Unmanned aerial vehicle detection method based on ecological restoration technology

Abstract

The invention discloses an unmanned aerial vehicle detection method based on an ecological restoration technology, belongs to the field of ecological restoration, and solves the problem that a monitoring camera cannot realize omnibearing coverage in the unmanned aerial vehicle monitoring process in the existing ecological restoration technology, and the method comprises the following steps: S1, before ecological restoration, carrying out large-scale investigation through an unmanned aerial vehicle; according to the method, partial core areas or areas worthy of attention are selected to carry out field detection, environmental elements (temperature, moisture and soil) are evaluated, a monitoring mechanism and a swing mechanism are arranged, the vegetation condition and terrain and landform data in the areas can be monitored in real time, a three-dimensional model of the areas is constructed through the monitored data subsequently, and the real-time monitoring of the areas is realized. According to the technical scheme, a corresponding ecological restoration plan can be conveniently made according to known data, the angle of the monitoring assembly can be flexibly adjusted in the monitoring process, the equipment can clearly and accurately recognize various conditions and data of the current area, the equipment monitoring accuracy is improved, and therefore the working quality of the equipment is improved.

Description

Technical Field

[0001] The present invention belongs to the technical field of ecological restoration, and in particular relates to a drone detection method based on ecological restoration technology. Background Art

[0002] The selection of plants or plant combinations used for ecological restoration often comes from experience or general restoration guidelines. However, in some special areas (such as steep slopes in mountainous canyon areas, mines), due to topography and local climate, the selected plants have poor adaptability and it is difficult to achieve the expected ecological restoration effect. In addition to the problem of plant species selection, there is a lack of accurate monitoring data and dynamic evaluation data in the plant restoration process, which makes it impossible to deal with problems in the restoration process in a timely manner, and the maintenance measures after restoration lack specificity. Now, drones are generally used to detect the surrounding topography in real time, combined with soil conditions to evaluate the ecological restoration of the current area.

[0003] Chinese invention patent CN118004424A discloses an ecological restoration partition spraying device based on a drone and a spraying method thereof. The ecological restoration partition spraying device based on a drone in the present invention comprises a drone body, and support legs are arranged at the bottom ends of both sides of the drone body. The drone body comprises a scanning mechanism, a spraying mechanism and a nozzle mechanism. When in use, the scanning mechanism of the drone itself can accurately identify geological features and ecological geological environment, and combined with the subsequent spraying mechanism, the management efficiency of ecological restoration can be improved;

[0004] The above-mentioned design can accurately scan the area to be repaired through the design of the scanning mechanism and the spraying mechanism, and then accurately spray the slurry according to the scanned terrain. However, there are certain problems in actual use. Specifically, when the drone scans the terrain of the area, the position of the overall components is fixed, and the shooting angle and shooting position of the detection camera cannot be flexibly adjusted. As a result, when scanning the terrain of the area, some areas are easily not completely scanned, resulting in the loss of final data, which affects the subsequent overall processing operations. Summary of the invention

[0005] The purpose of this section is to summarize some aspects of embodiments of the present invention and briefly introduce some preferred embodiments. Some simplifications or omissions may be made in this section and the specification abstract and the invention title of this application to avoid blurring the purpose of this section, the specification abstract and the invention title, and such simplifications or omissions cannot be used to limit the scope of the present invention.

[0006] In order to solve the problems raised in the above background technology, the present invention adopts the following technical solutions.

[0007] A drone detection method based on ecological restoration technology includes the following steps:

[0008] S1. Before ecological restoration, a large-scale survey is conducted by drones, and some core areas or areas of concern are selected for field investigations to evaluate environmental factors (light, temperature, water, soil), and local native ecosystems that are in a stable stage are selected as reference ecosystems to assist in establishing ecological restoration strategies;

[0009] S2. In ecological restoration, drones are used to conduct irregular regional monitoring. Environmental data and dynamic data on plant growth obtained from monitoring are used to accurately determine the restoration status of the current area, promptly identify problems in the current area, and solve them in a timely manner (such as through necessary irrigation and plant maintenance);

[0010] S3. In the later stage of ecological restoration, the growth of planted plants and restoration conditions in the area are observed by drones to assist in judging the restoration effect;

[0011] S4. Build a complete database; build a complete database by detecting the environmental data and plant growth data of the area.

[0012] As a preferred technical solution of the present invention, the drone used in step S1 and step S2 in claim 1 includes an aircraft body, a landing bracket and a wing assembly, a plurality of wing assemblies are fixedly installed on the side of the aircraft body, the landing brackets are symmetrically fixedly installed on both sides of the bottom of the aircraft body, a monitoring mechanism for detecting terrain and plant planting conditions is arranged at the bottom of the aircraft body, a monitoring component for automatically taking pictures of the current area and detecting plant growth conditions is arranged in the monitoring mechanism, and the monitoring component is used to timely respond to the restoration conditions of the current area, a swing mechanism for adjusting the angle of the monitoring mechanism itself is fixedly installed on the top of the monitoring mechanism, a defogger mechanism is arranged on one side of the bottom of the aircraft body, and a spraying mechanism is arranged on the side of the aircraft body.

[0013] As a preferred technical solution of the present invention, the monitoring mechanism includes a protective frame, a support frame, an upper limit frame and a monitoring component. The protective frame is arranged at the bottom end of the aircraft body, the support frame is fixedly installed at the bottom end of the protective frame, and the upper limit frame is fixedly installed at the top end of the protective frame. The protective frame, the support frame and the upper limit frame form a semi-enclosed shell with a side opening, and the monitoring component is arranged in the shell.

[0014] As a preferred technical solution of the present invention, the monitoring component is composed of a controller, a detection camera module and a laser radar module. The detection camera module takes pictures of the terrain, landform and plant growth conditions of the current area, and the laser radar module inputs the detected geological and terrain data into the controller.

[0015] As a preferred technical solution of the present invention, the swing mechanism includes a protection compartment, a reciprocating assembly, a rotating connecting rod and a connecting frame. The protection compartment is fixedly installed under the aircraft body, the reciprocating assembly is fixedly installed inside the protection compartment, the rotating connecting rod is rotatably installed at the bottom end of the reciprocating assembly, the connecting frame is fixedly installed at the end of the rotating connecting rod, and the connecting frame is fixedly connected to the monitoring mechanism.

[0016] As a preferred technical solution of the present invention, the reciprocating component includes a connecting column, a meshing gear, a sector-shaped tooth block, a main gear and a driving motor. The connecting column is symmetrically rotatably installed inside the protective bin, the meshing gear is fixedly installed outside the connecting column, the meshing gears are meshed with each other, the sector-shaped tooth block is fixedly installed at the bottom end of the connecting column, the main gear is rotatably installed at the end of the rotating connecting rod, the main gear is meshedly connected to the sector-shaped tooth block, the driving motor is fixedly installed on the upper surface of the protective bin, and the output end of the driving motor is fixedly connected to one group of connecting column ends.

[0017] As a preferred technical solution of the present invention, the defogger mechanism includes a hot air blower assembly, a conveying pipe and an air outlet. The hot air blower assembly is fixedly mounted on one side of the bottom end of the aircraft body, the air outlet end is fixedly mounted on the side of the monitoring mechanism, and a conveying pipe is fixedly mounted between the air outlet end and the hot air blower assembly.

[0018] As a preferred technical solution of the present invention, the air outlet end includes a guide plate, an additional side plate and an installation assembly. The additional side plate is fixedly installed on the side of the monitoring mechanism, the installation assembly is arranged at the end of the additional side plate, and the guide plate is fixedly installed on the side of the additional side plate through the installation assembly.

[0019] As a preferred technical solution of the present invention, the installation assembly consists of a threaded rod and a nut. The threaded rod passes through the guide plate and the additional side plate at the same time, and the nut is threadedly installed at the end of the threaded rod.

[0020] As a preferred technical solution of the present invention, the UAV detection method based on ecological restoration technology also includes a spraying mechanism, which includes a conveying assembly, a rotating frame and a spraying end. The conveying assembly is fixedly mounted on the side of the aircraft body, the rotating frame is arranged at the bottom of the aircraft body, and the spraying end is fixedly mounted on the side of the rotating frame.

[0021] Compared with the prior art, the present invention has the following beneficial effects:

[0022] (1) In the present invention, by setting up a monitoring mechanism and a swing mechanism, the vegetation conditions and topographic data in the area can be monitored in real time, and a three-dimensional model of the area can be constructed based on the monitored data, so as to facilitate the formulation of a corresponding ecological restoration plan based on the known data. In addition, during the monitoring process, the angle of the monitoring component can be flexibly adjusted, so that the equipment can clearly and accurately identify the various conditions and data in the current area, thereby improving the accuracy of the equipment during monitoring, thereby improving the working quality of the equipment itself;

[0023] (2) In the present invention, by providing a defogger mechanism and a spraying mechanism, the water mist generated on the lens surface can be removed to prevent the water mist from adhering to the lens surface and affecting the accuracy of the lens shooting picture and the collected data. Subsequently, the vegetation can be irrigated and nutrients can be sprayed in different areas according to the collected data, thereby improving the survival rate of plants in the vegetation and steadily advancing the process of ecological restoration. BRIEF DESCRIPTION OF THE DRAWINGS

[0024] Figure 1 It is a three-dimensional diagram of the overall structure of the present invention.

[0025] Figure 2 It is a three-dimensional diagram of the bottom structure of the aircraft body of the present invention.

[0026] Figure 3 It is a three-dimensional diagram of the monitoring mechanism structure of the present invention.

[0027] Figure 4 It is a schematic diagram of the structure of the monitoring component in the present invention.

[0028] Figure 5 It is a structural schematic diagram of the swing mechanism in the present invention.

[0029] Figure 6 It is a schematic diagram of the structure of the reciprocating component in the present invention.

[0030] Figure 7 It is a structural schematic diagram of the defogger mechanism in the present invention.

[0031] Figure 8 It is a structural schematic diagram of the gas outlet end in the present invention.

[0032] Fig. 9 It is a structural schematic diagram of the spraying mechanism in the present invention.

[0033] The corresponding relationship between the illustrations and component names in the figure is as follows:

[0034] 1. Aircraft body; 2. Landing bracket; 3. Wing assembly; 4. Monitoring mechanism; 41. Protection frame; 42. Support frame; 43. Upper limit frame; 44. Monitoring assembly; 441. Controller; 442. Detection camera module; 443. LiDAR module; 5. Swing mechanism; 51. Protection compartment; 52. Reciprocating assembly; 521. Connecting column; 522. Meshing gear; 523. Fan-shaped gear block; 524. Main gear; 525. Driving motor; 53. Rotating connecting rod; 54. Connecting frame; 6. Demisting mechanism; 61. Hot air blower assembly; 62. Delivery pipe; 63. Air outlet; 631. Guide plate; 632. Add side panel; 633. Installation assembly; 7. Spraying mechanism; 71. Delivery assembly; 72. Rotating frame; 73. Spraying end. DETAILED DESCRIPTION

[0035] In order to make the above-mentioned objects, features and advantages of the present invention more obvious and easy to understand, the specific implementation methods of the present invention are described in detail below in conjunction with the accompanying drawings.

[0036] In the following description, many specific details are set forth to facilitate a full understanding of the present invention, but the present invention may also be implemented in other ways different from those described herein, and those skilled in the art may make similar generalizations without violating the connotation of the present invention. Therefore, the present invention is not limited to the specific embodiments disclosed below.

[0037] Secondly, the term "one embodiment" or "embodiment" as used herein refers to a specific feature, structure or characteristic that may be included in at least one implementation of the present invention. The term "in one embodiment" that appears in different places in this specification does not refer to the same embodiment, nor is it a separate or selective embodiment that is mutually exclusive with other embodiments. The present invention provides the following embodiments.

[0038] A drone detection method based on ecological restoration technology includes the following steps:

[0039] S1. Before ecological restoration, a large-scale survey is conducted by drones, and some core areas or areas of concern are selected for field investigations to evaluate environmental factors (light, temperature, water, soil), and local native ecosystems that are in a stable stage are selected as reference ecosystems to assist in establishing ecological restoration strategies;

[0040] S2. In ecological restoration, drones are used to conduct irregular regional monitoring. Environmental data and dynamic data on plant growth obtained from monitoring are used to accurately determine the restoration status of the current area, promptly identify problems in the current area, and solve them in a timely manner (such as through necessary irrigation and plant maintenance);

[0041] S3. In the later stage of ecological restoration, the growth of planted plants and restoration conditions in the area are observed by drones to assist in judging the restoration effect;

[0042] S4. Construct a complete database. Construct a complete database by detecting the environmental data and plant growth data of the area.

[0043] By the attached Figure 1 and Figure 2 As shown, it is a structural schematic diagram of the UAV in this embodiment. The UAV used in step S1 and step S2 includes an aircraft body 1, a landing bracket 2 and a wing assembly 3. A plurality of wing assemblies 3 are fixedly installed on the side of the aircraft body 1, and the landing bracket 2 is symmetrically fixedly installed on both sides of the bottom of the aircraft body 1. A monitoring mechanism 4 for detecting terrain and plant planting conditions is arranged at the bottom of the aircraft body 1. A monitoring component 44 for automatically taking pictures of the current area and detecting plant growth conditions is arranged in the monitoring mechanism 4. The monitoring component 44 is used to timely reflect the restoration status of the current area. A swing mechanism 5 for adjusting the angle of the monitoring mechanism 4 itself is fixedly installed on the top of the monitoring mechanism 4. A defogger mechanism 6 is arranged on one side of the bottom of the aircraft body 1, and a spraying mechanism 7 is arranged on the side of the aircraft body 1.

[0044] During use, the cooperation between the aircraft body 1 and the wing assembly 3 enables the aircraft body 1 as a whole to fly over the area to be inspected, and then the monitoring mechanism 4 is used to inspect the passed area. The monitoring assembly 44 can detect the vegetation growth and topography of the current area in real time, and cooperate with the aircraft body 1 to collect the detected data, so as to facilitate the subsequent analysis of the restoration situation of the current area and the formulation of a corresponding restoration plan based on the detected data. The use of the swing mechanism 5 can drive the monitoring mechanism 4 to adjust at multiple angles, so that the monitoring mechanism 4 can comprehensively detect the area. Subsequently, with the cooperation of the defogger mechanism 6, the water mist generated on the surface of the internal components of the monitoring assembly 44 in the high altitude is cleaned, so that the overall detection effect is clearer and more accurate, thereby completing the ecological restoration of the area.

[0045] By the attached Figure 3 As shown, it is a schematic diagram of the structure of the monitoring mechanism 4 in this embodiment, the monitoring mechanism 4 includes a protective frame 41, a support frame 42, an upper limit frame 43 and a monitoring component 44, the protective frame 41 is arranged at the bottom end of the aircraft body 1, the support frame 42 is fixedly installed at the bottom end of the protective frame 41, the upper limit frame 43 is fixedly installed at the top end of the protective frame 41, the protective frame 41, the support frame 42 and the upper limit frame 43 form a semi-enclosed shell with a side opening, and the monitoring component 44 is arranged in the shell.

[0046] During use, the protective frame 41, the support frame 42 and the upper limit frame 43 are used to provide a semi-enclosed shell for the installation of the monitoring component 44, so that the monitoring component 44 can stably follow the aircraft body 1 to move synchronously. The subsequent monitoring component 44 can better capture various data and pictures of the current area to assist in the development of subsequent steps. The use of the monitoring component 44 can capture the vegetation growth conditions in the current area and scan the regional terrain, which is convenient for the subsequent construction of a three-dimensional model of the area, making the overall work quality more efficient.

[0047] By the attached Figure 4 As shown, it is a structural diagram of the monitoring component 44 in this embodiment. The monitoring component 44 is composed of a controller 441, a detection camera module 442 and a laser radar module 443. The detection camera module 442 takes pictures of the terrain, landform and plant growth conditions of the current area, and the laser radar module 443 inputs the detected geological and terrain data into the controller 441.

[0048] During use, the detection camera module 442 is used to photograph the terrain of the current area. After multiple shooting comparisons, the multispectral image of the area is obtained, and key parameters for ecological restoration monitoring such as vegetation index, vegetation coverage, and biomass are produced. Vegetation distribution maps, coverage distribution maps, and biomass distribution maps are made. The use of the lidar module 443 can perform a detailed scan of the topography of the area, which is convenient for the subsequent construction of a three-dimensional model of the area. By combining the underground soil ecological index measurement, key indicators for evaluating the ecological restoration effect of vegetation and soil parameters are formed. Based on the above data, the vegetation index, vegetation coverage and soil parameters when the vegetation growth in the study area is the worst and the best are produced, and a long-term series monitoring data set is formed to monitor and evaluate the entire ecological restoration process.

[0049] By the attached Figure 5 As shown, it is a structural schematic diagram of the swing mechanism 5 in this embodiment, the swing mechanism 5 includes a protection compartment 51, a reciprocating assembly 52, a rotating connecting rod 53 and a connecting frame 54, the protection compartment 51 is fixedly installed below the aircraft body 1, the reciprocating assembly 52 is fixedly installed inside the protection compartment 51, the rotating connecting rod 53 is rotatably installed at the bottom end of the reciprocating assembly 52, the connecting frame 54 is fixedly installed at the end of the rotating connecting rod 53, and the connecting frame 54 is fixedly connected to the monitoring mechanism 4.

[0050] During use, through the coordination and use of the protection bin 51 and the reciprocating assembly 52, the reciprocating assembly 52 drives the rotating connecting rod 53 to adjust and change at multiple angles, so that the monitoring mechanism 4 can rotate in a horizontal state, making the overall detection effect of the monitoring mechanism 4 more efficient and accurate, and expanding the working range of the monitoring mechanism 4 itself.

[0051] By the attached Figure 6 As shown, it is a structural schematic diagram of the reciprocating component 52 in this embodiment, the reciprocating component 52 includes a connecting column 521, a meshing gear 522, a sector tooth block 523, a main gear 524 and a driving motor 525, the connecting column 521 is symmetrically rotatably installed inside the protective bin 51, the meshing gear 522 is fixedly installed on the outside of the connecting column 521, the meshing gears 522 are meshed with each other, the sector tooth block 523 is fixedly installed at the bottom of the connecting column 521, the main gear 524 is rotatably installed at the end of the rotating connecting rod 53, the main gear 524 is meshedly connected with the sector tooth block 523, the driving motor 525 is fixedly installed on the upper surface of the protective bin 51, and the output end of the driving motor 525 is fixedly connected to one group of ends of the connecting column 521.

[0052] During use, the driving motor 525 is started to drive one of the groups of connecting rotating posts 521 to rotate. By utilizing the mutual meshing of the two groups of meshing gears 522, the two groups of connecting rotating posts 521 will rotate in different directions, so that the two groups of sector-shaped tooth blocks 523 will mesh with the main gear 524 in turn. Due to the different rotation directions of the two groups of sector-shaped tooth blocks 523 and the difference in the tooth block distribution of the sector-shaped tooth blocks 523 themselves, the main gear 524 will operate in a reciprocating 180° rotation manner, thereby driving the overall angle of the monitoring mechanism 4 to change by rotating the connecting rod 53 and the connecting frame 54.

[0053] By the attached Figure 7 As shown, it is a structural schematic diagram of the defogger mechanism 6 in this embodiment, the defogger mechanism 6 includes a hot air blower assembly 61, a delivery pipe 62 and an air outlet 63, the hot air blower assembly 61 is fixedly mounted on one side of the bottom end of the aircraft body 1, the air outlet 63 is fixedly mounted on the side of the monitoring mechanism 4, and a delivery pipe 62 is fixedly mounted between the air outlet 63 and the hot air blower assembly 61.

[0054] During use, the aircraft body 1 will fly over the area to be detected. As the overall altitude changes, a layer of water mist will adhere to the outer surface of the monitoring component 44 due to the water vapor in the air. At this time, through the use and operation of the hot air blower component 61, hot air of a certain temperature is generated. Then, with the cooperation and transportation of the delivery pipe 62, the air outlet end 63 is aligned with the lens surface of the monitoring component 44 for output, and the water vapor attached to the surface of the monitoring component 44 is cleaned, so as to ensure the stability of the monitoring component 44 during operation.

[0055] By the attached Figure 8 As shown, it is a structural schematic diagram of the air outlet end 63 in this embodiment, and the air outlet end 63 includes a guide plate 631, an additional side plate 632 and a mounting assembly 633. The additional side plate 632 is fixedly mounted on the side of the monitoring mechanism 4, and the mounting assembly 633 is arranged at the end of the additional side plate 632. The guide plate 631 is fixedly mounted on the side of the additional side plate 632 through the mounting assembly 633.

[0056] During use, the entire air outlet end 63 is installed on the top side of the monitoring mechanism 4 by adding the side panel 632. Then, the angle of the guide plate 631 is adjusted by using the mounting assembly 633 so that the output port of the guide plate 631 is aligned with the lens surface of the monitoring assembly 44. Then, the hot air is ejected by using the guide plate 631 to process the water mist attached to the lens surface of the monitoring assembly 44.

[0057] By the attached Figure 8 As shown, it is a structural schematic diagram of the installation component 633 in this embodiment. The installation component 633 consists of a threaded rod and a nut. The threaded rod passes through the guide plate 631 and the additional side plate 632 at the same time, and the nut is threadedly installed at the end of the threaded rod.

[0058] During use, the guide plate 631 is installed to the side opening of the additional side plate 632, and then the threaded rod is passed through the guide plate 631 and the additional side plate 632 at the same time. At this time, the nut is rotated along the external thread of the threaded rod. As the position of the nut changes, the raised end on the side of the additional side plate 632 is offset toward the middle end, thereby fixing the position and angle of the guide plate 631.

[0059] By the attached Fig. 9 As shown, it is a structural schematic diagram of the spraying mechanism 7 in this embodiment. The UAV detection method based on ecological restoration technology also includes a spraying mechanism 7, and the spraying mechanism 7 includes a conveying component 71, a rotating frame 72 and a spraying end 73. The conveying component 71 is fixedly mounted on the side of the aircraft body 1, the rotating frame 72 is arranged at the bottom of the aircraft body 1, and the spraying end 73 is fixedly mounted on the side of the rotating frame 72.

[0060] During use, the stored material is sprayed out through the spray end 73 by using the pump body installed inside the conveying component 71. By using the spray end 73, according to the results of the detection data analysis and the difference in terrain, the vegetation in different areas is irrigated with corresponding doses to assist the growth of vegetation in the area and complete the ecological restoration of the area.

[0061] The above content is a further detailed description of the present invention in combination with specific implementation methods. It cannot be determined that the specific implementation of the present invention is limited to these descriptions. For ordinary technicians in the technical field to which the present invention belongs, several simple deductions or substitutions can be made without departing from the concept of the present invention, which should be regarded as belonging to the scope of protection determined by the claims submitted for the present invention.

Claims

1. A drone detection method based on ecological restoration technology, characterized in that: The steps include: S1. Before ecological restoration, a large-scale survey is conducted by drones, and some core areas or areas of concern are selected for field investigations to evaluate environmental factors (light, temperature, water, soil), and local native ecosystems that are in a stable stage are selected as reference ecosystems to assist in establishing ecological restoration strategies; S2. In ecological restoration, drones are used to conduct irregular regional monitoring. Environmental data and dynamic data on plant growth obtained from monitoring are used to accurately determine the restoration status of the current area, promptly identify problems in the current area, and solve them in a timely manner (such as through necessary irrigation and plant maintenance); S3. In the later stage of ecological restoration, the growth of planted plants and restoration conditions in the area are observed by drones to assist in judging the restoration effect; S4. Build a complete database; build a complete database by detecting the environmental data and plant growth data of the area.

2. The method for detecting unmanned aerial vehicles based on ecological restoration technology according to claim 1 is characterized in that: The unmanned aerial vehicle used in step S1 and step S2 of claim 1 comprises an aircraft body (1), a landing bracket (2) and a wing assembly (3), wherein a plurality of wing assemblies (3) are fixedly mounted on the side of the aircraft body (1), the landing bracket (2) is symmetrically fixedly mounted on both sides of the bottom of the aircraft body (1), a monitoring mechanism (4) for detecting terrain and plant planting conditions is arranged at the bottom of the aircraft body (1), a monitoring component (44) for automatically taking pictures of the current area and detecting plant growth conditions is arranged in the monitoring mechanism (4), and the monitoring component (44) is used to timely reflect the restoration conditions of the current area, a swing mechanism (5) for adjusting the angle of the monitoring mechanism (4) is fixedly mounted on the top of the monitoring mechanism (4), a defogger mechanism (6) is arranged on one side of the bottom of the aircraft body (1), and a spraying mechanism (7) is arranged on the side of the aircraft body (1).

3. The method for detecting unmanned aerial vehicles based on ecological restoration technology according to claim 2 is characterized in that: The monitoring mechanism (4) comprises a protection frame (41), a support frame (42), an upper limit frame (43) and a monitoring component (44); the protection frame (41) is arranged at the bottom end of the aircraft body (1); the support frame (42) is fixedly mounted at the bottom end of the protection frame (41); the upper limit frame (43) is fixedly mounted at the top end of the protection frame (41); the protection frame (41), the support frame (42) and the upper limit frame (43) form a semi-enclosed shell with a side opening; and the monitoring component (44) is arranged in the shell.

4. The method for detecting unmanned aerial vehicles based on ecological restoration technology according to claim 3 is characterized in that: The monitoring component (44) is composed of a controller (441), a detection camera module (442) and a laser radar module (443). The detection camera module (442) takes pictures of the topography, landforms and plant growth conditions in the current area, and the laser radar module (443) inputs the detected geological and topographic data into the controller (441).

5. The method for detecting unmanned aerial vehicles based on ecological restoration technology according to claim 1 is characterized in that: The swing mechanism (5) comprises a protection chamber (51), a reciprocating assembly (52), a rotating connecting rod (53) and a connecting frame (54); the protection chamber (51) is fixedly mounted below the aircraft body (1); the reciprocating assembly (52) is fixedly mounted inside the protection chamber (51); the rotating connecting rod (53) is rotatably mounted at the bottom end of the reciprocating assembly (52); the connecting frame (54) is fixedly mounted at the end of the rotating connecting rod (53); and the connecting frame (54) is fixedly connected to the monitoring mechanism (4).

6. The method for detecting unmanned aerial vehicles based on ecological restoration technology according to claim 5 is characterized in that: The reciprocating assembly (52) comprises a connecting rotating column (521), a meshing gear (522), a sector gear block (523), a main gear (524) and a driving motor (525); the connecting rotating column (521) is symmetrically rotatably mounted inside the protection bin (51); the meshing gear (522) is fixedly mounted outside the connecting rotating column (521); the meshing gears (522) are meshed with each other; the sector gear block (523) is fixedly mounted at the bottom end of the connecting rotating column (521); the main gear (524) is rotatably mounted at the end of the rotating connecting rod (53); the main gear (524) is meshedly connected with the sector gear block (523); the driving motor (525) is fixedly mounted on the upper surface of the protection bin (51); and the output end of the driving motor (525) is fixedly connected to the end of one group of connecting rotating columns (521).

7. The method for detecting unmanned aerial vehicles based on ecological restoration technology according to claim 1 is characterized in that: The demisting mechanism (6) comprises a hot air blower assembly (61), a delivery pipe (62) and an air outlet (63); the hot air blower assembly (61) is fixedly mounted on one side of the bottom end of the aircraft body (1); the air outlet (63) is fixedly mounted on the side of the monitoring mechanism (4); and the delivery pipe (62) is fixedly mounted between the air outlet (63) and the hot air blower assembly (61).

8. The method for detecting unmanned aerial vehicles based on ecological restoration technology according to claim 7 is characterized in that: The air outlet end (63) comprises a guide plate (631), an additional side plate (632) and a mounting assembly (633); the additional side plate (632) is fixedly mounted on a side of the monitoring mechanism (4); the mounting assembly (633) is arranged at an end of the additional side plate (632); and the guide plate (631) is fixedly mounted on a side of the additional side plate (632) via the mounting assembly (633).

9. The method for detecting unmanned aerial vehicles based on ecological restoration technology according to claim 8, characterized in that: The mounting assembly (633) is composed of a threaded rod and a nut. The threaded rod passes through the guide plate (631) and the additional side plate (632) at the same time. The nut is threadedly mounted on the end of the threaded rod.

10. The method for detecting unmanned aerial vehicles based on ecological restoration technology according to claim 1, characterized in that: The unmanned aerial vehicle detection method based on ecological restoration technology also includes a spraying mechanism (7), the spraying mechanism (7) includes a conveying component (71), a rotating frame (72) and a spraying end (73), the conveying component (71) is fixedly mounted on the side of the aircraft body (1), the rotating frame (72) is arranged at the bottom end of the aircraft body (1), and the spraying end (73) is fixedly mounted on the side of the rotating frame (72).

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