CN205643719U - Unmanned aerial vehicle GPS localization tracking system - Google Patents
Unmanned aerial vehicle GPS localization tracking system Download PDFInfo
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- CN205643719U CN205643719U CN201521126898.3U CN201521126898U CN205643719U CN 205643719 U CN205643719 U CN 205643719U CN 201521126898 U CN201521126898 U CN 201521126898U CN 205643719 U CN205643719 U CN 205643719U
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- unmanned plane
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Abstract
The utility model relates to an unmanned aerial vehicle GPS localization tracking system is applicable to the unmanned aerial vehicle data acquisition that takes photo by plane. It includes processing module, the GPS module, and the GSMGPRS module, power module, data storage module, the lamp module piece is instructed, satellite receiving antenna, GSMGPRS antenna, remote monitoring platform to the function button module. The utility model discloses simple structure, low cost can in time know unmanned aerial vehicle's state of flight and position when the unmanned aerial vehicle operation. When suspending appeared in unmanned aerial vehicle data transmission link, the tracker can passback data in real time arrive remote control console very much, showed its flight orbit, showed the current electric quantity condition, current voltage, height, star number, coordinate. Appear that the accident is crashed or when flying to lose at unmanned aerial vehicle, also can in time look for the reason that unmanned aerial vehicle went wrong or fly to lose the place.
Description
Technical field
This utility model relates to unmanned air vehicle technique field, especially a kind of unmanned plane GPS location tracking system.
Background technology
Along with developing rapidly of unmanned plane new and high technology, unmanned plane market scale is grown rapidly so that the innovation of unmanned plane
Application service is in numerous industries: industry, agricultural, forestry, fishery, mining industry, the operation flight of building industry and health care, speedily carries out rescue work and rescues
Calamity, meteorological detection, ocean detection, scientific experiments, remote sensing mapping, education and training, culture and sports, the aspect such as go sightseeing, income
Gangster is shallow.Country is also formed without the technical quality standard of authority to civilian unmanned plane at present, but according to " the People's Republic of China (PRC)
Radio frequency divides regulation " and China's frequency spectrum service condition, plan 840.5-845MHz, 1430-1444MHz and 2408-
2440MHz frequency range is used for push-button aircraft system.Ministry of Industry and Information specifies the use frequency range of push-button aircraft system, by one
Step promotes the development of unmanned plane industry, and the application of unmanned plane will be more extensive.Although the wireless communication distance of unmanned plane can
To reach 100 kilometers, but radio communication may be blocked thing or other interference signals, cause communication disruption, manipulation
Personnel can not understand state of flight and the position of unmanned plane in time.Installing unmanned plane tracker can be in unmanned plane radio communication
State of flight and the position of unmanned plane is understood in time after disconnected.
Utility model content
The deficiency existed for prior art, the purpose of this utility model is to provide a kind of unmanned plane GPS location tracking system
System, when interrupting occurs in Unmanned Aerial Vehicle Data transmission link, tracing system can show nothing to remote console by return data in real time
Man-machine flight path, shows currently without man-machine electric quantity consumption situation, current voltage, highly, star number, coordinate, make manipulation people
Member can understand state of flight and the position of unmanned plane in time.
To achieve these goals, this utility model is to realize by the following technical solutions:
A kind of unmanned plane GPS location tracking system, is characterized in that: include processing module, GPS module, GSM/GPRS module,
Power module, data storage module, function button module, indicating lamp module, satellite earth antenna, GSM/GPRS antenna, remotely
Monitor supervision platform；Processing module respectively with GPS module, GSM/ GPRS module, power module, data storage module, function button mould
Block, indicating lamp module connect, and GPS module and satellite earth antenna, GSM/GPRS module is connected with GSM/GPRS antenna, GSM/
GPRS module is connected with remote monitoring platform by GSM/GPRS antenna and GSM/GPRS network.
Described function button module is arranged on the shell of unmanned plane tracker.
Described power module is directly connected to the electrokinetic cell of unmanned plane.
Described GPS module is GPS module, connects satellite reception data by satellite earth antenna.
Described indicating lamp module carries out the bright light instruction of different colours according to the work ruuning situation of tracker.
The coordinate information that described data storage module storage GPS module receives.
Described GSM/GPRS module comprises the global system for mobile communications of a user identification module card and general
Packet Wireless Services Module.
The described monitor supervision platform that remotely controls is mobile phone A PP or other platforms.
Advantage of the present utility model:
This utility model simple in construction, with low cost, the flight shape of unmanned plane can be understood in time when unmanned plane operation
State and position.Especially when interrupting occurs in Unmanned Aerial Vehicle Data transmission link, tracker can control to long-range by return data in real time
The flight path of platform display unmanned plane, shows currently without man-machine electric quantity consumption situation, current voltage, highly, star number, coordinate.
Occur that accident is crashed or when flying to lose at unmanned plane, it is also possible to find reason that unmanned plane goes wrong in time or fly to lose ground
Point.
Accompanying drawing explanation
Fig. 1 is structure connection diagram of the present utility model.
Fig. 2 and Fig. 3 is Welding Structure schematic diagram of the present utility model.
In figure shown in label: processing module 1, GPS module 2, GSM/GPRS module 3, power module 4, data storage module
5, function button module 6, indicating lamp module 7, satellite earth antenna 8, GSM/GPRS antenna 9, remote monitoring platform 10.
Detailed description of the invention
For a more detailed description to this utility model below in conjunction with accompanying drawing embodiment.
A kind of can passback in real time shows currently without man-machine voltage, highly, star number, and the unmanned plane GPS of coordinate information chases after
The Welding Structure of track system, is made up of the mainboard sheet of a generally rectangle, and mainboard sheet front is provided with processing module 1, GPS mould
Block 2, GSM/GPRS module 3, power module 4, indicating lamp module 7, GSM/GPRS antenna 9, wherein in the left side in mainboard sheet front
GPS module 2 is installed in portion, and power module 4 is installed in its bottom, left side；Its middle upper portion installation process module 1；On the right of it, top is installed
Be indicating lamp module 7, on the right of it middle part install GSM/GPRS module 3, on the right of it bottom install be GSM/GPRS antenna 9.
The mainboard sheet back side is provided with function button module 6, satellite earth antenna 8, data storage module 5, the wherein left side, the mainboard sheet back side
What top was installed is satellite earth antenna 8；What the middle part on the right of it was installed is data storage module 5；On the right of it, bottom is installed
It it is function button module 6.
Processing module 1 is pressed with GPS module 2, GSM/ GPRS module 3, power module 4, data storage module 5, function respectively
Key module 6, indicating lamp module 7 connect, GPS module 2 and satellite earth antenna 8, GSM/GPRS module 3 and GSM/GPRS antenna 9
Connecting, GSM/GPRS module 3 is connected with remote monitoring platform 10 by GSM/GPRS antenna 9 and GSM/GPRS network.
Described function button module 6 is positioned on the shell of unmanned plane tracker, can arrange nothing by operating this module
The startup of man-machine tracker, is realized location, status data retransmission function by GPS module 2.
Described power module 4 is to use the electrokinetic cell voltage range being directly connected to unmanned plane can reach 6V to 55V
Power taking, powers to modules in whole unmanned plane tracker.
Described GPS module 2 is GPS module, and connecting satellite reception data by satellite earth antenna 8 can
Obtain the location information of unmanned plane tracker.
Described indicating lamp module 7 carries out the bright light instruction of different colours according to the work ruuning situation of tracker.
Described data storage module 5 mainly stores the coordinate information that GPS module receives, and is also to process unmanned plane to be in partially
Distant mountain district etc. does not has under the extreme case of GSM/GPRS signal, and the flight path sum that after having signal, passback is lost at once it is believed that
Breath.
Described processing module 1 processes positional information and the unmanned plane during flying status information that GPS module 2 receives, and passes through
GSM/GPRS module 3 return data is to remote monitoring platform, and GSM/GPRS module 3 comprises a user identification module card
Global system for mobile communications and GPRS module.
Remotely controlling monitor supervision platform can be mobile phone A PP or other platforms.
The specific embodiments of described passback unmanned plane during flying status information (voltage, highly, star number, coordinate information):
Voltage is that processing module 1 is obtained by 2 divider resistance series-connected cell output head anodes, and then processing module 1 is led to
Cross GSM/GPRS module 3 return data to remote monitoring platform.
Unmanned plane height is GPS module 2, and to connect GPS, GLONASS, the Big Dipper, Galileo tetra-by satellite earth antenna 8 big
The satellite of satellite navigation system obtains elevation information, and then processing module 1 is supervised to long-range by GSM/GPRS module 3 return data
Control platform.
Unmanned plane star number is GPS module 2, and to connect GPS, GLONASS, the Big Dipper, Galileo tetra-by satellite earth antenna 8 big
The satellite of satellite navigation system obtains elevation information, and then processing module 1 is supervised to long-range by GSM/GPRS module 3 return data
Control platform.
Unmanned plane coordinate information is that GPS module 2 connects GPS, GLONASS, the Big Dipper, Galileo by satellite earth antenna 8
The satellite of four large satellite navigation system obtains elevation information, and then processing module 1 passes through GSM/GPRS module 3 return data to remote
Range monitoring platform.
The technology that this utility model relates generally to includes electronic information technology, PCB circuit engineering, communication technology.Mainly
Production procedure: electronic chip type selecting circuit design pcb board makes welding circuit test circuit and is installed to unmanned
Machine test test is by completing.
The main electronic chip used has, and processes chip ATMEGA328P, GSM/GPRS module SIM900, GPS module
M8N, power supply chip MP4560, LM1117, conventional resistance capacitance.
Claims (8)
1. a unmanned plane GPS location tracking system, is characterized in that: include processing module (1), GPS module (2), GSM/GPRS
Module (3), power module (4), data storage module (5), function button module (6), indicating lamp module (7), satellite reception sky
Line (8), GSM/GPRS antenna (9), remote monitoring platform (10)；Processing module (1) respectively with GPS module (2), GSM/ GPRS
Module, power module (4), data storage module (5), function button module (6), indicating lamp module (7) connect, GPS module (2)
With satellite earth antenna (8), GSM/GPRS module is connected with GSM/GPRS antenna (9), and GSM/GPRS module (3) passes through GSM/
GPRS antenna (9) and GSM/GPRS network are connected with remote monitoring platform (10).
Unmanned plane GPS location tracking system the most according to claim 1, is characterized in that: described function button module (6)
It is arranged on the shell of unmanned plane tracker.
Unmanned plane GPS location tracking system the most according to claim 1, is characterized in that: described power module (4) is direct
Connect the electrokinetic cell of unmanned plane.
Unmanned plane GPS location tracking system the most according to claim 1, is characterized in that: described GPS module (2) is complete
Ball positioning system modules, connects satellite reception data by satellite earth antenna (8).
Unmanned plane GPS location tracking system the most according to claim 1, is characterized in that: described indicating lamp module (7) root
The bright light instruction of different colours is carried out according to the work ruuning situation of tracker.
Unmanned plane GPS location tracking system the most according to claim 1, is characterized in that: described data storage module (5)
The coordinate information that storage GPS module (2) receives.
Unmanned plane GPS location tracking system the most according to claim 1, is characterized in that: described GSM/GPRS module bag
Global system for mobile communications and GPRS module containing a user identification module card.
Unmanned plane GPS location tracking system the most according to claim 1, is characterized in that: described remote monitoring platform
(10) it is mobile phone A PP.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521126898.3U CN205643719U (en) | 2015-12-31 | 2015-12-31 | Unmanned aerial vehicle GPS localization tracking system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521126898.3U CN205643719U (en) | 2015-12-31 | 2015-12-31 | Unmanned aerial vehicle GPS localization tracking system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205643719U true CN205643719U (en) | 2016-10-12 |
Family
ID=57077775
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201521126898.3U Active CN205643719U (en) | 2015-12-31 | 2015-12-31 | Unmanned aerial vehicle GPS localization tracking system |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107067617A (en) * | 2017-05-16 | 2017-08-18 | 京东方科技集团股份有限公司 | A kind of method for safety monitoring and safety monitoring system based on unmanned plane |
| WO2018072155A1 (en) * | 2016-10-19 | 2018-04-26 | 深圳市大疆创新科技有限公司 | Wearable device for controlling unmanned aerial vehicle and unmanned aerial vehicle system |
| CN109270561A (en) * | 2017-07-18 | 2019-01-25 | 深圳市道通智能航空技术有限公司 | Unmanned machine positioning device, ground control system, positioning system and unmanned plane |
-
2015
- 2015-12-31 CN CN201521126898.3U patent/CN205643719U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018072155A1 (en) * | 2016-10-19 | 2018-04-26 | 深圳市大疆创新科技有限公司 | Wearable device for controlling unmanned aerial vehicle and unmanned aerial vehicle system |
| CN107067617A (en) * | 2017-05-16 | 2017-08-18 | 京东方科技集团股份有限公司 | A kind of method for safety monitoring and safety monitoring system based on unmanned plane |
| CN109270561A (en) * | 2017-07-18 | 2019-01-25 | 深圳市道通智能航空技术有限公司 | Unmanned machine positioning device, ground control system, positioning system and unmanned plane |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: Unmanned aerial vehicle GPS localization tracking system Effective date of registration: 20190724 Granted publication date: 20161012 Pledgee: Nanning United Innovation Venture Capital Co., Ltd. Pledgor: NANNING HUISHI TECHNOLOGY CO., LTD. Registration number: 2019450000032 |
|
| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20200723 Granted publication date: 20161012 Pledgee: Nanning United Innovation Venture Capital Co.,Ltd. Pledgor: NANNING HUISHI TECHNOLOGY Co.,Ltd. Registration number: 2019450000032 |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A GPS positioning and tracking system for UAV Effective date of registration: 20200804 Granted publication date: 20161012 Pledgee: Nanning United Innovation Venture Capital Co.,Ltd. Pledgor: NANNING HUISHI TECHNOLOGY Co.,Ltd. Registration number: Y2020450000030 |
|
| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20210818 Granted publication date: 20161012 Pledgee: Nanning United Innovation Venture Capital Co.,Ltd. Pledgor: NANNING HUISHI TECHNOLOGY Co.,Ltd. Registration number: Y2020450000030 |