority
CN
China
Prior art keywords
central processing
processing unit
antenna
detection device
attitude detection
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
CN201620673335.4U
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Chinese (zh)
Inventor
李鑫
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.)
SICHUAN HUAZHI BAIRONG TECHNOLOGY Co Ltd
Original Assignee
SICHUAN HUAZHI BAIRONG TECHNOLOGY Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by SICHUAN HUAZHI BAIRONG TECHNOLOGY Co Ltd filed Critical SICHUAN HUAZHI BAIRONG TECHNOLOGY Co Ltd
Priority to CN201620673335.4U priority Critical patent/CN205879191U/en
Application granted granted Critical
Publication of CN205879191U publication Critical patent/CN205879191U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses an antenna gesture detection device, include central processing unit and satellite positioning appearance, gyroscope and the baroceptor be connected with central processing unit, central processing unit still with acceleration sensor, magnetic sensor and temperature sensor be connected, central processing unit passes through power supply unit and the remote radio head unit electricity that sets up on the basic station is connected. The utility model discloses utilize central processing unit and satellite positioning appearance, magnetic sensor, gyroscope, acceleration sensor and remote radio head unit connection, can be in real time, worker's information of joining of accurate, continuous monitor antenna, can insert customer's network in a flexible way moreover, realize the real time transport and the dynamic memory of data, it provides accuracy, reliable foundation to maintain for the antenna, simultaneously, it is poor to have overcome present antenna attitude parameter detection method real -time, and it is not convenient to operate, is unfavorable for realizing the network -based management's of data defect.

Description

A kind of antenna attitude detection device
Technical field
This utility model relates to communication equipment detection field, is specifically related to a kind of antenna attitude detection device.
Background technology
The azimuth of wireless base station antenna, the angle of pitch are engineering parameters important in mobile communication, and it determines nothing substantially The coverage of line signal.The azimuth of antenna for base station, the measurement of the angle of pitch and adjustment are depended on by telecom operators the most substantially at present By Traditional Man mode, still there is no the aid deflection of antenna, the angle of pitch can measured automatically, or some Method of adjustment can significantly alter the mounting means of existing antenna, brings the inconvenience of construction and the increase of cost.
Meanwhile, in existing antenna remote management technique, it is installed on the centralized Control main frame of machine room, is installed on antenna back Data sampling sensor, control main frame in machine room power taking, be connected with sensor by wired mode, it is achieved real-time Data Transmission And power taking, data are transmitted to controlling main frame by GPRS or short message mode.And then realization manages system with third party and carries out data Communication, reaches day lineman and joins the purpose of remote collection.And use the mode of GPRS or short message channel transmission to there is following defect: (1) because of the unstability being wirelessly transferred, packet can be caused to queue up and Loss, cause data back mistake;(2) use SIM, can take substantial amounts of SIM resource, will bring follow-up extra flow or short-message fee, increases maintenance cost;(3) sensing Wired connection between device and monitoring host computer, can bring the increase of difficulty of construction and cost.
Utility model content
The purpose of this utility model is to provide a kind of antenna attitude detection device, to solve in prior art manual measurement not Accurately, it is wirelessly transferred the unstable and problem of detection poor real.
For reaching above-mentioned purpose, this utility model be the technical scheme is that offer a kind of antenna attitude detection device, bag Include central processing unit and the global positioning system, gyroscope and the baroceptor that are connected with central processing unit;Central processing unit is also Being connected with acceleration transducer, geomagnetic sensor and temperature sensor, central processing unit passes through supply unit and is arranged on base Remote Radio Unit electrical connection on standing, supply unit includes 485 power conversion chips and communication module.
Preferably, gyroscope is connected with central processing unit by lightning protection device.
Preferably, 485 interfaces of communication module adjust interface to be connected with the electricity of Remote Radio Unit.
Preferably, antenna attitude detection device is arranged on antenna, and antenna is connected with pole by straight-bar and travel(l)ing rest.
In sum, this utility model has the advantage that
This utility model utilize central processing unit and global positioning system, geomagnetic sensor, gyroscope, acceleration transducer and Remote Radio Unit connects, it is possible to reaches the purpose of monitoring aerial work real-time, accurate, continuous ginseng information, and utilizes radio frequency to draw Remote unit accesses customer network, it is achieved the real-time Transmission of data and dynamic memory, provides accurately for antenna maintenance, depends on reliably According to;Meanwhile, overcoming existing antenna attitude parameter detection method poor real, it is the most convenient to operate, and is unfavorable for realizing the net of data The defect of networkization management.
Accompanying drawing explanation
Fig. 1 is the module map of this utility model antenna attitude detection device;
Fig. 2 is the scheme of installation of this utility model antenna attitude detection device;
Wherein, 1, pole;2, antenna;3, antenna attitude detection device;4, straight-bar;5, travel(l)ing rest.
Detailed description of the invention
Below in conjunction with the accompanying drawings detailed description of the invention of the present utility model is described in detail.
In an embodiment of the present utility model, as shown in Figure 1, it is provided that a kind of antenna attitude detection device, including in Central processor and the global positioning system, gyroscope and the baroceptor that are connected with central processing unit;Central processing unit also with add Velocity sensor, geomagnetic sensor and temperature sensor connect, and central processing unit passes through supply unit and is arranged on base station Remote Radio Unit electrical connection, supply unit includes 485 power conversion chips and communication module.This antenna attitude detection device By being connected the power supply obtaining base station with Remote Radio Unit, it is not necessary to external powering device.
Optimal enforcement example of the present utility model, as in figure 2 it is shown, gyroscope is connected with central processing unit by lightning protection device;Electricity Source apparatus includes 485 power conversion chips and communication module;485 interfaces of communication module adjust interface with the electric of Remote Radio Unit Connect;Antenna attitude detection device 3 is arranged on antenna 2, and antenna 2 is connected with pole 1 by straight-bar 4 and travel(l)ing rest 5.
Global positioning system obtains the location information data of current location, and gyroscope records current angular velocity, and will location Information data and angular velocity are to central processing unit, and baroceptor obtains the atmospheric pressure value of current location, and central authorities are given in output The atmospheric pressure value that processor, longitude and latitude data that central processing unit is gathered by global positioning system and baroceptor gather, calculates Go out longitude and latitude and the height above sea level of antenna for base station.
Acceleration transducer uses electric capacity miniature pendulum principle and terrestrial gravitation principle, when acceleration transducer tilts, Terrestrial gravitation acceleration can produce gravitational acceleration component on corresponding pendulum, and corresponding capacitance can change, by electricity Holding capacity component to amplify, filter, the acceleration component values of 3 axles of output is to central processing unit;Geomagnetic sensor processes with central authorities Device connect, the voltage of differential output can be converted magnetic fields to, by amplify, filtering, output 3 axles magnetic-field component value in Central processor;Temperature sensor is built in the digital acceleration sensor of acceleration transducer, be collection temperature induction unit, 12 Position A/D transducer, Programmable Temperature cross limit alarm and EBI in the digital temperature sensor of one, and temperature value is defeated Go out to central processing unit;Central processing unit acceleration component values, magnetic-field component value and temperature value to collecting carries out temperature and repaiies Just, non-liner revision and gradient correction, be calculated the angle of pitch and the azimuth of antenna of mobile communication base station.
Central processing unit is sent by communication module after the data of global positioning system He each sensor acquisition being computed To Remote Radio Unit (RRU), Remote Radio Unit (RRU) transfers out again, and background net management center (OMC) can be according to need Remote Radio Unit to be passed through (RRU) reads azimuth and the angle of pitch information of each antenna in cell, and exists as basic parameter Backstage stores, in order to use when carrying out the network planning and optimize.Additionally, background net management center can obtain certain position as required Put current antenna azimuth and angle of pitch information, judge antenna whether because the natural disaster weather such as wind, rain, snow or artificially because of Element causes a certain degree of change in location of antenna, in order to safeguard in time.
Although detailed description of the invention of the present utility model being described in detail in conjunction with accompanying drawing, but should not be construed as right The restriction of the protection domain of this patent.In the scope described by claims, those skilled in the art are without creative labor The dynamic various amendments that can make and deformation still belong to the protection domain of this patent.

Claims (4)

1. antenna attitude detection device, it is characterised in that: include central processing unit and defending of being connected with central processing unit Star position finder, gyroscope and baroceptor;Described central processing unit also with acceleration transducer, geomagnetic sensor and temperature Sensor connects, and described central processing unit is electrically connected with the Remote Radio Unit being arranged on base station by supply unit, described Supply unit includes 485 power conversion chips and communication module.
2. antenna attitude detection device as claimed in claim 1, it is characterised in that: described gyroscope is by lightning protection device and central authorities Processor connects.
3. antenna attitude detection device as claimed in claim 1, it is characterised in that: 485 interfaces of described communication module with penetrate Frequently the electricity of extension unit adjusts interface to connect.
4. antenna attitude detection device as claimed in claim 1, it is characterised in that: this antenna attitude detection device is arranged at sky On line, described antenna is connected with pole by straight-bar and travel(l)ing rest.
CN201620673335.4U 2016-06-30 2016-06-30 Antenna gesture detection device Expired - Fee Related CN205879191U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620673335.4U CN205879191U (en) 2016-06-30 2016-06-30 Antenna gesture detection device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620673335.4U CN205879191U (en) 2016-06-30 2016-06-30 Antenna gesture detection device

Publications (1)

Publication Number Publication Date
CN205879191U true CN205879191U (en) 2017-01-11

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Application Number Title Priority Date Filing Date
CN201620673335.4U Expired - Fee Related CN205879191U (en) 2016-06-30 2016-06-30 Antenna gesture detection device

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CN (1) CN205879191U (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108426559A (en) * 2018-02-27 2018-08-21 北京环境特性研究所 A kind of antenna attitude detection device and method
CN108592859A (en) * 2018-01-26 2018-09-28 东莞市日天通信科技有限公司 A kind of antenna for base station attitude measurement method based on global position system
WO2018219335A1 (en) * 2017-06-02 2018-12-06 华为技术有限公司 Mounting bracket for antenna information sensing unit, antenna information sensing unit, and antenna system
CN109586005A (en) * 2018-12-29 2019-04-05 京信通信技术(广州)有限公司 The mounting structure of antenna for base station and antenna attitude monitor
CN109612515A (en) * 2017-10-05 2019-04-12 罗德施瓦兹两合股份有限公司 The measuring system and method for temperatures research equipment under test about equipment under test
CN110301066A (en) * 2017-02-16 2019-10-01 凯瑟琳欧洲股份公司 Antenna, especially mobile phone antenna

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110301066A (en) * 2017-02-16 2019-10-01 凯瑟琳欧洲股份公司 Antenna, especially mobile phone antenna
US11375298B2 (en) 2017-02-16 2022-06-28 Telefonaktiebolaget Lm Ericsson (Publ) Antenna, in particular mobile phone antenna
WO2018219335A1 (en) * 2017-06-02 2018-12-06 华为技术有限公司 Mounting bracket for antenna information sensing unit, antenna information sensing unit, and antenna system
US11075437B2 (en) 2017-06-02 2021-07-27 Huawei Technologies Co., Ltd. Mounting bracket for antenna information sensing unit, antenna information sensing unit, and antenna system
CN109612515A (en) * 2017-10-05 2019-04-12 罗德施瓦兹两合股份有限公司 The measuring system and method for temperatures research equipment under test about equipment under test
CN109612515B (en) * 2017-10-05 2022-05-24 罗德施瓦兹两合股份有限公司 Measurement system and method for studying a device under test with regard to its temperature behavior
CN108592859A (en) * 2018-01-26 2018-09-28 东莞市日天通信科技有限公司 A kind of antenna for base station attitude measurement method based on global position system
CN108426559A (en) * 2018-02-27 2018-08-21 北京环境特性研究所 A kind of antenna attitude detection device and method
CN108426559B (en) * 2018-02-27 2020-07-24 北京环境特性研究所 Antenna attitude detection device and method
CN109586005A (en) * 2018-12-29 2019-04-05 京信通信技术(广州)有限公司 The mounting structure of antenna for base station and antenna attitude monitor
CN109586005B (en) * 2018-12-29 2023-09-29 京信通信技术(广州)有限公司 Mounting structure of base station antenna and antenna attitude monitor

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GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20170111

Termination date: 20180630

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