A drone landing platform

Abstract

The present invention discloses a drone landing platform, which relates to the field of drone technology. The drone landing platform includes a platform body and an edge processor. A plurality of support legs are evenly arranged on the circumference of the bottom of the platform body. A plurality of ventilation slots are evenly opened on the circumference of the top of the platform body, and a gas transmission component is arranged in the ventilation slot. A collection module is provided on the platform body for acquiring the landing data of the drone in real time and transmitting the landing data to the edge processor. The edge processor is fixedly installed on the top of the platform body. The edge processor is used to perform airflow adaptation analysis on the landing data and generate gas transmission control instructions. The gas transmission component is used to output airflow to the top of the platform body according to the gas transmission control instructions. The present invention solves the technical problem that the existing landing auxiliary equipment does not take into account that the downward airflow generated by the landing of the drone will be blocked by the landing auxiliary equipment and reflected upward, thereby interfering with the landing posture of the drone and reducing the safety of the drone.

Description

Technical Field

[0001] The present invention relates to the technical field of unmanned aerial vehicles (UAVs), and in particular to a landing platform for UAVs. Background Art

[0002] With the rapid development and widespread application of drone technology, the safety issues during landing have become increasingly prominent. In traditional landing methods, the drone's own weight creates a certain impact force when it contacts the ground, which is not conducive to the safe use of drones.

[0003] At present, although the existing landing assistance equipment is equipped with a buffer mechanism to cushion the impact force of the drone, it does not take into account that the downward airflow generated by the drone landing will be blocked by the landing assistance equipment and reflected upward, thereby interfering with the landing posture of the drone and reducing the safety of the drone. Summary of the Invention

[0004] The present invention provides a landing platform for a drone, which solves the technical problem that although the existing landing auxiliary equipment is provided with a buffer mechanism to buffer the impact force of the drone, it does not take into account that the downward airflow generated by the landing of the drone will be blocked by the landing auxiliary equipment and reflected upward, thereby interfering with the landing posture of the drone and reducing the safety of the drone.

[0005] A first aspect of the present invention provides a drone landing platform, comprising a platform body and an edge processor;

[0006] A plurality of supporting legs are evenly arranged on the circumference of the bottom of the platform body, a plurality of ventilation slots are evenly opened on the circumference of the top of the platform body, and a gas transmission component is arranged in the ventilation slots;

[0007] The platform body is provided with a collection module, which is used to obtain the landing data of the drone in real time and transmit the landing data to the edge processor;

[0008] The edge processor is fixedly mounted on the top of the platform body, and the edge processor, the acquisition module and the gas delivery component are electrically connected;

[0009] The edge processor is configured to perform airflow adaptation analysis on the landing data, generate an air delivery control instruction, and send the air delivery control instruction to the air delivery component;

[0010] The gas delivery component is used to output airflow above the platform body according to the gas delivery control instruction.

[0011] Optionally, the support leg includes a mounting block, a first support rod, a second support rod and a spiral connecting rod;

[0012] One end of the mounting block is fixedly mounted on the bottom of the platform body, and one end of the first support rod is rotatably connected to the other end of the mounting block via a connecting shaft;

[0013] A leveling motor is provided at the other end of the first support rod, and an output end of the leveling motor is fixedly connected to one end of the spiral connecting rod;

[0014] The other end of the spiral connecting rod is threadedly connected to one end of the second supporting rod.

[0015] Optionally, the gas delivery assembly includes a propeller, a drive assembly and a mounting platform;

[0016] The mounting platform is fixedly mounted on the bottom of the inner wall of the ventilation slot, and the driving assembly is fixedly mounted on the top of the mounting platform;

[0017] The output end of the driving component is fixedly connected to the propeller, and the driving component is electrically connected to the edge processor.

[0018] Optionally, the edge processor includes a communication module, an initial speed module, a speed adjustment module and a summing module;

[0019] The communication module is configured to receive the landing data sent by the acquisition module and transmit the landing data to the initial speed module, wherein the landing data includes position data, pressure data, airflow velocity data, and airflow direction data;

[0020] The initial rotation speed module is used to input the position data into a preset function of the propeller rotation speed to generate an initial rotation speed;

[0021] The initial speed function is:

[0022]

[0023] in, is the initial speed, is the height coefficient, is the vertical descent speed coefficient, is the horizontal velocity coefficient, is the vertical height, is the reference height, is the vertical descent speed, is the reference vertical descent speed, is the reference horizontal velocity, is the velocity of the horizontal x-axis, is the velocity of the horizontal y-axis, is the basic revolution number;

[0024] The speed adjustment module is used to input the initial speed, the position data, the airflow velocity data and the airflow direction data into a preset PID controller to obtain a speed compensation amount;

[0025] The summing module is configured to sum the initial rotational speed and the rotational speed compensation amount to generate a gas delivery control instruction, and send the gas delivery control instruction to the gas delivery component.

[0026] Optionally, the acquisition module includes a position sensor, an airflow velocity sensor, and an airflow direction sensor;

[0027] The position sensor is fixedly installed at the top center of the platform body, and is used to obtain the position data of the drone;

[0028] A plurality of airflow velocity sensors are evenly arranged on the top of the platform body, and the airflow velocity sensors are used to obtain the airflow velocity data above the platform body;

[0029] A plurality of airflow direction sensors are evenly arranged on the circumference of the top of the platform body, and the airflow direction sensors are used to obtain airflow direction data above the platform body.

[0030] Optionally, the acquisition module further includes a pressure sensor;

[0031] A plurality of pressure sensors are evenly arranged on the top of the platform body, and the pressure sensors are used to obtain the pressure data of the drone.

[0032] Optionally, the acquisition module further includes a level sensor;

[0033] The level sensor is fixedly installed on the platform body, and is used to measure the level data of the platform body and send the level data to the edge processor.

[0034] Optionally, the platform body is a circular platform.

[0035] Optionally, the surface of the platform body is covered with an anti-slip coating.

[0036] Optionally, a battery is provided on the top of the platform body;

[0037] The battery, the edge processor, the acquisition module, and the gas delivery component are electrically connected.

[0038] It can be seen from the above technical solutions that the present invention has the following advantages:

[0039] By providing an acquisition module on the platform body for acquiring the landing data of the drone in real time and transmitting the landing data to the edge processor, the edge processor performs airflow adaptation analysis on the landing data, generates an air supply control instruction, and uses the air supply control instruction to control the air supply component to output airflow above the platform body, thereby reducing the airflow on the platform when the drone lands, overcoming the technical problem that the existing landing assistance equipment does not take into account that the downward airflow generated by the landing of the drone will be blocked by the landing assistance equipment and reflected upward, thereby interfering with the landing posture of the drone and reducing the safety of the drone. Compared with the traditional landing platform, the present invention performs airflow adaptation analysis on the landing data acquired in real time by the acquisition module through the edge processor, thereby dynamically adjusting the airflow output by the air supply component, avoiding the situation that the downward airflow generated by the landing of the drone will be blocked by the landing assistance equipment and reflected upward, thereby interfering with the landing posture of the drone, and at the same time, it plays a buffering role on the drone and improves the safety of the drone. BRIEF DESCRIPTION OF THE DRAWINGS

[0040] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the following briefly introduces the drawings required for use in the embodiments or the description of the prior art. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying any creative work.

[0041] Figure 1 This is a schematic structural diagram of a UAV landing platform according to an embodiment of the present invention;

[0042] Figure 2 This is a schematic structural diagram of the platform body according to an embodiment of the present invention;

[0043] The meanings of the reference numerals are as follows:

[0044] 1. Platform body; 2. First support rod; 3. Connecting shaft; 4. Propeller; 5. Drive assembly; 6. Battery; 7. Edge processor; 8. Pressure sensor; 9. Position sensor; 10. Airflow velocity sensor; 11. Airflow direction sensor; 12. Mounting platform; 13. Mounting block; 14. Anti-slip coating; 15. Leveling motor; 16. Screw connecting rod; 17. Second support rod; 18. Level sensor. DETAILED DESCRIPTION

[0045] An embodiment of the present invention provides a drone landing platform, which is used to solve the technical problem that although the existing landing assistance equipment is provided with a buffer mechanism to cushion the impact force of the drone, it does not take into account that the downward airflow generated by the landing of the drone will be blocked by the landing assistance equipment and reflected upward, thereby interfering with the landing posture of the drone and reducing the safety of the drone.

[0046] In order to make the purpose, features, and advantages of the present invention more obvious and easy to understand, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Obviously, the embodiments described below are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative work are within the scope of protection of the present invention.

[0047] See also Figure 1-Figure 2 , the present invention provides a UAV landing platform, including a platform body 1 and an edge processor 7;

[0048] A plurality of supporting legs are evenly arranged on the bottom circumference of the platform body 1, and a plurality of ventilation slots are evenly opened on the top circumference of the platform body 1, and a gas transmission component is arranged in the ventilation slots;

[0049] The platform body 1 is provided with a collection module, which is used to obtain the landing data of the drone in real time and transmit the landing data to the edge processor 7;

[0050] The edge processor 7 is fixedly mounted on the top of the platform body 1, and the edge processor 7, the acquisition module and the gas transmission component are electrically connected;

[0051] Edge processor 7, used to perform airflow adaptation analysis on landing data, generate air delivery control instructions, and send the air delivery control instructions to the air delivery component;

[0052] The air delivery component is used to output air flow to the top of the platform body 1 according to the air delivery control instructions.

[0053] In an embodiment of the present invention, the drone landing platform includes a platform body 1 and an edge processor 7. A plurality of support legs are evenly arranged around the circumference of the bottom of the platform body 1, and four ventilation slots are evenly arranged around the circumference of the top of the platform body 1. A collection module is provided on the platform body 1 for acquiring the landing data of the drone in real time and transmitting the landing data to the edge processor 7. The edge processor 7 is installed on the top of the platform body 1 for performing airflow adaptation analysis on the landing data, generating air supply control instructions, and sending the air supply control instructions to the air supply component. A air supply component is provided in the ventilation slot for outputting airflow to the top of the platform body 1 according to the air supply control instructions, thereby controlling the airflow above the drone when the drone lands, and avoiding excessive airflow on the ground when the drone lands, which may cause rebound and lead to landing failure of the drone.

[0054] See Figure 1As shown, the support leg includes a mounting block 13, a first support rod 2, a second support rod 17 and a spiral connecting rod 16; one end of the mounting block 13 is fixedly mounted on the bottom of the platform body 1, and one end of the first support rod 2 is rotatably connected to the other end of the mounting block 13 through a connecting shaft 3; a leveling motor 15 is provided at the other end of the first support rod 2, and the output end of the leveling motor 15 is fixedly connected to one end of the spiral connecting rod 16; the other end of the spiral connecting rod 16 is threadedly connected to one end of the second support rod 17.

[0055] In an embodiment of the present invention, the support leg includes a mounting block 13, a first support rod 2, a second support rod 17 and a spiral connecting rod 16. One end of the mounting block 13 is fixedly mounted on the bottom of the platform body 1, and one end of the first support rod 2 is rotatably connected to the other end of the mounting block 13 through a connecting shaft 3, so that the angle of the support rod can be flexibly adjusted according to actual needs. When the drone landing platform needs to be stored or transported, the support rod can be rotated to a position parallel to the platform body 1, reducing the overall occupied space and making it convenient to carry and store. A leveling motor 15 is provided at the other end of the first support rod 2, and the output end of the leveling motor 15 is fixedly connected to one end of the spiral connecting rod 16, and the other end of the spiral connecting rod 16 is threadedly connected to one end of the second support rod 17. The leveling motor 15 can be precisely controlled according to the actual inclination of the drone landing platform. When the drone landing platform is on an uneven ground or tilted due to uneven load distribution, the leveling motor 15 is started, driving the spiral connecting rod 16 to rotate. Since the spiral connecting rod 16 is threadedly connected to the second support rod 17, the rotation of the spiral connecting rod 16 will cause the second support rod 17 to move along the thread direction, thereby adjusting the relative length between the first support rod 2 and the second support rod 17, thereby achieving precise leveling of the platform.

[0056] See Figure 1-2 As shown, the gas transmission component includes a propeller 4, a drive component 5 and a mounting platform 12; the mounting platform 12 is fixedly installed at the bottom of the inner wall of the ventilation slot, and the drive component 5 is fixedly installed at the top of the mounting platform 12; the output end of the drive component 5 is fixedly connected to the propeller 4, and the drive component 5 is electrically connected to the edge processor 7.

[0057] In this embodiment of the present invention, the gas delivery assembly includes a propeller 4, a drive assembly 5, and a mounting platform 12. The mounting platform 12 is fixedly mounted to the bottom of the inner wall of the ventilation slot. The drive assembly 5 is mounted on top of the mounting platform 12. The output end of the drive assembly 5 is fixedly connected to the propeller 4, and the drive assembly 5 is electrically connected to the edge processor 7. The drive assembly 5 includes a drive motor and an electronic speed controller (ESC). The ESC controls the drive motor to rotate the propeller 4 according to gas delivery control commands.

[0058] It should be noted that the edge processor 7 includes a communication module, an initial speed module, a speed adjustment module, and a summing module. The communication module is used to receive landing data from the acquisition module and transmit the landing data to the initial speed module, where the landing data includes position data, pressure data, airflow speed data, and airflow direction data. The initial speed module is used to input the position data into a preset function related to the propeller 4 speed to generate an initial speed.

[0059] The initial speed function is:

[0060]

[0061] in, is the initial speed, is the height coefficient, is the vertical descent speed coefficient, is the horizontal velocity coefficient, is the vertical height, is the reference height, is the vertical descent speed, is the reference vertical descent speed, is the reference horizontal velocity, is the velocity of the horizontal x-axis, is the velocity of the horizontal y-axis, is the basic revolution number;

[0062] The speed regulation module is used to input the initial speed, position data, airflow velocity data and airflow direction data into the preset PID controller to obtain the speed compensation; the summing module is used to sum the initial speed and the speed compensation to generate a gas transmission control instruction, and send the gas transmission control instruction to the gas transmission component.

[0063] In an embodiment of the present invention, the edge processor 7 includes a communication module, an initial speed module, a speed regulation module, and a summing module. The communication module is configured to receive landing data sent by the acquisition module and transmit the landing data to the initial speed module, wherein the landing data includes position data, pressure data, airflow velocity data, and airflow direction data. The initial speed module is configured to use the position data input as a preset function of the propeller 4 speed to generate an initial speed. The speed regulation module is configured to perform speed compensation processing on the initial speed, position data, airflow velocity data, and airflow direction data using a preset PID control algorithm to obtain a speed compensation value. The summing module is configured to sum the initial speed and the speed compensation value to generate a gas transmission control instruction and transmit the gas transmission control instruction to the gas transmission component.

[0064] It's worth mentioning that the PID control algorithm specifically proceeds as follows: 1. Calculate the position error between the drone's current position and the target position of platform 1. 2. Calculate the speed error between the drone's current speed and the desired speed. 3. Add the airflow velocity and the speed error to obtain the target speed error. 4. Weightedly sum the position error and the target speed error to obtain the total error. This total error is input into the PID controller's proportional, integral, and differential units, respectively, to obtain the proportional, integral, and differential values. 5. Add the proportional, integral, and differential values ​​to obtain the speed compensation.

[0065] See Figure 2 As shown, the acquisition module includes a position sensor 9, an airflow velocity sensor 10 and an airflow direction sensor 11; the position sensor 9 is fixedly installed at the center of the top of the platform body 1, and is used to obtain the position data of the drone; a plurality of airflow velocity sensors 10 are evenly arranged on the top of the platform body 1, and the airflow velocity sensors 10 are used to obtain the airflow velocity data above the platform body 1; a plurality of airflow direction sensors 11 are evenly arranged on the circumference of the top of the platform body 1, and the airflow direction sensors 11 are used to obtain the airflow direction data above the platform body 1.

[0066] In an embodiment of the present invention, the acquisition module includes a position sensor 9 (for example, a laser positioning or electromagnetic positioning sensor 9), an airflow velocity sensor 10, and an airflow direction sensor 11. The position sensor 9 is fixedly installed at the center of the top of the platform body 1 and is used to detect the relative position of the drone. A plurality of airflow velocity sensors 10 are evenly distributed in the center area and edge positions of the top of the platform body 1. The airflow velocity sensors 10 are used to obtain airflow velocity data above the platform body 1. Eight airflow direction sensors 11 are evenly arranged around the circumference of the top of the platform body 1, and each airflow direction sensor 11 is spaced 45 degrees apart. The airflow direction sensor 11 is used to obtain airflow direction data above the platform body 1.

[0067] It is worth mentioning that the airflow velocity sensor 10 is located in the center of the top of the platform body 1 to sense the main velocity of the airflow directly below the drone. The airflow velocity sensor 10 is located at the top edge of the platform body 1 to capture the changes in airflow velocity at the edge of the platform when the drone lands.

[0068] It is worth mentioning that the airflow direction sensor 11 is mainly installed in a weather vane style, which can intuitively measure the direction of the airflow above the platform.

[0069] See Figure 2 As shown, the acquisition module also includes a pressure sensor 8; a plurality of pressure sensors 8 are evenly arranged on the top of the platform body 1, and the pressure sensor 8 is used to obtain the pressure data of the drone.

[0070] In this embodiment of the present invention, the acquisition module also includes pressure sensors 8. Multiple pressure sensors 8 are evenly distributed across the surface of the platform body 1. When the drone lands, these sensors directly measure the pressure change generated by the moment the landing gear contacts the platform, thereby determining the drone's landing posture and impact force. Taking the 1.5-meter-diameter circular platform as an example, the platform surface can be divided into several concentric rings, with pressure sensors 8 evenly distributed within each area. Sensors can be densely distributed closer to the center.

[0071] It is worth mentioning that the pressure sensor 8 can be set at the connection between the mounting block 13 and the platform body 1 to monitor the pressure changes on the entire drone landing platform, to evaluate the impact of the drone landing on the drone landing platform, and to ensure the safety and stability of the drone landing platform.

[0072] See Figure 2 As shown, the acquisition module also includes a horizontal sensor 18; the horizontal sensor 18 is fixedly installed on the platform body 1, and the horizontal sensor 18 is used to measure the horizontal data of the platform body 1 and send the horizontal data to the edge processor 7.

[0073] In this embodiment of the present invention, the acquisition module further includes a level sensor 18. The level sensor 18 is fixedly mounted on the platform body 1. The level sensor 18 is used to measure the level data of the platform body 1 and send the level data to the edge processor 7. The edge processor 7 can control the leveling motor 15 to adjust the drone landing platform to a level level based on the level data.

[0074] It should be noted that the platform body 1 is a circular platform.

[0075] In this embodiment of the present invention, the platform body 1 is circular. When a circular platform is subjected to load, the force is evenly distributed across its entire circumference. Compared to other shapes (such as square or rectangular), a circular shape lacks sharp corners and edges, thus avoiding stress concentration. Furthermore, the circular platform's shape allows wind to flow more smoothly along its circumference when subjected to wind, reducing wind resistance and turbulence. Compared to a square platform, a circular platform does not generate significant vortices or airflow separation at its corners, thereby reducing the force exerted by the wind on the platform.

[0076] See Figure 2 As shown, the surface of the platform body 1 is covered with an anti-slip coating 14 .

[0077] In the embodiment of the present invention, the surface of the platform body 1 is covered with an anti-skid coating 14 . The anti-skid coating 14 may be a polyurethane coating or rubber with anti-skid particles.

[0078] See Figure 2As shown, a battery 6 is provided on the top of the platform body 1; the battery 6, the edge processor 7, the acquisition module, and the gas transmission component are electrically connected.

[0079] In an embodiment of the present invention, a battery 6 is provided on the top of the platform body 1, and the battery 6, the edge processor 7, the acquisition module, and the gas transmission component are electrically connected to supply power to the edge processor 7, the acquisition module, and the gas transmission component.

[0080] It is worth mentioning that each time the drone landing platform is used, the edge processor 7 will feedback the remaining power of the battery 6 to ensure normal use the next time it works.

[0081] In an embodiment of the present invention, a collection module is provided on the platform body for acquiring the landing data of the drone in real time and transmitting the landing data to the edge processor, and then the landing data is subjected to airflow adaptation analysis by the edge processor to generate an air supply control instruction, and the air supply control instruction is used to control the air supply component to output airflow above the platform body, thereby reducing the airflow on the platform when the drone lands. This overcomes the technical problem that the existing landing assistance equipment does not take into account that the downward airflow generated by the landing of the drone will be blocked by the landing assistance equipment and reflected upward, thereby interfering with the landing posture of the drone and reducing the safety of the drone. Compared with the traditional landing platform, the present invention uses the edge processor to perform airflow adaptation analysis on the landing data acquired in real time by the collection module, thereby dynamically adjusting the airflow output by the air supply component, avoiding the situation that the downward airflow generated by the landing of the drone will be blocked by the landing assistance equipment and reflected upward, thereby interfering with the landing posture of the drone. At the same time, it plays a buffering role on the drone and improves the safety of the drone.

[0082] Those skilled in the art will clearly understand that, for the convenience and brevity of description, the specific working processes of the systems, devices and units described above can refer to the corresponding processes in the aforementioned method embodiments and will not be repeated here.

[0083] In the several embodiments provided in this application, it should be understood that the disclosed systems, devices and methods can be implemented in other ways. For example, the device embodiments described above are merely schematic. For example, the division of units is only a logical function division. In actual implementation, there may be other division methods, such as multiple units or components can be combined or integrated into another system, or some features can be ignored or not executed. Another point is that the mutual coupling or direct coupling or communication connection shown or discussed can be an indirect coupling or communication connection through some interface, device or unit, which can be electrical, mechanical or other forms.

[0084] The above embodiments are only used to illustrate the technical solutions of the present invention, rather than to limit the same. Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that they can still modify the technical solutions described in the aforementioned embodiments, or make equivalent replacements for some of the technical features therein. However, these modifications or replacements do not deviate the essence of the corresponding technical solutions from the spirit and scope of the technical solutions of the various embodiments of the present invention.

Claims

1. A UAV landing platform, characterized in that: Including platform body and edge processor; A plurality of supporting legs are evenly arranged on the circumference of the bottom of the platform body, a plurality of ventilation slots are evenly opened on the circumference of the top of the platform body, and a gas transmission component is arranged in the ventilation slots; The platform body is provided with a collection module, which is used to obtain the landing data of the drone in real time and transmit the landing data to the edge processor; The edge processor is fixedly mounted on the top of the platform body, and the edge processor, the acquisition module and the gas delivery component are electrically connected; The edge processor is configured to perform airflow adaptation analysis on the landing data, generate an air delivery control instruction, and send the air delivery control instruction to the air delivery component; The gas delivery component is used to deliver airflow above the platform body according to the gas delivery control instruction; The edge processor includes a communication module, an initial speed module, a speed adjustment module and a summing module; The communication module is configured to receive the landing data sent by the acquisition module and transmit the landing data to the initial rotation speed module, wherein the landing data includes position data, pressure data, airflow velocity data, and airflow direction data; The initial rotation speed module is used to input the position data into a preset function of the propeller rotation speed to generate an initial rotation speed; The initial speed function is: ； in, is the initial speed, is the height coefficient, is the vertical descent speed coefficient, is the horizontal velocity coefficient, is the vertical height, is the reference height, is the vertical descent speed, is the reference vertical descent speed, is the reference horizontal velocity, is the velocity of the horizontal x-axis, is the velocity of the horizontal y-axis, is the basic revolution number; The speed adjustment module is used to input the initial speed, the position data, the airflow velocity data and the airflow direction data into a preset PID controller to obtain a speed compensation amount; The summing module is configured to sum the initial speed and the speed compensation amount to generate a gas delivery control instruction, and send the gas delivery control instruction to the gas delivery component; The acquisition module includes a position sensor, an airflow velocity sensor and an airflow direction sensor; The position sensor is fixedly installed at the top center of the platform body, and is used to obtain the position data of the drone; A plurality of airflow velocity sensors are evenly arranged on the top of the platform body, and the airflow velocity sensors are used to obtain the airflow velocity data above the platform body; A plurality of airflow direction sensors are evenly arranged on the circumference of the top of the platform body, and the airflow direction sensors are used to obtain airflow direction data above the platform body.

2. The UAV landing platform according to claim 1, characterized in that: The support leg includes a mounting block, a first support rod, a second support rod and a spiral connecting rod; One end of the mounting block is fixedly mounted on the bottom of the platform body, and one end of the first support rod is rotatably connected to the other end of the mounting block via a connecting shaft; A leveling motor is provided at the other end of the first support rod, and an output end of the leveling motor is fixedly connected to one end of the spiral connecting rod; The other end of the spiral connecting rod is threadedly connected to one end of the second supporting rod.

3. The UAV landing platform according to claim 1, characterized in that: The gas delivery assembly includes a propeller, a drive assembly and a mounting platform; The mounting platform is fixedly mounted on the bottom of the inner wall of the ventilation slot, and the driving assembly is fixedly mounted on the top of the mounting platform; The output end of the driving component is fixedly connected to the propeller, and the driving component is electrically connected to the edge processor.

4. The UAV landing platform according to claim 1, characterized in that: The acquisition module also includes a pressure sensor; A plurality of pressure sensors are evenly arranged on the top of the platform body, and the pressure sensors are used to obtain the pressure data of the drone.

5. The UAV landing platform according to claim 1, characterized in that: The acquisition module also includes a level sensor; The level sensor is fixedly installed on the platform body, and is used to measure the level data of the platform body and send the level data to the edge processor.

6. The UAV landing platform according to claim 1, characterized in that: The platform body is a circular platform.

7. The UAV landing platform according to claim 1, characterized in that: The surface of the platform body is covered with an anti-slip coating.

8. The UAV landing platform according to claim 1, characterized in that: A battery is provided on the top of the platform body; The battery, the edge processor, the acquisition module, and the gas delivery component are electrically connected.

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