Satellite data and unmanned aerial vehicle inspection data iteration artificial intelligence analysis system

Abstract

The invention discloses an iterative artificial intelligence analysis system for satellite data and unmanned aerial vehicle inspection data. The system comprises an online monitoring module, a video acquisition module, a satellite positioning module, a data processing module, a data analysis module, a prediction result output module, a terminal server and a feedback loop module. According to the invention, real-time acquisition and comprehensive analysis of monitoring data, inspection data and satellite data of an inspection area can be realized, real-time optimization effects on real-time discovery of abnormity, rapid identification of potential risks and the like can be realized, and visual display and feedback circulation of the data can be realized, so that various data and prediction results can be conveniently checked and understood; powerful information support is provided for workers when the workers deal with emergency situations, and the analysis processing flow can be continuously optimized, so that the working efficiency and the analysis accuracy are improved; and the ventilation quantity can be adjusted as required according to different environments, different occasions and different time in the heat dissipation process.

Description

Technical Field

[0001] The present invention relates to the technical field of intelligent data analysis. Specifically, it relates to an iterative artificial intelligence analysis system for satellite data and unmanned aerial vehicle (UAV) inspection data. Background Art

[0002] Intelligent data analysis refers to an analysis method that uses data analysis tools such as statistics, pattern recognition, machine learning, and data abstraction to discover knowledge from data. The purpose of intelligent data analysis is to directly or indirectly improve work efficiency, act as an intelligent assistant in actual use, enable staff to have the right information at the right time, and help them make correct decisions within a limited time.

[0003] With the acceleration of the urbanization process, there are more and more complex environments such as high-rise buildings, underground spaces, and large shopping malls, and the existing risks are also increasing. Therefore, to improve safety, a combination of UAVs and manual inspections is usually adopted for monitoring. However, there are a series of problems such as high risk of high-altitude operations for personnel, high cost of manual inspections, low efficiency of manual inspections, and it is difficult to collect, process, and analyze inspection data in real time and accurately analyze and predict risks.

[0004] At the same time, when performing data analysis, a terminal device is required.

[0005] The patent document with the publication number CN219999836U discloses a shell dust-proof mechanism and an intelligent analysis terminal device for UAV inspection data. By setting a plugging component and a fixing component, the heat dissipation channels of the terminal shell are opened during use and closed when not in use, achieving the effect that the heat dissipation channels are not easily accumulated with dust when heat dissipation is not in progress, which is beneficial to the service life of the entire heat dissipation device and also beneficial to the performance of the terminal in subsequent use. At the same time, a folding component and a support component are set, so that the terminal can adapt to various uneven ground surfaces to support and operate on the ground during outdoor operations, facilitating the staff and improving work efficiency. Through the industrial control computer component, hardware compatibility, structural rationality, operating power consumption, and heat dissipation are fully considered, greatly improving the performance of the intelligent analysis terminal, significantly enhancing the user experience, and being convenient for operation and use.

[0006] Although the above-mentioned shell dust-proof mechanism and intelligent analysis terminal device for UAV inspection data can solve corresponding technical problems, the open state of its plugging component is difficult to adjust, resulting in difficulty in ventilation regulation according to the increase in environmental temperature and difficulty in meeting the use of different ventilation conditions. When the heat dissipation channels are too large, it is easy for excessive external humid air to enter the shell, which is likely to damage the industrial control computer component inside the shell, thereby affecting the normal use of the industrial control computer component.

[0007] For this purpose, an iterative artificial intelligence analysis system for satellite data and UAV inspection data is proposed. Summary of the Invention

[0008] The technical task of the present invention is to provide an iterative artificial intelligence analysis system for satellite data and UAV inspection data to solve the above-mentioned problems in view of the above deficiencies.

[0009] To achieve the above object, the present invention provides the following technical solutions:

[0010] An iterative artificial intelligence analysis system for satellite data and UAV inspection data includes an online monitoring module, a video acquisition module, a satellite positioning module, a data processing module, a data analysis module, a prediction result output module, a terminal server, and a feedback loop module;

[0011] Among them, the online monitoring module is connected to the sensor device and is used to collect the real-time monitoring data of the sensor device;

[0012] The video acquisition module is connected to the UAV and is used to collect the inspection data of the UAV;

[0013] The satellite positioning module is used to obtain the position information of the sensor device and the UAV in real time and perform positioning;

[0014] The data processing module is used to process the collected monitoring data, inspection data, and satellite data;

[0015] The data analysis module is used to perform non-normal operation state, fault, or danger warning assessment on the processed monitoring data, inspection data, and satellite data, and plan the emergency measures for the inspection area according to the assessment level;

[0016] The terminal server is connected to the computer and is used to visually display the warning assessment;

[0017] The feedback loop module is used to continuously obtain user feedback and the operation data of the system itself, discover and correct its own deficiencies, so as to achieve continuous iterative optimization.

[0018] Preferably, the terminal server includes a housing, a shielding component, an adjusting component, a clamping component, and a supporting component;

[0019] The housing is used to provide an installation basis for the terminal server components. Two symmetrically arranged heat dissipation holes are provided on one side of the housing, and the heat dissipation holes are used to ventilate and dissipate heat when the terminal server components are running;

[0020] The shielding component is used to shield the heat dissipation holes. There are two shielding components provided on the housing, and the shielding components are arranged in one-to-one correspondence with the heat dissipation holes;

[0021] The adjusting component is used to adjust the opening and closing state of the shielding component, and the adjusting component is arranged between two shielding components;

[0022] The clamping component is used to lock the adjusting component, and the clamping component is arranged between the adjusting component and the housing;

[0023] The supporting component is used to support the housing, and the supporting component is arranged at the bottom of the housing.

[0024] Preferably, the shielding component includes a frame arranged on the housing, the frame is communicated with the heat dissipation holes, a plurality of equally spaced baffles are rotatably connected in the inner cavity of the frame from top to bottom in sequence, and two adjacent baffles are in two states of vertical contact and inclined parallel, a filter screen is arranged between the frame and the housing, mounting plates are integrally formed at the top and bottom of the frame, the mounting plates are detachably connected to the housing through screws, an installation groove adapted to the filter screen is formed on one side of the frame facing the housing, and the filter screen is clamped into the inner cavity of the installation groove.

[0025] Preferably, the adjusting component includes a shield respectively fixedly connected to opposite sides of two frames, gears with the same number as the baffles in the frame are arranged up and down in the inner cavity of the shield, the gears are arranged in one-to-one correspondence with the baffles, a rotating rod is fixedly connected to one side of the gear, one end of the rotating rod penetrates into the adjacent frame and is fixedly connected to the corresponding baffle, a rack is movably connected in the inner cavity of the shield, and a plurality of gears in the shield are all meshed with the rack, a convex strip is fixedly connected to one side of the rack away from the gear, a groove is formed on the inner wall surface of the shield, and one side of the convex strip penetrates into the inner cavity of the groove and is slidably connected to the inner wall surface of the groove.

[0026] Preferably, a connecting rod is fixedly connected between the two racks, a through groove for the connecting rod to pass through is formed on the shield, the inner wall surface of the through groove is slidably connected to the surface of the connecting rod, a folding baffle curtain is fixedly connected to the top and bottom of the inner wall surface of the through groove, opposite sides of the two folding baffle curtains are fixedly connected to the corresponding connecting rod, and both sides of the folding baffle curtain are slidably connected to the inner wall surface of the through groove.

[0027] Preferably, the clamping component includes a convex block fixedly connected to the center of the top of the connecting rod, two groups of blocking blocks are fixedly connected to the surface of the housing and on the same side of the heat dissipation holes, the two groups of blocking blocks are respectively located on both sides of the convex block, at least four blocking blocks are arranged up and down in each group, a clamping groove is formed between two adjacent blocking blocks up and down, and a kneading piece matched with the clamping groove is arranged on each side of the convex block.

[0028] Preferably, the kneading member includes a clamping block movably disposed on one side of the bump. The clamping block is clamped into a corresponding card slot. One end of the clamping block is fixedly connected to a finger plate. Two first lugs arranged vertically are fixedly connected to the finger plate. A shaft rod movably penetrates between the two first lugs. Both ends of the shaft rod are fixedly connected to a second lug. One side of the second lug is fixedly connected to the bump. A torsion spring is sleeved on the surface of the shaft rod. Both ends of the torsion spring are respectively connected to the bump and the finger plate.

[0029] Preferably, the support assembly includes a bottom plate disposed at the bottom of the housing. Legs are rotatably connected to the four corners of the bottom of the bottom plate. At least two symmetrically arranged connecting members are provided between the bottom plate and the housing.

[0030] Preferably, the connecting member includes a dovetail groove opened at the top of the bottom plate. One end of the dovetail groove is open, and the other end is closed. A dovetail bar is slidably connected to the inner cavity of the dovetail groove. The top of the dovetail bar is fixedly connected to the bottom of the housing. A blocking member is provided on the bottom plate at the opening of the dovetail groove.

[0031] Preferably, the blocking member includes a dovetail tenon movably connected to the opening of the inner cavity of the dovetail groove. One side of the dovetail tenon contacts one end of the dovetail bar. A U-shaped seat is integrally formed at the bottom of the bottom plate. The bottom of the dovetail tenon penetrates to the inner cavity of the U-shaped seat. A first magnetic block is embedded at the top of the dovetail tenon. A second magnetic block is embedded at the bottom of the housing. The first magnetic block is magnetically adsorbed to the bottom of the second magnetic block. A limiting member is provided between the dovetail tenon and the U-shaped seat.

[0032] Compared with the prior art, the advantages and positive effects of the present invention are as follows:

[0033] 1. In the present invention, through the combined use of the on-line monitoring module, video acquisition module, satellite positioning module, data processing module, data analysis module, prediction result output module, terminal server and feedback loop module, it is possible to realize the real-time acquisition and comprehensive analysis of the monitoring data, inspection data and satellite data in the inspection area, timely obtain the actual situation of the inspection area, perform target positioning and early warning in the inspection area, play a real-time optimization role in real-time discovery of abnormalities and rapid identification of potential risks, and the visual display and feedback loop of data can not only facilitate the viewing and understanding of various data and prediction results, provide strong information support for the staff in dealing with emergencies, help them make more scientific and accurate decisions, but also continuously optimize the analysis and processing process, continuously adjust and optimize the early warning model and threshold, enable the system to have the ability of self-learning and optimization, gradually improve the accuracy of prediction and early warning, and thus improve the work efficiency and the accuracy of analysis;

[0034] 2. In the present invention, through the movable connecting rod, a plurality of baffles within two frames can be driven to rotate synchronously, such that two adjacent baffles are in a vertically contacting or inclined parallel state, thereby achieving the functions of shielding against dust and ventilation and heat dissipation. The operation is simple and convenient. At the same time, when the connecting rod is moved to different positions, the rotation angle of the baffle can change accordingly. When the inclination angle of the baffle is small, the gap between two adjacent baffles is small, and thus the ventilation volume decreases accordingly. When the inclination angle of the baffle is large, the gap between two adjacent baffles is large, and thus the ventilation volume increases accordingly. Therefore, the ventilation volume can be adjusted as needed according to different environments, different occasions, and different times during the heat dissipation process, and the inner cavity of the frame can be sealed during the dust prevention process, which is convenient to use.

[0035] 3. In the present invention, by squeezing two squeezing members towards each other, the adjusting assembly can be unlocked, so that the clamping assembly can be used as a handle to move the connecting rod. After the connecting rod is moved to the desired position, release the squeezing members, and the clamping block is clamped into the corresponding card slot, thereby locking the adjusting assembly. Furthermore, the adjusting assembly and the shielding assembly can be stably maintained in the desired state to improve the ventilation or dust prevention effect. BRIEF DESCRIPTION OF THE DRAWINGS

[0036] In order to more clearly illustrate the technical solutions in the embodiments of the present invention or the prior art, the following will briefly introduce the drawings required for use in the embodiments. Obviously, the following described drawings are only some embodiments of the present invention. For those of ordinary skill in the art, without creative efforts, other drawings can be obtained based on these drawings.

[0037] Figure 1 It is a schematic structural diagram of a terminal server in an iterative artificial intelligence analysis system for satellite data and unmanned aerial vehicle inspection data according to an embodiment of the present invention;

[0038] Figure 2 It is an exploded schematic structural diagram of the housing and the shielding assembly of a terminal server in an iterative artificial intelligence analysis system for satellite data and unmanned aerial vehicle inspection data according to an embodiment of the present invention;

[0039] Figure 3 It is a schematic structural diagram of the shielding assembly, the adjusting assembly, and the clamping assembly of a terminal server in an iterative artificial intelligence analysis system for satellite data and unmanned aerial vehicle inspection data according to an embodiment of the present invention;

[0040] Figure 4 It is an exploded schematic structural diagram of the shielding assembly and the adjusting assembly of a terminal server in an iterative artificial intelligence analysis system for satellite data and unmanned aerial vehicle inspection data according to an embodiment of the present invention;

[0041] Figure 5Schematic diagram of the partial structure of the shielding component and the adjusting component of the terminal server in the satellite data and UAV inspection data iterative artificial intelligence analysis system according to the embodiment of the present invention;

[0042] Figure 6 Schematic diagram of the structure of the baffle and the rotating rod of the terminal server in the satellite data and UAV inspection data iterative artificial intelligence analysis system according to the embodiment of the present invention;

[0043] Figure 7 Schematic diagram of the structure of the outer shell and the clamping component of the terminal server in the satellite data and UAV inspection data iterative artificial intelligence analysis system according to the embodiment of the present invention;

[0044] Figure 8 Exploded schematic diagram of the structure of the bump and the kneading piece of the terminal server in the satellite data and UAV inspection data iterative artificial intelligence analysis system according to the embodiment of the present invention;

[0045] Figure 9 Exploded schematic diagram of the structure of the outer shell and the supporting component of the terminal server in the satellite data and UAV inspection data iterative artificial intelligence analysis system according to the embodiment of the present invention;

[0046] Figure 10 For Figure 9 Enlarged schematic diagram of the structure at A in

[0047] Figure 11 Exploded schematic diagram of the structure of the bottom plate and the blocking piece of the terminal server in the satellite data and UAV inspection data iterative artificial intelligence analysis system according to the embodiment of the present invention.

[0048] In the figure: 100, outer shell;

[0049] 200, shielding component; 210, frame; 211, mounting plate; 212, mounting groove; 220, baffle; 230, filter screen;

[0050] 300, adjusting component; 310, shield; 311, groove; 320, gear; 330, rotating rod; 340, rack; 341, rib; 350, connecting rod; 360, through groove; 370, folding curtain;

[0051] 400, clamping component; 410, bump; 420, block; 430, kneading piece; 431, clamping block; 432, finger plate; 433, first lug; 434, shaft rod; 435, second lug; 436, torsion spring; 440, T-shaped block;

[0052] 500. Support component; 510. Base plate; 520. Leg; 530. Connecting piece; 531. Dovetail groove; 532. Dovetail bar; 533. Blocking piece; 5331. Dovetail tenon; 5332. U-shaped seat; 5333. First magnetic block; 5334. Second magnetic block; 5335. Slide groove; 5336. Slide block; 5337. Projection. Detailed implementation manner

[0053] In order to more clearly understand the above-mentioned objects, features and advantages of the present invention, the present invention will be further described below with reference to the drawings and embodiments. It should be noted that, without conflict, the embodiments of the present application and the features in the embodiments may be combined with each other.

[0054] The present invention will be further described below with reference to the drawings and specific embodiments.

[0055] Embodiment 1

[0056] A satellite data and UAV inspection data iterative artificial intelligence analysis system according to an embodiment of the present invention includes an online monitoring module, a video acquisition module, a satellite positioning module, a data processing module, a data analysis module, a prediction result output module, a terminal server, and a feedback loop module;

[0057] Among them, the online monitoring module is connected to the sensor device and is used to collect the real-time monitoring data of the sensor device;

[0058] The video acquisition module is connected to the UAV and is used to collect the inspection data of the UAV;

[0059] The satellite positioning module is used to obtain the position information of the sensor device and the UAV in real time and perform positioning;

[0060] The data processing module is used to process the collected monitoring data, inspection data, and satellite data, including data cleaning, format conversion, and data encryption operations. Let the original monitoring data be Dm, the original inspection data be Dp, and the original satellite data be Ds. After data cleaning and format conversion, the data availability improvement coefficient is k1 (0≤k1≤1), and the data accuracy improvement coefficient is k2 (0≤k2≤1). Then the processed data Dt can be expressed as: Dt = k1k2(Dm + Dp + Ds). Encrypting the data can prevent the data from being illegally obtained or tampered with. In addition, data cleaning and format conversion operations can improve the availability and accuracy of the data;

[0061] The data analysis module is used to conduct abnormal operation status, fault or danger early warning assessments on the processed monitoring data, inspection data, and satellite data, and plan emergency measures for the inspection area according to the assessment level. Let the assessment level be L, the weight vector of each data feature in the processed data Dt be w = [w1, w2, …, wn], the data feature value vector be x = [x1, x2, …, xn], and the early warning threshold be T. Then the calculation formula for the assessment level L is:

[0062] And plan emergency measures for the inspection area according to the assessment level;

[0063] The terminal server is connected to the computer and is used for visual display of the early warning assessment, including visual display of the early warning assessment and report generation of the early warning assessment;

[0064] The feedback loop module is used to continuously obtain user feedback and the system's own operation data, discover and correct its own deficiencies, so as to achieve continuous iterative optimization.

[0065] Let the initial performance index of the system be P0, the user feedback correction coefficient be k3 (0 ≤ k3 ≤ 1), and the system's own operation data correction coefficient be k4 (0 ≤ k4 ≤ 1). The performance index Pn after n iterations can be expressed as:

[0066]

[0067] Among them, Fi is the user feedback correction amount for the i-th iteration, and Si is the system's own operation data correction amount for the i-th iteration.

[0068] Embodiment 2

[0069] Such as Figures 1-11 As shown, a satellite data and UAV inspection data iterative artificial intelligence analysis system provided in this embodiment is different from that in Embodiment 1 in that:

[0070] The terminal server includes a housing 100, a shielding component 200, an adjusting component 300, a clamping component 400, and a supporting component 500;

[0071] The housing 100 is used to provide an installation basis for the terminal server components. Two symmetrically arranged heat dissipation holes are opened on one side of the housing 100, and the heat dissipation holes are used to ventilate and dissipate heat when the terminal server components are running;

[0072] The shielding component 200 is used to shield the heat dissipation holes. There are two shielding components 200 provided on the housing 100, and the shielding component 200 is arranged in one-to-one correspondence with the heat dissipation holes;

[0073] The adjusting component 300 is used to adjust the opening and closing state of the shielding component 200, and the adjusting component 300 is arranged between two shielding components 200;

[0074] The clamping component 400 is used to lock the adjusting component 300, and the clamping component 400 is arranged between the adjusting component 300 and the housing 100;

[0075] The supporting component 500 is used to support the housing 100, and the supporting component 500 is arranged at the bottom of the housing 100.

[0076] Embodiment 3

[0077] As Figures 1-11 shown, the difference between the satellite data and UAV inspection data iterative artificial intelligence analysis system provided in this embodiment and Embodiment 2 is as follows:

[0078] The shielding component 200 includes a frame 210 arranged on the housing 100. The frame 210 is communicated with the heat dissipation holes. A plurality of equally spaced baffles 220 are rotatably connected in the inner cavity of the frame 210 from top to bottom through a rotating shaft. The adjacent two baffles 220 are in two states of vertical contact and inclined parallel. When the adjacent two baffles 220 are in a vertically contacting state, the inner cavity of the frame 210 can be completely blocked; when the adjacent two baffles 220 are in an inclined parallel state, the frame 210 and the heat dissipation holes can cooperate to realize the ventilation and heat dissipation function. A filter screen 230 is arranged between the frame 210 and the housing 100. The filter screen 230 can play a dust-proof role during the ventilation and heat dissipation process, further improving the dust-proof effect and being beneficial to the operation of the terminal server component in the housing 100. Installation plates 211 are integrally formed at the top and bottom of the frame 210. The installation plates 211 are detachably connected to the housing 100 through screws. An installation groove 212 adapted to the filter screen 230 is formed on one side of the frame 210 facing the housing 100. The filter screen 230 is clamped into the inner cavity of the installation groove 212. By adopting a detachable connection between the frame 210 and the housing 100 and between the filter screen 230 and the frame 210, it is convenient to disassemble, clean or replace the filter screen 230 later, which helps to improve the ventilation effect and the dust-proof effect.

[0079] The adjusting assembly 300 includes a baffle 310 fixedly connected to the opposite sides of the two frames 210 respectively. The inner cavity of the baffle 310 is provided with gears 320 in the up and down direction, and the number of gears 320 is the same as that of the inner baffles 220 of the frame 210. The gears 320 are arranged in one-to-one correspondence with the baffles 220. One side of the gear 320 is fixedly connected with a rotating rod 330. One end of the rotating rod 330 penetrates into the adjacent frame 210 and is fixedly connected with the corresponding baffle 220. The inner cavity of the baffle 310 is movably connected with a vertically arranged rack 340. A plurality of gears 320 in the baffle 310 are all engaged with the rack 340. By moving the rack 340 up and down, the teeth can drive a plurality of gears 320 to rotate synchronously, and then the plurality of baffles 220 in the frame 210 can be adjusted synchronously in angle, which is convenient for operation. One side of the rack 340 away from the gear 320 is fixedly connected with a convex strip 341. A groove 311 is formed on the inner wall surface of the baffle 310. One side of the convex strip 341 penetrates into the inner cavity of the groove 311 and is slidably connected with the inner wall surface of the groove 311. When the rack 340 moves up and down, it can drive the convex strip 341 to slide in the inner cavity of the groove 311, and then can play a guiding role for the rack 340, so that the rack 340 can move up and down stably; A horizontally arranged connecting rod 350 is fixedly connected between the two racks 340. A through groove 360 for the connecting rod 350 to pass through is formed on the baffle 310. The inner wall surface of the through groove 360 is slidably connected with the surface of the connecting rod 350. A folding curtain 370 is fixedly connected to the top and bottom of the inner wall surface of the through groove 360. One side of the two folding curtains 370 opposite to each other is fixedly connected to the corresponding connecting rod 350. Both sides of the folding curtain 370 are slidably connected with the inner wall surface of the through groove 360. The through groove 360 can not only provide a moving space for the connecting rod 350, so that the connecting rod 350 can drive the two racks 340 to move up and down at the same time, but also play a limiting role for the connecting rod 350, so that the connecting rod 350 can move up and down stably. The folding curtain 370 can not only block the through groove 360 to prevent dust and other impurities from entering the baffle 310 through the through groove 360, but also can perform telescopic operation along with the movement of the connecting rod 350 to ensure the normal up and down movement of the connecting rod 350 in the through groove 360.

[0080] The snap - fit component 400 includes a bump 410 fixedly connected to the center of the top of the connecting rod 350. On the surface of the outer shell 100 and on the same side of the heat dissipation holes, two groups of stoppers 420 are fixedly connected. The two groups of stoppers 420 are respectively located on both sides of the bump 410. Each group of stoppers 420 is arranged vertically with at least four. A clamping groove is formed between two adjacent stoppers 420 up and down. On both sides of the bump 410, there is respectively a kneading member 430 for cooperating with the clamping groove. By snapping the kneading member 430 into the corresponding clamping groove, the connecting rod 350 can be locked, so that the connecting rod 350 is stably maintained in the required position, avoiding the accidental movement of the connecting rod 350 due to its own gravity or the collision of external forces, and further enabling the baffle 220 to be stably maintained in a certain state; The kneading member 430 includes a clamping block 431 movably arranged on one side of the bump 410 and having an L - shaped structure. The clamping block 431 is snapped into the corresponding clamping groove. One end of the clamping block 431 is fixedly connected with a finger plate 432. Two first lugs 433 arranged vertically are fixedly connected to the finger plate 432. A shaft rod 434 is movably penetrated between the two first lugs 433. Both ends of the shaft rod 434 are fixedly connected with a second lug 435. One side of the second lug 435 is fixedly connected with the bump 410. A torsion spring 436 is sleeved on the surface of the shaft rod 434. Both ends of the torsion spring 436 are respectively connected to the bump 410 and the finger plate 432. By squeezing the two finger plates 432 towards each other, the clamping block 431 can be driven to rotate around the shaft rod 434, so that the clamping block 431 can be disengaged from the clamping groove to realize the unlocking operation of the connecting rod 350, and then the connecting rod 350 can be moved by using the kneading member 430; Due to the elastic force of the torsion spring 436, the finger plate 432 and the clamping block 431 can be automatically reset, and the clamping block 431 can be stably snapped into the clamping groove. A T - shaped block 440 is integrally formed on the side of the bump 410 away from the outer shell 100. When the clamping block 431 is disengaged from the clamping groove, the finger plate 432 can contact the T - shaped block 440, which can limit the movement of the finger plate 432 and avoid excessive movement of the finger plate 432 and damage to the torsion spring 436.

[0081] The support assembly 500 includes a bottom plate 510 provided at the bottom of the outer shell 100. Legs 520 are rotatably connected to the four corners of the bottom of the bottom plate 510 through damping rotating shafts. At least two symmetrically arranged connecting members 530 are provided between the bottom plate 510 and the outer shell 100. The connecting member 530 includes a dovetail groove 531 opened at the top of the bottom plate 510. One end of the dovetail groove 531 is open, and the other end is closed. A dovetail bar 532 is slidably connected to the inner cavity of the dovetail groove 531. The top of the dovetail bar 532 is fixedly connected to the bottom of the outer shell 100. A blocking member 533 is provided on the bottom plate 510 at the opening of the dovetail groove 531. The detachable connection between the outer shell 100 and the bottom plate 510 can be realized through the connecting member 530, which is convenient for assembling or disassembling the outer shell 100 and the bottom plate 510 according to actual use requirements in the future. The blocking member 533 includes a dovetail tenon 5331 movably connected to the opening of the inner cavity of the dovetail groove 531. One side of the dovetail tenon 5331 contacts one end of the dovetail bar 532. A U-shaped seat 5332 is integrally formed at the bottom of the bottom plate 510. The bottom of the dovetail tenon 5331 penetrates to the inner cavity of the U-shaped seat 5332. A first magnetic block 5333 is embedded at the top of the dovetail tenon 5331. A second magnetic block 5334 is embedded at the bottom of the outer shell 100. The first magnetic block 5333 is magnetically adsorbed to the bottom of the second magnetic block 5334. The dovetail bar 532 can be blocked by the blocking member 533, so that the dovetail bar 532 can be stably placed in the dovetail groove 531 and prevent the dovetail bar 532 from slipping out of the dovetail groove 531. A limiting member is provided between the dovetail tenon 5331 and the U-shaped seat 5332. The limiting member includes a chute 5335 opened on the inner wall surface of the U-shaped seat 5332. A slider 5336 is fixedly connected to the surface of the dovetail tenon 5331. One side of the slider 5336 penetrates to the inner cavity of the chute 5335 and is slidably connected to the inner wall surface of the chute 5335. The dovetail tenon 5331 can be guided by the limiting member, so that the dovetail tenon 5331 can move up and down stably and prevent the dovetail tenon 5331 from slipping out of the inner cavity of the U-shaped seat 5332. A protrusion 5337 is integrally formed on one side of the dovetail tenon 5331 away from the dovetail bar 532. The friction between the hand and the dovetail tenon 5331 can be increased through the protrusion 5337, which is convenient for the hand to dial the dovetail tenon 5331.

[0082] It should be noted that the structure and working principle of the above-mentioned leg 520 are the same as those of the support assembly in the shell dust-proof mechanism and the UAV inspection data intelligent analysis terminal device disclosed in the existing patent No. CN219999836U, and it can adapt to various uneven ground surfaces. It is prior art, so it will not be elaborated too much in this technical solution.

[0083] Working principle:

[0084] Assembly of the housing 100 and the support component 500: Align the dovetail bar 532 with the open end of the dovetail groove 531 and slide it in so that the dovetail bar 532 gradually slides into the dovetail groove 531 until the maximum limit is reached to achieve the preliminary connection between the housing 100 and the support component 500. Then, use the protrusion 5337 to push up the dovetail tenon 5331, so that the dovetail tenon 5331 drives the first magnet block 5333 and the slider 5336 to move upward synchronously. The slider 5336 slides in the inner cavity of the chute 5335 until the first magnet block 5333 is magnetically adsorbed to the bottom of the corresponding second magnet block 5334, so that the dovetail tenon 5331 blocks one end of the dovetail bar 532, making it difficult for the dovetail bar 532 to slide out of the inner cavity of the dovetail groove 531 to achieve the reconnection between the housing 100 and the support component 500. Thus, the assembly operation of the housing 100 and the support component 500 can be completed. By rotating the leg 520 to make the leg 520 in a vertical state and adjusting the support height of the leg 520 according to the terrain, the support operation for the housing 100 can be completed;

[0085] Analysis and early warning: The data processing module collects the monitoring data, inspection data, and satellite data of the inspection area in real time to timely obtain the actual situation of the inspection area, and the data analysis module comprehensively analyzes the monitoring data, inspection data, and satellite data. According to the formula calculate the evaluation level, which can perform target positioning and early warning in the inspection area. By using the terminal server and the computer in cooperation, the early warning evaluation is visually displayed, which can conveniently view and understand various data and prediction results, providing strong information support for the staff when dealing with emergencies and helping them make more scientific and accurate decisions. Through the feedback loop module, according to the formula iteratively optimize the system performance, which can continuously optimize the analysis and processing process, continuously adjust and optimize the early warning model and threshold, enable the system to have the ability of self-learning and optimization, gradually improve the accuracy of prediction and early warning, and thus improve the work efficiency and the accuracy of analysis;

[0086] Ventilation and heat dissipation: Squeeze the two finger plates 432 towards each other, so that the finger plates 432 drive the latch 431 and the first lug 433 to rotate around the shaft rod 434. The finger plates 432 squeeze the torsion spring 436, causing the torsion spring 436 to deform under force until the finger plates 432 contact the T-shaped block 440. At this time, the latch 431 disengages from the inner cavity of the card slot to achieve the unlocking effect on the connecting rod 350. Then move the finger plates 432 upward, so that the finger plates 432 drive the first lug 433, the latch 431, the shaft rod 434, the second lug 435, the torsion spring 436, the convex block 410 and the T-shaped block 440 to move upward synchronously. The convex block 410 drives the connecting rod 350, the rack 340 and the convex strip 341 to move synchronously. The connecting rod 350 slides in the inner cavity of the through groove 360, and the folding curtain 370 is stretched or contracted under force. The convex strip 341 slides in the inner cavity of the groove 311. The teeth of the rack 340 drive the gear 320 to rotate, and the gear 320 drives the rotating rod 330 and the baffle 220 to rotate synchronously around the rotating rod 330 to achieve the angle adjustment of the baffle 220, so that two adjacent baffles 220 are in an inclined parallel state. After adjusting the baffle 220 to the required angle according to different environments, different occasions and different times, release the finger plates 432. Through the elastic restoring force of the torsion spring 436, the finger plates 432, the first lug 433 and the latch 431 are automatically reset, and then the latch 431 is clamped into the corresponding card slot to achieve the locking effect on the connecting rod 350, so that external air can enter the frame 210 through the gap between two adjacent baffles 220, and the heat inside the housing 100 can be discharged into the frame 210 through the gap between two adjacent baffles 220, and the ventilation and heat dissipation operation of the terminal server components in the housing 100 can be completed.

[0087] Shielding and dust prevention: Squeeze the two finger plates 432 towards each other, so that the latch 431 disengages from the inner cavity of the card slot to achieve the unlocking effect on the connecting rod 350. Then move the finger plates 432 downward until the maximum limit, and then release the finger plates 432. Through the elastic restoring force of the torsion spring 436, the finger plates 432, the first lug 433 and the latch 431 are automatically reset, and then the latch 431 is clamped into the corresponding card slot to achieve the locking effect on the connecting rod 350, so that two adjacent baffles 220 are in a vertically contacting state to achieve the blocking effect on the inside of the frame 210, and the shielding and dust prevention operation of the terminal server components in the housing 100 can be completed.

[0088] Through the above specific embodiments, those skilled in the art of the present invention can easily implement the present invention. However, it should be understood that the present invention is not limited to the above specific embodiments. Based on the disclosed embodiments, those skilled in the art can arbitrarily combine different technical features to achieve different technical solutions.

Claims

1. An iterative artificial intelligence analysis system for satellite data and drone inspection data, characterized in that: It includes online monitoring module, video acquisition module, satellite positioning module, data processing module, data analysis module, prediction result output module, terminal server and feedback loop module; Wherein, the online monitoring module is connected to the sensor device and is used to collect real-time monitoring data of the sensor device; The video acquisition module is connected to the drone and is used to collect inspection data of the drone; The satellite positioning module is used to obtain the position information of the sensor device and the drone in real time and perform positioning; The data processing module is used to process the collected monitoring data, inspection data and satellite data; The data analysis module is used to evaluate abnormal operating status, fault or danger warning of the processed monitoring data, inspection data and satellite data, and plan emergency measures for the inspection area according to the evaluation level; The terminal server is connected to a computer and is used to visualize the early warning assessment; The feedback loop module is used to continuously obtain user feedback and the system's own operating data, discover and correct its own deficiencies, and achieve continuous iterative optimization.

2. The satellite data and drone inspection data iterative artificial intelligence analysis system according to claim 1 is characterized by: The terminal server comprises a housing (100), a shielding component (200), an adjustment component (300), a clamping component (400) and a supporting component (500); The housing (100) is used to provide an installation base for the terminal server component, and one side of the housing (100) is provided with two symmetrically arranged heat dissipation holes, and the heat dissipation holes are used to provide ventilation and heat dissipation for the terminal server component during operation; The shielding assembly (200) is used to shield the heat dissipation holes, and two shielding assemblies (200) are provided on the housing (100), and the shielding assemblies (200) are arranged in a one-to-one correspondence with the heat dissipation holes; The adjusting component (300) is used to adjust the opening and closing state of the shielding component (200), and the adjusting component (300) is arranged between the two shielding components (200); The clamping assembly (400) is used to lock the adjusting assembly (300), and the clamping assembly (400) is arranged between the adjusting assembly (300) and the housing (100); The support assembly (500) is used to support the outer shell (100), and the support assembly (500) is arranged at the bottom of the outer shell (100).

3. The satellite data and drone inspection data iterative artificial intelligence analysis system according to claim 2 is characterized by: The shielding assembly (200) comprises a frame (210) arranged on the outer shell (100), the frame (210) being connected to the heat dissipation hole, the inner cavity of the frame (210) being rotatably connected to a plurality of equally spaced baffles (220) from top to bottom, two adjacent baffles (220) being in two states of vertical contact and inclined parallelism, a filter screen (230) being arranged between the frame (210) and the outer shell (100), a mounting plate (211) being integrally formed at the top and bottom of the frame (210), the mounting plate (211) being detachably connected to the outer shell (100) by means of screws, a mounting groove (212) matching the filter screen (230) being provided on a side of the frame (210) facing the outer shell (100), the filter screen (230) being snapped into the inner cavity of the mounting groove (212).

4. The satellite data and drone inspection data iterative artificial intelligence analysis system according to claim 3 is characterized by: The adjustment assembly (300) comprises a baffle (310) fixedly connected to opposite sides of two frames (210), the inner cavity of the baffle (310) is provided with gears (320) in the upper and lower parts, the same number as the baffles (220) in the frames (210), the gears (320) and the baffles (220) are arranged in a one-to-one correspondence, one side of the gear (320) is fixedly connected to a rotating rod (330), one end of the rotating rod (330) penetrates into the adjacent frame (210) and is connected to the corresponding The baffle (220) is fixedly connected, the inner cavity of the baffle cover (310) is movably connected with a rack (340), a plurality of gears (320) in the baffle cover (310) are all meshed with the rack (340), a side of the rack (340) away from the gear (320) is fixedly connected with a convex strip (341), the inner wall surface of the baffle cover (310) is provided with a groove (311), one side of the convex strip (341) penetrates into the inner cavity of the groove (311) and is slidably connected with the inner wall surface of the groove (311).

5. The satellite data and drone inspection data iterative artificial intelligence analysis system according to claim 4 is characterized by: A connecting rod (350) is fixedly connected between the two racks (340), a through slot (360) is provided on the shield (310) for the connecting rod (350) to pass through, the inner wall surface of the through slot (360) is slidably connected to the surface of the connecting rod (350), the top and bottom of the inner wall surface of the through slot (360) are fixedly connected to a folding curtain (370), the opposite sides of the two folding curtains (370) are fixedly connected to the corresponding connecting rod (350), and both sides of the folding curtain (370) are slidably connected to the inner wall surface of the through slot (360).

6. The satellite data and drone inspection data iterative artificial intelligence analysis system according to claim 5, characterized in that: The clamping assembly (400) comprises a protrusion (410) fixedly connected to the center of the top of the connecting rod (350), and two groups of blocks (420) are fixedly connected to the surface of the housing (100) and located on the same side of the heat dissipation hole, and the two groups of blocks (420) are respectively located on both sides of the protrusion (410), and each group of blocks (420) is provided with at least four blocks in an upper and lower arrangement, and a clamping groove is formed between two adjacent blocks (420) in an upper and lower arrangement, and a kneading piece (430) used in conjunction with the clamping groove is respectively provided on both sides of the protrusion (410).

7. The satellite data and drone inspection data iterative artificial intelligence analysis system according to claim 6, characterized in that: The kneading member (430) comprises a clamping block (431) movably arranged on one side of the protrusion (410), the clamping block (431) being clamped into a corresponding clamping slot, one end of the clamping block (431) being fixedly connected to a finger plate (432), two first lugs (433) arranged vertically are fixedly connected to the finger plate (432), an axle rod (434) is movably penetrated between the two first lugs (433), both ends of the axle rod (434) are fixedly connected to a second lug (435), one side of the second lug (435) is fixedly connected to the protrusion (410), a torsion spring (436) is sleeved on the surface of the axle rod (434), and the two ends of the torsion spring (436) are respectively connected to the protrusion (410) and the finger plate (432).

8. The satellite data and drone inspection data iterative artificial intelligence analysis system according to claim 2, characterized in that: The support assembly (500) comprises a bottom plate (510) arranged at the bottom of the housing (100), the four corners of the bottom of the bottom plate (510) are rotatably connected to legs (520), and at least two symmetrically arranged connecting members (530) are provided between the bottom plate (510) and the housing (100).

9. The satellite data and drone inspection data iterative artificial intelligence analysis system according to claim 8, characterized in that: The connecting member (530) comprises a dovetail groove (531) opened on the top of the bottom plate (510), one end of the dovetail groove (531) is open, and the other end of the dovetail groove (531) is closed. A dovetail strip (532) is slidably connected to the inner cavity of the dovetail groove (531), and the top of the dovetail strip (532) is fixedly connected to the bottom of the housing (100). A blocking member (533) is provided on the bottom plate (510) at the opening of the dovetail groove (531).

10. The satellite data and drone inspection data iterative artificial intelligence analysis system according to claim 9, characterized in that: The blocking member (533) comprises a dovetail tenon (5331) movably connected to the inner opening of the dovetail groove (531), one side of the dovetail tenon (5331) contacts one end of the dovetail strip (532), a C-shaped seat (5332) is integrally formed at the bottom of the bottom plate (510), the bottom of the dovetail tenon (5331) penetrates into the inner cavity of the C-shaped seat (5332), a first magnet block (5333) is embedded at the top of the dovetail tenon (5331), a second magnet block (5334) is embedded at the bottom of the housing (100), the first magnet block (5333) is adsorbed to the bottom of the second magnet block (5334) by magnetic force, and a limiting member is provided between the dovetail tenon (5331) and the C-shaped seat (5332).

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