CN108454831A - One kind is taken photo by plane unmanned plane Intelligence Feedback control system - Google Patents
One kind is taken photo by plane unmanned plane Intelligence Feedback control system Download PDFInfo
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- CN108454831A CN108454831A CN201810416661.0A CN201810416661A CN108454831A CN 108454831 A CN108454831 A CN 108454831A CN 201810416661 A CN201810416661 A CN 201810416661A CN 108454831 A CN108454831 A CN 108454831A
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- 238000004891 communication Methods 0.000 claims abstract description 11
- 239000004065 semiconductor Substances 0.000 claims description 21
- 238000012544 monitoring process Methods 0.000 claims description 14
- 230000009471 action Effects 0.000 claims description 8
- 230000005611 electricity Effects 0.000 claims description 7
- 206010037660 Pyrexia Diseases 0.000 claims description 5
- 230000017525 heat dissipation Effects 0.000 claims description 5
- 229910021421 monocrystalline silicon Inorganic materials 0.000 claims description 3
- 238000005057 refrigeration Methods 0.000 claims description 3
- 230000005540 biological transmission Effects 0.000 abstract description 4
- 238000012546 transfer Methods 0.000 abstract description 3
- 230000000694 effects Effects 0.000 description 6
- 238000000034 method Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 4
- 238000001816 cooling Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 238000004364 calculation method Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 238000012790 confirmation Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C19/00—Aircraft control not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/20—Remote controls
Abstract
It takes photo by plane unmanned plane Intelligence Feedback control system the invention discloses one kind, includes audible-visual annunciator for controlling the ground control system of body state of flight, reporting for dangerous information, 5G communication modules, the flight module for providing body high-altitude flight work and the power supply module powered for circuit system received and dispatched for wireless data information；The output end of the ground control system is electrically connected the input terminal of audible-visual annunciator, this unmanned plane Intelligence Feedback control system of taking photo by plane, the wireless connection of ground control system and flight module is realized by 5G communication modules, it avoids other wireless devices and interference is generated to the control of body, and make more stablizing for data information transfer, transmission range is farther, it is rainy when detecting, when flight temperature is higher and body flight is unbalance, ground control system can control audible-visual annunciator to report dangerous information, to make staff that can withdraw body, largely reduce the damage of body and flight module.
Description
Technical field
The present invention relates to unmanned aerial vehicle control system technical field, specially one kind is taken photo by plane unmanned plane Intelligence Feedback control system
System.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft, or fully or intermittently automatically operated by car-mounted computer.
Compared with manned aircraft, unmanned plane is often more suitable for the task of those too " slow-witted, dirty or dangerous ".Nobody
Machine press application field, can be divided into it is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane
+ sector application, which is unmanned plane, really just have been needed；At present take photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief,
Observe wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field
Application, greatly expanded the purposes of unmanned plane itself, developed country is also in actively extension sector application and development unmanned plane
Technology.
The unmanned plane of present technology has the following disadvantages：1, radio robot uses 2.4G frequency ranges, present family
Wireless routing is all made of 2.4G mold segments, although transmission power is not high, the quantity of metropolitan district is big, can inevitably interfere remote controler
Wireless manipulation, causes out of control；2, most unmanned machine equipments are without water-proof function, and do not have sleety weather information monitoring function,
Therefore the water droplet of sleet formation can influence the case where short circuit of aircraft electrical sub-circuit portion or electric leakage, next mechanical structure portion part
For metal materials such as iron or steel, it can corrode or get rusty after water inlet, influence mechanical movement normal operation；3, when unmanned plane during flying, only
It can be powered by internal battery, cause the cruising ability of unmanned plane during flying poor；4, most of unmanned planes are using air-cooled
Natural heat dissipation, environment temperature are got over hour with the aircraft running temperature temperature difference, and heat dissipation is slower.For this purpose, the nothing it is proposed that one kind is taken photo by plane
It is man-machine to use Intelligence Feedback control system.
Invention content
It takes photo by plane unmanned plane Intelligence Feedback control system the purpose of the present invention is to provide one kind, to solve above-mentioned background skill
The problem of being proposed in art.
To achieve the above object, the present invention provides the following technical solutions：One kind take photo by plane unmanned plane Intelligence Feedback control system
System includes audible-visual annunciator for controlling the ground control system of body state of flight, reporting for dangerous information, for nothing
Line data information transmitting-receiving 5G communication modules, for provide body high-altitude flight work flight module and for circuit system supply
The power supply module of electricity；
The output end of the ground control system is electrically connected the input terminal of audible-visual annunciator, and ground control system is also logical
It crosses 5G communication modules to be wirelessly connected with flight module, the output end of the power supply module electrically connects with the circuit system of flight module
It connects；
The flight module includes the airborne computer converted for data-signal, half for cooling down to airborne computer
Conductor cooling piece, the radiator for sending out semiconductor chilling plate hot-side heat dissipation, the servo action mould for driving body to fly
Block, for flight environment of vehicle prospecting monitoring modular and for body flight position confirm locating module, the radiator it is defeated
The fever end of outlet and semiconductor chilling plate connects, and the refrigeration end of the semiconductor chilling plate is connect with airborne computer, and machine
The output end for carrying computer is electrically connected the input terminal of semiconductor chilling plate, radiator and servo action module, the monitoring mould
The output end of block and locating module is electrically connected with the input terminal of airborne computer.
Preferably, the monitoring modular includes for detecting the Raindrop sensor of Weather information, for detecting flight temperature
Temperature sensor and gyroscope for detecting body flight attitude, the Raindrop sensor, temperature sensor and gyroscope
Output end be electrically connected the input terminal of airborne computer.
Preferably, the Raindrop sensor is fixed on the top of body.
Preferably, the locating module includes baroceptor for detecting body flying height and is used for computer body
The output end of the light stream sensor of location information, the baroceptor and light stream sensor is electrically connected the defeated of airborne computer
Enter end.
Preferably, the locating module further includes the ultrasonic sensor for detecting obstacle distance, the ultrasonic wave
Sensor is electrically connected the input terminal of airborne computer.
Preferably, the power supply module includes that rechargeable battery power supply module and for converting solar energy into electrical energy simultaneously
For the solar powered module of flight module for power supply, the output end of the battery powered module and solar powered module is electrical
Connect the circuit system of flight module.
Preferably, the solar powered module includes for absorbing the solar panel of solar energy, for controlling
The anti-reverse charging diode of current direction, the accumulator for storing electric energy and the inverter converted for electric current, the solar energy
The output end of solar panel is electrically connected the input terminal of anti-reverse charging diode, and the output end of the anti-reverse charging diode, which is electrically connected, to be stored
The input terminal of battery, the output end of the accumulator are electrically connected the input terminal of inverter, and the output end of the inverter is electrical
The circuit system of flight module is connected, the output end of the airborne computer is electrically connected the input terminal of accumulator.
Preferably, the solar panel is made of monocrystalline silicon.
Preferably, the solar panel is fixed on the top of body, and is distributed in the outside of Raindrop sensor.
Compared with prior art, the beneficial effects of the invention are as follows：
1, the present invention realizes the wireless connection of ground control system and flight module by 5G communication modules, avoids other
Wireless device generates interference to the control of body, and makes more stablizing for data information transfer, and transmission range is farther.
2, the present invention can detect whether rainy and rainfall size by Raindrop sensor, can detect machine by temperature sensor
The temperature of body flight, the degree of balance of body flight is can detect by gyroscope, when detecting that rainy, flight temperature is higher and body
When flying unbalance, ground control system can control audible-visual annunciator to report dangerous information, to make staff that can incite somebody to action
Body is withdrawn, and largely reduces the damage of body and flight module.
3, the present invention can play airborne computer by semiconductor chilling plate the effect of temperature with high efficiency, avoid airborne meter
Calculation machine can dissipate the fever end of semiconductor chilling plate by radiator because high temperature damages or cause the reduction of its calculating speed
Heat, it is therefore prevented that the damage of semiconductor chilling plate.
4, the present invention absorbs sunlight by solar panel, by solar radiant energy by photoelectric effect or
Photochemical effect is converted directly or indirectly into electric energy, is then stored in accumulator, carries out continued power to flight module, passes through
Anti-reverse charging diode can avoid since solar panel when not generating electricity or short trouble occur at overcast and rainy and night, and accumulator is logical
Solar panel electric discharge is crossed, one-way conduction is played.
Description of the drawings
Fig. 1 is overall structure of the present invention；
Fig. 2 is monitoring modular structural schematic diagram of the present invention；
Fig. 3 is locating module structural schematic diagram of the present invention；
Fig. 4 is solar powered module structural schematic diagram of the present invention；
Fig. 5 is airborne computer of the present invention and accumulator attachment structure schematic diagram.
In figure：1- ground control systems；2- audible-visual annunciators；3-5G communication modules；4- flight modules；5- power supply modules；
6- airborne computers；7- semiconductor chilling plates；8- radiators；9- servo action modules；10- monitoring modulars；11- locating modules；
12- Raindrop sensors；13- temperature sensors；14- gyroscopes；15- baroceptors；16- light stream sensors；17- ultrasonic waves pass
Sensor；18- battery powered modules；19- solar powered modules；20- solar panels；21- anti-reverse charging diodes；22- stores
Battery；23- inverters.
Specific implementation mode
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation describes, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
- 5 are please referred to Fig.1, the present invention provides a kind of technical solution：One kind is taken photo by plane unmanned plane Intelligence Feedback control system,
Include audible-visual annunciator 2 for controlling the ground control system 1 of body state of flight, reporting for dangerous information, be used for nothing
Line data information transmitting-receiving 5G communication modules 3, for provide body high-altitude flight work flight module 4 and be used for circuit system
The power supply module 5 of power supply；
The output end of the ground control system 1 is electrically connected the input terminal of audible-visual annunciator 2, and ground control system 1
It is also wirelessly connected by 5G communication modules 3 and flight module 4, the output end of the power supply module 5 and the circuit system of flight module 4
System is electrically connected；
The flight module 4 includes the airborne computer 6 converted for data-signal, for cooling down to airborne computer 6
Semiconductor chilling plate 7, for semiconductor chilling plate 7 send out hot-side heat dissipation radiator 8, for drive body fly servo
Action module 9, the monitoring modular 10 for flight environment of vehicle prospecting and the locating module 11 for the confirmation of body flight position, it is described
The output end of radiator 8 is connect with the fever end of semiconductor chilling plate 7, the refrigeration end of the semiconductor chilling plate 7 and airborne meter
Calculation machine 6 connects, and the output end of airborne computer 6 is electrically connected semiconductor chilling plate 7, radiator 8 and servo action module 9
Input terminal, the monitoring modular 10 and the output end of locating module 11 are electrically connected with the input terminal of airborne computer 6.
The monitoring modular 10 includes for detecting the Raindrop sensor 12 of Weather information, the temperature for detecting flight temperature
Spend sensor 13 and the gyroscope 14 for detecting body flight attitude, the Raindrop sensor 12, temperature sensor 13 and top
The output end of spiral shell instrument 14 is electrically connected the input terminal of airborne computer 6, is believed the environment that body flies by monitoring modular 10
Breath is detected.
The Raindrop sensor 12 is fixed on the top of body, makes the accuracy of detection higher of Raindrop sensor 12.
The locating module 11 includes baroceptor 15 for detecting body flying height and is used for computer position
The output end of the light stream sensor 16 of confidence breath, the baroceptor 15 and light stream sensor 16 is electrically connected airborne computer
6 input terminal can mark the position of body by locating module 11.
The locating module 11 further includes the ultrasonic sensor 17 for detecting obstacle distance, the supersonic sensing
Device 17 is electrically connected the input terminal of airborne computer 6, can prevent body from being collided with barrier by ultrasonic sensor 17.
The power supply module 5 includes that rechargeable battery power supply module 18 and for converting solar energy into electrical energy and being winged
The output end of the solar powered module 19 that row module 4 is powered, the battery powered module 18 and solar powered module 19 is equal
It is electrically connected the circuit system of flight module 4, electric energy is provided to the flight of body by power supply module 5.
The solar powered module 19 includes for absorbing the solar panel 20 of solar energy, for controlling electric current
The anti-reverse charging diode 21 of flow direction, the accumulator 22 for storing electric energy and the inverter 23 converted for electric current, the sun
The output end of energy solar panel 20 is electrically connected the input terminal of anti-reverse charging diode 21, the output end electricity of the anti-reverse charging diode 21
Property connection accumulator 22 input terminal, the output end of the accumulator 22 is electrically connected the input terminal of inverter 23, the inversion
The output end of device 23 is electrically connected the circuit system of flight module 4, and the output end of the airborne computer 6 is electrically connected accumulator
22 input terminal is powered body by the way that solar powered module 19 is sustainable.
The solar panel 20 is made of monocrystalline silicon, and sun absorbing properties are strong.
The solar panel 20 is fixed on the top of body, and is distributed in the outside of Raindrop sensor 12, makes the sun
Energy solar panel 20 obtains maximizing covering.
Operation principle：
1, the wireless connection that ground control system 1 and flight module 4 are realized by 5G communication modules 3, avoids other nothings
Line equipment generates interference to the control of body, and makes more stablizing for data information transfer, and transmission range is farther.
2, rainy and rainfall size can detect whether by Raindrop sensor 12, body can detect by temperature sensor 13
The temperature of flight can detect the degree of balance of body flight by gyroscope 14, when detecting that rainy, flight temperature is higher and body
When flying unbalance, ground control system 1 can control audible-visual annunciator 2 to report dangerous information, to make staff can
Body is withdrawn, the damage of body and flight module 4 is largely reduced.
3, the effect that can play temperature with high efficiency to airborne computer 6 by semiconductor chilling plate 7, avoids airborne computer
6, because high temperature damages or cause the reduction of its calculating speed, can dissipate the fever end of semiconductor chilling plate 7 by radiator 8
Heat, it is therefore prevented that the damage of semiconductor chilling plate 7.
4, sunlight is absorbed by solar panel 20, solar radiant energy is passed through into photoelectric effect or photochemical
It learns effect and is converted directly or indirectly into electric energy, be then stored in accumulator 22, continued power is carried out to flight module 4, is passed through
Anti-reverse charging diode 21 can avoid since solar panel 20 when not generating electricity or short trouble occur at overcast and rainy and night, electric power storage
Pond 22 is discharged by solar panel 20, plays one-way conduction.
It should be noted that herein, relational terms such as first and second and the like are used merely to a reality
Body or operation are distinguished with another entity or operation, are deposited without necessarily requiring or implying between these entities or operation
In any actual relationship or order or sequence.Moreover, the terms "include", "comprise" or its any other variant are intended to
Non-exclusive inclusion, so that the process, method, article or equipment including a series of elements is not only wanted including those
Element, but also include other elements that are not explicitly listed, or further include for this process, method, article or equipment
Intrinsic element.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
Understanding without departing from the principles and spirit of the present invention can carry out these embodiments a variety of variations, modification, replace
And modification, the scope of the present invention is defined by the appended.
Claims (9)
- The unmanned plane Intelligence Feedback control system 1. one kind is taken photo by plane, it is characterised in that：Include for controlling body state of flight Ground control system (1), the audible-visual annunciator (2) for dangerous information report, the 5G communications for wireless data information transmitting-receiving Module (3), the flight module (4) for providing body high-altitude flight work and the power supply module (5) powered for circuit system；The output end of the ground control system (1) is electrically connected the input terminal of audible-visual annunciator (2), and ground control system (1) it is also wirelessly connected by 5G communication modules (3) and flight module (4), output end and the flight module of the power supply module (5) (4) circuit system is electrically connected；The flight module (4) includes the airborne computer (6) converted for data-signal, for being dropped to airborne computer (6) The semiconductor chilling plate (7) of temperature is used to send out the radiator (8) of hot-side heat dissipation, for driving body to fly to semiconductor chilling plate (7) Capable servo action module (9) is determined for the monitoring modular (10) of flight environment of vehicle prospecting and for what body flight position confirmed Position module (11), the output end of the radiator (8) are connect with the fever end of semiconductor chilling plate (7), the semiconductor refrigerating The refrigeration end of piece (7) is connect with airborne computer (6), and the output end of airborne computer (6) is electrically connected semiconductor chilling plate (7), the input terminal of radiator (8) and servo action module (9), the output end of the monitoring modular (10) and locating module (11) It is electrically connected with the input terminal of airborne computer (6).
- The unmanned plane Intelligence Feedback control system 2. one kind according to claim 1 is taken photo by plane, it is characterised in that：The monitoring Module (10) include for detecting the Raindrop sensor of Weather information (12), the temperature sensor (13) for detecting flight temperature With the gyroscope (14) for detecting body flight attitude, the Raindrop sensor (12), temperature sensor (13) and gyroscope (14) output end is electrically connected the input terminal of airborne computer (6).
- The unmanned plane Intelligence Feedback control system 3. one kind according to claim 2 is taken photo by plane, it is characterised in that：The raindrop Sensor (12) is fixed on the top of body.
- The unmanned plane Intelligence Feedback control system 4. one kind according to claim 3 is taken photo by plane, it is characterised in that：The positioning Module (11) includes for detecting the baroceptor of body flying height (15) and for the light stream of computer body location information The output end of sensor (16), the baroceptor (15) and light stream sensor (16) is electrically connected airborne computer (6) Input terminal.
- The unmanned plane Intelligence Feedback control system 5. one kind according to claim 4 is taken photo by plane, it is characterised in that：The positioning Module (11) further includes for detecting the ultrasonic sensor of obstacle distance (17), and the ultrasonic sensor (17) electrically connects Connect the input terminal of airborne computer (6).
- The unmanned plane Intelligence Feedback control system 6. one kind according to claim 5 is taken photo by plane, it is characterised in that：The power supply Module (5) includes that rechargeable battery power supply module (18) and for converting solar energy into electrical energy and being supplied for flight module (4) The output end of the solar powered module (19) of electricity, the battery powered module (18) and solar powered module (19) is electrical Connect the circuit system of flight module (4).
- The unmanned plane Intelligence Feedback control system 7. one kind according to claim 6 is taken photo by plane, it is characterised in that：The sun Energy power supply module (19) includes for absorbing the solar panel of solar energy (20), the anti-reverse charging for controlling current direction Diode (21), the accumulator (22) for storing electric energy and the inverter (23) converted for electric current, the solar cell The output end of plate (20) is electrically connected the input terminal of anti-reverse charging diode (21), the output end electricity of the anti-reverse charging diode (21) Property connection accumulator (22) input terminal, the output end of the accumulator (22) is electrically connected the input terminal of inverter (23), institute The output end for stating inverter (23) is electrically connected the circuit system of flight module (4), the output end electricity of the airborne computer (6) Property connection accumulator (22) input terminal.
- The unmanned plane Intelligence Feedback control system 8. one kind according to claim 7 is taken photo by plane, it is characterised in that：The sun Energy solar panel (20) is made of monocrystalline silicon.
- The unmanned plane Intelligence Feedback control system 9. one kind according to claim 8 is taken photo by plane, it is characterised in that：The sun Energy solar panel (20) is fixed on the top of body, and is distributed in the outside of Raindrop sensor (12).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810416661.0A CN108454831A (en) | 2018-05-03 | 2018-05-03 | One kind is taken photo by plane unmanned plane Intelligence Feedback control system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810416661.0A CN108454831A (en) | 2018-05-03 | 2018-05-03 | One kind is taken photo by plane unmanned plane Intelligence Feedback control system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108454831A true CN108454831A (en) | 2018-08-28 |
Family
ID=63215054
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810416661.0A Pending CN108454831A (en) | 2018-05-03 | 2018-05-03 | One kind is taken photo by plane unmanned plane Intelligence Feedback control system |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112255655A (en) * | 2020-08-24 | 2021-01-22 | 江苏中智腾飞信息科技有限公司 | Unmanned aerial vehicle positioning system based on 5G network |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN112255655A (en) * | 2020-08-24 | 2021-01-22 | 江苏中智腾飞信息科技有限公司 | Unmanned aerial vehicle positioning system based on 5G network |
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