CN207703821U - Unmanned plane Atmosphere Environment Monitoring System Bases based on big data - Google Patents
Unmanned plane Atmosphere Environment Monitoring System Bases based on big data Download PDFInfo
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- CN207703821U CN207703821U CN201820056430.9U CN201820056430U CN207703821U CN 207703821 U CN207703821 U CN 207703821U CN 201820056430 U CN201820056430 U CN 201820056430U CN 207703821 U CN207703821 U CN 207703821U
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Abstract
A kind of unmanned plane Atmosphere Environment Monitoring System Bases based on big data, it includes UAV system detection device, the UAV system detection device includes shell and the electric device that is arranged in shell, the shell of detection device is at least divided into two chambers, and gas content sensor and PM sensor of dust concentration are separately positioned in two chambers.The utility model is arranged by the sensor of PM dust and for measuring the sensor of other gas contents in different chambers, substantially increases measurement accuracy.
Description
Technical field
The utility model provides a kind of unmanned plane atmospheric environmental monitoring system based on big data, belongs to measuring technique neck
Domain.
Background technology
In recent years, with the raising of the development of social economy and industrial automatization, the operating of various mechanical equipments is public
Road motor vehicle is increasingly incremental, and all the time all in burns gasoline or coal, a large amount of nitrogen oxides, vulcanization are discharged to air
Object, coal dust cigarette.Various weather, haze PM2.5, CO, SO2、NO2、O3The pollutants such as gas make the trip of people, health
At very big puzzlement, environmental improvement is very urgent.
However we can also be clearly seen that, prediction and actual environment made by point ground detection data are controlled according to state
Still there is larger gap in the development of pollution situation, in addition, being spilt according to the governing measure that ground monitoring data are implemented, such as ground
The schemes such as water, construction site cover, traffic is restricted driving, industrial limited production, boiler improvement, desulphurization denitration are handled, effect is not yet
It is fully up to expectations.
As the unmanned aerial vehicle remote sensing technology of the 3rd generation remote sensing technology after Aeronautics and Astronautics remote sensing, there is three-dimensional prison
Survey, fast response time, monitoring range is wide, landform interferes the advantages that small, is to carry out air accident pollution sources from now on to know
Other and concentration monitor one of important development direction.Gaseous environment is surveyed using UAV system measuring apparatus in the prior art
Amount, the sensor for measuring PM dust and the sensor for measuring CO, SO2, NO2, O3, H2S, NH3 etc. are handled in same
Chamber so that measure being coated by dust for the sensor probe of CO, SO2, NO2, O3, H2S, NH3 etc., reduce measurement accuracy.
Utility model content
To overcome disadvantage existing in the prior art, the utility model to provide a kind of unmanned plane atmospheric based on big data
Environmental monitoring system is arranged by the sensor of PM dust and for measuring the sensor of other gas contents in different chambers
In, substantially increase measurement accuracy.
To realize that goal of the invention, the utility model provide a kind of unmanned plane Atmosphere Environment Monitoring System Bases based on big data,
It includes the UAV system detection device connected by Radio Link and ground-based server, wherein UAV system detection device packet
The electric device for including shell and being arranged in shell, electric device include gas content sensor, PM sensor of dust concentration,
One processor, positioning time service module, first memory and first communication module, positioning time service module are used to obtain the position of unmanned plane
Confidence ceases temporal information when carrying out data acquisition with detection device；The gas content sensor is for obtaining residing for unmanned plane
Multiple gases content at position, and send Gas content to first processor；The PM sensor of dust concentration is for obtaining
PM dust concentrations at unmanned plane present position, and concentration information is supplied to first processor, the first processor is by gas
Body content data, PM dust concentrations, location information and temporal information carry out fusion treatment, are then sensed to ground by communication module
Face server, which is characterized in that shell is at least divided into two chambers, gas content sensor and PM sensor of dust concentration point
It is not arranged in first chamber and second chamber.
Preferably, first chamber includes at least air admission hole and gas vent, the upstream of air-flow is provided with microfilter, institute
Microfilter is stated for filtering PM dust.
Preferably, it is additionally provided with air pump in the first chamber, the air inlet of the air pump is communicated in the exhaust outlet of filter,
The exhaust outlet of air pump is communicated in the chamber portion for being set to gas content sensor probe.
Preferably, UAV system detection device is fixed on by gondola on the body of unmanned plane, and the gondola includes first
Mounting plate and the second mounting plate are provided with screw hole on the first mounting plate, are fixed on the first mounting plate by screw hole using screw
On the shell of detection device, dove-tail form fin is provided on the first mounting plate；It is provided with screw hole on second mounting plate, utilizes screw
The second mounting plate is fixed on the body of unmanned plane by spiral shell, is provided on the second mounting plate matched with dove-tail form fin
Dovetail groove.
Preferably, ground-based server includes at least second communication module, second processor, display and second memory,
The second communication module is stored in for receiving the data that detection device is sent in second memory, and described second deposits
Gas analysis application program is also stored in reservoir, the second processor calls the gas analysis stored in second memory to answer
With program, and received data is handled, is then shown over the display.
Preferably, the gas analysis application program include at least real time data display module, the inquiry of historical data module,
Regional pollution probability analysis and pollution ranking statistics module, wherein the real time data display module, by the detection device of reception
Transmission carrys out the data that sensor is detected and carries out comprehensive display, and different levels of contamination are represented with different colors.
Preferably, the gas parameter of each position is stored sequence by the inquiry of historical data module, set-up time, when
When user needs to inquire the data of certain time, processor shows the data of the time over the display.
Preferably, regional pollution probability analysis module calculated in a period of time, the gas content and dust concentration in each region,
Statistics pollutes exceeded probability so as to the region polluted frequent occurrence.
Preferably, pollution ranking statistics module is ranked up the gas content and dust concentration in each region.
Preferably, gas content sensor includes but not limited to：Carbon monoxide transducer, nitrogen dioxide sensor, vulcanization
Hydrogen sensor, ammonia gas sensor and ozone sensor, the PM dust concentrations include PM10 sensor of dust concentration and PM2.5 powder
Dust concentration sensor.
Compared with prior art, since the utility model will measure CO, SO2、NO2、O3、H2S、NH3Probe and PM dust
Probe is arranged in different chambers so that measures CO, SO2、NO2、O3、H2S、NH3The measurement accuracy of equal size greatly improves.
Description of the drawings
Fig. 1 is the electric device composition frame chart of UAV system detection device provided by the utility model；
Fig. 2 is the unmanned shell schematic diagram for carrying detection device provided by the utility model；
Fig. 3 is the composition schematic diagram of the test air chamber of UAV system detection device provided by the utility model；
Fig. 4 is the composite structural diagram that the utility model provides gondola；
Fig. 5 is the circuit diagram of data collector provided by the utility model；
Fig. 6 is the circuit diagram of signal conditioner provided by the utility model；
Fig. 7 is the circuit diagram of air pump driver provided by the utility model；
Fig. 8 is the composition frame chart of ground-based server provided by the utility model.
Specific implementation mode
The technical solution of the utility model is clearly and completely described below in conjunction with attached drawing, it is clear that described
Embodiment is the utility model a part of the embodiment, instead of all the embodiments.Based on the embodiments of the present invention, originally
The every other embodiment that field those of ordinary skill is obtained without making creative work, belongs to this practicality
Novel protected range.
In the description of the present invention, it should be noted that term " first ", " second " etc. are used for description purposes only,
It is not understood to indicate or imply relative importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " phase
Even ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or be integrally connected；It can
To be electrical connection, it can also be to be connected directly, can also can also be inside two elements indirectly connected through an intermediary
Connection, for the ordinary skill in the art, can understand the tool of above-mentioned term in the present invention with concrete condition
Body meaning.
According to one embodiment, the unmanned plane Atmosphere Environment Monitoring System Bases provided by the utility model based on big data include
The UAV system detection device and ground-based server connected by Radio Link, wherein UAV system detection device includes shell
With the electric device being arranged in shell.
Fig. 1 is the composition frame chart of the electric device of UAV system detection device provided by the utility model, as shown in Figure 1,
Detection device includes at least processor 10, memory and data collector 15, and processor 10 is, for example, CPU, and data are acquired
The data that device 15 obtains are stored in memory, and the memory includes EEPROM and RAM；The data collector is for acquiring
The gas content and PM dust concentrations of local environment, such as CO, SO2、NO2、O3、H2S、NH3With PM dust concentrations etc., data collector
Include including at least the sensor for the physical signal acquired to be converted to electric signal, the signal for providing sensor
The program-controlled big device and programmable logic device being amplified, the programmable logic device are used to provide control letter to programmable amplifier
Number, subsequently it is described in detail in conjunction with Fig. 5 and Fig. 6.The sensor includes gas content sensor and PM dust concentrations sensing
Device, the gas content sensor is used to obtain the multiple gases content at unmanned plane present position, and Gas content is sent to
Processor, gas content sensor include and are not limited to CO, SO2、NO2、O3、H2S、NH3Sensor；The PM dust concentrations pass
Sensor is used to obtain the PM dust concentrations at unmanned plane present position, and concentration information is supplied to processor, the PM dust
Concentration sensor includes and is not limited to PM10 sensor of dust concentration and PM2.5 sensor of dust concentration.UAV system detects
Equipment further includes positioning time service module 14, is used to obtain time letter when the location of detection device and detection gas content
Breath, the positioning time service module 14 can be GPS module, can also be Big Dipper positioning time service module.The processor is by gas
Content data, PM dust concentrations, location information and temporal information carry out fusion treatment, are then sensed to ground by communication module
Server, shell are at least divided into two chambers, and gas content sensor and PM sensor of dust concentration are separately positioned on the first chamber
In room and second chamber.
UAV system detection device further includes communication unit（Communication module）13, the signal that processor is provided carries out letter
Source volume, channel coding, are then modulated on carrier frequency, are then sent to space by antenna, wireless to be carried out with ground-based server
Link, to ground-based server into row data communication.
UAV system detection device provided by the utility model further includes air pump driver 16 and air pump 17, and the air pump drives
Dynamic device 16 provides signal according to the instruction of processor to air pump driver 16, and institute's art air pump 17 carries out driving work by motor, uses
It is pumped into data collector in by the gas under test gas environment, the first air cavity residing for a part of sensor probe, separately
The second air cavity residing for a part of sensor probe is subsequently described in detail air pump driver 16 in conjunction with Fig. 8.
Fig. 2 is the unmanned shell schematic diagram for carrying detection device provided by the utility model, as shown in Fig. 2, UAV system is examined
The shell of measurement equipment is oblate spherical shape, and upper surface is plane, and the side of shell is adjacent to have arranged the first air inlet（Air admission hole）101
With the second air inlet（Air admission hole）102, it is symmetrically arranged with first row gas port with the first air inlet 101 and the second air inlet 102（Row
Stomata）And second exhaust port（Gas vent）, the internal cavity of shell is divided into three chambers, the first chamber is provided with below enclosure interior
Room and second chamber, first chamber are connected to the first air inlet 101 and first row gas port, second chamber and the second air inlet 102
It is connected to second exhaust port.The detection of carbon monoxide, nitrogen dioxide, sulfur dioxide, ozone and ammonia etc. in data collector
Head is set in first chamber；PM10 dust sensors are popped one's head in and PM2.5 dust sensors probe is set in second chamber, if
The third chamber on first chamber and second chamber is set for placing circuit board and battery etc..Have in the side wall of shell and also sets
It is equipped with antenna 103, one end of the antenna 103 is set to the side wall of shell by hinge element, and antenna 103 is just shape antenna.Outside
The upper surface of shell is provided with gondola 200, and the concrete structure of gondola is described in detail subsequently through Fig. 4.
Fig. 3 is the composition schematic diagram of the test air chamber of UAV system detection device provided by the utility model, such as Fig. 3 institutes
Show, first chamber 104 includes at least air inlet 101 and exhaust outlet 106, and microfilter is provided at air inlet 103, described
Microfilter can so make the spy of carbon monoxide, nitrogen dioxide, sulfur dioxide, ozone and ammonia etc. for filtering PM dust
Gauge head long-lasting cleanliness to provide measurement accuracy, and improves working life.It is additionally provided with air pump in first chamber 104,
The air inlet of the air pump is communicated in the exhaust outlet 106 of filter, and the exhaust outlet of air pump, which is communicated in, is set to gas sensor spy
The chamber of head.Second chamber 105 includes at least air inlet 102 and exhaust outlet 107, and dust sensing is provided in second chamber 105
Device is used to detect dust concentration.
Fig. 4 is the composite structural diagram that the utility model provides gondola, as shown in figure 4, UAV system detection device is by hanging
Cabin 200 is fixed on the body of unmanned plane, and the gondola includes the first mounting plate 201 and the second mounting plate 202, the first mounting plate
It is provided with screw hole on 201, the first mounting plate 201 is fixed on the shell of detection device by screw hole using screw, the first peace
Dove-tail form fin is provided in loading board；It is provided with screw hole on second mounting plate 202, using screw by screw hole by the second mounting plate
202 are fixed on the body of unmanned plane, are provided on the second mounting plate 202 and the matched dovetail groove of dove-tail form fin.
Fig. 5 is the circuit diagram of data collector provided by the utility model.As shown in figure 5, data collector includes being used for
Gas signal is converted into multiple gas content sensors of electric signal and dust concentration passes sensor, multiple gas content sensings
Device is for example including CO, SO2、NO2、O3、H2S、NH3Sensor, sensor of dust concentration is for example including PM10 sensor of dust concentration
With PM2.5 sensor of dust concentration.Data collector further includes multiplexer, will be passed all the way by time-multiplexed mode
Sensor is connected to signal conditioner.Data collector further includes for being amplified signal condition to the signal that sensor provides
Device；The programming amplifying that the signal that signal conditioner provides is amplified by the control signal provided according to programmable journey logic device
Device；The filter of high-frequency components in signal for filtering out programmable amplifier offer, the signal for providing filter into
The analog-digital converter and programmable logic device of row analog-to-digital conversion, the programmable logic device are used to provide control to processing amplifier
Signal, wherein the signal output end of signal conditioner is connected to programmable amplifier by capacitance C1, and the capacitance C1 is coupling electricity
Hold.
Data collector further includes constant-current source, includes digital analog converter per road constant-current source（D/A）, operational amplifier OP301,
Field-effect tube T301, the digital controlled signal that the mode converter D/A is used to provide programmable logic device to operational amplifier
It is converted to analog control signal and is connected to the in-phase end of operational amplifier OP301, operational amplifier OP301 by resistance R304
Reverse side the drain electrode of field-effect tube T301 is connected to by resistance R302, the output end of operational amplifier OP301, which leads to, to be connected to
The grid of field-effect tube；The drain electrode of field-effect tube T301 is connected to power supply 24V, the source electrode warp of field-effect tube T301 through resistance R301
Resistance R303 is connected to the signal end of gas sensor.Resistance is preferably zero ohms.
In the utility model, circuit shown in fig. 6 may be used in the signal conditioner in data acquisition device.Such as Fig. 6 institutes
Show, signal conditioner provided by the utility model includes first order amplifier and second level amplifier, wherein first order amplifier
Including operational amplifier OP301, transistor T302, resistance R307 and resistance R311, the signal output end of gas sensor connects
In the first end of resistance R305, the second end of resistance R5 is connected to the in-phase end of operational amplifier OP301；Operational amplifier
The in-phase end of OP301 is also connected to ground through resistance R6；The output end of operational amplifier OP301 is connected to the base of transistor T302
Pole.The base stage of transistor T302 is connected to ground through resistance R311；Collector is connected to power supply+EC, transistor through resistance R307
The emitter of T302 is connected to the reverse side of operational amplifier OP302.Second level amplifier includes operational amplifier OP303, field
Effect pipe T303, resistance R306, resistance R309 and resistance R310, first order amplifier signal output end, i.e. transistor T302's
Collector is connected to the in-phase end of operational amplifier OP303；The output end of operational amplifier OP303 is connected to field through resistance R309
The grid of effect pipe T303.The drain electrode of field-effect tube T303 is connected to power supply 24V through resistance R310, and source electrode is provided out letter
Number.The drain electrode of field-effect tube T303 is also connected to the reverse side of operational amplifier OP303 through resistance R308.Power supply 24V is filtered
Capacitance C2 is connected to ground.
Fig. 7 is the circuit diagram of air pump driver provided by the utility model, as shown in fig. 7, for executing current vector control
The air pump driver of system includes control circuit, phase driver, phase inverter, the first splitter, the second splitter and third splitter,
The phase inverter includes multiple switch element T1 ~ T6 and the phase driving circuit for on-off driving switch element T1 ~ T6.
Mos field effect transistor is used in switch element T1 ~ T6（MOSFET）Or insulated gate bipolar transistor
（IGBT）Constant power semiconductor element.In addition, being connected in parallel recirculation diode in each switch element T1 ~ T6.
First splitter can be connected to the switch element T2 in phase inverter and between ground, and first splitter is preferably sharp
It is realized with resistance R1；Second splitter can be connected to the switch element T4 in phase inverter and between ground, stop the second splitter
It is realized preferably by resistance R2；Third splitter can be connected to the switch element T6 in phase inverter and between ground, stopped third
Splitter is realized preferably by resistance R3.
Control circuit includes motor controller, biasing circuit OF1T and amplifier CO1, and the amplifier CO1 is for amplifying
The voltage signal that is there is provided from the first splitter is simultaneously supplied to biasing circuit OF1, and the biasing circuit OF1 is used for amplifier CO1
The signal of offer is compared to generate digital signal ADC1 with the reference voltage Vref provided by controller, and is supplied to control
Device processed.
Control circuit further includes biasing circuit OF2 and amplifier CO2, the amplifier CO2 for amplifying from the second branch
The voltage signal of device offer is simultaneously supplied to biasing circuit OF2, the signal that the biasing circuit OF2 is used to provide amplifier CO2
It is compared to generate digital signal ADC2 with the reference voltage Vref provided by controller, and is supplied to controller.
Control circuit further includes biasing circuit OF3 and amplifier CO3, the amplifier CO3 for amplifying from third branch
The voltage signal of device offer is simultaneously supplied to biasing circuit OF3, the signal that the biasing circuit OF3 is used to provide amplifier CO3
It is compared to generate digital signal ADC3 with the reference voltage Vref provided by controller, and is supplied to controller.
Motor controller generates pwm signal according to digital signal ADC1, ADC2 and ADC2.Control circuit further includes logic control
Pwm signal is converted to the parallel letter for controlling phase driver by device processed, logic controller response pwm signal and clock signal
Number.Logic controller can transmit error signal to motor controller, respond error signal, motor controller can give logic control
Device processed provides the clock signal of the pwm signal and correction of a correction.
Parallel signal is responded, phase driver can generate grid signal to open or close the multiple switch in phase inverter
Element T1 ~ T6.Grid signal is responded, phase inverter can generate an ac current signal with drive motor, to make motor certainly
Dynamic speed governing.
Fig. 8 is the composition frame chart of ground-based server, as shown in figure 8, ground-based server provided by the utility model includes place
Manage device 20, input/output interface 21, network adapter 23, communication module 23, dual-mode antenna 24 and memory 25, wherein transmitting-receiving
Antenna 24 is used to spatial electromagnetic wave signal being converted to electric signal, and is supplied to communication module 23, and communication module 23 includes number
Base Band Unit and modulation unit, when transmitting, the information that the digital baseband unit is used to be transmitted processor carries out information source volume
Code and channel coding, then send modulation unit to, and the modulation unit includes transmitter, and the transmitter is used for digital base
The information that tape cell transmission comes, which is spread and is modulated in carrier signal, then carries out power amplifier, and sky is emitted to finally by antenna
Between；Modulation unit further includes receiver, and receiver is used to antenna received signal carrying out demodulation despreading, then sends out data
Digital baseband unit is given, digital baseband unit is used to digital baseband signal carrying out channel decoding, source coding, takes out nobody
The data that airborne equipment is sent.Processor 20 to the data frame that UAV system equipment is sent unpack and in display 26
On shown, processor is handled acquired data according to user instruction.Ground-based server by received nobody
It is printed by printer with the information that equipment is sent is carried, can also store in memory 25, also pass through network adapter
It is sent to other users or server.Input/output interface 21 can also connect keyboard and mouse, keyboard for input instruction or
Person executes certain operations, and mouse is for executing certain operations.
Gas analysis application program is also stored in the memory 25, the processor calls the gas stored in memory
Body analyzes application program, and handles received data, is then shown on the display 26.The gas analysis
Application program includes at least real time data display module, the inquiry of historical data module, regional pollution probability analysis and pollution ranking
Statistical module, wherein the real time data display module, by the transmission of the detection device of reception come data that sensor is detected into
Row comprehensive display represents different levels of contamination with different colors.
The gas analysis application program at least further includes the inquiry of historical data module, will be sequentially by everybody according to the time
The gas parameter set is stored, and when user needs to inquire the data of certain time, processor is showing the data of the time
It is shown on device.
The gas analysis application program at least further includes that regional pollution probability analysis module calculated in a period of time, each area
The gas parameter in domain, statistics pollute exceeded cumulative probability so as to the region polluted frequent occurrence.
The gas analysis application program at least further includes polluting ranking statistics module to carry out the gas parameter in each region
Sequence.
It is described in detail the utility model above in association with attached drawing, but what specification was only for interpreting the claims.
But the scope of protection of the utility model is not limited to specification.Any one skilled in the art is new in this practicality
Type disclose technical scope in, the variation or replacement that can be readily occurred in, should all cover the scope of protection of the utility model it
It is interior.Therefore, the scope of protection of the utility model should be subject to the scope of protection of the claims.
Claims (10)
1. a kind of unmanned plane Atmosphere Environment Monitoring System Bases based on big data comprising the UAV system connected by Radio Link
Detection device and ground-based server, wherein UAV system detection device includes shell and the electric device that is arranged in shell, electricity
Device of air includes gas content sensor, PM sensor of dust concentration, first processor, positioning time service module, first memory
And first communication module, positioning time service module be used for obtain unmanned plane location information and detection device carry out data acquisition when
Temporal information；The gas content sensor is used to obtain multiple gases content at unmanned plane present position, and by Gas content
Send first processor to；The PM sensor of dust concentration is used to obtain the PM dust concentrations at unmanned plane present position, and
Concentration information is supplied to first processor, the first processor by gas content data, PM dust concentrations, location information and
Temporal information carries out fusion treatment, is then sensed to ground-based server by communication module, which is characterized in that at least divide shell
At two chambers, gas content sensor and PM sensor of dust concentration are separately positioned in first chamber and second chamber.
2. the unmanned plane Atmosphere Environment Monitoring System Bases according to claim 1 based on big data, which is characterized in that the first chamber
Room includes at least air admission hole and gas vent, the upstream of air-flow is provided with microfilter, the microfilter is for filtering
PM dust.
3. the unmanned plane Atmosphere Environment Monitoring System Bases according to claim 2 based on big data, which is characterized in that first
Air pump is additionally provided in chamber, the air inlet of the air pump is communicated in the exhaust outlet of filter, and the exhaust outlet of air pump, which is communicated in, to be set
It is placed in the chamber portion of gas content sensor probe.
4. the unmanned plane Atmosphere Environment Monitoring System Bases according to claim 3 based on big data, which is characterized in that unmanned plane
Detection device is carried to be fixed on the body of unmanned plane by gondola, the gondola includes the first mounting plate and the second mounting plate, the
It is provided with screw hole on one mounting plate, the first mounting plate is fixed on the shell of detection device by screw hole using screw, first
Dove-tail form fin is provided on mounting plate；It is provided with screw hole on second mounting plate, is consolidated the second mounting plate by spiral shell using screw
Due on the body of unmanned plane, being provided on the second mounting plate and the matched dovetail groove of dove-tail form fin.
5. the unmanned plane Atmosphere Environment Monitoring System Bases according to claim 4 based on big data, which is characterized in that ground takes
Device be engaged in including at least second communication module, second processor, display and second memory, the second communication module is for connecing
The data that detection device is sent are received, and are stored in second memory, gas analysis is also stored in the second memory
Application program, the second processor call the gas analysis application program stored in second memory, and the number to being received
According to being handled, then shown over the display.
6. the unmanned plane Atmosphere Environment Monitoring System Bases according to claim 5 based on big data, which is characterized in that the gas
Body analyzes application program and includes at least real time data display module, the inquiry of historical data module, regional pollution probability analysis and dirt
Contaminate ranking statistics module, wherein the detection device transmission of reception is come what sensor was detected by the real time data display module
Data carry out comprehensive display, and different levels of contamination are represented with different colors.
7. the unmanned plane Atmosphere Environment Monitoring System Bases according to claim 6 based on big data, which is characterized in that history number
According to enquiry module, the gas parameter of each position is stored sequence by the set-up time, when user needs to inquire certain time
When data, processor shows the data of the time over the display.
8. the unmanned plane Atmosphere Environment Monitoring System Bases according to claim 6 based on big data, which is characterized in that region is dirty
Contaminate probability analysis module to calculate in a period of time, the gas content and dust concentration in each region, statistics pollute exceeded probability from
And the region that can be polluted frequent occurrence.
9. the unmanned plane Atmosphere Environment Monitoring System Bases according to claim 8 based on big data, which is characterized in that pollution row
Name statistical module is ranked up the gas content and dust concentration in each region.
10. according to any unmanned plane Atmosphere Environment Monitoring System Bases based on big data of claim 1-9, wherein gas
Content level sensor includes but not limited to：Carbon monoxide transducer, nitrogen dioxide sensor, hydrogen sulfide sensor, ammonia gas sensor
And ozone sensor, the PM dust concentrations include PM10 sensor of dust concentration and PM2.5 sensor of dust concentration.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820056430.9U CN207703821U (en) | 2018-01-15 | 2018-01-15 | Unmanned plane Atmosphere Environment Monitoring System Bases based on big data |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820056430.9U CN207703821U (en) | 2018-01-15 | 2018-01-15 | Unmanned plane Atmosphere Environment Monitoring System Bases based on big data |
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| CN207703821U true CN207703821U (en) | 2018-08-07 |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108267548A (en) * | 2018-01-15 | 2018-07-10 | 北京神鹫智能科技有限公司 | Unmanned plane Atmosphere Environment Monitoring System Bases based on big data |
| CN110316375A (en) * | 2019-06-24 | 2019-10-11 | 浙江华奕航空科技有限公司 | A kind of atmosphere environment supervision unmanned plane |
| CN111003175A (en) * | 2019-10-11 | 2020-04-14 | 浙江华奕航空科技有限公司 | Air inlet processing method of atmospheric environment monitoring unmanned aerial vehicle |
| CN112730527A (en) * | 2020-12-18 | 2021-04-30 | 中国科学技术大学 | Gas detection system based on MEMS gas sensor array |
-
2018
- 2018-01-15 CN CN201820056430.9U patent/CN207703821U/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108267548A (en) * | 2018-01-15 | 2018-07-10 | 北京神鹫智能科技有限公司 | Unmanned plane Atmosphere Environment Monitoring System Bases based on big data |
| CN110316375A (en) * | 2019-06-24 | 2019-10-11 | 浙江华奕航空科技有限公司 | A kind of atmosphere environment supervision unmanned plane |
| CN111003175A (en) * | 2019-10-11 | 2020-04-14 | 浙江华奕航空科技有限公司 | Air inlet processing method of atmospheric environment monitoring unmanned aerial vehicle |
| CN112730527A (en) * | 2020-12-18 | 2021-04-30 | 中国科学技术大学 | Gas detection system based on MEMS gas sensor array |
| CN112730527B (en) * | 2020-12-18 | 2022-05-13 | 中国科学技术大学 | Gas detection system based on MEMS gas sensor array |
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