CN110803282A - Detection positioning type unmanned aerial vehicle and operating system thereof - Google Patents
Detection positioning type unmanned aerial vehicle and operating system thereof Download PDFInfo
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- CN110803282A CN110803282A CN201911178100.2A CN201911178100A CN110803282A CN 110803282 A CN110803282 A CN 110803282A CN 201911178100 A CN201911178100 A CN 201911178100A CN 110803282 A CN110803282 A CN 110803282A
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- 238000001514 detection method Methods 0.000 title claims abstract description 15
- 238000003860 storage Methods 0.000 claims abstract description 52
- 230000005540 biological transmission Effects 0.000 claims abstract description 40
- 238000001179 sorption measurement Methods 0.000 claims abstract description 25
- 229920000742 Cotton Polymers 0.000 claims abstract description 19
- 230000007246 mechanism Effects 0.000 claims description 23
- 238000012544 monitoring process Methods 0.000 claims description 21
- 238000001228 spectrum Methods 0.000 claims description 16
- 238000012545 processing Methods 0.000 claims description 15
- 230000005855 radiation Effects 0.000 claims description 15
- 238000005192 partition Methods 0.000 claims description 8
- 239000000284 extract Substances 0.000 claims description 5
- 238000000034 method Methods 0.000 claims description 4
- 230000008569 process Effects 0.000 claims description 4
- 238000004140 cleaning Methods 0.000 abstract description 5
- 239000000428 dust Substances 0.000 abstract description 2
- 239000011435 rock Substances 0.000 abstract description 2
- 241000883990 Flabellum Species 0.000 description 7
- 230000002159 abnormal effect Effects 0.000 description 6
- 238000010521 absorption reaction Methods 0.000 description 6
- 238000009434 installation Methods 0.000 description 5
- 238000009826 distribution Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000005389 magnetism Effects 0.000 description 2
- 238000012546 transfer Methods 0.000 description 2
- 238000013459 approach Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000000151 deposition Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008054 signal transmission Effects 0.000 description 1
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- 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C19/00—Aircraft control not otherwise provided for
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- 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
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- 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
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- 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
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- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
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Abstract
The invention discloses a detection positioning type unmanned aerial vehicle, which comprises an unmanned aerial vehicle body, wherein unmanned aerial vehicle supporting frames are symmetrically arranged at the bottom end of the unmanned aerial vehicle body, and an unmanned aerial vehicle camera is arranged at the center of the bottom end of the unmanned aerial vehicle body, the structure of the invention is scientific and reasonable, the use is safe and convenient, the storage cover plate can be overturned through the arranged electric telescopic rod, the connecting rod, the transmission toothed chain, the first elastic connecting belt and the second elastic connecting belt, the unmanned aerial vehicle camera is stored in a storage bin, the unmanned aerial vehicle camera is stored and protected, sudden extreme weather is reduced, the damage to the camera is reduced, the camera can be cleaned through the arranged cleaning motor, the cleaning plate, the cleaning cotton, the adsorption rod and the adsorption seat, the camera shooting part of the unmanned aerial vehicle camera can be cleaned, dust and stains attached to the unmanned aerial vehicle camera can be conveniently cleaned, and the storage cover plate can be stably, avoid accomodating the apron and produce and rock, influence the use.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to a detection positioning type unmanned aerial vehicle and an operating system thereof.
Background
Unmanned aerial vehicle is called unmanned aerial vehicle for short, it is the unmanned aerial vehicle who utilizes radio remote control equipment and self-contained program control device to control, or by the on-vehicle computer independently operate completely or intermittently, unmanned aerial vehicle is because advantages such as its control is stable, but unmanned aerial vehicle receives people's liking widely, but unmanned aerial vehicle is in the use, at the airport, place such as military control area all are forbidden to fly, the user then ignores this point easily when using unmanned aerial vehicle, consequently need design an unmanned aerial vehicle and operating system to the no-fly region carries out monitoring, monitor the unmanned aerial vehicle that gets into in the guard area scope.
Disclosure of Invention
The technical scheme provided by the invention can effectively solve the problems that the places such as airports, military control areas and the like are forbidden to fly and users are easy to ignore the situation when using the unmanned aerial vehicle, which are provided by the background technology.
In order to achieve the purpose, the invention provides the following technical scheme: a detection positioning type unmanned aerial vehicle comprises an unmanned aerial vehicle body, wherein unmanned aerial vehicle support frames are symmetrically installed at the bottom end of the unmanned aerial vehicle body, and an unmanned aerial vehicle camera is installed in the center of the bottom end of the unmanned aerial vehicle body;
the storage protection mechanism is arranged at the joint of the unmanned aerial vehicle body and the unmanned aerial vehicle camera and comprises a storage bin, an electric telescopic rod, a connecting plate, a mounting groove, a transmission gear, a transmission toothed chain, a connecting rod, a first elastic connecting belt, an arc-shaped bump, a second elastic connecting belt, a guide wheel, a fixing block and a storage cover plate;
the bottom end of the unmanned aerial vehicle body is provided with a containing bin corresponding to the outer side position of the unmanned aerial vehicle camera, the bottom end of the unmanned aerial vehicle body is connected with an electric telescopic rod corresponding to the inner position of the containing bin, the bottom end of the electric telescopic rod is provided with a connecting plate, the outer side of the connecting plate is provided with a mounting groove, the inner wall of the mounting groove is symmetrically and rotatably provided with transmission gears, the outer sides of the two transmission gears are meshed and connected with transmission toothed chains, the outer sides of the transmission toothed chains are provided with connecting rods corresponding to the inner position of the containing bin, the bottom end of the connecting rods is connected with a first elastic connecting belt, the bottom end of the containing bin is provided with an arc-shaped lug corresponding to the position of the first elastic connecting belt, the outer sides of the transmission toothed chains are connected with, a storage cover plate is rotatably arranged at the bottom end of the storage bin, and a fixed block is connected to the top end of the storage cover plate;
electric telescopic handle's input electric connection unmanned aerial vehicle power's output.
Preferably, the other end and the fixed block fixed connection of second elastic connecting band, the other end and the bottom fixed connection who accomodates the apron of first elastic connecting band.
Preferably, the top end of the unmanned aerial vehicle body is provided with a fan blade accommodating mechanism, and the fan blade accommodating mechanism comprises an accommodating box, a partition plate, a tool accommodating cavity, a fan blade accommodating cavity, an accommodating clamp, an accommodating plate, a moving groove, an installing column, a clamping plate, a clamping cotton pad, a clamping spring and an accommodating cover plate;
the receiver is installed on the top of unmanned aerial vehicle body, the bottom inner wall connection of receiver has the baffle, the inside of receiver is separated by the baffle and is placed the chamber for the instrument and place the chamber with the flabellum, the instrument is placed the bottom inner wall in chamber and is evenly connected with and place the clamp, the flabellum is placed the inner wall fixed mounting in chamber and is placed the board, the top of placing the board has been seted up the shifting chute, the instrument is placed the one end inner wall in chamber and is corresponded shift chute below position department and be connected with the erection column, the outside slidable mounting of erection column has the grip block, the one end of grip block corresponds places board top position department and is connected with the cotton pad of centre gripping, the outside of erection column corresponds two grip block intermediate position departments and installs the centre gripping.
Preferably, place and carry out fixed mounting through the bolt between apron and the receiver, sliding connection between the outside of grip block and the shifting chute.
Preferably, the top end of the placing cover plate is provided with a wiping fixing mechanism, and the wiping fixing mechanism comprises a wiping motor, a rotating seat, a wiping plate, wiping cotton, an adsorption seat and an adsorption rod;
a wiping motor is installed at the top end of the placing cover plate, a rotating seat is installed at the bottom end of the wiping motor through a rotating shaft, a wiping plate is fixedly connected to the bottom end of the rotating seat, wiping cotton is attached to the bottom end of the wiping plate, an adsorption seat is installed at the position, corresponding to one side of the wiping motor, of the top end of the placing cover plate, and an adsorption rod is installed at the position, corresponding to the adsorption seat, of the bottom end of the unmanned aerial vehicle body;
the input end electric connection who cleans the motor is the output of unmanned aerial vehicle power.
Preferably, the bottom ends of the adsorption seat and the adsorption rod are both magnetic, and the top magnetic pole of the adsorption seat is opposite to the bottom magnetic pole of the adsorption rod.
A required operating system of a detection positioning type unmanned aerial vehicle comprises a control end, a monitoring end, an identification end and a transmission end;
the control end comprises an unmanned aerial vehicle body and remote control equipment;
the monitoring end comprises a radio monitor, a radar monitor and a visible light infrared monitor;
the identification end comprises an analysis processor, a frequency spectrum characteristic identifier and an image processing identifier;
the transmission end comprises a signal receiver and a signal transmitter;
the input of control end is connected with the output of monitoring end, the output of monitoring end is connected with the input of discernment end, the output of transmission end is connected with the input of discernment end.
According to the technical characteristics, the monitoring end comprises a radio monitor, a radar monitor and a visible light infrared monitor, the radio monitor is used for intercepting remote control signals received by the unmanned aerial vehicle through a signal detection technology, extracting relevant signal characteristics and transmitting the extracted signal characteristics, the radar monitor is used for scanning and detecting a no-fly area by using a radar and monitoring the unmanned aerial vehicle which deviates from a flight plan obviously and breaks into the flight plan, and the visible light infrared monitor is used for shooting and collecting infrared radiation information emitted from the no-fly area by adopting an infrared radiation detection technology and extracting infrared waveband information for transmission.
According to the technical characteristics, the identification end comprises an analysis processor, a spectrum feature identifier and an image processing identifier, the analysis processor is used for receiving the transmitted results of the radio monitor, the radar monitor and the visible light infrared monitor and analyzing and processing the results, the spectrum feature identifier is used for receiving the results of the radio monitor and identifying the spectrum feature information of the unmanned aerial vehicle, and the image processing identifier is used for receiving the image information and the infrared radiation information which are shot and collected and processing and identifying the image information and the infrared radiation information.
According to the technical characteristics, the transmission end comprises a signal receiver and a signal transmitter, the signal receiver specifically receives a control signal of the remote control device and transmits the control signal to the unmanned aerial vehicle body, and the signal transmitter receives the acquired image information and the acquired infrared radiation information and transmits the received information to the remote control device.
Compared with the prior art, the invention has the beneficial effects that: the invention has scientific and reasonable structure and safe and convenient use:
1. through the electric telescopic handle who sets up, the connecting rod, the transmission toothed chain, first elastic connection area and second elastic connection area, can be when electric telescopic handle contracts, drive first elastic connection area and second elastic connection area and remove, overturn the apron of accomodating, accomodate the unmanned aerial vehicle camera and get into in the storage storehouse, accomodate the protection to the unmanned aerial vehicle camera through accomodating the apron, be convenient for accomodate the protection to the unmanned aerial vehicle camera, reduce the extreme weather that appears suddenly, the damage that causes the camera.
2. Through the motor of cleaning, the cleaning plate that sets up, clean the cotton, adsorb pole and absorption seat, the motor operation is cleaned to the accessible, cleans the position of making a video recording of unmanned aerial vehicle camera, is convenient for clean adnexed dust and spot when shooing the unmanned aerial vehicle camera to through adsorbing the magnetism looks between pole and the absorption seat, can stabilize the placing to accomodating the apron, avoid accomodating the apron and produce and rock, influence the use.
3. Through the setting place the apron, place box, flabellum and place the chamber and the chamber is placed to the instrument, can place the flabellum on placing the board, through two grip blocks and centre gripping spring, can carry out the centre gripping to the flabellum and place, combine the cotton pad of centre gripping of grip block one end, can stabilize the centre gripping to the flabellum to can place the instrument and place on placing the clamp, carry out the centre gripping, be convenient for placing and depositing of flabellum and maintenance tool, it is more convenient to use.
4. The radio monitor, the radar monitor and the visible light infrared monitor are erected to monitor the distribution control area in real time, the flying-forbidden area is monitored in various modes, the monitoring effect is better, the monitored area is wider, the unmanned aerial vehicle body is controlled to fly through the remote control equipment, monitoring the area where the abnormal unmanned aerial vehicle is located, shooting the abnormal unmanned aerial vehicle by using an unmanned aerial vehicle camera, analyzing and processing shot information together with information obtained by a radio monitor, a radar monitor and a visible light infrared monitor to obtain frequency spectrum characteristic information of the unmanned aerial vehicle, longitude and latitude height information of the unmanned aerial vehicle, carrier frequency information of the unmanned aerial vehicle and remote control position information of the unmanned aerial vehicle, and classify, show on remote control equipment after arranging analysis processes's information afterwards, the efficiency of no-fly area unmanned aerial vehicle discernment is higher, and unmanned aerial vehicle monitoring effect is better.
Drawings
The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the principles of the invention and not to limit the invention.
In the drawings:
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic structural view of the stowing and guarding mechanism of the invention;
FIG. 3 is a schematic structural view of the area A in FIG. 2 according to the present invention;
FIG. 4 is a schematic structural view of a blade receiving mechanism according to the present invention;
FIG. 5 is a schematic view of the mounting structure of the clamping plate and the clamping spring according to the present invention;
FIG. 6 is a schematic view of the wiper fixture mechanism of the present invention;
FIG. 7 is a schematic diagram of the system architecture of the present invention;
FIG. 8 is a schematic diagram of the system connection of the present invention;
reference numbers in the figures: 1. an unmanned aerial vehicle body; 2. an unmanned aerial vehicle support frame; 3. an unmanned aerial vehicle camera;
4. a storage protection mechanism; 401. a storage bin; 402. an electric telescopic rod; 403. a connecting plate; 404. mounting grooves; 405. a transmission gear; 406. a transmission gear chain; 407. a connecting rod; 408. a first elastic connecting band; 409. an arc-shaped bump; 410. a second elastic connecting band; 411. a guide wheel; 412. a fixed block; 413. a storage cover plate;
5. a fan blade storage mechanism; 501. a storage box; 502. a partition plate; 503. a tool placement cavity; 504. a fan blade placing cavity; 505. placing a clamp; 506. placing the plate; 507. a moving groove; 508. mounting a column; 509. a clamping plate; 510. clamping the cotton pad; 511. a clamping spring; 512. placing a cover plate;
6. a wiping fixing mechanism; 601. wiping the motor; 602. a rotating seat; 603. wiping the board; 604. wiping cotton; 605. an adsorption seat; 606. an adsorption rod.
Detailed Description
The preferred embodiments of the present invention will be described in conjunction with the accompanying drawings, and it will be understood that they are described herein for the purpose of illustration and explanation and not limitation.
Example 1: as shown in fig. 1-6, the invention provides a technical scheme that a detection positioning type unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, unmanned aerial vehicle support frames 2 are symmetrically installed at the bottom end of the unmanned aerial vehicle body 1, and an unmanned aerial vehicle camera 3 is installed at the center of the bottom end of the unmanned aerial vehicle body 1;
a storage protection mechanism 4 is installed at the joint of the unmanned aerial vehicle body 1 and the unmanned aerial vehicle camera 3, and the storage protection mechanism 4 comprises a storage bin 401, an electric telescopic rod 402, a connecting plate 403, a mounting groove 404, a transmission gear 405, a transmission toothed chain 406, a connecting rod 407, a first elastic connecting belt 408, an arc-shaped bump 409, a second elastic connecting belt 410, a guide wheel 411, a fixing block 412 and a storage cover plate 413;
a containing bin 401 is arranged at the position, corresponding to the outer side of the unmanned aerial vehicle camera 3, of the bottom end of an unmanned aerial vehicle body 1, an electric telescopic rod 402 is connected to the position, corresponding to the inner position of the containing bin 401, of the bottom end of the unmanned aerial vehicle body 1, a connecting plate 403 is arranged at the bottom end of the electric telescopic rod 402, an installing groove 404 is formed in the outer side of the connecting plate 403, transmission gears 405 are symmetrically and rotatably installed on the inner wall of the installing groove 404, transmission toothed chains 406 are meshed and connected to the outer sides of the two transmission gears 405, a connecting rod 407 is installed at the position, corresponding to the inner position of the containing bin 401, of the outer side of the transmission toothed chains 406, a first elastic connecting belt 408 is connected to the bottom end of the connecting rod 407, an arc-shaped bump 409 is installed at the position, corresponding to the position of the outer, a storage cover 413 is rotatably mounted at the bottom end of the storage bin 401, and a fixed block 412 is connected to the top end of the storage cover 413;
electric telescopic handle 402's input electric connection unmanned aerial vehicle power's output, the other end and the fixed block 412 fixed connection of second elastic connecting band 410, the other end of first elastic connecting band 408 with accomodate the bottom fixed connection of apron 413, be convenient for connect the drive to accomodating apron 413 through first elastic connecting band 408 and second elastic connecting band 410.
The top end of the unmanned aerial vehicle body 1 is provided with a fan blade accommodating mechanism 5, and the fan blade accommodating mechanism 5 comprises an accommodating box 501, a partition plate 502, a tool accommodating cavity 503, a fan blade accommodating cavity 504, an accommodating clamp 505, an accommodating plate 506, a moving groove 507, an installation column 508, a clamping plate 509, a clamping cotton pad 510, a clamping spring 511 and an accommodating cover plate 512;
a storage box 501 is arranged at the top end of the unmanned aerial vehicle body 1, a partition plate 502 is connected with the bottom end inner wall of the storage box 501, the interior of the storage box 501 is divided into a tool placing cavity 503 and a fan blade placing cavity 504 by the partition plate 502, placing clamps 505 are evenly connected with the bottom end inner wall of the tool placing cavity 503, a placing plate 506 is fixedly arranged on the inner wall of the fan blade placing cavity 504, a moving groove 507 is arranged at the top end of the placing plate 506, an installation column 508 is connected with the inner wall of one end of the tool placing cavity 503 at a position corresponding to the lower part of the moving groove 507, a clamping plate 509 is slidably arranged on the outer side of the installation column 508, a clamping cotton pad 510 is connected with one end of the clamping plate 509 at a position corresponding to the upper part of the placing plate 506, a clamping spring 511 is arranged at the outer side of the installation column, the outer side of the clamping plate 509 is slidably connected with the moving groove 507, so that the installation and fixation between the cover plate 512 and the storage box 501 are convenient.
The top end of the placing cover plate 512 is provided with a wiping fixing mechanism 6, and the wiping fixing mechanism 6 comprises a wiping motor 601, a rotating seat 602, a wiping plate 603, wiping cotton 604, an adsorption seat 605 and an adsorption rod 606;
a wiping motor 601 is installed at the top end of the placing cover plate 512, a rotating seat 602 is installed at the bottom end of the wiping motor 601 through a rotating shaft, a wiping plate 603 is fixedly connected to the bottom end of the rotating seat 602, wiping cotton 604 is attached to the bottom end of the wiping plate 603, an adsorption seat 605 is installed at the position, corresponding to one side of the wiping motor 601, of the top end of the placing cover plate 512, and an adsorption rod 606 is installed at the position, corresponding to the adsorption seat 605, of the bottom end of the unmanned aerial vehicle body 1;
the input electric connection of wiping motor 601's output of unmanned aerial vehicle power, the bottom of adsorbing seat 605 and absorption pole 606 all has magnetism, and the top magnetic pole of adsorbing seat 605 is opposite with the bottom magnetic pole of absorption pole 606, is convenient for adsorb the absorption between seat 605 and the absorption pole 606.
Example 2: as shown in fig. 7-8, the present invention provides a technical solution, a required operating system for detecting a positioning type unmanned aerial vehicle, which includes a control end, a monitoring end, an identification end and a transmission end;
the control end comprises an unmanned aerial vehicle body and remote control equipment;
the monitoring end comprises a radio monitor, a radar monitor and a visible light infrared monitor;
the identification end comprises an analysis processor, a frequency spectrum characteristic identifier and an image processing identifier;
the transmission end comprises a signal receiver and a signal transmitter;
the input end of the control end is connected with the output end of the monitoring end, the output end of the monitoring end is connected with the input end of the identification end, and the output end of the transmission end is connected with the input end of the identification end.
According to the technical characteristics, the monitoring end includes radio monitor, radar monitor and visible light infrared monitor, radio monitor is the passing signal detection technique, the remote control signal to unmanned aerial vehicle receipt is intercepted, and extract relevant signal characteristic, the signal characteristic that will extract is transmitted, radar monitor is that use the radar to carry out scanning detection to the no-fly area, the unmanned aerial vehicle to obviously deviating flight plan and break into is monitored, visible light infrared monitor is that adopt infrared radiation detection technique, the infrared radiation information that gives off in the no-fly area is shot and is gathered, and extract infrared wave band information and transmit.
According to the technical characteristics, the identification end comprises an analysis processor, a spectrum characteristic identifier and an image processing identifier, the analysis processor is used for receiving the transmitted results of the radio monitor, the radar monitor and the visible light infrared monitor, converting the received signal data into electric signals and analyzing and processing the results, the spectrum characteristic identifier is used for receiving the results of the radio monitor, analyzing and calculating the wave band and spectrum information in the received radio data and identifying the spectrum characteristic information of the unmanned aerial vehicle, and the image processing identifier is used for receiving the shot and collected image information and infrared radiation information and processing and identifying the image information and the infrared radiation information.
According to above-mentioned technical characteristics, the transmission end includes signal receiver and signal transfer ware, and signal receiver specifically refers to the control signal who receives remote control equipment to control signal transmission to the unmanned aerial vehicle body, signal transfer ware refers to the image information and the infrared radiation information that receive and transmit the information of receiving to remote control equipment.
The working principle and the using process of the invention are as follows: when the unmanned aerial vehicle is used, when the electric telescopic rod 402 contracts, the connecting plate 403 and the unmanned aerial vehicle camera 3 can be driven to move upwards, the connecting rod 407 is driven to move downwards, the transmission toothed chain 406 is driven to move, when the transmission toothed chain 406 moves, the first elastic connecting belt 408 and the second elastic connecting belt 410 can be driven to move, the first elastic connecting belt 408 and the second elastic connecting belt 410 are conducted by combining the installed guide wheel 411 and the arc-shaped bump 409, the accommodating cover plate 413 can be driven to turn over, and when the unmanned aerial vehicle camera 3 is accommodated into the accommodating bin 401, the unmanned aerial vehicle camera 3 is accommodated and protected through the accommodating cover plate 413;
after the unmanned aerial vehicle camera 3 is stored in the storage bin 401, the unmanned aerial vehicle camera 3 can be manually controlled to rotate, the camera shooting part of the unmanned aerial vehicle camera 3 is rotated to be directed under, the rotating seat 602 and the wiping plate 603 can be driven to rotate through the rotating shaft, the camera shooting part of the unmanned aerial vehicle camera 3 is wiped through the wiping cotton 604 at the bottom end of the wiping plate 603, when the unmanned aerial vehicle camera 3 is used, the storage cover plate 413 can be stably placed through magnetic attraction between the adsorption rod 606 and the adsorption seat 605, and the storage cover plate 413 is prevented from shaking to influence use;
when the unmanned aerial vehicle body 1 is damaged or needs to be maintained, the placing cover plate 512 can be taken down from the storage box 501, the fan blades placed in the fan blade placing cavity 504 and tools stored in the tool placing cavity 503 can be taken out, the fan blades can be placed on the placing plate 506 when the fan blades need to be stored, the fan blades can be clamped and placed through the two clamping plates 509 and the clamping springs 511, and the fan blades can be stably clamped by combining the clamping cotton pads 510 at one ends of the clamping plates 509, so that the fan blades can be conveniently placed and stored;
when the operation system of the detection positioning type unmanned aerial vehicle is used, firstly, a user sets up a radio monitor, a radar monitor and a visible light infrared monitor according to the area size of a distribution control area, real-time monitoring is carried out on the distribution control area, when the radio monitor, the radar monitor and the visible light infrared monitor reach an abnormal unmanned aerial vehicle, the user can control the unmanned aerial vehicle body to fly through a remote control device, the area where the abnormal unmanned aerial vehicle is located is monitored, when the unmanned aerial vehicle body approaches the abnormal unmanned aerial vehicle, the abnormal unmanned aerial vehicle is shot through an unmanned aerial vehicle camera, shot information can be transmitted to an analysis processor together with information from the radio monitor, the radar monitor and the visible light infrared monitor to be analyzed, the acquired information is transmitted to a spectrum characteristic recognizer and an image processing recognizer, and the spectrum characteristic information of the unmanned aerial vehicle is analyzed, Unmanned aerial vehicle longitude and latitude height information, unmanned aerial vehicle carrier frequency information and unmanned aerial vehicle remote control position information to categorised, show on the remote control equipment after arranging analysis processes' information afterwards.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that changes may be made in the embodiments and/or equivalents thereof without departing from the spirit and scope of the invention. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (10)
1. The utility model provides a survey location type unmanned aerial vehicle, includes unmanned aerial vehicle body (1), its characterized in that: an unmanned aerial vehicle support frame (2) is symmetrically installed at the bottom end of the unmanned aerial vehicle body (1), and an unmanned aerial vehicle camera (3) is installed at the center of the bottom end of the unmanned aerial vehicle body (1);
a storage protection mechanism (4) is installed at the joint of the unmanned aerial vehicle body (1) and the unmanned aerial vehicle camera (3), and the storage protection mechanism (4) comprises a storage bin (401), an electric telescopic rod (402), a connecting plate (403), a mounting groove (404), a transmission gear (405), a transmission toothed chain (406), a connecting rod (407), a first elastic connecting belt (408), an arc-shaped bump (409), a second elastic connecting belt (410), a guide wheel (411), a fixing block (412) and a storage cover plate (413);
the bottom of the unmanned aerial vehicle body (1) corresponds to the outer side position of the unmanned aerial vehicle camera (3) and is provided with a storage bin (401), the bottom of the unmanned aerial vehicle body (1) corresponds to the inner side position of the storage bin (401) and is connected with an electric telescopic rod (402), the bottom of the electric telescopic rod (402) is provided with a connecting plate (403), the outer side of the connecting plate (403) is provided with a mounting groove (404), the inner wall of the mounting groove (404) is symmetrically and rotatably provided with a transmission gear (405), the outer sides of the two transmission gears (405) are meshed and connected with a transmission toothed chain (406), the outer side of the transmission toothed chain (406) corresponds to the inner side position of the storage bin (401) and is provided with a connecting rod (407), the bottom of the connecting rod (407) is connected with a first elastic connecting belt (408), the bottom of the storage bin (401, a second elastic connecting belt (410) is connected to the outer side of the transmission toothed chain (406) corresponding to the outer side of the storage bin (401), a guide wheel (411) is connected to the outer side of the storage bin (401) corresponding to the second elastic connecting belt (410), a storage cover plate (413) is rotatably mounted at the bottom end of the storage bin (401), and a fixing block (412) is connected to the top end of the storage cover plate (413);
the input end of the electric telescopic rod (402) is electrically connected with the output end of the unmanned aerial vehicle power supply.
2. The unmanned aerial vehicle of claim 1, wherein the other end of the second elastic connecting band (410) is fixedly connected with a fixing block (412), and the other end of the first elastic connecting band (408) is fixedly connected with the bottom end of the storage cover plate (413).
3. The unmanned aerial vehicle of claim 1, wherein a fan blade storage mechanism (5) is mounted at the top end of the unmanned aerial vehicle body (1), and the fan blade storage mechanism (5) comprises a storage box (501), a partition plate (502), a tool placement cavity (503), a fan blade placement cavity (504), a placement clamp (505), a placement plate (506), a moving groove (507), a mounting column (508), a clamping plate (509), a clamping cotton pad (510), a clamping spring (511) and a placement cover plate (512);
the unmanned aerial vehicle comprises an unmanned aerial vehicle body (1), a storage box (501) is installed at the top end of the unmanned aerial vehicle body (1), a partition plate (502) is connected to the inner wall of the bottom end of the storage box (501), the interior of the storage box (501) is divided into an tool placing cavity (503) and a fan blade placing cavity (504) by the partition plate (502), a placing clamp (505) is evenly connected to the inner wall of the bottom end of the tool placing cavity (503), a placing plate (506) is fixedly installed on the inner wall of the fan blade placing cavity (504), a moving groove (507) is formed in the top end of the placing plate (506), an installing column (508) is connected to the position, corresponding to the moving groove (507), of the inner wall of one end of the tool placing cavity (503), a clamping plate (509) is slidably installed on the outer side of the installing column, a clamping spring (511) is installed at the position, corresponding to the upper position of the placing plate (506), and a clamping cotton, the top end of the storage box (501) is provided with a placing cover plate (512).
4. The unmanned aerial vehicle of claim 3, wherein the placing cover plate (512) is fixedly installed on the storage box (501) through bolts, and the outer side of the clamping plate (509) is slidably connected with the moving groove (507).
5. The unmanned aerial vehicle of claim 3, wherein a wiping fixing mechanism (6) is installed at the top end of the placing cover plate (512), and the wiping fixing mechanism (6) comprises a wiping motor (601), a rotating seat (602), a wiping plate (603), a wiping cotton (604), an adsorption seat (605) and an adsorption rod (606);
a wiping motor (601) is installed at the top end of the placing cover plate (512), a rotating seat (602) is installed at the bottom end of the wiping motor (601) through a rotating shaft, a wiping plate (603) is fixedly connected to the bottom end of the rotating seat (602), wiping cotton (604) is attached to the bottom end of the wiping plate (603), an adsorption seat (605) is installed at the position, corresponding to one side of the wiping motor (601), of the top end of the placing cover plate (512), and an adsorption rod (606) is installed at the position, corresponding to the adsorption seat (605), of the bottom end of the unmanned aerial vehicle body (1);
the input end of the wiping motor (601) is electrically connected with the output end of the unmanned aerial vehicle power supply.
6. The unmanned aerial vehicle of claim 5, wherein the bottom ends of the suction base (605) and the suction rod (606) are magnetic, and the magnetic poles of the top end of the suction base (605) and the magnetic poles of the bottom end of the suction rod (606) are opposite.
7. The system for detecting the required operation of the positioning type unmanned aerial vehicle according to any one of claims 1 to 6, characterized by comprising a control end, a monitoring end, an identification end and a transmission end;
the control end comprises an unmanned aerial vehicle body and remote control equipment;
the monitoring end comprises a radio monitor, a radar monitor and a visible light infrared monitor;
the identification end comprises an analysis processor, a frequency spectrum characteristic identifier and an image processing identifier;
the transmission end comprises a signal receiver and a signal transmitter;
the input of control end is connected with the output of monitoring end, the output of monitoring end is connected with the input of discernment end, the output of transmission end is connected with the input of discernment end.
8. The system of claim 7, wherein the monitoring end comprises a radio monitor, a radar monitor and a visible light infrared monitor, the radio monitor intercepts the remote control signal received by the unmanned aerial vehicle through a signal detection technology, extracts relevant signal features, and transmits the extracted signal features, the radar monitor scans and detects a no-fly area by using a radar to monitor the unmanned aerial vehicle which deviates from a flight plan and breaks into the flight plan, and the visible light infrared monitor photographs and collects infrared radiation information emitted from the no-fly area by using an infrared radiation detection technology and extracts infrared band information for transmission.
9. The system according to claim 7, wherein the identification terminal includes an analysis processor, a spectrum feature identifier and an image processing identifier, the analysis processor is configured to receive the transmitted results of the radio monitor, the radar monitor and the visible light infrared monitor and analyze the results, the spectrum feature identifier is configured to receive the results of the radio monitor and identify the spectrum feature information of the drone therefrom, and the image processing identifier is configured to receive the captured image information and the captured infrared radiation information and process and identify the image information and the infrared radiation information.
10. The system of claim 7, wherein the transmission end comprises a signal receiver and a signal transmitter, the signal receiver specifically receives a control signal from a remote control device and transmits the control signal to the main body of the drone, and the signal transmitter receives the collected image information and infrared radiation information and transmits the received information to the remote control device.
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