CN205809700U - Air quality detection system based on unmanned plane - Google Patents
Air quality detection system based on unmanned plane Download PDFInfo
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- CN205809700U CN205809700U CN201620742020.0U CN201620742020U CN205809700U CN 205809700 U CN205809700 U CN 205809700U CN 201620742020 U CN201620742020 U CN 201620742020U CN 205809700 U CN205809700 U CN 205809700U
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Abstract
The quality detecting system based on unmanned plane that this utility model provides, arranges ground surface end and aircraft end, user reach to specify position to carry out data acquisition at ground remote control aircraft end, and data are transmitted back to ground surface end, breach the restriction that detection range is little；The data gathered include that air index, humiture and atmospheric pressure, above-mentioned data have comprehensive and representative, can improve the accuracy of air quality assessment；When using aircraft detection to control quality, the attitude of real-time sense aircraft, height and location information, position adjustment can be carried out in real time, the position that user sets can be precisely positioned to, be accurately positioned collecting location, improve the representativeness of data further.
Description
Technical field
This utility model relates to intelligent air quality testing field, particularly relates to Detection of Air Quality based on unmanned plane
System.
Background technology
Reason and the phenomenon of air pollution are the most complex, pollutant levels can in time, place produce change, for administer
Atmospheric pollution, needs fixed point, regularly, continuously, dynamically gathers data in air and be analyzed, the mode of existing Detection of Air Quality
Being typically to set up several monitoring stations, detect in each monitoring station, its shortcoming is: owing to detection position is fixed, cause inspection
Survey is limited in scope；Air pollutants can produce diffusion in various degree, detecting position along with the change of other environmental factors in air
Put fixing, cause the data obtained not possess representativeness so that the later stage produces deviation to air quality assessment；Set up multiple can not
Gather the monitoring station of data flexibly, and the data collected also need manually to fetch, and cause expending a large amount of manpower and materials.
Utility model content
This utility model provides air quality detection system based on unmanned plane, solves to exist in existing Detection of Air Quality
Detection range little, obtain data influence air quality assessment problem.
This utility model solves the problems referred to above by the following technical programs:
Air quality detection system based on unmanned plane, is made up of ground surface end and aircraft end, and described ground surface end is by ground
RCU and data receipt unit composition, described flight end is made up of flying vehicles control unit and data acquisition transmitter unit；
Described flying vehicles control unit includes remote control reception module, aircraft side controller module and motor；Described data acquisition is launched
Unit includes air detection module, humiture collection module, atmospheric pressure acquisition module, collection terminal controller module and wireless transmit
Module；Described ground remote control unit sends a command to remote control reception module, and aircraft side controller module is according to described instruction control
Motor processed, makes aircraft by instruction execution action；Air detection module is Real-time Collection under the control of collection terminal controller module
Air index, humiture collection module is Real-time Collection humiture under the control of collection terminal controller module, and atmospheric pressure gathers mould
Block is Real-time Collection atmospheric pressure under the control of collection terminal controller module；Above-mentioned air index, humiture and atmospheric pressure data warp
Wireless transmitter module sends to data receipt unit.
Further, described flying vehicles control unit farther includes Posture acquisition module, and described Posture acquisition module is adopted
The attitude of collection aircraft, input is to aircraft side controller module.
Further, described flying vehicles control unit farther includes height acquisition module, and described height acquisition module is adopted
The height of collection aircraft, input is to aircraft side controller module.
Further, described flying vehicles control unit farther includes GPS navigation module, and described GPS navigation module gathers
The positional information of aircraft, input is to aircraft side controller module.
Further, described data receipt unit is made up of wireless receiving module and receiving terminal controller module；Described nothing
Line receiver module receives the information of data acquisition transmitter unit, inputs to receiving terminal controller module；Described receiving terminal controls
Device module enters data into external management terminal.
Compared with prior art, have a characteristic that
1, ground surface end and aircraft end are set, user reach to specify position to carry out data acquisition at ground remote control aircraft end
Collection, and data are transmitted back to ground surface end, breach the restriction that detection range is little；The data gathered include air index, humiture
And atmospheric pressure, above-mentioned data have comprehensive and representative, can improve the accuracy of air quality assessment；
When 2, using aircraft detection to control quality, the attitude of real-time sense aircraft, height and location information, can be real-time
Carry out position adjustment, the position that user sets can be precisely positioned to, be accurately positioned collecting location, improve the generation of data further
Table.
Accompanying drawing explanation
Fig. 1 is theory diagram of the present utility model.
Detailed description of the invention
Below in conjunction with embodiment, the utility model is described in further detail, but this utility model is not limited to these enforcement
Example.
Air quality detection system based on unmanned plane, is made up of ground surface end and aircraft end, and ground surface end is by ground remote control
Unit and data receipt unit composition, flight end is made up of flying vehicles control unit and data acquisition transmitter unit；Aircraft control
Unit processed includes remote control reception module, aircraft side controller module and motor；Data acquisition transmitter unit includes air detection
Module, humiture collection module, atmospheric pressure acquisition module, collection terminal controller module and wireless transmitter module, can be according to demand
Increase the detection module of other data further；Ground remote control unit sends a command to remote control reception module, and aircraft end controls
Device module controls motor rotation according to instruction, makes aircraft by instruction execution action；Air detection module is at collection terminal controller
Real-time Collection air index under the control of module, humiture collection module is Real-time Collection under the control of collection terminal controller module
Humiture, atmospheric pressure acquisition module is Real-time Collection atmospheric pressure under the control of collection terminal controller module；Above-mentioned air index, temperature
Humidity and atmospheric pressure data send to data receipt unit through wireless transmitter module.
Ground surface end is used for sending instruction and receiving data, and at aircraft end, aircraft is in the control of flying vehicles control unit
Under, carry data acquisition transmitter unit and gather data, and by data back to data receipt unit.Ground remote control unit is to flight
Device end sends instruction, for controlling the flight position of aircraft, it is simple to data acquisition transmitter unit in corresponding station acquisition, send out
Penetrate data.Remote control reception module is 2.4GHz wireless module, after this module receives the instruction of ground remote control unit, will instruct defeated
Enter to aircraft side controller module, aircraft side controller module control the operation of motor so that aircraft flight is to phase
The position answered.
Air detection module includes that PM2.5 gathers submodule and PM10 gathers submodule, and two submodules are in collection terminal control
Gather PM2.5 and PM10 concentration under the control of device module processed respectively, and enter data into collection terminal controller module.PM2.5
The particulate matter of 2.5 microns it is less than or equal to, for lung particulate matter can be entered for diameter in air.PM2.5 is to air quality and visibility
Etc. there being important impact, its particle diameter is little, rich in substantial amounts of poisonous and harmful substances, and time of staying length in an atmosphere, conveying away from
Away from from, thus the impact on health and atmosphere quality is bigger, and therefore, this utility model arranges PM2.5 and gathers submodule
Block.PM10 is the pellet that diameter is less than or equal to 10 microns, and long-term accumulated can cause respiratory system disease, as tachypnea,
Cough, induction asthma, chronic bronchitis, chronic pneumonia etc., therefore, this utility model arranges PM10 and gathers submodule.
Humiture collection module is for gathering the humiture of aircraft position, and humiture is the finger of assessment air quality
One of mark；Atmospheric pressure acquisition module is for gathering the atmospheric value of aircraft position, under different atmospheric value, humiture,
The regime values scope of PM2.5, PM10 is different, and the data therefore gathering atmospheric pressure are used as reference.
Aircraft side controller module and collection terminal controller module are STC12C5A60S2, are respectively used to use existing
Technology realizes data and processes, instructs transmission and data transmission.Wireless transmitter module is nRF2401 monolithic radio frequency transceiving chip, work
Making in 2.4～2.5GHz ISM bands, energy consumption is the lowest, and during with the power emission of-5dBm, operating current only has 10.5mA, connects
Time receiving operating current only has 18mA, multiple low-power working mode, energy-conservation, convenience, is highly suitable for this utility model.
Flying vehicles control unit farther includes Posture acquisition module, and Posture acquisition module gathers the attitude of aircraft, defeated
Enter to aircraft side controller module.Flying vehicles control unit farther includes height acquisition module, height acquisition module collection
The height of aircraft, input is to aircraft side controller module.Flying vehicles control unit farther includes GPS navigation module, GPS
Navigation module gathers the positional information of aircraft, and input is to aircraft side controller module.
The purpose arranging Posture acquisition module, height acquisition module and GPS navigation module is the reality in order to monitor aircraft
In-position, border, and adjusted motor in real time by aircraft side controller module so that the position being actually reached and the finger received
The position that order requires is consistent, it is simple to confirm the accuracy of position, above-mentioned relate to position gap comparison, produce and adjust position
Control instruction, is prior art.Attitude, height and the information input of GPS location control to flight side controller module, flight end
Device module uses existing gesture stability algorithm, Altitude control algorithm to carry out attitude and the control of height, and uses prior art
Carry out flow-disturbing between the arrangement of aircraft center and slurry to process.
Data receipt unit is made up of wireless receiving module and receiving terminal controller module；Wireless receiving module receives data
Gather the information of transmitter unit, input to receiving terminal controller module；Receiving terminal controller module enters data into outside
Management terminal.Wireless receiving module is identical with wireless transmitter module, is nRF2401 monolithic radio frequency transceiving chip, wireless receiving
Module works in reception state, and wireless transmitter module works in emission state.
In this utility model, ground surface end and aircraft end wireless connections.Ground remote control unit and remote control reception module without
Line connects；The outfan of remote control reception module is connected with aircraft side controller module；The control end of motor and aircraft end control
Device module processed is connected；Posture acquisition module is connected with aircraft side controller module respectively with the outfan of height acquisition module；
GPS navigation module is connected with aircraft side controller module；Air detection module, humiture collection module and atmospheric pressure gather mould
Block is connected with collection terminal controller module respectively；The input of wireless transmitter module is connected with collection terminal controller module；Wireless
Transmitter module is wireless with wireless receiving module to be connected；Wireless receiving module is connected with receiving terminal controller module；Receiving terminal controls
Device module is connected with external management terminal.
Work process of the present utility model is: in the input instruction of ground remote control unit, after this instruction transmission to aircraft end,
Remote control reception module receives this instruction, and inputs instruction to aircraft side controller module, by aircraft side controller module
Controlling motor to run so that aircraft flight is to specifying position, meanwhile, gather attitude, altitude information, these data position with GPS
Information is transmitted together to aircraft side controller module, it is simple to aircraft side controller module is as data basis, by control
Motor processed adjusts attitude and the height of aircraft；Aircraft flight postpones to specific bit, and data acquisition transmitter unit starts to gather
Air index, humiture and atmospheric pressure data, these data are sent to collection terminal controller module, and by wireless transmit mould
Block sends to data receipt unit, after data receipt unit receives data, enters data into external management terminal.
Claims (5)
1. air quality detection system based on unmanned plane, is made up of ground surface end and aircraft end, it is characterised in that:
Described ground surface end is made up of ground remote control unit and data receipt unit, and described flight end is by flying vehicles control unit sum
According to gathering transmitter unit composition；
Described flying vehicles control unit includes remote control reception module, aircraft side controller module and motor；Described data acquisition
Transmitter unit includes air detection module, humiture collection module, atmospheric pressure acquisition module, collection terminal controller module and wireless
Transmitter module；
Described ground remote control unit sends a command to remote control reception module, and aircraft side controller module controls according to described instruction
Motor, makes aircraft by instruction execution action；Air detection module Real-time Collection under the control of collection terminal controller module is empty
Gas index, humiture collection module is Real-time Collection humiture under the control of collection terminal controller module, atmospheric pressure acquisition module
Real-time Collection atmospheric pressure under the control of collection terminal controller module；Above-mentioned air index, humiture and atmospheric pressure data are through nothing
Line transmitter module sends to data receipt unit.
Air quality detection system based on unmanned plane the most according to claim 1, it is characterised in that:
Described flying vehicles control unit farther includes Posture acquisition module, and described Posture acquisition module gathers the appearance of aircraft
State, input is to aircraft side controller module.
Air quality detection system based on unmanned plane the most according to claim 1, it is characterised in that:
Described flying vehicles control unit farther includes height acquisition module, and described height acquisition module gathers the height of aircraft
Degree, input is to aircraft side controller module.
Air quality detection system based on unmanned plane the most according to claim 1, it is characterised in that:
Described flying vehicles control unit farther includes GPS navigation module, and described GPS navigation module gathers the position letter of aircraft
Breath, input is to aircraft side controller module.
Air quality detection system based on unmanned plane the most according to claim 1, it is characterised in that:
Described data receipt unit is made up of wireless receiving module and receiving terminal controller module；Described wireless receiving module receives
The information of data acquisition transmitter unit, inputs to receiving terminal controller module；Described receiving terminal controller module is defeated by data
Enter to external management terminal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620742020.0U CN205809700U (en) | 2016-07-14 | 2016-07-14 | Air quality detection system based on unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620742020.0U CN205809700U (en) | 2016-07-14 | 2016-07-14 | Air quality detection system based on unmanned plane |
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| CN205809700U true CN205809700U (en) | 2016-12-14 |
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| CN201620742020.0U Expired - Fee Related CN205809700U (en) | 2016-07-14 | 2016-07-14 | Air quality detection system based on unmanned plane |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107121162A (en) * | 2017-04-28 | 2017-09-01 | 广东容祺智能科技有限公司 | A kind of intelligent air quality monitoring UAS |
| CN107228920A (en) * | 2017-05-26 | 2017-10-03 | 成都润泰茂成科技有限公司 | A kind of air-quality monitoring system for being capable of detecting when pollution type |
| CN107367581A (en) * | 2017-07-24 | 2017-11-21 | 合肥星袖机械科技有限公司 | A kind of environment monitoring equipment based on unmanned plane |
| CN107516451A (en) * | 2017-10-08 | 2017-12-26 | 景遥（上海）信息技术有限公司 | Fixed-wing UAV Intelligent flight training system |
| CN108254493A (en) * | 2016-12-29 | 2018-07-06 | 北京卓翼智能科技有限公司 | Atmosphere environment supervision method and system |
-
2016
- 2016-07-14 CN CN201620742020.0U patent/CN205809700U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108254493A (en) * | 2016-12-29 | 2018-07-06 | 北京卓翼智能科技有限公司 | Atmosphere environment supervision method and system |
| CN107121162A (en) * | 2017-04-28 | 2017-09-01 | 广东容祺智能科技有限公司 | A kind of intelligent air quality monitoring UAS |
| CN107228920A (en) * | 2017-05-26 | 2017-10-03 | 成都润泰茂成科技有限公司 | A kind of air-quality monitoring system for being capable of detecting when pollution type |
| CN107367581A (en) * | 2017-07-24 | 2017-11-21 | 合肥星袖机械科技有限公司 | A kind of environment monitoring equipment based on unmanned plane |
| CN107516451A (en) * | 2017-10-08 | 2017-12-26 | 景遥（上海）信息技术有限公司 | Fixed-wing UAV Intelligent flight training system |
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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: 20161214 Termination date: 20170714 |