CN116896611B - Remote monitoring system and monitoring method for smart city safety management - Google Patents
Remote monitoring system and monitoring method for smart city safety management Download PDFInfo
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- CN116896611B CN116896611B CN202311162401.2A CN202311162401A CN116896611B CN 116896611 B CN116896611 B CN 116896611B CN 202311162401 A CN202311162401 A CN 202311162401A CN 116896611 B CN116896611 B CN 116896611B
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- 238000012544 monitoring process Methods 0.000 title claims abstract description 132
- 238000000034 method Methods 0.000 title claims abstract description 16
- 238000012806 monitoring device Methods 0.000 claims abstract description 32
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- 238000012545 processing Methods 0.000 claims abstract description 26
- 238000007726 management method Methods 0.000 claims description 31
- 230000000903 blocking effect Effects 0.000 claims description 19
- 229910000831 Steel Inorganic materials 0.000 claims description 18
- 239000010959 steel Substances 0.000 claims description 18
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- 230000007246 mechanism Effects 0.000 claims description 11
- 241000237983 Trochidae Species 0.000 claims description 8
- 230000008569 process Effects 0.000 claims description 7
- 230000001105 regulatory effect Effects 0.000 claims description 6
- 230000002159 abnormal effect Effects 0.000 claims description 5
- 238000001514 detection method Methods 0.000 claims description 5
- 238000005265 energy consumption Methods 0.000 claims description 4
- 206010000117 Abnormal behaviour Diseases 0.000 claims description 3
- 206010039203 Road traffic accident Diseases 0.000 claims description 3
- 208000027418 Wounds and injury Diseases 0.000 claims description 3
- 230000004044 response Effects 0.000 claims description 3
- 239000000779 smoke Substances 0.000 claims description 3
- 230000005856 abnormality Effects 0.000 claims description 2
- 230000006399 behavior Effects 0.000 claims description 2
- 230000008054 signal transmission Effects 0.000 claims description 2
- 230000000007 visual effect Effects 0.000 claims description 2
- 230000010354 integration Effects 0.000 abstract description 2
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/80—Arrangement of on-board electronics, e.g. avionics systems or wiring
- B64U20/87—Mounting of imaging devices, e.g. mounting of gimbals
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
- B64U70/30—Launching, take-off or landing arrangements for capturing UAVs in flight by ground or sea-based arresting gear, e.g. by a cable or a net
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- G—PHYSICS
- G08—SIGNALLING
- G08B—SIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
- G08B31/00—Predictive alarm systems characterised by extrapolation or other computation using updated historic data
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N7/00—Television systems
- H04N7/18—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast
- H04N7/181—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast for receiving images from a plurality of remote sources
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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
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
- B64U2101/31—UAVs specially adapted for particular uses or applications for imaging, photography or videography for surveillance
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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)
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- Mechanical Engineering (AREA)
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- Business, Economics & Management (AREA)
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention relates to the technical field of monitoring systems, and discloses a remote monitoring system and a monitoring method for smart city safety management, wherein the remote monitoring system comprises the following steps: the system comprises a fixed monitoring device, a movable monitoring device, data transmission equipment, a data processing device and a management platform; the fixed monitoring device comprises a fixed camera; the data transmission equipment can send video data captured by the fixed monitoring device and the movable monitoring device to the inside of the data processing device for summarizing in a network transmission mode; the management platform can display real-time monitoring video pictures in the city. The invention adopts a mode of combining urban internal fixed monitoring and movable monitoring, ensures the whole coverage of an urban internal monitoring area, ensures the integration of the ejection and landing of the unmanned aerial vehicle in the unmanned aerial vehicle cruise monitoring, reduces the area of an unmanned aerial vehicle take-off and landing area, improves the take-off and landing efficiency of the unmanned aerial vehicle, and shortens the non-monitoring vacuum period of the cruise monitoring.
Description
Technical Field
The invention relates to the technical field of monitoring systems, in particular to a remote monitoring system and a monitoring method for smart city safety management.
Background
In the smart city, various city facilities and infrastructures are connected through the Internet, and through data interaction and intelligent processing, the efficient operation and collaborative development of various fields in the city are realized, the intelligent traffic system is utilized to optimize road flow, public traffic network and parking management, traffic efficiency and congestion reduction are improved, clean energy and intelligent power grid technology is integrated, efficient utilization and sustainable development of energy are realized, environmental elements such as air quality, garbage treatment and water resources are monitored and managed in real time through an environment monitoring and early warning system, an intelligent security system is established, urban security management and emergency response capability is improved through technical means such as video monitoring, face recognition and big data analysis, comprehensive promotion of urban informatization management and electronic government service is realized by adopting an electronic government service platform, intelligent building design and management are integrated, and resource utilization efficiency and comfort of buildings are improved through technologies such as sustainable building, energy saving control and intelligent home.
In the prior art, remote monitoring in smart city security management refers to monitoring and managing various security devices and facilities in a city range in real time or periodically through network and video technology. The remote monitoring system can cover various fields in the smart city, including traffic safety, environmental safety etc., the remote monitoring coverage in the present smart city safety management receives the restriction of camera equipment quantity and position, leads to there is the monitoring blind area, can't in time acquire the control picture of all key areas to unmanned aerial vehicle takes off and land and shares same runway in the current unmanned aerial vehicle remote monitoring that cruises, needs to increase extra restriction and restraint in planning and management, leads to the decline of taking off and land efficiency, and the take off and land area is great, can't extensively popularize and use.
Disclosure of Invention
The invention aims to provide a remote monitoring system and a remote monitoring method for smart city safety management, which are used for solving the problems in the background technology.
In order to achieve the above purpose, the present invention provides the following technical solutions: a remote monitoring system for smart city security management, comprising: the system comprises a fixed monitoring device, a movable monitoring device, data transmission equipment, a data processing device and a management platform;
The fixed monitoring device comprises fixed cameras, the number and the positions of the fixed cameras to be installed are determined according to planning and safety requirements of smart cities, and key areas, hot spot areas and high risk areas are selected to serve as deployment sites of the fixed cameras;
the data transmission equipment is arranged according to regional division according to the planning of the smart city, and can send video data captured by the fixed monitoring device and the movable monitoring device to the inside of the data processing device for summarization in a network transmission mode;
the data processing device can send summarized video data to the inside of the management platform, and the data processing device can run a detection algorithm, the video data uploaded by the data transmission equipment are analyzed, abnormal behavior of travelers, traffic accidents and abnormal activities of fire smoke are detected, and corresponding alarm information is generated;
the management platform can display a real-time monitoring video picture in the city, and can receive alarm information sent by the data processing device and inform related departments or personnel.
Preferably, the movable monitoring device includes: the system comprises an underground platform, a lifting mechanism, a control room, a control system, a network system, a hydraulic supply system, a power distribution system and a cruise monitoring unmanned aerial vehicle; the lifting mechanism is arranged in the underground platform; the control room is arranged at the front side of the top of the underground platform; the control system is arranged at the central position inside the control room; the network system is arranged in the control room and is positioned at the left side of the control system, the network system is electrically connected with the control system, and the network system can be connected with an external data transmission device through a remote network; the hydraulic supply system is arranged in the control room and is positioned on the right side of the control system, and the hydraulic supply system is electrically connected with the control system; the power distribution system is arranged at the left side of the inside of the control room and is electrically connected with the control system; the cruise monitoring unmanned aerial vehicle is arranged outside the underground platform and is connected with a network system remote network.
Preferably, the lifting mechanism comprises: the device comprises a shell, a lifting part, a direction adjusting part, a telescopic carrying part, a fixed seat, a rotating seat, a supporting seat and an electric telescopic rod; the shell is arranged on the right side of the interior of the underground platform; the lifting component is arranged at the rear side of the inner cavity of the shell along the up-down direction, and is electrically connected with the control system; the direction adjusting component is arranged at the top of the lifting end of the lifting component and is electrically connected with the control system; the telescopic carrying component is arranged at the right lower part of the inner cavity of the shell and is electrically connected with the control system; the fixed seat is fixedly arranged in the underground platform and positioned at the left lower part of the shell; the rotating seat is rotationally connected to the inner side of the fixed seat through a pin shaft; the supporting seat is fixedly arranged at the top of the rotating seat along the left-right direction; the number of the electric telescopic rods is three, one end of each electric telescopic rod is rotationally connected to the inside of the underground platform from front to back through a pin shaft seat, the other end of each electric telescopic rod is rotationally connected to the left side of the bottom end of the supporting seat from front to back through a pin shaft seat, and the electric telescopic rods are electrically connected with the control system.
Preferably, the lifting mechanism further comprises: the device comprises a mounting frame, a tank shell, an ejection part, an electromagnetic chuck seat and a landing assembly; the number of the mounting frames is three, and the three electric telescopic rods are arranged at the top of the supporting seat from left to right; the tank body shell is arranged at the bottoms of the three mounting frames along the left-right direction; the ejection component is arranged on the inner side of the tank body shell along the left-right direction and is electrically connected with the control system; the electromagnetic chuck seat is arranged at the moving end of the ejection component and is electrically connected with the control system; the landing assembly is arranged on the top of the three installation frames.
Preferably, the landing assembly comprises: the landing assembly comprises a landing assembly shell, a first groove body, a hydraulic reducing rod, a driving vehicle, a base, a height adjusting part, a rotating arm, an electric winder and a blocking steel rope; the landing component shell is arranged at the top of the three mounting frames along the left-right direction; the number of the first groove bodies is two, and the two first groove bodies are respectively arranged at the left ends of the front side and the rear side of the inner cavity of the landing component shell along the left-right direction; the number of the hydraulic deceleration rods is two, the two hydraulic deceleration rods are respectively arranged at the front end and the rear end of the left side of the bottom end of the inner cavity of the landing assembly shell along the left-right direction, and the hydraulic deceleration rods are connected with the hydraulic supply system through a guide pipe; the driving vehicle is arranged at the left lower part of the inner cavity of the landing assembly shell and is electrically connected with the control system; the base is arranged at the top of the driving vehicle along the front-back direction, and the front side and the back side of the base respectively penetrate through the inner cavities of the front first groove body and the back first groove body; the two height adjusting parts are respectively arranged at the front side and the rear side of the landing assembly shell along the up-down direction, and are electrically connected with the control system; the number of the rotating arms is two, each group of the rotating arms is two, and the two groups of the rotating arms are respectively connected to the left side and the right side of the lifting ends of the front and the rear height adjusting parts through pin shafts in a rotating way; the number of the electric winders is two, the number of each electric winders is two, the two electric winders are respectively arranged at the outer ends of the two rotating arms, and the electric winders are electrically connected with the control system; the number of the blocking steel cables is two, and two ends of the blocking steel cables are respectively wound in the middle, front and rear electric winders of the two groups of electric winders.
Preferably, the landing assembly further comprises: the device comprises a second groove body, a tractor, a bottom frame, a first rotating frame, a second rotating frame, a lifting frame, a first mounting frame, a driving motor, a second mounting frame, a screw nut, a screw rod, a top shell, a horizontal moving part, a horizontal rotating part and a clamping part; the second groove body is arranged in the middle of the right side of the top end of the inner cavity of the landing component shell along the left-right direction; the tractor is arranged in the inner cavity of the landing assembly shell and is electrically connected with the control system; the bottom frame is fixedly arranged at the top of the tractor; one end of the first rotating frame is rotationally connected to the inner side of the bottom frame through a pin shaft; one end of the second rotating frame is rotatably connected to the inner side of the bottom frame through a pin shaft and is positioned above the first rotating frame; the lifting frame is rotatably connected to the outer sides of the other ends of the first rotating frame and the second rotating frame through pin shafts; the first installation frame is installed in the middle of the left bottom end of the bottom frame; the driving motor is rotationally connected to the inner side of the first mounting frame through a pin shaft, and the driving motor is electrically connected with the control system; the second installation frame is installed in the middle of the left side of the first rotation frame; the screw nut is rotationally connected to the inner side of the second mounting frame through a pin shaft; the screw rod is fixedly arranged at the top of the rotating end of the driving motor, and is in threaded connection with the inner side of the screw nut; the top shell is arranged at the top of the lifting frame; the horizontal moving component is arranged on the inner side of the top shell along the left-right direction and is electrically connected with the control system; the horizontal rotating component is arranged at the top of the moving end of the horizontal moving component and is electrically connected with the control system; the clamping component is arranged at the top of the rotating end of the horizontal rotating component, and the clamping component is electrically connected with the control system.
A remote monitoring method for smart city security management comprises the following steps:
step one: according to urban planning and safety requirements, the number and positions of fixed monitoring devices, movable monitoring devices and data transmission equipment to be installed are determined so as to ensure full coverage of urban internal monitoring and signal transmission;
step two: deploying and installing a fixed camera, ensuring the monitoring angle and the visual field of the fixed camera, and configuring the parameters of the fixed camera and the network connection of data transmission equipment in the current area;
step three: the cruise monitoring unmanned aerial vehicle carries out cruise shooting monitoring in the urban upper air, remotely sends data to the inside of a network system and uploads the data to data transmission equipment in an external area through the network system;
step four: the cruise monitoring unmanned aerial vehicle contacts with the electric winder in the process of gliding and landing along the top of the landing component shell after the cruise shooting is finished, so that the driving vehicle moves to the right side and the driving base contacts with the hydraulic speed reducing rod to generate energy consumption, the speed reducing effect of the first groove body is realized, and the cruise monitoring unmanned aerial vehicle is ensured to stop at a preset position;
step five: the driving motor drives the screw rod to rotate, the screw rod nut drives the first rotating frame to rotate upwards, the top shell moves out of the inner cavity of the second groove body, the horizontal rotating component drives the clamping component to rotate to clamp and fix the bottom of the cruise monitoring unmanned aerial vehicle and continuously move upwards, so that the cruise monitoring unmanned aerial vehicle is separated from being connected with the blocking steel cable, the tractor moves to the right side, the horizontal rotating component drives the clamping component to drive the cruise monitoring unmanned aerial vehicle to rotate horizontally, the horizontal moving component drives the clamping component to drive the cruise monitoring unmanned aerial vehicle to move to the position above the direction regulating component, and the clamping component is separated from and fixed with the clamping of the cruise monitoring unmanned aerial vehicle, so that the cruise monitoring unmanned aerial vehicle is transported to the top of the direction regulating component;
Step six: the lifting part drives the direction adjusting part to move downwards so as to drive the cruise monitoring unmanned aerial vehicle to enter the inside of the shell, and a worker can enter the inside of the underground platform to maintain and charge the cruise monitoring unmanned aerial vehicle, so that preparation before flying is completed;
step seven: the direction adjusting component adjusts the position direction of the cruising monitoring unmanned aerial vehicle, the telescopic carrying component moves the cruising monitoring unmanned aerial vehicle to the top of the electromagnetic chuck seat through self extension and clamping, and the electromagnetic chuck seat is magnetically connected with the cruising monitoring unmanned aerial vehicle, so that secondary take-off cruising preparation is realized;
step eight: the electric telescopic rod drives the supporting seat to rotate upwards by self extension by taking the inner axle center of the fixed seat as an axial direction under the cooperation of the rotating seat, the electric telescopic rod enables the tank body shell to rotate upwards to the tilting device under the cooperation of the supporting seat and the mounting frame, and the left side of the tank body shell moves upwards out of the interior of the underground platform;
step nine: the ejection component drives the electromagnetic chuck seat to move at a high speed in the inner cavity of the tank body shell, and drives the cruise monitoring unmanned aerial vehicle to move at a high speed under the cooperation of the electromagnetic chuck seat to obtain a larger initial speed so as to eject the cruise monitoring unmanned aerial vehicle, and the cruise monitoring unmanned aerial vehicle flies and carries out high-altitude monitoring again after starting an engine and adjusting the gesture;
Step ten: the data transmission equipment transmits the image data uploaded by the fixed monitoring device and the movable monitoring device to the data processing device, the data processing device runs internal image processing and computer vision algorithm, analyzes and processes the captured video data, detects a moving object, recognizes a target, analyzes behaviors, generates corresponding data and alarm information, optimizes and adjusts abnormality detection and early warning rules by combining historical data and real-time conditions, generates corresponding alarm information and transmits the alarm information to the inside of the management platform;
step eleven: the management platform triggers an alarm to inform related departments or personnel and provides corresponding suggestions and guidance according to abnormal conditions detected by the early warning rules and algorithms, and starts corresponding emergency response systems and equipment to dispatch on-site monitoring personnel or emergency teams for processing and disposal.
Compared with the prior art, the invention has the beneficial effects that:
1. through cruise control unmanned aerial vehicle along descending subassembly shell top gliding landing in-process with electric winder contact, and then under the cooperation of stopping cable wire, electric winder, the rotor arm, altitude mixture control part and base, ensure to cruise control unmanned aerial vehicle and stop on predetermined tractor top position, horizontal rotation part drive clamping part horizontal rotation is to the perpendicular position department below the control unmanned aerial vehicle that cruises, clamping part is fixed to cruise control unmanned aerial vehicle bottom right side position centre gripping, clamping part continues to upwards move and makes the control unmanned aerial vehicle that cruises break away from with stopping cable wire connected state, the tractor moves to direction adjustment part corresponding position department along second cell body lower right side, horizontal rotation part drive clamping part drives the control unmanned aerial vehicle horizontal rotation that cruises, horizontal movement part drive horizontal rotation part horizontal right side removes, and make the control unmanned aerial vehicle that cruises move to direction adjustment part top position under the cooperation of clamping part, clamping part breaks away from with the control unmanned aerial vehicle's that cruises centre gripping is fixed, in order to realize the control unmanned aerial vehicle's that cruises.
2. The position direction of the cruising monitoring unmanned aerial vehicle is adjusted through the direction adjusting component, the telescopic carrying component moves the cruising monitoring unmanned aerial vehicle to the top of the electromagnetic chuck base through self extension and clamping, the electromagnetic chuck base is magnetically attracted with the cruising monitoring unmanned aerial vehicle, the electric telescopic rod rotates upwards by taking the inner axis of the fixing base as the axial direction under the cooperation of the rotating base through the self extension driving supporting base, the electric telescopic rod enables the tank shell to rotate upwards to move out of the underground platform under the cooperation of the supporting base and the mounting frame, the ejection component drives the electromagnetic chuck base to move at a high speed in the inner cavity of the tank shell, so that the electromagnetic chuck base drives the cruising monitoring unmanned aerial vehicle to obtain a large initial speed, the electromagnetic chuck base stops being magnetically attracted with the cruising monitoring unmanned aerial vehicle, and a preset program in the control system flies after the cruising monitoring unmanned aerial vehicle starts an engine and adjusts the gesture through a network system remote control.
In summary, the method adopts a mode of combining urban internal fixed monitoring and movable monitoring, ensures the whole coverage of an urban internal monitoring area, ensures the integration of the ejection and landing of the unmanned aerial vehicle in the unmanned aerial vehicle cruise monitoring, reduces the area of the unmanned aerial vehicle landing area, improves the unmanned aerial vehicle landing efficiency, and shortens the non-monitoring vacuum period of the cruise monitoring.
Drawings
FIG. 1 is a schematic diagram of the present invention.
Fig. 2 is a schematic structural diagram of a movable monitoring device according to the present invention.
Fig. 3 is an exploded view of the landing gear of fig. 2.
Fig. 4 is an exploded view of the landing assembly of fig. 3.
Fig. 5 is an enlarged view at a of fig. 4.
Fig. 6 is a schematic view of a partial structure of the landing assembly of fig. 4.
In the figure: 1. an underground platform; 2. a lifting mechanism; 21. a housing; 22. a lifting member; 23. a direction adjustment member; 24. a telescopic carrying member; 25. a fixing seat; 26. a rotating seat; 27. a support base; 28. an electric telescopic rod; 29. a mounting frame; 210. a tank body housing; 211. an ejection member; 212. an electromagnetic chuck seat; 3. a landing assembly; 31. a landing assembly housing; 32. a first tank body; 33. a hydraulic deceleration rod; 34. a drive vehicle; 35. a base; 36. a height adjusting member; 37. a rotating arm; 38. an electric winder; 39. blocking the steel cable; 310. a second tank body; 311. a tractor; 312. a bottom frame; 313. a first rotating frame; 314. a second turret; 315. a lifting frame; 316. a first mounting frame; 317. a driving motor; 318. a second mounting frame; 319. a lead screw nut; 320. a lead screw rod; 321. a top housing; 322. a horizontal moving member; 323. a horizontal rotation member; 324. a clamping member; 4. a control room; 5. a control system; 6. a network system; 7. a hydraulic supply system; 8. a power distribution system; 9. cruise monitoring unmanned aerial vehicle.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
Referring to fig. 1-6, the present invention provides a technical solution: a remote monitoring system for smart city security management, comprising: the system comprises a fixed monitoring device, a movable monitoring device, data transmission equipment, a data processing device and a management platform; the fixed monitoring device comprises fixed cameras, the number and the positions of the fixed cameras to be installed are determined according to planning and safety requirements of smart cities, and key areas, hot spot areas and high risk areas are selected to serve as deployment sites of the fixed cameras; the data transmission equipment is arranged according to regional division according to the planning of the smart city, and can send video data captured by the fixed monitoring device and the movable monitoring device to the inside of the data processing device for summarization in a network transmission mode; the data processing device can send summarized video data to the inside of the management platform, and the data processing device can run a detection algorithm, the video data uploaded by the data transmission equipment are analyzed, abnormal behavior of travelers, traffic accidents and abnormal activities of fire smoke are detected, and corresponding alarm information is generated; the management platform can display a real-time monitoring video picture in the city, and can receive alarm information sent by the data processing device and inform related departments or personnel.
As a preferred solution, as shown in fig. 2, the mobile monitoring device includes: the system comprises an underground platform 1, a take-off and landing mechanism 2, a control room 4, a control system 5, a network system 6, a hydraulic supply system 7, a power distribution system 8 and a cruise monitoring unmanned aerial vehicle 9, wherein the underground platform 1 is additionally provided with an unmanned aerial vehicle charging device and an unmanned aerial vehicle maintenance device according to actual needs; the lifting mechanism 2 is arranged inside the underground platform 1; the control room 4 is arranged on the top front side of the underground platform 1; the control system 5 is arranged at the central position inside the control room 4, and a prefabricated program is arranged inside the control system 5 and can carry out logic sequence control on electric devices inside the device; the network system 6 is arranged in the control room 4 and is positioned at the left side of the control system 5, the network system 6 is electrically connected with the control system 5, the network system 6 can be in remote network connection with external data transmission equipment, the network system 6 uploads data signals to the external data transmission equipment, and the network system 6 can send control signals of the control system 5 to the cruise monitoring unmanned aerial vehicle 9; the hydraulic supply system 7 is arranged in the control room 4 and is positioned on the right side of the control system 5, the hydraulic supply system 7 is electrically connected with the control system 5, the hydraulic supply system 7 is controlled by the control system 5, and the hydraulic supply system 7 injects or extracts hydraulic oil into the hydraulic deceleration rod 33; the power distribution system 8 is arranged at the left side of the inside of the control room 4, the power distribution system 8 is electrically connected with the control system 5, and the power distribution system 8 supplies power for electric devices in the device; the cruise monitoring unmanned aerial vehicle 9 is arranged outside the underground platform 1, the cruise monitoring unmanned aerial vehicle 9 is connected with the network system 6 in a remote network mode, the cruise monitoring unmanned aerial vehicle 9 adopts electric or fuel oil as power according to actual needs, a connecting piece matched with blocking landing and catapult take-off is mounted inside the cruise monitoring unmanned aerial vehicle 9, and the cruise monitoring unmanned aerial vehicle 9 performs cruise shooting monitoring in the urban upper air and remotely transmits data to the inside of the network system 6.
As a preferred solution, as shown in fig. 3, the lifting mechanism 2 includes: the device comprises a shell 21, a lifting part 22, a direction adjusting part 23, a telescopic carrying part 24, a fixed seat 25, a rotating seat 26, a supporting seat 27, an electric telescopic rod 28, a mounting frame 29, a tank shell 210, an ejection part 211, an electromagnetic chuck seat 212 and a landing assembly 3; the outer shell 21 is arranged on the right side of the interior of the underground platform 1; the lifting component 22 is arranged at the rear side of the inner cavity of the shell 21 along the up-down direction, the lifting component 22 is electrically connected with the control system 5, the lifting component 22 is controlled by the control system 5, and the lifting component 22 can drive the direction adjusting component 23 to lift to a designated height position; the direction adjusting component 23 is arranged at the top of the lifting end of the lifting component 22, the direction adjusting component 23 is electrically connected with the control system 5, the direction adjusting component 23 is controlled by the control system 5, the direction adjusting component 23 can drive the internal rotating disc to rotate to a specified direction position, and then the position of the cruise monitoring unmanned aerial vehicle 9 is adjusted and matched for subsequent catapult-assisted take-off; the telescopic carrying member 24 is arranged at the right lower part of the inner cavity of the housing 21, the telescopic carrying member 24 is electrically connected with the control system 5, the telescopic carrying member 24 is controlled by the control system 5, the telescopic carrying member 24 can horizontally move by stretching and shortening the driving clamping part by itself, and the cruise monitoring unmanned aerial vehicle 9 can be clamped and carried; the fixed seat 25 is fixedly arranged inside the underground platform 1 and positioned at the left lower part of the shell 21; the rotating seat 26 is rotatably connected to the inner side of the fixed seat 25 through a pin shaft; the supporting seat 27 is fixedly arranged at the top of the rotating seat 26 along the left-right direction, and the rotating seat 26 can rotate at the inner side of the fixed seat 25; the number of the electric telescopic rods 28 is three, one end of each electric telescopic rod 28 is rotatably connected in the underground platform 1 from front to back through a pin shaft seat, the other end of each electric telescopic rod 28 is rotatably connected to the left side of the bottom end of the supporting seat 27 from front to back through a pin shaft seat, each electric telescopic rod 28 is electrically connected with the control system 5, the electric telescopic rods 28 are controlled by the control system 5, and the electric telescopic rods 28 can be stretched and shortened by themselves to drive the supporting seat 27 to rotate to a specified angle direction; the number of the mounting frames 29 is three, and three electric telescopic rods 28 are arranged at the top of the supporting seat 27 from left to right; the tank housing 210 is provided at the bottoms of the three mounting frames 29 in the left-right direction; the ejection component 211 is arranged on the inner side of the tank body shell 210 along the left-right direction, the ejection component 211 is electrically connected with the control system 5, the ejection component 211 is controlled by the control system 5, and the ejection component 211 can drive the electromagnetic chuck base 212 to move at a high speed; the electromagnetic chuck base 212 is arranged at the moving end of the ejection component 211, the electromagnetic chuck base 212 is electrically connected with the control system 5, the electromagnetic chuck base 212 is controlled by the control system 5, and the electromagnetic chuck base 212 can be fixedly connected with the bottom of the cruise monitoring unmanned aerial vehicle 9 through magnetic attraction; the drop assembly 3 is disposed on top of three mounts 29.
As a preferred solution, as shown in fig. 4, 5 and 6, the landing assembly 3 further comprises: landing assembly housing 31, first tank 32, hydraulic reduction bar 33, drive truck 34, base 35, height adjustment member 36, rotating arm 37, electric retractor 38, arresting cable 39, second tank 310, tractor 311, bottom frame 312, first rotating frame 313, second rotating frame 314, lifting frame 315, first mounting frame 316, drive motor 317, second mounting frame 318, screw nut 319, screw 320, top housing 321, horizontal movement member 322, horizontal rotation member 323, and clamping member 324; the landing assembly housing 31 is provided on top of the three mounting frames 29 in the left-right direction; the number of the first groove bodies 32 is two, and the two first groove bodies 32 are respectively arranged at the left ends of the front side and the rear side of the inner cavity of the landing component shell 31 along the left-right direction; the number of the hydraulic reducing rods 33 is two, the two hydraulic reducing rods 33 are respectively arranged at the front and rear ends of the left side of the bottom end of the inner cavity of the landing component shell 31 along the left-right direction, the hydraulic reducing rods 33 are connected with the hydraulic supply system 7 through a guide pipe, kinetic energy can be converted into oil pressure in the hydraulic reducing rods 33 in the process of contacting the base 35 with the hydraulic reducing rods 33, and energy consumption is generated through resistance and friction, so that the speed reducing effect on the cruise monitoring unmanned aerial vehicle 9 is realized; the driving vehicle 34 is arranged at the left lower part of the inner cavity of the landing assembly shell 31, and the driving vehicle 34 is electrically connected with the control system 5; the base 35 is arranged at the top of the driving vehicle 34 along the front-rear direction, and the front side and the rear side of the base 35 respectively penetrate through the inner cavities of the front first groove body 32 and the rear first groove body 32; the number of the height adjusting parts 36 is two, the two height adjusting parts 36 are respectively arranged at the front side and the rear side of the landing assembly shell 31 along the up-down direction, the height adjusting parts 36 are electrically connected with the control system 5, the height adjusting parts 36 are controlled by the control system 5, and the height adjusting parts 36 can drive the rotating arms 37 to lift to the designated height position; the number of the rotating arms 37 is two, the number of each group of rotating arms 37 is two, the two groups of rotating arms 37 are respectively connected to the left side and the right side of the lifting end of the front and rear height adjusting parts 36 through pin shafts in a rotating manner, and the rotating arms 37 can rotate by taking the pin shaft rotation connection parts of the lifting ends of the height adjusting parts 36 as shafts so as to avoid hard contact between the blocking steel cable 39 and the cruise monitoring unmanned aerial vehicle 9; the number of the electric winders 38 is two, the number of each electric winders 38 is two, the two electric winders 38 are respectively arranged at the outer ends of the two groups of rotating arms 37, the electric winders 38 are electrically connected with the control system 5, and the electric winders 38 can be controlled by the control system 5 to drive the internal winding disc to rotate so as to realize winding and unwinding of the blocking steel cable 39; the number of the blocking steel ropes 39 is two, and two ends of the two blocking steel ropes 39 are respectively wound inside the middle, front and rear electric winders 38 of the two groups of electric winders 38; the second groove 310 is arranged at the middle part of the right side of the top end of the inner cavity of the landing component shell 31 along the left-right direction; the tractor 311 is arranged in the inner cavity of the landing assembly shell 31, and the tractor 311 is electrically connected with the control system 5; the bottom bracket 312 is fixedly mounted on top of the towing vehicle 311; one end of the first rotating frame 313 is rotatably connected to the inner side of the bottom frame 312 through a pin shaft; one end of the second rotating frame 314 is rotatably connected to the inner side of the bottom frame 312 through a pin shaft and is positioned above the first rotating frame 313; the lifting frame 315 is rotatably connected to the outer sides of the other ends of the first rotating frame 313 and the second rotating frame 314 through a pin shaft; the first mounting frame 316 is installed at the middle of the left bottom end of the bottom frame 312; the driving motor 317 is rotatably connected to the inner side of the first mounting frame 316 through a pin shaft, the driving motor 317 is electrically connected with the control system 5, the driving motor 317 can be controlled by the control system 5, the driving motor 317 drives the screw rod 320 to rotate, and the driving motor 317 can deflect with the connection part with the rotation of the pin shaft on the inner side of the first mounting frame 316 as a shaft in the process of driving the screw rod 320 to rotate; the second mounting bracket 318 is mounted at the left middle of the first rotating bracket 313; the screw nut 319 is rotatably connected to the inner side of the second mounting frame 318 through a pin shaft, and the screw rod 320 can deflect with the connection part of the screw nut with the rotation of the inner side pin shaft of the second mounting frame 318 as a shaft; the lead screw 320 is fixedly arranged at the top of the rotating end of the driving motor 317, and the lead screw 320 is in threaded connection with the inner side of the lead screw nut 319; the top housing 321 is disposed on top of the lift frame 315; the horizontal moving part 322 is arranged at the inner side of the top shell 321 along the left-right direction, the horizontal moving part 322 is electrically connected with the control system 5, the horizontal moving part 322 can be controlled by the control system 5, and the horizontal moving part 322 can drive the horizontal rotating part 323 to horizontally move to a designated position; the horizontal rotating component 323 is arranged at the top of the moving end of the horizontal moving component 322, the horizontal rotating component 323 is electrically connected with the control system 5, the horizontal rotating component 323 can be controlled by the control system 5, and the horizontal rotating component 323 drives the clamping component 324 to rotate to a specified angle direction; the clamping part 324 sets up at the rotation end top of horizontal rotation part 323, and clamping part 324 and control system 5 electric connection, clamping part 324 can be controlled by control system 5, and clamping part 324 can be fixed to cruise control unmanned aerial vehicle 9 bottom centre gripping.
The working principle is as follows:
step 1: the cruise monitoring unmanned aerial vehicle 9 carries out cruise shooting monitoring in urban upper air, data are remotely sent to the inside of the network system 6 and uploaded to external data transmission equipment through the network system 6, after the cruise monitoring unmanned aerial vehicle 9 finishes cruise shooting, a program is preset in the control system 5 to control the starting of the hydraulic supply system 7, the driving vehicle 34 and the electric winder 38, the hydraulic supply system 7 injects hydraulic oil into the hydraulic reduction rod 33, the driving vehicle 34 drives the base 35 to move to the left end position of the inner cavity of the landing component shell 31 along the first groove bodies 32 on the front side and the rear side, the electric winder 38 winds the blocking steel rope 39 to enable the blocking steel rope 39 to be in a tight state, the cruise monitoring unmanned aerial vehicle 9 is contacted with the electric winder 38 in the process of gliding along the top of the landing component shell 31, and then under the cooperation of the blocking steel rope 39, the electric winder 38, the rotating arm 37, the height adjusting component 36 and the base 35, the driving vehicle 34 moves rightward along the inner cavity of the landing assembly shell 31, the base 35 is contacted with the hydraulic reducing rod 33 to convert kinetic energy into oil pressure in the hydraulic reducing rod 33, energy consumption is generated through resistance and friction, the speed reducing effect on the cruise monitoring unmanned aerial vehicle 9 is achieved, further, the cruise monitoring unmanned aerial vehicle 9 is ensured to stop at a position above the preset traction vehicle 311, the electric winding device 38 winds the blocking steel rope 39 to enable the blocking steel rope 39 to be in a tightening and loosening state, a preset program in the control system 5 controls the driving motor 317, the horizontal rotating part 323, the clamping part 324, the traction vehicle 311 and the horizontal moving part 322 to start, the driving motor 317 drives the lead screw 320 to rotate, the lead screw nut 319 moves downwards under the action of the rotation force of the lead screw 320, and the lead screw nut 319 deflects with the rotation joint of a pin shaft on the inner side of the second mounting frame 318 as an axis, the first rotating frame 313 is driven to rotate upwards in an axial direction at the position which is in pin shaft rotation connection with the bottom frame 312, the lifting frame 315 is driven to move upwards under the cooperation of the second rotating frame 314, the top shell 321 is moved out of the inner cavity of the second groove body 310, the horizontal rotating part 323 drives the clamping part 324 to horizontally rotate to a position which is vertical to the lower side of the cruise monitoring unmanned aerial vehicle 9, the clamping part 324 clamps and fixes the right side of the bottom of the cruise monitoring unmanned aerial vehicle 9, meanwhile, the clamping part 324 continues to move upwards, the cruise monitoring unmanned aerial vehicle 9 is separated from the connection state with the blocking steel rope 39, the tractor 311 moves to the right side along the lower side of the second groove body 310 to the position corresponding to the direction regulating part 23, the horizontal rotating part 323 drives the clamping part 324 to horizontally rotate for one hundred eighty degrees, the horizontal moving part 322 drives the horizontal rotating part 323 to horizontally move to the right side, and the cruise monitoring unmanned aerial vehicle 9 is moved to the upper side of the direction regulating part 23 under the cooperation of the clamping part 324, and the clamping part 324 breaks away from the clamping and fixes the bottom of the cruise monitoring unmanned aerial vehicle 9, so that the cruise monitoring unmanned aerial vehicle 9 is realized;
Step 2: the control system 5 is internally provided with a program to control the lifting part 22 to start, the lifting part 22 drives the direction adjusting part 23 to move downwards to drive the cruise monitoring unmanned aerial vehicle 9 to enter the shell 21, a worker can enter the underground platform 1 to maintain and charge the cruise monitoring unmanned aerial vehicle 9, when the cruise is carried out again, the control system 5 is internally provided with the program to control the direction adjusting part 23, the telescopic carrying part 24, the electromagnetic chuck base 212, the electric telescopic rod 28, the ejection part 211 and the network system 6 to start, the direction adjusting part 23 adjusts the position direction of the cruise monitoring unmanned aerial vehicle 9, the telescopic carrying part 24 moves the cruise monitoring unmanned aerial vehicle 9 to the top of the electromagnetic chuck base 212 through self extension and clamping, the electromagnetic chuck base 212 is in magnetic attraction connection with the cruise monitoring unmanned aerial vehicle 9, the electric telescopic rod 28 rotates upwards by taking the inner side axle center of the fixed seat 25 as an axial direction under the cooperation of the rotating seat 26 through the self-extension driving supporting seat 27, the electric telescopic rod 28 enables the groove body shell 210 to rotate upwards to move out of the inside of the underground platform 1 under the cooperation of the supporting seat 27 and the mounting frame 29, the ejection part 211 drives the electromagnetic chuck seat 212 to move at a high speed in the inner cavity of the groove body shell 210, the electromagnetic chuck seat 212 is driven to move at a high speed under the cooperation of the electromagnetic chuck seat 212 to obtain a larger initial speed, the electromagnetic chuck seat 212 stops the magnetic attraction connection with the cruise monitoring unmanned aerial vehicle 9 when moving to the left end position of the inner cavity of the groove body shell 210, and a preset program in the control system 5 remotely controls the cruise monitoring unmanned aerial vehicle 9 to start an engine and adjust the gesture through the network system 6 to fly.
Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (4)
1. A remote monitoring system for smart city security management, comprising: the system comprises a fixed monitoring device, a movable monitoring device, data transmission equipment, a data processing device and a management platform;
the fixed monitoring device comprises fixed cameras, the number and the positions of the fixed cameras to be installed are determined according to planning and safety requirements of smart cities, and key areas, hot spot areas and high risk areas are selected to serve as deployment sites of the fixed cameras;
the data transmission equipment is arranged according to regional division according to the planning of the smart city, and can send video data captured by the fixed monitoring device and the movable monitoring device to the inside of the data processing device for summarization in a network transmission mode;
the data processing device can send summarized video data to the inside of the management platform, and the data processing device can run a detection algorithm, the video data uploaded by the data transmission equipment are analyzed, abnormal behavior of travelers, traffic accidents and abnormal activities of fire smoke are detected, and corresponding alarm information is generated;
The management platform can display a real-time monitoring video picture in the city, can receive alarm information sent by the data processing device and inform related departments or personnel;
the movable monitoring device comprises:
an underground platform (1);
the lifting mechanism (2) is arranged inside the underground platform (1);
the control room (4) is arranged at the front side of the top of the underground platform (1);
a control system (5) arranged at the central position inside the control room (4);
the network system (6) is arranged in the control room (4) and is positioned at the left side of the control system (5), the network system (6) is electrically connected with the control system (5), and the network system (6) can be in remote network connection with external data transmission equipment;
the hydraulic supply system (7) is arranged in the control room (4) and is positioned on the right side of the control system (5), and the hydraulic supply system (7) is electrically connected with the control system (5);
the power distribution system (8) is arranged at the left side inside the control room (4), and the power distribution system (8) is electrically connected with the control system (5);
the cruise monitoring unmanned aerial vehicle (9) is arranged outside the underground platform (1), and the cruise monitoring unmanned aerial vehicle (9) is connected with a network system (6) in a remote network manner;
The take-off and landing mechanism (2) comprises:
a housing (21) provided on the right side of the inside of the underground platform (1);
the lifting component (22) is arranged at the rear side of the inner cavity of the shell (21) along the up-down direction, and the lifting component (22) is electrically connected with the control system (5);
the direction adjusting component (23) is arranged at the top of the lifting end of the lifting component (22), and the direction adjusting component (23) is electrically connected with the control system (5);
the telescopic conveying component (24) is arranged at the right lower part of the inner cavity of the shell (21), and the telescopic conveying component (24) is electrically connected with the control system (5);
the fixed seat (25) is fixedly arranged in the underground platform (1) and positioned at the left lower part of the shell (21);
the rotating seat (26) is rotationally connected to the inner side of the fixed seat (25) through a pin shaft;
the supporting seat (27) is fixedly arranged at the top of the rotating seat (26) along the left-right direction;
the three electric telescopic rods (28) are rotatably connected with the inside of the underground platform (1) through pin shaft seats from front to back, the other ends of the three electric telescopic rods (28) are rotatably connected with the left side of the bottom end of the supporting seat (27) through pin shaft seats from front to back, and the electric telescopic rods (28) are electrically connected with the control system (5);
The take-off and landing mechanism (2) further comprises:
the number of the mounting frames (29) is three, and the three electric telescopic rods (28) are arranged at the top of the supporting seat (27) from left to right;
the tank body shell (210) is arranged at the bottoms of the three mounting frames (29) along the left-right direction;
the ejection component (211) is arranged on the inner side of the tank body shell (210) along the left-right direction, and the ejection component (211) is electrically connected with the control system (5);
the electromagnetic chuck base (212) is arranged at the moving end of the ejection component (211), and the electromagnetic chuck base (212) is electrically connected with the control system (5);
and the landing assembly (3) is arranged on the top of the three mounting frames (29).
2. A remote monitoring system for smart city security management according to claim 1, characterized in that said landing assembly (3) comprises:
a landing assembly housing (31) provided on top of the three mounting frames (29) in the left-right direction;
the number of the first groove bodies (32) is two, and the two first groove bodies (32) are respectively arranged at the left ends of the front side and the rear side of the inner cavity of the landing component shell (31) along the left-right direction;
The hydraulic speed reducing rods (33) are arranged in number, the two hydraulic speed reducing rods (33) are respectively arranged at the front end and the rear end of the left side of the bottom end of the inner cavity of the landing assembly shell (31) along the left-right direction, and the hydraulic speed reducing rods (33) are connected with the hydraulic supply system (7) through a guide pipe;
the driving vehicle (34) is arranged at the left lower part of the inner cavity of the landing component shell (31), and the driving vehicle (34) is electrically connected with the control system (5);
the base (35) is arranged at the top of the driving vehicle (34) along the front-back direction, and the front side and the back side of the base (35) respectively penetrate through the inner cavities of the front first groove body (32) and the back first groove body (32);
the height adjusting parts (36) are arranged in number, the two height adjusting parts (36) are respectively arranged at the front side and the rear side of the landing assembly shell (31) along the up-down direction, and the height adjusting parts (36) are electrically connected with the control system (5);
the number of the rotating arms (37) is two, the number of each group of the rotating arms (37) is two, and the two groups of the rotating arms (37) are respectively connected to the left side and the right side of the lifting ends of the front and rear two height adjusting parts (36) in a rotating way through pin shafts;
The number of the electric winders (38) is two, the number of each electric winder (38) is two, the two electric winders (38) are respectively arranged at the outer ends of the two groups of rotating arms (37), and the electric winders (38) are electrically connected with the control system (5);
the number of the blocking steel ropes (39) is two, and two ends of the blocking steel ropes (39) are respectively wound inside the middle, front and rear electric winders (38) of the two groups of electric winders (38).
3. A remote monitoring system for smart city security management according to claim 2, characterized in that said landing assembly (3) further comprises:
the second groove body (310) is arranged at the middle part of the right side of the top end of the inner cavity of the landing component shell (31) along the left-right direction;
the tractor (311) is arranged in the inner cavity of the landing component shell (31), and the tractor (311) is electrically connected with the control system (5);
a bottom frame (312) fixedly mounted on top of the tractor (311);
a first rotating frame (313), one end of which is rotatably connected to the inner side of the bottom frame (312) through a pin shaft;
A second rotating frame (314), one end of which is rotatably connected to the inner side of the bottom frame (312) through a pin shaft and is positioned above the first rotating frame (313);
the lifting frame (315) is rotatably connected to the outer sides of the other ends of the first rotating frame (313) and the second rotating frame (314) through pin shafts;
a first mounting frame (316) mounted in the middle of the left bottom end of the bottom frame (312);
the driving motor (317) is rotationally connected to the inner side of the first mounting frame (316) through a pin shaft, and the driving motor (317) is electrically connected with the control system (5);
a second mounting frame (318) mounted in the middle of the left side of the first rotating frame (313);
the screw nut (319) is rotationally connected to the inner side of the second mounting frame (318) through a pin shaft;
the screw rod (320) is fixedly arranged at the top of the rotating end of the driving motor (317), and the screw rod (320) is in threaded connection with the inner side of the screw nut (319);
a top housing (321) disposed on top of the lift frame (315);
the horizontal moving component (322) is arranged on the inner side of the top shell (321) along the left-right direction, and the horizontal moving component (322) is electrically connected with the control system (5);
The horizontal rotating component (323) is arranged at the top of the moving end of the horizontal moving component (322), and the horizontal rotating component (323) is electrically connected with the control system (5);
the clamping component (324) is arranged at the top of the rotating end of the horizontal rotating component (323), and the clamping component (324) is electrically connected with the control system (5).
4. A remote monitoring method for smart city security management, which is applied to a remote monitoring system for smart city security management as claimed in claim 3, comprising the steps of:
step one: according to urban planning and safety requirements, the number and positions of fixed monitoring devices, movable monitoring devices and data transmission equipment to be installed are determined so as to ensure full coverage of urban internal monitoring and signal transmission;
step two: deploying and installing a fixed camera, ensuring the monitoring angle and the visual field of the fixed camera, and configuring the parameters of the fixed camera and the network connection of data transmission equipment in the current area;
step three: the cruise monitoring unmanned aerial vehicle (9) carries out cruise shooting monitoring in the urban upper air, remotely sends data to the inside of the network system (6) and uploads the data to data transmission equipment in an external area through the network system (6);
Step four: the cruise monitoring unmanned aerial vehicle (9) contacts with the electric winder (38) in the process of gliding along the top of the landing component shell (31) after the cruise shooting is finished, so that the driving vehicle (34) moves rightwards and the driving base (35) contacts with the hydraulic speed reducing rod (33) to generate energy consumption, the speed reducing effect on the first groove body (32) is realized, and the cruise monitoring unmanned aerial vehicle (9) is ensured to stop at a preset position;
step five: the driving motor (317) drives the screw rod (320) to rotate, the screw nut (319) drives the first rotating frame (313) to rotate upwards, the top shell (321) is enabled to move out of the inner cavity of the second groove body (310), the horizontal rotating component (323) drives the clamping component (324) to rotate to clamp and fix the bottom of the cruise monitoring unmanned aerial vehicle (9) and continuously move upwards, so that the cruise monitoring unmanned aerial vehicle (9) is separated from being connected with the blocking steel cable (39), the tractor (311) moves to the right side, the horizontal rotating component (323) drives the clamping component (324) to drive the cruise monitoring unmanned aerial vehicle (9) to rotate horizontally, the horizontal moving component (322) drives the horizontal rotating component (323) to drive the clamping component (324) to enable the cruise monitoring unmanned aerial vehicle (9) to move to the position above the direction regulating component (23), and the clamping component (324) is separated from being clamped and fixed with the cruise monitoring unmanned aerial vehicle (9), so that the cruise monitoring unmanned aerial vehicle (9) is transported to the top of the direction regulating component (23);
Step six: the lifting part (22) drives the direction adjusting part (23) to move downwards so as to drive the cruise monitoring unmanned aerial vehicle (9) to enter the shell (21), and a worker can enter the underground platform (1) to maintain and charge the cruise monitoring unmanned aerial vehicle (9) to finish preparation before flying;
step seven: the direction adjusting component (23) adjusts the position direction of the cruise monitoring unmanned aerial vehicle (9), the telescopic carrying component (24) moves the cruise monitoring unmanned aerial vehicle (9) to the top of the electromagnetic chuck base (212) through self extension and clamping, and the electromagnetic chuck base (212) is magnetically connected with the cruise monitoring unmanned aerial vehicle (9) to realize secondary take-off cruise preparation;
step eight: the electric telescopic rod (28) drives the supporting seat (27) to rotate upwards by self extension under the cooperation of the rotating seat (26) by taking the inner side axle center of the fixed seat (25) as an axial direction, the electric telescopic rod (28) enables the tank shell (210) to rotate upwards to the tilting device under the cooperation of the supporting seat (27) and the mounting frame (29), and enables the left side of the tank shell (210) to move upwards out of the interior of the underground platform (1);
step nine: the ejection component (211) drives the electromagnetic chuck base (212) to move at a high speed in the inner cavity of the tank body shell (210), and drives the cruise monitoring unmanned aerial vehicle (9) to move at a high speed under the cooperation of the electromagnetic chuck base (212) to obtain an initial speed so as to eject the cruise monitoring unmanned aerial vehicle, and the cruise monitoring unmanned aerial vehicle (9) flies and carries out high-altitude monitoring again after starting an engine and adjusting the gesture;
Step ten: the data transmission equipment transmits the image data uploaded by the fixed monitoring device and the movable monitoring device to the data processing device, the data processing device runs internal image processing and computer vision algorithm, analyzes and processes the captured video data, detects a moving object, recognizes a target, analyzes behaviors, generates corresponding data and alarm information, optimizes and adjusts abnormality detection and early warning rules by combining historical data and real-time conditions, generates corresponding alarm information and transmits the alarm information to the inside of the management platform;
step eleven: the management platform triggers an alarm to inform related departments or personnel and provides corresponding suggestions and guidance according to abnormal conditions detected by the early warning rules and algorithms, and starts corresponding emergency response systems and equipment to dispatch on-site monitoring personnel or emergency teams for processing and disposal.
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