CN206243480U - A kind of integrated form measurement apparatus based on unmanned plane - Google Patents
A kind of integrated form measurement apparatus based on unmanned plane Download PDFInfo
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- CN206243480U CN206243480U CN201621344666.XU CN201621344666U CN206243480U CN 206243480 U CN206243480 U CN 206243480U CN 201621344666 U CN201621344666 U CN 201621344666U CN 206243480 U CN206243480 U CN 206243480U
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- control system
- unmanned plane
- flight control
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- data
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Abstract
The utility model discloses a kind of integrated form measurement apparatus based on unmanned plane, opened up exclusively for the add-on module for carrying DATA REASONING device service by flight control system of increasing income, allow that add-on module gets the information of other fixing equipments in flight control system by routine call；And then be fused in the information of carrying equipment.It is corresponding, special passage can be set on ground surface end remote control to control the working condition of add-on module.The add-on module can connect flight control system and carrying DATA REASONING equipment by data wire, it is also possible to directly increase built-in subroutine in flight control system.The utility model realizes the shared of measuring instrument using the instrument that unmanned vehicle is carried, and reduces load-carrying, improves the utilization rate of resource so that unmanned plane more facilitates what DATA REASONING field used.
Description
Technical field
The utility model is related to unmanned plane applied technical field, and in particular to a kind of integrated form measurement dress based on unmanned plane
Put.
Background technology
At present, unmanned plane because its handling, reliability, the advantage of duties and be used widely.Taking photo by plane,
The fields such as plant protection are ripe, and survey and draw, monitor, industry quickly grows field of express delivery in recent years, especially sampling it is difficult, obtain number
Received much concern according to difficult meteorology, ocean, environmental area.
Characterizing atmospheric physics state, every key element of physical phenomenon mainly has:Temperature, air pressure, wind, humidity, cloud, precipitation with
And various weather phenomena.In addition, each key element for characterizing ocean also has water Inversion phenomenon etc.；The key element for characterizing haze is mainly
PM2.5.The data that we obtain at present are substantially from sampling mechanisms such as weather bureau, ocean office, environment offices.They can provide
Large range of factor data, but these data are generally the average data in certain region.If obtaining the data in certain place,
Can only be by the measuring instrument of hand-held, but this method can only measure ground, cannot be measured for high-altitude data.
Attempted on miniature DATA REASONING instrument integration to unmanned plane now with many scientific research personnel, carried out by unmanned plane
Vertical and remote DATA REASONING；But their integrated unmanned plane that typically uses is used as power supply and carrying platform, this collection
It is exactly that each measuring instrument is required for a d GPS locating module into the influence that mode is brought, so just can know that surveyed data
Be when and where；And in order to obtain these data in real time, measuring instrument needs to carry data transmission device, this is again and unmanned plane
The number for carrying is passed and repeated.
Utility model content
For above-mentioned the deficiencies in the prior art, the utility model provides a kind of integrated form measurement apparatus based on unmanned plane,
Can solve the problem that existing UAV system DATA REASONING instrument needs to carry the problem of the devices such as multiple GPS module sums biographies.
To achieve the above object, the utility model is adopted the following technical scheme that：
A kind of integrated form measurement apparatus based on unmanned plane, including the DATA REASONING carried on unmanned plane, and unmanned plane
Device and add-on module；The unmanned plane includes that flight control system, PMU, GPS, number are passed；The power management
Unit connects GPS, flight control system, add-on module by data wire respectively；The PMU is used to give its company
The equipment for connecing is powered, and plays switching effect so that can mutually be accessed between connected equipment；The flight control system
System is passed by data wire connection number, passes transmission information to number, and receive the control instruction that number passes transmission；
The add-on module includes microprocessing unit, decoding unit；Microprocessing unit connects DATA REASONING by data wire
Device, the weather information that data measurement unit will be collected is sent to microprocessing unit；Microprocessing unit connects decoding unit,
Acquired weather information is sent to decoding unit；Decoding unit is decoded to acquired weather information, is complied with
The requirement of flight control system；Acted on by the switching of PMU and send to flight control decoded weather information
System, flight control system sends that information to count biography, and number biography sends it to ground receiving wastewater facility.
Further, the data measurement unit is mobile weather station, PM2.5 sensors.
The beneficial effects of the utility model are：During the information such as UAV flight's data measurement unit measurement meteorological element, have
The effect device such as make use of the GPS sums that unmanned plane carries to pass, it is not necessary to which repetition installs instruments, and improves working platform efficiency；Subtract
Few unmanned plane load-carrying, improves the availability of unmanned plane.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model；
Fig. 2 is signal flow graph of the present utility model；
Label in figure：1st, PMU；2nd, flight control system；3rd, number is passed；4、GPS；5th, data measurement unit；6、
Microprocessing unit；7th, decoding unit.
Specific embodiment
In order that the purpose of utility model, technical scheme and advantage are more clearly, it is right below in conjunction with accompanying drawing and example
The utility model is further described.It should be appreciated that specific embodiment described herein is only used to explain the utility model,
It is not used to limit the utility model.
As shown in figure 1, PMU 1 connects GPS4, flight control system 2, add-on module by data wire respectively
Connection, number passes 3 (wireless digital broadcasting stations) and connects flight control system 2 by steering wheel line, and data measurement unit 5 is connected by data wire
Connect add-on module.Add-on module includes microprocessing unit 6, decoding unit 7, the connection decoding unit 7 of microprocessing unit 6.Microprocessor
Unit 6 connects data measurement unit 5, the connection PMU 1 of decoding unit 7.PMU 1 is used to being connected thereto
Equipment power, and play switching effect so that can mutually be accessed between connected equipment.
As shown in Fig. 2 surveyed weather information is sent to microprocessing unit 6 by data measurement unit 5, microprocessing unit 6 will
Weather information is sent to decoding unit 7, and decoding unit 7 decodes weather information, complies with the communication protocols of flight control system 2
View requirement, is then acted on by the switching of PMU 1, and decoded weather information is sent into flight control system 2.
The unmanned plane positional information that flight control system 2 gathers weather information and GPS4 passes 3 and is sent to unmanned aerial vehicle station by number.
The control instruction that unmanned aerial vehicle station sends passes 3 and is sent to flight control system 2 by number.
Flight control system 2 can move weather station or PM2.5 sensors, and mobile weather station can use WX200 types
Number AIRMAR movement weather station.PM2.5 sensors can use [SDS011] high-precision laser PM2.5 sensor assemblies.
By above connect setting, it is possible to achieve gps data, PMU and flight control system these three modules
Data sharing, the data for being obtained can be not only superimposed upon on the relevant parameter of data measurement unit, can also borrow nobody
The number that machine is carried passes device and passes data back ground surface end, and eliminating data measurement unit needs to carry the fiber crops of GPS module sum biography
It is tired, load-carrying is reduced, improve the overall application efficiency of unmanned plane.
Above-described all parts are existing commercial module, and those skilled in the art can be by corresponding
Means are acquired, for example, flight control system may be selected PIX flies control, number biography may be selected remote powerful 900M numbers and pass.
It is annexation and unmanned plane Deep integrating measuring instrument mode between modules that the utility model is claimed.
Claims (2)
1. a kind of integrated form measurement apparatus based on unmanned plane, it is characterised in that including what is carried on unmanned plane, and unmanned plane
Data measurement unit and add-on module；The unmanned plane includes that flight control system, PMU, GPS, number are passed；It is described
PMU connects GPS, flight control system, add-on module by data wire respectively；The PMU is used to
Powered to connected equipment, and play switching effect so that can mutually accessed between connected equipment；It is described to fly
Row control system connects number and passes by data wire, passes transmission information to number, and receive the control instruction that number biography sends；
The add-on module includes microprocessing unit, decoding unit；Microprocessing unit connects data measurement unit by data wire,
The weather information that data measurement unit will be collected is sent to microprocessing unit；Microprocessing unit connects decoding unit, by institute
The weather information of acquisition is sent to decoding unit；Decoding unit is decoded to acquired weather information, complies with flight
The requirement of control system；Acted on by the switching of PMU and send to flight control system decoded weather information
System, flight control system sends that information to count biography, and number biography sends it to ground receiving wastewater facility.
2. a kind of integrated form measurement apparatus based on unmanned plane according to claim 1, it is characterised in that the data are surveyed
Amount device is mobile weather station, PM2.5 sensors.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621344666.XU CN206243480U (en) | 2016-12-09 | 2016-12-09 | A kind of integrated form measurement apparatus based on unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621344666.XU CN206243480U (en) | 2016-12-09 | 2016-12-09 | A kind of integrated form measurement apparatus based on unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206243480U true CN206243480U (en) | 2017-06-13 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621344666.XU Expired - Fee Related CN206243480U (en) | 2016-12-09 | 2016-12-09 | A kind of integrated form measurement apparatus based on unmanned plane |
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| CN (1) | CN206243480U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112093065A (en) * | 2020-09-30 | 2020-12-18 | 浙江安防职业技术学院 | Surveying and mapping scanning equipment based on unmanned aerial vehicle technology |
-
2016
- 2016-12-09 CN CN201621344666.XU patent/CN206243480U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112093065A (en) * | 2020-09-30 | 2020-12-18 | 浙江安防职业技术学院 | Surveying and mapping scanning equipment based on unmanned aerial vehicle technology |
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170613 Termination date: 20181209 |
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| CF01 | Termination of patent right due to non-payment of annual fee |