CN111026158A - Unmanned aerial vehicle monitoring platform based on radar - Google Patents
Unmanned aerial vehicle monitoring platform based on radar Download PDFInfo
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- CN111026158A CN111026158A CN201911345932.9A CN201911345932A CN111026158A CN 111026158 A CN111026158 A CN 111026158A CN 201911345932 A CN201911345932 A CN 201911345932A CN 111026158 A CN111026158 A CN 111026158A
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- 238000012544 monitoring process Methods 0.000 title claims abstract description 88
- 239000004744 fabric Substances 0.000 claims abstract description 18
- 238000010248 power generation Methods 0.000 claims abstract description 7
- 229920003023 plastic Polymers 0.000 claims description 41
- 239000004033 plastic Substances 0.000 claims description 41
- 230000000694 effects Effects 0.000 claims description 10
- 238000009826 distribution Methods 0.000 claims description 3
- 230000007123 defense Effects 0.000 description 13
- 238000010586 diagram Methods 0.000 description 5
- 230000009471 action Effects 0.000 description 4
- 238000013461 design Methods 0.000 description 3
- 230000001105 regulatory effect Effects 0.000 description 3
- 230000001276 controlling effect Effects 0.000 description 2
- 239000002699 waste material Substances 0.000 description 2
- 238000013527 convolutional neural network Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 239000003814 drug Substances 0.000 description 1
- 229940079593 drug Drugs 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/02—Heads
- F16M11/04—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/20—Undercarriages with or without wheels
- F16M11/24—Undercarriages with or without wheels changeable in height or length of legs, also for transport only, e.g. by means of tubes screwed into each other
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/88—Radar or analogous systems specially adapted for specific applications
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- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
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- Mechanical Engineering (AREA)
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- Computer Networks & Wireless Communication (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Photovoltaic Devices (AREA)
Abstract
The invention discloses an unmanned aerial vehicle monitoring platform based on a radar, which comprises an unmanned aerial vehicle monitoring platform, wherein an adjusting and supporting device is installed below the unmanned aerial vehicle monitoring platform, a controller is installed on the lower surface of the unmanned aerial vehicle monitoring platform, a flying device is installed above the unmanned aerial vehicle monitoring platform, and adjusting type solar power generation devices are installed on two sides of the unmanned aerial vehicle monitoring platform. Through the rotation of brushless motor drive rotary wing, thereby drive unmanned aerial vehicle monitoring platform and fly, make the quick cloth of carrying on of unmanned aerial vehicle monitoring platform prevent, thereby the effectual required time of cloth of having practiced thrift, the cooperation through rotatory sleeve axle and rotation axis drives the flexible sleeve pipe with flexible pipe flexible, thereby quick completion flexible solar module's shrink, through turning into solar energy the electric energy, can effectual extension operating time, and through flexible solar module, can effectual reduction device's weight itself.
Description
Technical Field
The invention relates to the related field of unmanned aerial vehicle positioning and tracking, in particular to an unmanned aerial vehicle monitoring platform based on radar.
Background
At present, unmanned aerial vehicles in China are in the first echelon with the United states and European countries represented by the United kingdom and the France, regardless of civil use or military use, and the market share of consumption-level civil unmanned aerial vehicles in China accounts for more than 70% of the global market. However, unmanned aerial vehicles also bring a series of unsafe problems such as peeking at privacy crisis, falling of goods transported by unmanned aerial vehicles, and smuggling of drugs in frontier of unmanned aerial vehicles.
In patent CN 201810957784.5-positioning and tracking method and system for fast moving civil multi-rotor unmanned aerial vehicle, a pan tilt radar camera is used to detect and pick up images of a target, a convolutional neural network is used to identify the target, the characteristics of the unmanned aerial vehicle are updated dynamically at intervals (i.e. the characteristics are updated by key frames and transmitted by non-key frames), a laser radar is used to perform accurate distance measurement on the target, and a CCD camera is used to perform real-time tracking and shooting, so that the object tracking is more stable and accurate, and real-time tracking is achieved.
And in large-scale activity, often need ensure the safety of activity and go on, need carry out unmanned aerial vehicle monitoring and control, and control are motor-driven formula control and control, and current equipment when control and control, can waste a large amount of time and carry out the installation distribution of equipment, can't quick completion control and control.
Disclosure of Invention
The invention aims to solve the problems, and designs an unmanned aerial vehicle monitoring platform based on a radar, which has the function of high deployment and control speed, solves the problem that the existing unmanned aerial vehicle monitoring platform needs manual assistance to deploy and control during deployment and control and wastes a large amount of time.
The technical scheme of the invention is that the radar-based unmanned aerial vehicle monitoring platform comprises an unmanned aerial vehicle monitoring platform, wherein an adjusting and supporting device is arranged below the unmanned aerial vehicle monitoring platform, a controller is arranged on the lower surface of the unmanned aerial vehicle monitoring platform, a flying device is arranged above the unmanned aerial vehicle monitoring platform, and adjusting solar power generation devices are arranged on two sides of the unmanned aerial vehicle monitoring platform;
the flying device comprises an unmanned aerial vehicle monitoring platform, rotor wing branch pipes are mounted at four corners of the outer surface of the unmanned aerial vehicle monitoring platform, a motor base is mounted at one end of each rotor wing branch pipe, a brushless motor is mounted inside the motor base, a rotating wing is mounted at a rotating end of the brushless motor, a storage battery box is mounted at the center inside the unmanned aerial vehicle monitoring platform, a first storage battery pack is mounted at one side inside the storage battery box, a second storage battery pack is mounted at the other side inside the storage battery box, a photovoltaic inverter is mounted above the first storage battery pack, a three-coordinate phased array radar is mounted on the lower surface of the storage battery box;
the adjustable solar power generation device comprises an unmanned aerial vehicle monitoring platform, wherein telescopic grooves are formed in two ends of the side surface of each side of the unmanned aerial vehicle monitoring platform, a micro motor is arranged in each telescopic groove, a rotating sleeve shaft is arranged at the rotating end of each micro motor, a plurality of rotating shafts are arranged in each rotating sleeve shaft, the rotating shafts are sequentially sleeved in the rotating sleeve shafts, the rotating sleeve shafts are limited through a first limiting slider, the rotating shafts and the rotating shafts are limited through a second limiting slider, telescopic sleeves are arranged in the telescopic grooves, a plurality of telescopic pipes are arranged in the telescopic sleeves, the telescopic pipes are sequentially sleeved in the telescopic sleeves, one telescopic pipe is in threaded connection with the telescopic sleeves, the telescopic pipes are in threaded connection with the telescopic sleeves, the number of the telescopic pipes and the number of the rotating shafts are the same, and the telescopic pipes in adjacent two threaded connections are limited, install the soft cloth of plastics on the surface of unmanned aerial vehicle monitoring platform both sides side, install flexible solar module on the soft cloth of plastics, connect through axle sleeve and two sets of plastics axles between the soft cloth of plastics, two sets of crisscross distributions of plastics axle, the plastics lantern ring is installed at the both ends of one set of plastics axle wherein, the plastics lantern ring suit is on flexible pipe, the plastics ring of outer end and the flexible pipe fixed connection of inner most, install the elasticity rope between another set of plastics axle, the elasticity rope is located the both ends of plastics axle.
Adjust strutting arrangement and include battery box upper surface center department installs horizontal sensor, adjusting sleeve is installed to the motor base below, adjusting sleeve internally mounted has adjusting motor, adjusting motor's rotatory end is installed the regulating spindle, the regulation screwed pipe is installed to the lower extreme of regulating spindle, adjusting screwed pipe and adjusting sleeve threaded connection, the hollow ball that moves about is installed to the lower extreme of adjusting screwed pipe, the support base is installed to the below of hollow ball that moves about, support base and hollow ball swing joint move about.
The photovoltaic inverter is electrically connected with the storage battery pack.
And the flexible solar cell modules are electrically connected with the photovoltaic inverter after being connected in series.
The charging interface is arranged on the upper surface of the storage battery box and is electrically connected with the storage battery pack II.
The rotating shaft is connected with the rotating sleeve shaft in a sliding mode, and the rotating shaft is connected with the rotating sleeve shaft in a sliding mode.
The three-coordinate phased array radar is connected with the first storage battery pack through a miniature transformer.
The controller is connected with an external remote control device through wireless signals.
The radar-based unmanned aerial vehicle monitoring platform manufactured by the technical scheme of the invention comprises the following steps:
according to the unmanned aerial vehicle monitoring platform, the brushless motor drives the rotary wings to rotate, so that the unmanned aerial vehicle monitoring platform is driven to fly, and the unmanned aerial vehicle monitoring platform can quickly perform defense deployment, so that the time required by the defense deployment is effectively saved, manual operation is reduced, and the device is more rapid and convenient to use;
according to the unmanned aerial vehicle monitoring platform, the telescopic sleeve and the telescopic pipe are driven to stretch through the matching of the rotary sleeve shaft and the rotary shaft, so that the flexible solar cell module is quickly contracted, solar energy is converted into electric energy through the flexible solar cell module, the working time of the device can be effectively prolonged, the device can normally run when large-scale activities are carried out, the weight of the device can be effectively saved through the flexible solar cell module, and the unmanned aerial vehicle monitoring platform can be ensured to smoothly fly and lay;
this unmanned aerial vehicle monitoring platform, through the cooperation of level sensor, accommodate motor, adjusting sleeve and regulation screwed pipe to through activity clean shot and support base, thereby make unmanned aerial vehicle monitoring platform when the defence, support that can be quick, can guarantee unmanned aerial vehicle monitoring platform's stationarity again simultaneously.
Drawings
Fig. 1 is a schematic structural diagram of a radar-based unmanned aerial vehicle monitoring platform according to the present invention;
FIG. 2 is a schematic structural diagram of a radar-based UAV monitoring platform according to the present invention;
FIG. 3 is a schematic structural diagram of a radar-based UAV monitoring platform according to the present invention;
FIG. 4 is a schematic structural diagram of a radar-based UAV monitoring platform according to the present invention;
FIG. 5 is a schematic structural diagram of a radar-based UAV monitoring platform according to the present invention;
in the figure, 1, an unmanned aerial vehicle monitoring platform; 2. a controller; 3. a rotor branch pipe; 4. a motor base; 5. a brushless motor; 6. a rotary wing; 7. a battery case; 8. a first storage battery pack; 9. a second storage battery pack; 10. a photovoltaic inverter; 11. a three-coordinate phased array radar; 12. a high-definition camera; 13. a telescopic groove; 14. a micro motor; 15. rotating the sleeve shaft; 16. a rotating shaft; 17. a first limiting sliding block; 18. a second limiting sliding block; 19. a telescopic sleeve; 20. a telescopic pipe; 21. a limit stop block; 22. plastic soft cloth; 23. a flexible solar cell assembly; 24. a shaft sleeve; 25. a plastic shaft; 26. a plastic collar; 27. an elastic cord; 28. a level sensor; 29. an adjustment sleeve; 30. adjusting the motor; 31. an adjustment shaft; 32. adjusting the threaded pipe; 33. a movable hollow sphere; 34. a support base; 35. a charging interface; 36. a micro-transformer.
Detailed Description
The invention is described in detail below with reference to the accompanying drawings, as shown in FIG. 1, in this embodiment:
in the device, the device supplies power through a first storage battery pack 8 and a second storage battery pack 9, the second storage battery pack 9 is connected with an external power supply through a charging interface 35 and an external charger for charging, the second storage battery pack 9 is electrically connected with a controller 2, a brushless motor 5 and an adjusting motor 30 for supplying power, the first storage battery pack 8 converts solar energy into electric energy through a flexible solar battery assembly 23 and charges the first storage battery pack 8 under the action of a photovoltaic inverter 10, the first storage battery pack 8 supplies power through being electrically connected with a three-coordinate phased array radar 11, a high-definition camera 12 and a micro motor 14, the controller 2 is a FX2N-16EYT type PLC controller, a control signal output end of the controller 2 is electrically connected with the brushless motor 5, the three-coordinate phased array radar 11, the camera 12, the micro motor 14 and the adjusting motor 30 through transistors respectively, the signal receiving terminal of the controller 2 is electrically connected to the signal transmitting terminal of the level sensor 28 through a transistor, thereby controlling the operation of the apparatus.
The invention is characterized in the structural design of a flying device, and by combining the attached drawings, the flying device comprises an unmanned aerial vehicle monitoring platform 1, wherein rotor branch pipes 3 are arranged at four corners of the outer surface of the unmanned aerial vehicle monitoring platform 1, a motor base 4 is arranged at one end of each rotor branch pipe 3, a brushless motor 5 is arranged in each motor base 4, a rotating wing 6 is arranged at the rotating end of each brushless motor 5, a storage battery box 7 is arranged at the center of the inside of the unmanned aerial vehicle monitoring platform 1, a first storage battery pack 8 is arranged at one side of the inside of each storage battery box 7, a second storage battery pack 9 is arranged at the other side of the inside of each storage battery box 7, a photovoltaic inverter 10 is arranged above the first storage battery pack 8; drive high-speed rotation of rotor 6 through brushless motor 5, thereby make unmanned aerial vehicle monitoring platform 1 can fly, thereby the effectual time of having saved to large-scale activity cloth defense, it is simple more fast to make cloth defense, carry out two-way power supply through storage battery 8 and storage battery two 9 simultaneously, thereby the required electric energy of effectual assurance unmanned aerial vehicle monitoring platform 1 flight, make the more simple and convenient of device control, avoided three-coordinate phased array radar 11 and camera 12 power consumption too much and lead to the problem that unmanned aerial vehicle monitoring platform 1 can't fly.
The invention is characterized in that the structure design of the adjustable solar power generation device is combined with the attached drawing, the adjustable solar power generation device comprises an unmanned aerial vehicle monitoring platform 1, telescopic grooves 13 are formed in two ends of the side surfaces of two sides of the unmanned aerial vehicle monitoring platform 1, micro motors 14 are installed in the telescopic grooves 13, rotating sleeve shafts 15 are installed at the rotating ends of the micro motors 14, a plurality of rotating shafts 16 are arranged in the rotating sleeve shafts 15, the rotating shafts 16 are sequentially sleeved in the rotating sleeve shafts 15, the rotating sleeve shafts 15 and the rotating shafts 16 are limited through limiting sliders I17, the rotating shafts 16 and the rotating shafts 16 are limited through limiting sliders II 18, telescopic sleeves 19 are installed in the telescopic grooves 13, a plurality of telescopic pipes 20 are arranged in the telescopic sleeves 19, the telescopic pipes 20 are sequentially sleeved in the telescopic sleeves 19, one telescopic pipe 20 is in threaded connection with the telescopic sleeve 19, and, the number of the extension tubes 20 is the same as that of the rotating shaft 16, the adjacent two extension tubes 20 in threaded connection are in limited rotation through limit stops 21, the side surfaces of two sides of the unmanned aerial vehicle monitoring platform 1 are provided with plastic soft cloth 22, the plastic soft cloth 22 is provided with a flexible solar cell module 23, the plastic soft cloth 22 is connected with two groups of plastic shafts 25 through shaft sleeves 24, the two groups of plastic shafts 25 are distributed in a staggered manner, two ends of one group of plastic shafts 25 are provided with plastic lantern rings 26, the plastic lantern rings 26 are sleeved on the extension tubes 20, the plastic ring 26 at the outermost end is fixedly connected with the extension tube 20 at the innermost end, an elastic rope 27 is arranged between the other group of plastic shafts 25, and the elastic rope 27 is positioned at two ends of; convert solar energy into the electric energy through flexible solar module 23, thereby the endurance of an effectual assurance storage battery 8, make the operation that three-coordinate phased array radar 11 can be long-time, simultaneously flexible solar module 23's weight is lighter, can effectual reducing mechanism's weight, avoided the device overweight and lead to the problem that unmanned aerial vehicle monitoring platform 1 can't fly, cooperation through rotatory cover axle 15 and rotation axis 16 drives the flexible 19 and flexible 20's of telescopic tube, thereby make flexible solar module 23 can expand fast and contract, thereby make things convenient for unmanned aerial vehicle monitoring platform 1 to fly.
In this device, adjust strutting arrangement and detect the levelness of unmanned aerial vehicle monitoring platform 1 when descending through level sensor 28 to adjust the height that supports base 34 through accommodate motor 30, regulating spindle 31, regulation screwed pipe 32 and adjusting sleeve 29's cooperation, simultaneously through the loose hollow ball 33 with support base 34's swing joint, can make support base 34 can be steady support unmanned aerial vehicle monitoring platform 1.
The working principle of the device is as follows: when the unmanned aerial vehicle detection is needed, a worker determines the defense deployment position of the unmanned aerial vehicle monitoring platform 1 according to the actual situation, and after the defense deployment position of the unmanned aerial vehicle monitoring platform 1 is determined, the worker transports the unmanned aerial vehicle monitoring platform 1 to the vicinity of the defense deployment position;
the unmanned aerial vehicle monitoring platform 1 is driven to fly above a defense deployment position by the rotation of the rotary wing 6, the high-definition camera 12 is controlled to start working at the moment, the high-definition camera 12 shoots actual conditions at the defense deployment position and transmits the shot signals to the remote control device through wireless signals, and a worker descends the unmanned aerial vehicle monitoring platform 1 to a proper position by observing the actual conditions at the defense deployment position;
when the unmanned aerial vehicle monitoring platform 1 falls, the supporting base 34 is in contact with the ground at the defense deployment position, the device stably falls on the ground at the defense deployment position under the action of the movable hollow ball 33, the horizontal sensor 28 is controlled to work at the moment, the horizontal sensor 28 starts to detect the levelness of the unmanned aerial vehicle monitoring platform 1 and starts to work by controlling the corresponding adjusting motor 30, the adjusting motor 30 drives the adjusting shaft 31 to rotate, the adjusting shaft 31 drives the adjusting threaded pipe 32 to rotate, the adjusting threaded pipe 32 starts to rotate and ascend and descend through threaded connection with the adjusting sleeve 29, so that the levelness of the unmanned aerial vehicle monitoring platform 1 starts to be adjusted, and when a levelness signal monitored by the horizontal sensor 28 reaches a set value, the adjusting motor 30 and the horizontal sensor 28 are controlled to stop working at the moment;
at the moment, the micro motor 14 is controlled to start working, the micro motor 14 drives the rotary sleeve shaft 15 to start rotating, the rotary sleeve shaft 15 enables all the rotary shafts 16 to start rotating through the action of the first limit sliding blocks 17 and the second limit sliding blocks 18, the rotary shafts 16 drive all the extension tubes 20 to start rotating through the action of the limit stop blocks 21, the threaded connection between the extension tubes 20 and the extension sleeve 19 enable the extension tubes 20 to extend out of the extension sleeve 19 while rotating, the extension tubes 20 drive the plastic shafts 25 to start moving, thereby unfolding the plastic soft cloth 22, enabling the flexible solar cell module 23 on the plastic soft cloth 22 to be in contact with the solar energy, thereby charging the storage battery pack I8, enabling the storage battery pack I8 to continuously supply power to the three-coordinate phased array radar 11, meanwhile, when the plastic soft cloth 22 is unfolded, the elastic ropes 27 on the other group of plastic shafts 25 are pulled;
at the moment, the unmanned aerial vehicle monitoring platform 1 finishes defense deployment, when monitoring is needed, the three-coordinate phased array radar 11 is controlled to start working, the first storage battery pack 8 starts to supply power to the three-coordinate phased array radar 11 through voltage transformation of the miniature transformer 36, so that the three-coordinate phased array radar 11 starts to supply power, and the three-coordinate phased array radar 11 starts to monitor the unmanned aerial vehicle condition in the monitoring range of the three-coordinate phased array radar 11 through three-dimensional global automatic scanning;
when the unmanned aerial vehicle is found by scanning, a signal is sent to the remote control device, and the worker determines the position of the unmanned aerial vehicle at the moment through the information on the remote control device, so that the motor-driven personnel can interfere the signal of the unmanned aerial vehicle and force to land through the unmanned aerial vehicle interference equipment, and normal operation of large-scale activities is effectively guaranteed;
after the monitoring is finished, the micro motor 14 is controlled to start to rotate reversely, the micro motor 14 rotates reversely, the rotating sleeve shaft 15 starts to drive the rotating shaft 16 to rotate reversely, so that the telescopic pipe 20 rotates reversely, the telescopic pipe 20 contracts back into the telescopic sleeve 19 through the reverse rotation of the telescopic pipe 20, and meanwhile, the plastic soft cloth 22 starts to be folded through the elastic tension of the elastic rope 27, so that the flexible solar cell module 23 contracts;
after the flexible solar cell module 23 is completely contracted, the brushless motor 5 is controlled to start working at the moment, so that the unmanned aerial vehicle monitoring platform 1 is recovered through the rotation of the rotary wings 6, and the whole monitoring activity of the unmanned aerial vehicle is completed;
in this device, when the telescopic tube 20 is rotated and extended, the telescopic tube 20 is rotated to the outer end of the telescopic tube 20, and then the telescopic tube 20 is driven to rotate by the shielding of the limit stopper 21, so that the telescopic tube 20 can be smoothly extended and retracted.
The technical solutions described above only represent the preferred technical solutions of the present invention, and some possible modifications to some parts of the technical solutions by those skilled in the art all represent the principles of the present invention, and fall within the protection scope of the present invention.
Claims (8)
1. An unmanned aerial vehicle monitoring platform based on radar comprises an unmanned aerial vehicle monitoring platform (1), wherein an adjusting and supporting device is installed below the unmanned aerial vehicle monitoring platform (1), and a controller (2) is installed on the lower surface of the unmanned aerial vehicle monitoring platform (1), and is characterized in that a flying device is installed above the unmanned aerial vehicle monitoring platform (1), and adjusting type solar power generation devices are installed on two sides of the unmanned aerial vehicle monitoring platform (1);
the flying device comprises an unmanned aerial vehicle monitoring platform (1), rotor branch pipes (3) are arranged at four corners of the outer surface of the unmanned aerial vehicle monitoring platform, a motor base (4) is arranged at one end of the rotor wing branch pipe (3), a brushless motor (5) is arranged in the motor base (4), a rotating wing (6) is installed at the rotating end of the brushless motor (5), a storage battery box (7) is installed at the center of the interior of the unmanned aerial vehicle monitoring platform (1), a first storage battery pack (8) is arranged on one side in the storage battery box (7), a second storage battery pack (9) is arranged on the other side in the storage battery box (7), a photovoltaic inverter (10) is arranged above the first storage battery pack (8), a three-coordinate phased array radar (11) is arranged on the lower surface of the storage battery box (7), high-definition cameras (12) are mounted at two ends below the unmanned aerial vehicle monitoring platform (1);
the adjustable solar power generation device comprises an unmanned aerial vehicle monitoring platform (1), wherein telescopic grooves (13) are formed in two ends of the side surface of two sides of the unmanned aerial vehicle monitoring platform (1), micro motors (14) are installed in the telescopic grooves (13), rotating sleeves (15) are installed at the rotating ends of the micro motors (14), a plurality of rotating shafts (16) are arranged in the rotating sleeves (15), the rotating shafts (16) are sequentially sleeved in the rotating sleeves (15), the rotating sleeves (15) and the rotating shafts (16) are limited through first limiting sliders (17), the rotating shafts (16) and the rotating shafts (16) are limited through second limiting sliders (18), telescopic pipes (19) are installed in the telescopic grooves (13), a plurality of telescopic pipes (20) are arranged in the telescopic pipes (19), and the telescopic pipes (20) are sequentially sleeved in the telescopic pipes (19), one of them flexible pipe (20) and telescopic tube (19) threaded connection, threaded connection between flexible pipe (20) and the flexible pipe (20), flexible pipe (20) are the same with the quantity of rotation axis (16), carry out spacing rotation through limit stop (21) between two adjacent threaded connection's flexible pipe (20), install soft cloth of plastics (22) on unmanned aerial vehicle monitoring platform (1) both sides side surface, install flexible solar module (23) on the soft cloth of plastics (22), connect through axle sleeve (24) and two sets of plastics axle (25) between the soft cloth of plastics (22), two sets of plastics axle (25) crisscross distribution, the plastics lantern ring (26) is installed at the both ends of one of them set of plastics axle (25), the suit of plastics lantern ring (26) is on flexible pipe (20), the plastics ring (26) of outer end and the flexible pipe (20) fixed connection of innermost, an elastic rope (27) is arranged between the other group of plastic shafts (25), and the elastic rope (27) is positioned at two ends of the plastic shafts (25).
2. The unmanned aerial vehicle based on radar monitoring platform of claim 1, characterized in that, adjust strutting arrangement include battery box (7) upper surface center department installs level sensor (28), adjusting sleeve (29) are installed to motor base (4) below, adjusting sleeve (29) internally mounted has adjusting motor (30), adjusting shaft (31) are installed to the rotatory end of adjusting motor (30), adjusting screwed pipe (32) are installed to the lower extreme of adjusting shaft (31), adjusting screwed pipe (32) and adjusting sleeve (29) threaded connection, activity clean shot (33) are installed to the lower extreme of adjusting screwed pipe (32), support base (34) are installed to the below of activity clean shot (33), support base (34) and activity clean shot (33) swing joint.
3. The radar-based unmanned aerial vehicle monitoring platform of claim 1, wherein the photovoltaic inverter (10) is electrically connected to the first battery pack (8).
4. The radar-based unmanned aerial vehicle monitoring platform of claim 1, wherein the flexible solar modules (23) are electrically connected to the photovoltaic inverter (10) after being connected in series.
5. The radar-based unmanned aerial vehicle monitoring platform of claim 1, wherein a charging interface (35) is mounted on the upper surface of the storage battery box (7), and the charging interface (35) is electrically connected with the second storage battery pack (9).
6. A radar-based drone monitoring platform according to claim 1, characterized by a sliding connection between the rotation shaft (16) and the rotation sleeve shaft (15), the sliding connection between the rotation shaft (16) and the rotation shaft (16).
7. A radar-based drone monitoring platform according to claim 1, characterised in that the three-coordinate phased array radar (11) is connected to the first battery pack (8) by a micro-transformer (36).
8. A radar-based drone monitoring platform according to claim 1, characterised in that the controller (2) is connected with an external remote control by wireless signals.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911345932.9A CN111026158A (en) | 2019-12-24 | 2019-12-24 | Unmanned aerial vehicle monitoring platform based on radar |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201911345932.9A CN111026158A (en) | 2019-12-24 | 2019-12-24 | Unmanned aerial vehicle monitoring platform based on radar |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111661346A (en) * | 2020-07-04 | 2020-09-15 | 河北柒壹壹玖工业自动化技术有限公司 | Unmanned aerial vehicle device based on flexible solar energy thin film battery |
| CN113223082A (en) * | 2021-05-12 | 2021-08-06 | 武汉中仪物联技术股份有限公司 | Pipeline scanning method, scanning device, radar crawler and electronic equipment |
| CN115071436A (en) * | 2022-07-22 | 2022-09-20 | 佛山市神风航空科技有限公司 | Unmanned aerial vehicle mesh device and application method thereof |
-
2019
- 2019-12-24 CN CN201911345932.9A patent/CN111026158A/en not_active Withdrawn
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111661346A (en) * | 2020-07-04 | 2020-09-15 | 河北柒壹壹玖工业自动化技术有限公司 | Unmanned aerial vehicle device based on flexible solar energy thin film battery |
| CN113223082A (en) * | 2021-05-12 | 2021-08-06 | 武汉中仪物联技术股份有限公司 | Pipeline scanning method, scanning device, radar crawler and electronic equipment |
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Application publication date: 20200417 |