A drone parking system

Abstract

The utility model provides a kind of unmanned plane residence system, belong to unmanned plane equipment technical field. Including nest main body, top cover mechanism, charging locking mechanism and control system. The solar panel of top cover mechanism can be rotatably installed on nest main body, can be switched between the horizontal protection position of covering bottom plate and the vertical open position exposed to outside, with protection and power generation function. The charging locking mechanism includes at least a pair of locking execution components that can move linearly towards each other, the driving member of which can drive the charging contact to move towards each other to clamp the corresponding part of the unmanned plane parked on the bottom plate, thereby synchronously achieving physical locking and electrical connection charging. The utility model solves the problems of existing residence system off-grid deployment difficulty, single protection and unstable charging through integrated design, realizes energy self-consistency, charging locking linkage and protection power generation integration, significantly improves the long-term autonomous operation capability of unmanned plane in unsupported environment such as field.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) equipment technology, and in particular to a UAV dwelling system. Background Technology

[0002] In recent years, with the deepening application of drones in the industry, drone hangar systems (or "drone hangars") that can automatically deploy, retrieve, and recharge drones have gradually moved from concept to commercial use, becoming an important infrastructure for improving the level of operational automation.

[0003] However, the design and service scenarios of existing mainstream drone loitering systems still have the following significant limitations: First, energy supply relies on fixed infrastructure, limiting deployment flexibility. The vast majority of automated hangars need to be connected to the municipal power grid or rely on high-power generators to ensure continuous operation and charging. This severely restricts deployment to the grid's coverage area, making it difficult to deploy quickly and cost-effectively in the wild, remote areas, disaster emergency sites, or areas with weak infrastructure. Consequently, it cannot truly support long-term autonomous operation of drones in "unsupported" environments.

[0004] Secondly, their protective functions are limited and inadequate for handling complex natural environments. Most drone dwelling systems prioritize "storage" over "protection." Their cabin designs are primarily dustproof, offering insufficient protection against harsh natural conditions such as prolonged exposure to sunlight, heavy rain, and salt spray corrosion. While some have simple top covers, they lack coordinated management with the charging process, leaving the drone vulnerable to moisture and dust intrusion even with the charging interface exposed, affecting electrical safety and equipment lifespan.

[0005] Third, the charging process lacks an active stabilization mechanism, resulting in poor environmental adaptability. Existing contact or wireless charging solutions typically begin charging after the drone lands and positions itself, but they do not fully consider dynamic factors such as wind disturbance and vibration in outdoor environments. Charging contacts may disconnect or generate arcs due to slight displacement of the drone caused by wind, leading to unstable charging efficiency and potential safety hazards. The drone dwelling system lacks a mechanism to physically lock or adaptively clamp the drone during charging, making it difficult to ensure the continuity and reliability of the charging process in inclement weather.

[0006] Fourth, the system suffers from low integration and energy efficiency due to its modular design. Some attempts to integrate solar energy often treat photovoltaic panels as independent, fixed auxiliary power supply units, resulting in large footprints and a lack of integrated design with the protective structure of the drone landing system. The overall system is bulky, and the coordination efficiency of energy collection, storage, and utilization is low, failing to achieve "structural reuse" (such as using the protective top cover as a power generation panel) to achieve a compact and efficient system design.

[0007] Therefore, under the current technological background, an integrated autonomous drone system that possesses off-grid self-sufficiency capability, strong environmental protection, and ensures stable and reliable charging remains a challenge. As drone applications continue to extend beyond grid coverage areas, developing an autonomous drone system that integrates "off-grid energy self-sufficiency, charging and stabilization linkage, and protection and power generation" is of urgent practical significance for expanding the operational boundaries of drones, reducing maintenance costs, and improving system reliability. Summary of the Invention

[0008] To overcome the shortcomings of existing hangars, such as reliance on fixed facilities for energy supply, limited protective functions, lack of stable charging mechanisms, and low system integration, this utility model provides a drone dwelling system. Designed for field operations and scenarios without a stable power grid, it aims to achieve fully automated drone support integrating autonomous power supply, intelligent charging, stable locking, and active protection, effectively expanding the sustainable operational capabilities and deployment range of drones.

[0009] The technical solution adopted by this utility model to solve its technical problem is: A drone dwelling system is provided, including a drone nest body, a top cover mechanism, a charging and locking mechanism, and a control system.

[0010] The main body of the drone housing includes a base plate, support plates, and a lower shell. There are at least two support plates, the lower ends of which are fixedly installed at both ends of the base plate. The base plate is fixedly installed on the lower shell, together forming a stable platform for supporting the drone.

[0011] The top cover mechanism includes a solar panel and a drive assembly for driving its movement. The solar panel is mounted on a support plate via a rotating connector and is driven by the drive assembly (preferably a motor reduction mechanism) to switch between a horizontal protective position covering the bottom plate and a vertical open position with the bottom plate open.

[0012] The charging locking mechanism includes a locking execution component mounted on the base plate. The locking execution component includes at least one pair of electrically driven push rods capable of linear motion towards each other, and charging contacts mounted on the movable ends of each push rod. The surface of each charging contact is provided with an anti-oxidation treatment layer and is electrically connected to a battery within the system, and then to a solar panel. The locking execution component is configured such that, driven by the electric push rods, the two charging contacts move towards each other and clamp the UAV landing gear, thereby simultaneously achieving a stable physical constraint and electrical connection. The charging contacts are electrically connected to the battery and solar panel within the system. The locking execution component is also configured such that, driven by the electric push rods, the charging contacts contact the corresponding interfaces mounted on the UAV, thereby simultaneously achieving an electrical connection and physical constraint on the UAV.

[0013] The control system includes a wireless receiving circuit and a wireless remote control module communicating with it. The control system is electrically connected to the drive component and the locking execution component, and is used to receive control commands and coordinate the actions of the top cover mechanism and the charging locking mechanism. Preferably, the control system is configured to have an automatic operating mode: upon receiving a signal that the drone has completed landing (based on pressure sensors and vision sensors mounted on the base plate to identify the drone's landing or takeoff), it can automatically control the top cover mechanism to move to a horizontal protective position, and subsequently automatically control the charging locking mechanism to perform clamping and charging actions, realizing a fully automated unattended protection process. The control system is also configured to: upon receiving a signal that the drone has completed landing, automatically execute the process of closing the top cover, extending the charging locking mechanism, and detecting contact resistance in sequence.

[0014] Furthermore, the surface of the charging contact is provided with an anti-oxidation treatment layer or a self-cleaning scraper (not shown in the figure) to improve its long-term contact reliability in outdoor environments.

[0015] Furthermore, to enhance the system's intelligence and environmental adaptability, an environmental sensor group (such as photosensors, raindrop sensors, and wind sensors, not shown in the figure) can be integrated. The signals of these sensors are connected to the control system to enable automatic optimization of the solar panel angle or automatic closing protection under severe weather conditions.

[0016] Furthermore, the system is also equipped with an emergency manual operation interface, including a handle for manually operating the top cover mechanism and a release button for manually unlocking, in response to power or control failures.

[0017] Furthermore, the position of the charging contact is adjustable to accommodate the landing gear spacing of different drone models.

[0018] Furthermore, in the horizontally protected state, the outer contour of the solar panel covers the base plate and the drone parked on it.

[0019] Compared with the prior art, the beneficial effects of this utility model are: 1. It achieves off-grid deployment and energy self-sufficiency, significantly improving the system's deployment flexibility. Through integrated solar panels and batteries working together for power supply, the system is freed from dependence on fixed municipal power grids, enabling rapid deployment and long-term autonomous operation in the field, remote areas, and emergency scenarios, significantly expanding the sustainable operational boundaries of drones.

[0020] 2. The intelligent linkage between the charging process and physical locking ensures operational reliability in harsh environments. Through an external metal contact plate structure driven by an electrically operated push rod, the drone's landing gear is adaptively pressed and locked simultaneously with the charging contacts. This mechanism effectively avoids the risk of charging interruptions or arcing due to wind or vibration, ensuring the continuity and safety of the charging process in complex outdoor environments.

[0021] 3. The protective structure and power generation function are highly integrated, resulting in a highly integrated and efficient system. The solar panels are designed as an openable top cover, which serves as a protective shield for the drone while maintaining power generation in a horizontal position, and is exposed to sunlight for efficient power generation in a vertical position. This reusable structural design solves the two major problems of equipment protection and energy harvesting simultaneously without increasing the additional footprint, making the system more compact, efficient, and reliable. Attached Figure Description

[0022] The present invention will be further described below with reference to the accompanying drawings and embodiments.

[0023] Figure 1 This is a schematic diagram of the structure of the solar panel of this utility model in a horizontal state.

[0024] Figure 2 This is a schematic diagram of the structure of the solar panel of this utility model in a vertical state.

[0025] Figure 3 This is a partial structural schematic diagram of the present invention.

[0026] Figure 4 This is the circuit diagram of this utility model. Detailed Implementation

[0027] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0028] Figure 1 , 2As shown in Figures 3 and 4, the drone dwelling system provided by this utility model includes a base plate 1, a support plate 2, a lower shell 3, a solar panel G1, a battery G2, a wireless remote control module E2, a motor reduction mechanism M1, a wireless receiving circuit 4, a power supply mechanism 5, a movable plate 8, and an electric push rod M2. There are two support plates 2. The lower ends of the two support plates 2 are fixedly installed on the left and right ends of the base plate 1, respectively. The base plate 1 is fixedly installed on the outer end of the lower housing 3. The lower housing 3 is installed on a base (not shown in the figure) that is high off the ground. A bearing seat 6 is fixedly installed on the upper rear part of the left support plate 2, and a support seat 7 is fixedly installed on the upper rear part of the right support plate 2. The motor reduction mechanism M1 is fixedly installed on the support seat 7. The frame of the solar panel G1 is fixedly installed on the movable plate 8. A shaft 81 is horizontally fixedly installed on the left and right sides of the rear end of the movable plate 8. The left shaft 81 is fixedly installed in the inner ring of the bearing seat 6, and the right shaft 81 is fixedly installed together with the left end of the power output shaft of the motor reduction mechanism M1. The power supply mechanism 5 includes two electric push rods M2 and two semi-circular outer metal contact pieces 51. The insulation on one side of the two outer metal contact pieces 51 is fixedly installed on the front end of the movable column of the two electric push rods M2. The two electric push rods M2 are fixedly installed face-to-face at a distance from each other on the left and right ends of the middle of the base plate 1. The outer sides of the two outer metal contact pieces 51 are respectively connected to the two poles of the storage battery G2, the solar panel G1, and the power input terminals 1 and 2 of the wireless receiving circuit module E1 via wires. An insulating sleeve 92 is fixedly installed on the outer end of each of the two support frames 91 of the UAV 9. An arc-shaped inner metal contact piece 93 is fixedly installed on the outer side of the sleeve 92. The inner sides of the two inner metal contact pieces 93 are respectively connected to the two poles of the storage battery (the main power source of the UAV) via wires. The other end of the power output terminal of the wireless receiving circuit, the other end of the power switch S1 and the other normally open contact of the relay J1, the other end of the power switch S2 and the other normally open contact of the relay J2, and the positive and negative and negative positive power input terminals of the motor reduction mechanism M1 are respectively connected via wires. The two normally open contacts of the relays J3 and J4 are respectively connected to the positive and negative and negative positive and negative positive power input terminals of the two electric push rods M2 via wires. The battery G2 and the wireless receiving circuit 4 are installed on the circuit board inside the lower housing 3, and the wireless remote control module E2 is installed on the side of the drone remote control device.

[0029] Figure 1 , 2As shown in Figures 3 and 4, when the movable plate 8 and solar panel G1 are in a vertical position, the distance between the lower ends of the movable plate 8 and solar panel G1 and the upper ends of the two support plates 2 is [not specified]. The arc-shaped openings of the two outer metal contact pieces 51 and the two inner metal contact pieces 93 are in a face-to-face structure. The outer diameters of the solar panel G1 and movable plate 8 are the same as the outer diameters of the base plate 1 and lower shell 3, and the outer diameter of the base plate 1 is larger than the external dimensions of the UAV 9. When the solar panel G1 is in a horizontal structure, the distance between its lower end and the upper end of the base plate 1 is greater than the height of the UAV 9. When the movable columns of the two electric push rods M2 are at their outer stops, the distance between the two outer metal contact pieces 51 is greater than the distance between the outer sides of the two support frames 91 of the UAV. The wireless receiving circuit includes a wireless receiving circuit module E1 and relays J1, J2, J3, and J4 connected via circuit board wiring, and power switches S1 and S2 (for overload protection). The positive power input terminal 1 of the wireless receiving circuit module E1 is connected to the positive control power input terminals of the four relays J1, J2, J3, and J4. The four power output terminals 3, 4, 5, and 6 of the wireless receiving circuit module E1 are respectively connected to the positive power input terminals of the four relays J1, J2, J3, and J4. The negative power input terminal 2 of the wireless receiving circuit module E1 is connected to the negative power input terminals and negative control power input terminals of the four relays J1, J2, J3, and J4. One normally open power output terminal of the first relay J1 is connected to one end of the first power switch S1, and one normally open power output terminal of the second relay J2 is connected to one end of the second power switch S2. The power switches S1 and S2 of the wireless receiving circuit are normally closed contact push-button power switches. There is an opening on the front of the left support plate 2 and the rear of the right support plate 2 of the base plate, respectively. The two power switches S1 and S2 are insulated and fixedly installed in the two openings with their buttons facing upwards. When the solar panel G1 is in a horizontal position, its lower left front end is located on the button of the first power switch S1, and the internal contacts of the first power switch S1 are open. When the solar panel G1 is in a vertical position, its lower right rear end is located on the button of the second power switch S2, and the internal contacts of the second power switch S2 are open.

[0030] Figure 1 , 2As shown in Figures 3 and 4, when the solar panel G1 is in a nearly horizontal position under normal conditions, it emits approximately 24V DC power when exposed to outdoor sunlight. This power is supplied to the battery G2 and the power input of the wireless receiver module E1. The battery G2 stores power, allowing the drone 9 to be charged even on cloudy or rainy days. After the wireless receiver module E1 is powered on, if charging the drone is not required, the user can press the first transmit button on the wireless remote control module E2. The wireless remote control module E2 will then transmit the first wireless closed signal. Upon receiving this signal, pin 3 of the wireless receiver module E1 will output a high level to the positive power input of the relay J1. The relay J1 will then close its control power input and normally open contact. Consequently, the positive and negative power inputs of the motor reduction mechanism M1 will be energized, and its shaft will drive the movable plate and the solar panel to rotate counterclockwise. When the solar panel G1 is in a nearly horizontal position, the button on the lower left side of the first power switch S1 will be activated. When the internal contacts of the first power switch S1 are open, the motor reduction mechanism M1 will lose power and stop working, preventing excessive counterclockwise rotation of the motor reduction mechanism and damage due to excessive load. When the user presses the first transmit button of the wireless remote control module E2 again, the wireless remote control module E2 transmits the first wireless open-circuit signal. After receiving the signal, the wireless receiving circuit module E1 will stop outputting a high level to the positive power input terminal of the relay J1. The relay J1 will lose power and no longer engage, opening the control power input terminal and the normally open contact terminal. Consequently, the positive and negative power input terminals of the motor reduction mechanism M1 will lose power, and its shaft will no longer drive the movable plate and solar panel to rotate counterclockwise. When the wireless receiver module E1 is powered on, if the drone needs to be charged, the user presses the second transmit button on the wireless remote control module E2. The wireless remote control module E2 transmits a second wireless closed signal. After receiving the signal, the wireless receiver module E1 outputs a high level from pin 4 to the positive power input terminal of the relay J2. The relay J2 is energized and its control power input terminal and normally open contact terminal close. Consequently, the negative and positive power input terminals of the motor reduction mechanism M1 are energized, and its shaft drives the movable plate and solar panel to rotate clockwise. When the solar panel G1 is rotated to a near-vertical position, its lower right rear end is positioned on the button of the second power switch S2. When the internal contacts of the second power switch S2 are open, the motor reduction mechanism M1 will lose power and stop working, preventing excessive clockwise rotation of the motor reduction mechanism from causing excessive load and damage. When the user presses the second transmit button of the wireless remote control module E2 again, the wireless remote control module E2 transmits the second wireless open-circuit signal. After the wireless receiving circuit module E1 receives it, its pin 4 will stop outputting a high level to the positive power input terminal of the relay J2. The relay J2 loses power and no longer engages, opening the control power input terminal and the normally open contact terminal. Consequently, the negative and positive power input terminals of the motor reduction mechanism M1 will lose power, and its shaft will no longer drive the movable plate and solar panel to rotate clockwise.When the solar panel is in a vertical position, the user can wirelessly control the drone 9 to fly and dock on the base plate 1 (the drone's two support frames 91 are located between the outer contact metal plates of the two electric push rods). After the drone is in place, the user can control the solar panel to be in a horizontal position, which will provide shade for the drone 9 from sunlight and rain.

[0031] Figure 1 , 2 As shown in Figures 3 and 4, when the drone 9 is docked and needs charging, the user presses the third transmit button on the wireless remote control module E2. The wireless remote control module E2 transmits a third wireless closed signal. After receiving the signal, the wireless receiving circuit module E1 outputs a high level at pin 5 to the positive power input terminal of the relay J3. The relay J3 is energized and its control power input terminal and normally open contact terminal close. Consequently, the positive and negative power input terminals of the two electric push rods M2 are energized, and their movable columns drive the two outer metal contact pieces 51 to move inward. The two outer metal contact pieces 51 contact the inner metal contact pieces 93 on the outer side of the two support frames of the drone and are electrically connected. (At this moment, the power output from battery G2 and solar panel G1 will enter the battery power input terminal of the drone to charge the drone battery.) Then, the user presses the third transmit button of the wireless remote control module E2 again. The wireless remote control module E2 transmits the third wireless open circuit signal. After the wireless receiving circuit module E1 receives it, its pin 5 will stop outputting a high level to the positive power input terminal of relay J3. The relay J3 is de-energized and no longer engages its control power input terminal and normally open contact terminal. Consequently, the positive and negative power input terminals of the two electric push rods M2 will be de-energized, and their moving columns will no longer drive the two outer metal contact pieces 51 to move inward. When the wireless receiver module E1 is powered on, if the drone does not need to be charged (or the drone is about to take off), the user presses the fourth transmit button on the wireless remote control module E2. The wireless remote control module E2 then transmits a fourth wireless closed signal. Upon receiving this signal, the wireless receiver module E1 outputs a high level from pin 6 to the positive power input terminal of relay J4. Relay J4 is energized, closing its control power input terminal and normally open contact. Consequently, the negative and positive power input terminals of the two electric push rods M2 are energized, and their movable columns respectively drive the two outer metal contact pieces 51 to move outwards. The contact piece 51 is spaced apart from the inner metal contact piece 93 on the outer side of the two support frames of the drone. Then, the user presses the fourth transmit button of the wireless remote control module E2 again. The wireless remote control module E2 transmits the fourth wireless open circuit signal. After the wireless receiving circuit module E1 receives it, its 6th pin will stop outputting a high level to the positive power input terminal of the relay J4. The relay J4 is de-energized and no longer closes its control power input terminal and normally open contact terminal. Consequently, the positive and negative power input terminals of the two electric push rods M2 will be de-energized, and their movable columns will no longer drive the two outer metal contact pieces 51 to move outward.

[0032] As an example, relays J1, J2, J3, and J4 are DC 24V relays; battery G2 is a 24V / 100Ah lithium battery; solar panel G1 has a power of 200W; motor reduction mechanism M1 is a 300W coaxial motor gear reducer with a shaft speed of 6 revolutions per minute; electric push rod M2 is a 30W reciprocating electric telescopic rod; wireless remote control module E2 and wireless receiving circuit module E1 are finished wireless transmitting and receiving module components of model TX315B1 (with the same working principle as wireless transmitting and receiving module components used in vehicles, etc.). All components used in this application are prior art, and their structure and working principle will not be described in detail here.

[0033] As another optional embodiment, the system can also integrate environmental sensors such as photosensors and raindrop sensors (not shown in the figure), whose signal output terminals are connected to a specific I / O port of the wireless receiving circuit module E1. The control system can be programmed to automatically control the motor reduction mechanism M1 to rotate the solar panel G1 to a horizontal protective position when the raindrop sensor is triggered.

[0034] In the automatic operating mode of the system, its control logic follows a reliable sequence of protection first, followed by locking and charging. Specifically, after the drone 9 lands on the base plate 1 and triggers a positioning signal (such as a pressure sensor or visual signal), the control system (via the wireless receiving circuit module E1 and a relay) first drives the motor reduction mechanism M1 to rotate the solar panel G1 to a horizontal protective position, providing shelter for the drone. After confirming that the top cover is closed (e.g., through the state of the limit switch S1), the control system drives the electric push rod M2 to move the charging contacts 51 towards each other, clamping the drone landing gear and establishing an electrical connection to begin charging. This sequential control fundamentally avoids the electrical risks and instability that may arise from connecting the charging interface when the top cover is open and exposed to rain, snow, wind, or other environmental conditions.

[0035] In addition, the drone dwelling system is also equipped with an emergency manual operation interface, including: (1) The manual opening and closing handle of the solar panel is located on the side of the support base 7, and can be manually rotated to open the solar panel when the power is off; (2) The manual release button for the electric actuator is located on the side of the electric actuator M2. Pressing it allows for manual adjustment of the contact plate position.

[0036] In summary, this utility model systematically solves three major challenges faced by drones in field deployment through structural innovation: First, the design of an openable and closable solar top cover integrates power generation and protection, solving the energy supply problem for off-grid deployment; second, the charging-locking linkage mechanism physically locks the drone while the charging contacts are connected, solving the reliability problem of outdoor charging being susceptible to environmental interference; third, the combination of the above two aspects enables the system to have fully automatic protection capabilities without the need for an external power grid, significantly expanding the operational boundaries and deployment flexibility of drones.

[0037] The foregoing has shown and described the basic principles, main features, and advantages of this utility model. It will be apparent to those skilled in the art that this utility model is limited to the details of the exemplary embodiments described above, and that it can be implemented in other specific forms without departing from the spirit or basic characteristics of this utility model. Therefore, the embodiments should be considered exemplary and non-limiting in all respects. The scope of this utility model is defined by the appended claims rather than the foregoing description, and thus all variations falling within the meaning and scope of equivalents of the claims are intended to be included within this utility model.

[0038] Furthermore, it should be understood that although this specification describes the embodiments, the embodiments do not necessarily contain only one independent technical solution. This way of describing the specification is only for clarity. Those skilled in the art should regard the specification as a whole. The technical solutions in the embodiments can also be appropriately combined to form other embodiments that can be understood by those skilled in the art.

Claims

1. A drone dwelling system, characterized in that, include: The nest body includes a base plate for supporting the drone; a top cover mechanism including a solar panel and a drive assembly, the solar panel being rotatably connected to the nest body and switchable between a horizontally protected position covering the base plate and a vertically open position exposed to the outside; and a charging locking mechanism including a locking execution assembly disposed on the base plate, the locking execution assembly including at least a pair of drive assemblies capable of linear motion toward each other, and charging contacts mounted on the movable ends of each drive assembly. The charging contacts are used to move towards each other and clamp the corresponding parts of the drone that are stationed on the base plate under the drive of the drive component, thereby simultaneously realizing physical constraint and electrical connection; the control system is electrically connected to the drive component and the locking execution component respectively, and is used to receive control commands and coordinate the operation of the top cover mechanism and the charging locking mechanism.

2. The unmanned aerial vehicle (UAV) dwelling system according to claim 1, characterized in that, The main body of the solar cell also includes at least two support plates and a shell. The lower end of the support plate is fixed to the base plate, the shell is connected to the bottom of the base plate, and the solar panel is connected to the support plate through a rotating shaft.

3. The unmanned aerial vehicle (UAV) hovering system according to claim 1, characterized in that, The drive component is a motor reduction mechanism, whose output shaft is connected to the rotating shaft of the solar panel.

4. The unmanned aerial vehicle (UAV) dwelling system according to claim 1, characterized in that, The drive component is an electric actuator.

5. The unmanned aerial vehicle (UAV) dwelling system according to claim 1, characterized in that, The contact surface of the charging contact is provided with an anti-oxidation treatment layer or is equipped with a self-cleaning scraper.

6. The unmanned aerial vehicle (UAV) hovering system according to claim 1, characterized in that, It also includes an environmental sensor array whose signals are connected to the control system to enable automatic optimization of the solar panel angle or automatic closure protection in severe weather.

7. The unmanned aerial vehicle (UAV) dwelling system according to claim 1, characterized in that, It also includes an emergency manual operation interface located on the main body of the nest, including a handle for manually operating the top cover mechanism and a release button for manually unlocking, in response to power or control failures.

8. The unmanned aerial vehicle (UAV) hovering system according to claim 1, characterized in that, In the horizontally protected state, the outer contour of the solar panel covers the base plate and the drone parked on it.

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