CN106680896A - Unmanned aerial vehicle upper-air meteorological detection system - Google Patents
Unmanned aerial vehicle upper-air meteorological detection system Download PDFInfo
- Publication number
- CN106680896A CN106680896A CN201611150588.4A CN201611150588A CN106680896A CN 106680896 A CN106680896 A CN 106680896A CN 201611150588 A CN201611150588 A CN 201611150588A CN 106680896 A CN106680896 A CN 106680896A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- aerial vehicle
- unmanned aerial
- central processing
- processing unit
- 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.)
- Pending
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01W—METEOROLOGY
- G01W1/00—Meteorology
- G01W1/02—Instruments for indicating weather conditions by measuring two or more variables, e.g. humidity, pressure, temperature, cloud cover or wind speed
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01W—METEOROLOGY
- G01W1/00—Meteorology
- G01W1/08—Adaptations of balloons, missiles, or aircraft for meteorological purposes; Radiosondes
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/12—Supports; Mounting means
- H01Q1/22—Supports; Mounting means by structural association with other equipment or articles
- H01Q1/225—Supports; Mounting means by structural association with other equipment or articles used in level-measurement devices, e.g. for level gauge measurement
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/36—Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith
- H01Q1/38—Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith formed by a conductive layer on an insulating support
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
- Y02A90/00—Technologies having an indirect contribution to adaptation to climate change
- Y02A90/10—Information and communication technologies [ICT] supporting adaptation to climate change, e.g. for weather forecasting or climate simulation
Landscapes
- Environmental & Geological Engineering (AREA)
- Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Atmospheric Sciences (AREA)
- Biodiversity & Conservation Biology (AREA)
- Ecology (AREA)
- Environmental Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Arrangements For Transmission Of Measured Signals (AREA)
Abstract
The present invention discloses an unmanned aerial vehicle upper-air meteorological detection system. The system comprises an unmanned aerial vehicle body and a detection circuit arranged in the unmanned aerial vehicle body; the detection circuit comprises a central processing unit and a temperature sensor, a wind speed sensor and an ozone concentration monitoring unit which are in signal connection with the central processing unit; and the temperature sensor is configured to detect temperature, the wind speed sensor is configured to detect wind speed, and the ozone concentration monitoring unit detects the ozone concentration. The unmanned aerial vehicle upper-air meteorological detection system greatly facilitates the detection and reduces the cost.
Description
Technical field
The present invention relates to a kind of unmanned plane aerological sounding system.
Background technology
UAS using increasingly being popularized, but in meteorological detection also using common balloon sounding, no
Convenient, high cost if unmanned plane replaces, then greatly facilitates detection and also reduces cost.
The content of the invention
It is an object of the invention to overcome disadvantages described above, there is provided a kind of unmanned plane aerological sounding system.
For achieving the above object, concrete scheme of the invention is as follows：A kind of unmanned plane aerological sounding system, includes
Unmanned plane body, located at the intrinsic detection circuit of unmanned plane；The detection circuit includes central processing unit, with central authorities' process
The temperature sensor of device signal connection, air velocity transducer, ozone concentration monitoring means；The temperature sensor is used to detect temperature
Degree, air velocity transducer are used to detect wind speed, ozone concentration monitoring means detection ozone concentration.
Wherein, the radio communication device includes communication chip and communication antenna.
Wherein, recording equipment is also included, the recording equipment is used for real time record detection information.
Wherein, photographic head is also included, for shooting overhead imagery；Photographic head is connected with central processing unit signal；
Wherein, positioner is also included, for positioning；Positioner is connected with central processing unit signal；
Wherein, display lamp is also included, for indicating position；Display lamp is connected with central processing unit signal；
Beneficial effects of the present invention are：Greatly facilitate detection and also reduce cost.
Description of the drawings
Fig. 1 is the schematic diagram of the present invention；
Fig. 2 is the top view of the communication antenna of the present invention；
Fig. 3 is oscillator chip architecture schematic diagram of the present invention；
Fig. 4 is the schematic rear view of the communication antenna of the present invention；
Fig. 5 is the directional diagram of the antenna of the present invention；
Description of reference numerals in Fig. 1 to Fig. 5：
11- base plates；12- Electricity Federations portion；13- shielded microstrip line units；14- raises one's arm on basis；141- first combines arm；15- first shakes
Portion；The second vibrations of 16- portion；161- protruded arms；162- first lacks sky；163- second lacks sky；The 3rd vibrations portions of 17-；18- second
Close arm；19- laterally restrains unit；191-30 degree breach.
Specific embodiment
The present invention is further detailed explanation with specific embodiment below in conjunction with the accompanying drawings, is not the reality the present invention
Apply scope and be confined to this.
As shown in Figures 1 to 5, a kind of unmanned plane aerological sounding system described in the present embodiment, includes unmanned plane
Body, located at the intrinsic detection circuit of unmanned plane；The detection circuit includes central processing unit, with central processing unit signal
The temperature sensor of connection, air velocity transducer, ozone concentration monitoring means；The temperature sensor is used to detect temperature, wind speed
Sensor is used to detect wind speed, ozone concentration monitoring means detection ozone concentration.
A kind of unmanned plane aerological sounding system described in the present embodiment, the radio communication device include communication core
Piece and communication antenna.
In a kind of unmanned plane aerological sounding system described in the present embodiment, recording equipment, the record are also included
Device is used for real time record detection information.
A kind of unmanned plane aerological sounding system described in the present embodiment, also includes photographic head, for shooting high-altitude
Image；Photographic head is connected with central processing unit signal；
A kind of unmanned plane aerological sounding system described in the present embodiment, also includes positioner, for positioning；Positioning dress
Put and be connected with central processing unit signal；
A kind of unmanned plane aerological sounding system described in the present embodiment, also includes display lamp, for indicating position；Indicate
Lamp is connected with central processing unit signal；Greatly facilitate detection and also reduce cost.
The communication antenna includes a base plate 11, and the base plate 11 is provided with symmetrical two oscillator pieces, often
Individual oscillator piece includes trapezoidal basis and raises one's arm 14, and the basis is raised one's arm and 14 extends upward the first joint arm 141, the first joint
Arm 141 extends upward the first trapezoidal vibrations portion 15, the short base and basis in the first vibrations portion 15 raise one's arm 14 it is short
Basis is raised one's arm and 14 combines arm 141 with first and be connected, and the long base in the first vibrations portion 15 extends upward the of rectangle
Two vibrations portions 16, the second vibrations portion 16 of the rectangle extend upward the 3rd trapezoidal vibrations portion 17, the 3rd vibrations portion
17 long base is connected with the second vibrations portion 16, and the short base in the 3rd vibrations portion 17 extends upward the second joint arm 18,
Second joint, 18 free end of arm is vertically connected with the horizontal convergence unit 19 of a track type, the horizontal convergence unit 19
Top is provided with 30 degree of breach 191；The both sides in the second vibrations portion 16 protrude protruded arm 161；In the second vibrations portion 16
It is provided with the first of two rectangles and lacks empty 162, two first lacks empty 162 and are respectively arranged on 15 both sides of the first vibrations portion, first shake
Second that multiple horizontal spread configurations are additionally provided with dynamic portion 15 lacks empty 163；Electricity Federation portion 12 is additionally provided with, Electricity Federation portion 12 is located at two
In the middle of oscillator piece, for feeding coupling；By the microstrip circuit structure design not less than 300 times, and by being not less than 500 times
Under test and parameter adjustment, above-mentioned antenna structure is finally determined, in the case where its Electromagnetic Interference environment is simulated, the antenna exists
700MHZ to 1000MHZ frequency ranges (conventional communication band) show excellent communication electric parameter performance, and specifically, radiation is single
Than more than 31dB before and after the minimum frequency of unit, than being averagely more than 35dB before and after frequency band is interior；Low frequency dot gains are more than 9.37dBi, frequency band
Interior average gain is more than 9.8dBi.Such as Fig. 5, its gain pattern, omnidirectional's performance are very excellent.In addition, from concrete test
Test result and simulation result are basically identical, above-mentioned antenna be non-dimensional requirement antenna, if on overbending direction, arrange lack
Above-mentioned requirements are reached in mode that is empty, lacking sky, can reach above-mentioned experimental result.
11 back side of the base plate is provided with the shielded microstrip line unit 13 of multiple matrix arrangements, and shielded microstrip line unit is octagon
Structure, the setting of the structure are very ingenious, and experiment finds, when shielded microstrip line unit 13 is provided with, the not only isolation of antenna
Degree has certain increase, and standing-wave ratio reduces 0.8, is implemented as 1.07 or so, and gain increases 2dBi, needs exist for
It is bright, during when octagon micro-strip 13 arranging other antennas are identical, on analogous location, it is only capable of increasing isolation, it is impossible to increase
Plus antenna other performances, it is seen that the setting of octagon micro-strip 13 meets the Performance Match with antenna, and unique improves antenna
Current average, setting have reached the result for more optimizing together, support each other.
Specifically, above-mentioned antenna is non-dimensional requirement antenna, as long as on overbending direction, the side that is scarce empty, lacking sky of setting
Above-mentioned requirements are reached in formula；But if need more preferably stable performance, the concrete size of this antenna can be optimized for：Base plate 11
Transverse width be 48mm, it is a height of:31mm；Basis raise one's arm 14 it is a height of:3.7mm, long base are 12.5mm, and short base is
5.3mm；First joint 141 length and width of arm is respectively：1.1mm and 1.34mm；First vibrations portion 15,17 and of the 3rd vibrations portion
Basis raise one's arm 14 size it is identical, second joint arm 18 with first joint arm 141 size it is identical；The second vibrations portion 16
Width and height are respectively：12.8mm and 12.5mm；The radius of protruded arm 161 is 1mm；First lacks empty 162 live width is：
1.2mm, a length of 11.8mm；Described second quantity for lacking sky 163 is 8, and two adjacent second distances for lacking empty 163 are 1mm；
Described first live width for lacking sky 162 is 0.6mm, a length of 4.8mm；Laterally the live width of convergence unit 19 is 1.5mm, a length of
12.5mm；The angle of 30 degree of breach 191 is 30 degree.
The above is only a preferred embodiment of the present invention, therefore all structures according to described in present patent application scope
Make, the equivalence changes done by feature and principle or modification, be included in the protection domain of present patent application.
Claims (3)
1. a kind of unmanned plane aerological sounding system, it is characterised in that：Unmanned plane body is included, it is internal located at unmanned plane sheet
Detection circuit；The detection circuit includes central processing unit, the temperature sensor that is connected with central processing unit signal, wind speed
Sensor, ozone concentration monitoring means；The temperature sensor is used to detect temperature, and air velocity transducer is used to detect wind speed, smelly
Oxygen concentration monitoring means detect ozone concentration.
2. a kind of unmanned plane aerological sounding system according to claim 1, it is characterised in that：The radio communication dress
Put and include communication chip and communication antenna.
3. a kind of unmanned plane aerological sounding system according to claim 1, it is characterised in that：Record dress is included also
Put, the recording equipment is used for real time record detection information.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611150588.4A CN106680896A (en) | 2016-12-14 | 2016-12-14 | Unmanned aerial vehicle upper-air meteorological detection system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611150588.4A CN106680896A (en) | 2016-12-14 | 2016-12-14 | Unmanned aerial vehicle upper-air meteorological detection system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106680896A true CN106680896A (en) | 2017-05-17 |
Family
ID=58869126
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611150588.4A Pending CN106680896A (en) | 2016-12-14 | 2016-12-14 | Unmanned aerial vehicle upper-air meteorological detection system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106680896A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109188565A (en) * | 2018-10-15 | 2019-01-11 | 南京信息工程大学 | A kind of the digital meteorological sounding meter and its sounding system with camera |
| CN109541963A (en) * | 2018-11-12 | 2019-03-29 | 北京应用气象研究所 | A kind of unmanned plane survey wind modeling technique based on sideslip angle information |
| CN109665119A (en) * | 2018-12-19 | 2019-04-23 | 华南农业大学 | A kind of arrow carries three-dimensional height wind velocity measurement system and its measurement method in real time |
| CN111025427A (en) * | 2019-12-02 | 2020-04-17 | 成都信息工程大学 | Meteorological data real-time acquisition system based on space flyer |
-
2016
- 2016-12-14 CN CN201611150588.4A patent/CN106680896A/en active Pending
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109188565A (en) * | 2018-10-15 | 2019-01-11 | 南京信息工程大学 | A kind of the digital meteorological sounding meter and its sounding system with camera |
| CN109541963A (en) * | 2018-11-12 | 2019-03-29 | 北京应用气象研究所 | A kind of unmanned plane survey wind modeling technique based on sideslip angle information |
| CN109541963B (en) * | 2018-11-12 | 2021-06-25 | 北京应用气象研究所 | Unmanned aerial vehicle wind measurement modeling method based on sideslip angle information |
| CN109665119A (en) * | 2018-12-19 | 2019-04-23 | 华南农业大学 | A kind of arrow carries three-dimensional height wind velocity measurement system and its measurement method in real time |
| CN109665119B (en) * | 2018-12-19 | 2021-07-23 | 华南农业大学 | Rocket-borne three-dimensional height real-time wind speed measurement system and measurement method thereof |
| CN111025427A (en) * | 2019-12-02 | 2020-04-17 | 成都信息工程大学 | Meteorological data real-time acquisition system based on space flyer |
| CN111025427B (en) * | 2019-12-02 | 2021-07-16 | 成都信息工程大学 | Meteorological data real-time acquisition system based on space flyer |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106680896A (en) | Unmanned aerial vehicle upper-air meteorological detection system | |
| CN204011731U (en) | Complex media microstrip antenna | |
| CN204088565U (en) | WIFI antenna and apply the radio communication device of this WIFI antenna | |
| CN104347938A (en) | Antenna unit, antenna array and road side unit | |
| CN106680897A (en) | Locatable unmanned plane high-altitude meteorology detection system | |
| CN204118258U (en) | A kind of miniaturized symmetrical dipole omnidirectional antenna | |
| CN106680898A (en) | Unmanned aerial vehicle high-altitude meteorological detection system | |
| CN106646673A (en) | Indicator light unmanned aerial vehicle high-altitude meteorological detection system | |
| CN106646672A (en) | UAV high-altitude meteorological detection system having image function | |
| CN105004980B (en) | A kind of transformer station discharge signal detection device | |
| KR101519875B1 (en) | Microstrip patch array antenna with flat-top and low side lobe beam pattern | |
| CN105021964B (en) | A kind of transformer station partial discharge signals detecting system | |
| CN106652095A (en) | Automobile status monitoring system with driving recorder | |
| CN106643887A (en) | Humidity monitoring indoor environment monitor | |
| CN106681401A (en) | Vegetable greenhouse environmental monitoring system with carbon dioxide monitoring function | |
| CN106527552A (en) | Greenhouse environment monitoring system | |
| CN106683327A (en) | Shopping mall early warning system capable of registering attendance | |
| CN105021965B (en) | High sensitivity transformer station discharge signal monitoring device | |
| CN106652093A (en) | Automobile state monitoring system | |
| CN106627436A (en) | Anti-speeding automobile condition monitoring system | |
| CN106677826A (en) | Down-hole monitoring system provided with smoke detector | |
| CN106683403A (en) | Road capture device with horn warning | |
| CN106600875A (en) | Shopping mall early warning system | |
| CN106652318A (en) | Shopping mall early-warning system | |
| CN106683326A (en) | Visitors flow rate monitoring type shopping mall early-warning system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170517 |
|
| WD01 | Invention patent application deemed withdrawn after publication |