Unmanned aerial vehicle take-off and landing system integrating sensing, computing and intelligence

Abstract

The utility model discloses an unmanned aerial vehicle take-off and landing system with integrated communication, calculation and intelligence, relates to the technical field of unmanned aerial vehicles, and solves the technical problem that an unmanned aerial vehicle take-off and landing field management and control system is difficult to meet the use requirements of the unmanned aerial vehicle in complex tasks and diversified scenes. The system comprises a space capsule, a take-off and landing platform, an all-in-one machine and a control box. The take-off and landing platform is arranged at the top of the space capsule and used for providing a take-off and landing place for the unmanned aerial vehicle; the all-in-one machine is arranged at the top of the space capsule and used for monitoring the take-off and landing environment of the take-off and landing platform; the control box is arranged in the space capsule, electrically connected with the all-in-one machine and used for providing power supply and network connection for the all-in-one machine; the space capsule is used for bearing the take-off and landing platform, the all-in-one machine and the control box and further used for providing sites with different purposes for users. According to the utility model, the use requirements of the unmanned aerial vehicle in complex tasks and diversified scenes can be met.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) technology, and in particular to an integrated sensing, computing and intelligence UAV take-off and landing system. Background Technology

[0002] With the rapid development of drone technology, drones are increasingly being used in logistics, aerial photography, agricultural monitoring, and emergency rescue. To ensure the efficient operation of drones in various tasks, especially their ability to quickly take off and begin operations in emergencies, or to perform data log downloads while powered on, the design and optimization of drone takeoff and landing site control systems are crucial. Traditional takeoff and landing site control systems typically combine ground-based takeoff and landing sites with integrated control units. While this approach meets the basic requirements for drone takeoff, landing, and control to some extent, it still has many shortcomings.

[0003] First, traditional take-off and landing site control systems require a large land area for construction, which not only increases land use costs but also limits the system's deployment flexibility. This is especially true in densely populated urban areas or regions with limited land resources, where securing land for take-off and landing sites is difficult, making it hard to meet the needs for rapid deployment and flexible scheduling of drones. Second, traditional systems have limited adaptability, typically operating from a single fixed location and unable to be moved or adjusted according to actual needs. This is particularly inconvenient when dealing with emergencies or temporary missions. Furthermore, traditional take-off and landing site control systems are functionally limited, often only possessing basic take-off, landing, and control functions, lacking comprehensive support for diverse needs such as drone logistics transportation, aerial photography, equipment storage, and refueling.

[0004] In the process of developing this utility model, the applicant discovered at least the following problems in the prior art:

[0005] Current drone take-off and landing site management systems are insufficient to meet the needs of drones in complex missions and diverse scenarios. Utility Model Content

[0006] The purpose of this invention is to provide an integrated sensing, computing, and intelligent drone take-off and landing system to solve the technical problem that existing drone take-off and landing site control systems cannot meet the usage requirements of drones in complex tasks and diverse scenarios. The various technical effects of the preferred solutions among the many technical solutions provided by this invention are detailed below.

[0007] To achieve the above objectives, the present invention provides the following technical solution:

[0008] This utility model provides an integrated sensing and computing intelligent drone take-off and landing system, including a space capsule, a take-off and landing platform, an integrated unit, and a control box. The take-off and landing platform is located on top of the space capsule, providing a place for drones to take off and land. The integrated unit is located on top of the space capsule, used to monitor the take-off and landing environment of the take-off and landing platform. The control box is located inside the space capsule and electrically connected to the integrated unit, used to provide power and network connectivity to the integrated unit. The space capsule is used to house the take-off and landing platform, the integrated unit, and the control box, and also provides users with office space and storage and charging space for the drones.

[0009] Optionally, the integrated unit includes a weather station, a rain gauge, a camera device, and a support structure; the bottom of the support structure is fixedly connected to the top of the spacecraft; the weather station, rain gauge, and camera device are all fixedly connected to the top of the support structure; the weather station is used to detect and record the environmental and meteorological data of the take-off and landing platform in real time through the camera device; the rain gauge is used to measure precipitation.

[0010] Optionally, the support structure includes an upright, a first horizontal bar, a second horizontal bar, and a third horizontal bar; one end of the first horizontal bar, one end of the second horizontal bar, and one end of the third horizontal bar are all fixedly connected to the top of the upright; the rain gauge is fixedly connected to the first horizontal bar; and the weather station is fixedly connected to the second horizontal bar.

[0011] Optionally, the camera device includes an outdoor camera and a panoramic camera; the outdoor camera is fixedly connected to the third crossbar and is used to capture the environment of the take-off and landing platform; the panoramic camera is fixedly connected to the bottom of the first crossbar by a fastener and is used to capture the environment of the entire top of the spacecraft.

[0012] Optionally, the all-in-one machine also includes a floodlight and a megaphone; the floodlight is fixedly connected to the first crossbar and is used to provide illumination and warning lights; the megaphone is fixedly connected to the pole and is used to support the user to make announcements.

[0013] Optionally, the control box includes a power supply, a switch, a main network router, a wireless router, a server, a network video recorder, and a gateway mounted on the control panel; the power supply is used to convert AC power to 48V and 12V, providing 48V power to the switch and 12V power to the gateway, the main network router, the weather station, and the rain gauge; the server, the wireless router, and the network video recorder are connected to the AC power via power strips.

[0014] Optionally, the WAN interface of the main network router is connected to the main network; the four LAN interfaces of the main network router are respectively connected to the switch, the wireless router, the server, and the network video recorder; the switch is connected to the network port inside the space capsule to support data transmission within the space capsule; the wireless router is connected to the network port inside the space capsule to provide a wireless network within the space capsule; the switch is also connected to the weather station and the rain gauge through the gateway to support data exchange between the weather station and the rain gauge; the server is connected to the megaphone through an audio RCA connector to transmit audio signals to the megaphone.

[0015] Optionally, the control box also includes an air circuit breaker, which is installed between the mains power and the power supply, switch, main network router, wireless router, server, network video recorder and gateway, and is used to automatically cut off the current when the control box is overloaded or short-circuited.

[0016] Optionally, the control box further includes a control switch; the floodlight is connected to the mains power supply via the control switch.

[0017] Optionally, a staircase is provided on the side of the space capsule to assist users in accessing the top of the space capsule from the ground.

[0018] Implementing one of the above-described technical solutions of this utility model has the following advantages or beneficial effects:

[0019] This utility model provides an integrated sensing and computing-based UAV take-off and landing system. The integrated unit and take-off and landing platform are integrated into the roof of a space capsule, forming a control system for the UAV and the take-off and landing site. Power and network data are connected to the cabin via a control box, facilitating user office and control within the capsule. Furthermore, the integrated cabin eliminates the need for ground construction, occupies a small area, and is easy to transport and deploy. It is compatible with traditional take-off and landing site applications and is suitable for a wider variety of scenarios, meeting the needs of UAVs in complex missions and diverse environments. Attached Figure Description

[0020] To more clearly illustrate the technical solutions of the embodiments of this utility model, the drawings used in the description of the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort. In the drawings:

[0021] Figure 1 This is a first structural schematic diagram of the integrated sensing, computing, and intelligence drone take-off and landing system according to an embodiment of this utility model;

[0022] Figure 2 This is a schematic diagram of the second structure of the integrated sensing and computing intelligent drone take-off and landing system according to an embodiment of this utility model;

[0023] Figure 3 This is a schematic diagram of the structure of the all-in-one machine according to an embodiment of this utility model;

[0024] Figure 4 This is a schematic diagram of the control box in an embodiment of the present invention;

[0025] Figure 5 This is an electrical diagram of the control box according to an embodiment of this utility model;

[0026] Figure 6 This is a network diagram of the control box in an embodiment of this utility model;

[0027] In the diagram: 1. Space capsule; 2. Take-off and landing platform; 3. All-in-one machine; 31. Weather station; 32. Rain gauge; 33. Camera device; 331. Outdoor camera; 332. Panoramic camera; 333. Fixture; 34. Support structure; 341. Pole; 342. First crossbar; 343. Second crossbar; 344. Third crossbar; 35. Floodlight; 36. Megaphone; 4. Control box; 41. Power supply; 42. Switch; 43. Main network router; 44. Wireless router; 45. Server; 46. Network video recorder; 47. Gateway; 48. Circuit breaker; 49. Control switch; 410. Power strip; 5. Ladder; 6. Drone. Detailed Implementation

[0028] To make the objectives, technical solutions, and advantages of this utility model clearer, various exemplary embodiments described below will be referenced to the accompanying drawings, which form part of the exemplary embodiments, illustrating various exemplary embodiments that may be adopted to implement this utility model. Unless otherwise indicated, the same numbers in different drawings represent the same or similar elements. The embodiments described in the following exemplary embodiments do not represent all embodiments consistent with this disclosure. It should be understood that they are merely examples of processes, methods, and apparatuses consistent with some aspects of this utility model disclosed as detailed in the appended claims, and other embodiments may be used, or structural and functional modifications may be made to the embodiments listed herein without departing from the scope and spirit of this utility model.

[0029] In the description of this utility model, it should be understood that the terms "center," "longitudinal," "lateral," etc., indicate the orientation or positional relationship based on the accompanying drawings, and are only for the convenience of describing this utility model and simplifying the description, and do not indicate or imply that the referred element must have a specific orientation, or be constructed and operated in a specific orientation. The terms "first," "second," etc., are used for descriptive purposes only and should not be construed as indicating or implying relative importance or implicitly specifying the number of indicated technical features. The term "multiple" means two or more. The terms "connected" and "linked" should be interpreted broadly, for example, they can be fixed connections, detachable connections, integral connections, mechanical connections, electrical connections, communication connections, direct connections, indirect connections through an intermediate medium, and can be the internal connection of two elements or the interaction relationship between two elements. The term "and / or" includes any and all combinations of one or more of the related listed items. Those skilled in the art can understand the specific meaning of the above terms in this utility model according to the specific circumstances.

[0030] To illustrate the technical solution described in this utility model, specific embodiments are described below, showing only the parts related to the embodiments of this utility model.

[0031] Example 1:

[0032] like Figure 1 and Figure 2 As shown, this utility model provides an integrated sensing and computing intelligent drone take-off and landing system, including a space capsule 1, a take-off and landing platform 2, an all-in-one machine 3, and a control box 4. The take-off and landing platform 2 is located on top of the space capsule 1, providing a place for the drone 6 to take off and land. The all-in-one machine 3 is located on top of the space capsule 1, used to monitor the take-off and landing environment of the take-off and landing platform 2. The control box 4 is located inside the space capsule 1 and is electrically connected to the all-in-one machine 3, providing power and network connectivity to the all-in-one machine 3. The space capsule 1 is used to carry the take-off and landing platform 2, the all-in-one machine 3, and the control box 4, and also provides a space for users to work, as well as for storing and charging the drone 6. The space capsule 1 is a customized multi-functional cabin system that can be designed into spaces for different purposes, such as living cabins, working cabins, meeting cabins, and command centers, according to different needs. This allows the system provided in this embodiment to be applied to various scenarios, such as temporary residences, mobile offices, emergency rescue command centers, or special mission operation bases, greatly expanding the application scenarios.

[0033] The integrated sensing and computing intelligent UAV 6 takeoff and landing system provided in this embodiment integrates the all-in-one unit 3 and the takeoff and landing platform 2 into the roof of the space capsule 1, forming a control system for the UAV 6 and the takeoff and landing site on the roof. Power and network data are connected to the cabin through the control box 4, facilitating user office and control within the cabin. Moreover, the integrated cabin eliminates the need for ground construction, occupies a small area, and is easy to transport and deploy. It is not only compatible with traditional takeoff and landing site applications but also suitable for a wider variety of application scenarios, meeting the usage requirements of the UAV 6 in complex missions and diverse scenarios.

[0034] Below, in conjunction with Figures 1-6 The construction of the integrated sensing, computing, and intelligence-based UAV takeoff and landing system provided in the embodiments is described in detail below:

[0035] like Figure 1 As shown, the takeoff and landing platform 2, made of lightweight materials and technology, is integrated into the roof of the space capsule 1, providing a takeoff and landing site for the UAV 6. This platform 2 not only boasts excellent durability and stability but also supports customization, allowing for the addition of various markings, paint schemes, or special functional modules according to user requirements. To ensure the efficient operation of the UAV 6 under different environmental and mission conditions, the surface texture of the platform 2 has been improved to enhance its anti-slip capabilities, and a precise positioning system and rapid deployment mechanism have been incorporated, providing a safe and reliable takeoff and landing environment. Furthermore, the platform is compatible with various models of the UAV 6 and can adapt to different weather conditions and terrain, making it an ideal choice for diverse missions such as reconnaissance, surveillance, and logistics transportation. By perfectly integrating the takeoff and landing platform 2 with the capsule, not only is the safety and convenience of operating the UAV 6 improved, but it also brings users more flexible and diverse application possibilities. Whether navigating between urban skyscrapers or performing emergency rescue missions in remote areas, the platform 2 ensures that the UAV 6 can successfully complete every takeoff and landing.

[0036] like Figure 3 As shown, the integrated unit 3 includes a weather station 31, a rain gauge 32, a camera device 33, and a support structure 34, providing comprehensive monitoring and management facilities for the take-off and landing platform 2. The bottom of the support structure 34 is fixedly connected to the top of the space capsule 1. The weather station 31, rain gauge 32, and camera device 33 are all fixedly connected to the top of the support structure 34. The weather station 31 is used to detect and record environmental and meteorological data of the take-off and landing platform 2 in real time through the camera device 33, such as wind speed, wind direction, temperature, humidity, and air pressure, so that managers can understand and grasp the on-site conditions. The rain gauge 32 is used to measure precipitation. The integrated unit 3 can also measure precipitation through the rain gauge 32, helping managers predict and prevent the impact of rain on the take-off and landing of the platform.

[0037] Furthermore, the support structure 34 includes a vertical pole, a first horizontal bar 342, a second horizontal bar 343, and a third horizontal bar 344; one end of the first horizontal bar 342, one end of the second horizontal bar 343, and one end of the third horizontal bar 344 are all fixedly connected to the top of the vertical pole; the rain gauge 32 is fixedly connected to the first horizontal bar 342; and the weather station 31 is fixedly connected to the second horizontal bar 343. Integrating the weather station 31, the rain gauge 32, and the camera device 33 onto a single vertical pole results in a compact structure and a small footprint.

[0038] The camera device 33 includes an outdoor camera 331 and a panoramic camera 332. The outdoor camera 331 is fixedly connected to the third crossbar 344 and is used to capture the environment of the take-off and landing platform 2. The outdoor camera 331 faces the take-off and landing platform 2 and can capture and record the take-off and landing of the drone 6 on the platform 2 in real time, providing clear and accurate on-site images for management personnel, which helps to promptly detect and handle various emergencies. The panoramic camera 332 is fixedly connected to the bottom of the first crossbar 342 via a fastener 333 and is used to capture the environment of the entire top of the space capsule 1. The panoramic camera 332 can capture the external environment with 360° coverage, providing reliable environmental information to the weather station 31.

[0039] The integrated unit 3 also includes a floodlight 35 and a megaphone 36; the floodlight 35 is fixedly connected to the first crossbar 342 to provide illumination and warning lights; the megaphone 36 is fixedly connected to the pole to support the user's announcements. For example, when the drone 6 malfunctions at night, the personnel inside the capsule 1 can adjust the floodlight 35 to change the light color through the control box 4, or directly announce the situation through the megaphone 36 to the personnel on the top of the capsule 1, so that appropriate measures can be taken in a timely manner to ensure the safe take-off and landing of the drone 6.

[0040] Furthermore, such as Figure 4 and Figure 5 As shown, the control box 4 includes a power supply 41, a switch 42, a main network router 43, a server 45, a network video recorder 46, and a gateway 47, all mounted on the control panel. The power supply 41 converts AC mains power into 48V and 12V power, providing 48V to the switch 42 and 12V to the gateway 47, main network router 43, weather station 31, and rain gauge 32. The server 45, main network router 43, and network video recorder 46 are connected to AC mains power via a power strip 410. The power supply 41 is directly connected to AC mains power; after AC mains power is input, it is converted into 48V and 12V power. The power supply 41 delivers 48V to the switch 42 and 12V to the gateway 47, main network router 43, weather station 31, and rain gauge 32. The server 45, main network router 43, and network video recorder 46 are directly powered by AC mains power via the power strip 410.

[0041] like Figure 6 As shown, the WAN interface of the main network router 43 connects to the main network, enabling the main router to forward data between the local network and the main network, thus facilitating communication and data exchange between local devices and other devices on the main network. The four LAN interfaces of the main network router 43 connect to the switch 42, the main network router 43, the server 45, and the network video recorder 46, respectively. The main network router 43 is one of the core devices of the entire network, responsible for connecting the external network and the internal LAN. The LAN interfaces are used for communication with other devices on the internal network. Connecting to the switch 42 expands the number of network interfaces, allowing more devices to access the network. The main network router 43 provides wireless network signals, enabling wireless devices to access the network, allowing administrators in capsule 1 to use the wireless network. The server 45 provides various services, such as file storage and data processing. The network video recorder 46 is mainly used for storing and managing surveillance video and related data. Through this connection method, these devices can communicate with each other within the same LAN, jointly building a complete network environment.

[0042] Switch 42 is connected to the network port inside Space Capsule 1 to support data transmission within Space Capsule 1; Main Network Router 43 is also connected to the network port inside Space Capsule 1 to provide wireless network access within Space Capsule 1; Switch 42 is also connected to Weather Station 31 and Rain Gauge 32 via Gateway 47 to support data exchange between Weather Station 31 and Rain Gauge 32. Gateway 47 acts as a relay and coordinator for communication, enabling Switch 42 to perform data transmission and interaction with Weather Station 31 and Rain Gauge 32; Gateway 47 communicates with Weather Station 31 and Rain Gauge 32 using the RS-485 protocol. This ensures that the data collected by Weather Station 31 and Rain Gauge 32 is accurately transmitted to Gateway 47, and then transmitted to administrators via the network port inside Space Capsule 1 for analysis and processing. Server 45 is connected to megaphone 36 via an audio RCA connector to transmit audio signals to megaphone 36; server 45 transmits audio signals to megaphone 36 via audio RCA connector to realize sound playback and broadcasting functions.

[0043] The control box 4 is integrated into the cabin of the space capsule 1 and electrically connected to the all-in-one unit 3. This integrated design simplifies the installation and maintenance process and may improve the system's compactness and aesthetics. The control box 4 not only provides power and network connectivity but also supports data exchange, providing the necessary infrastructure for low-altitude command of the UAV 6. The control box 4 integrates edge computing power, enabling it to process and analyze locally generated data, reducing reliance on remote data centers, lowering latency, and improving response speed. A secure storage mechanism based on blockchain encryption ensures the integrity, immutability, and security of the data.

[0044] As an alternative implementation, the control box 4 also includes an air circuit breaker 48, which is installed between the mains power supply 41, the switch 42, the main network router 43, the server 45, the network video recorder 46, and the gateway 47. It is used to automatically cut off the current when the control box 4 is overloaded or short-circuited, so as to ensure the circuit safety of the all-in-one machine 3.

[0045] As an alternative implementation, the control box 4 also includes a control switch 49; the floodlight 35 is connected to the mains power through the control switch 49 to ensure the nighttime lighting function of the floodlight.

[0046] As an alternative implementation, a staircase 5 is provided on the side of the space capsule 1 to assist users in accessing the top of the space capsule 1 from the ground. Management personnel can use the staircase 5 to access the top of the space capsule 1 from the ground to facilitate the inspection and maintenance of the take-off and landing platform 2 and the integrated machine 3.

[0047] The UAV 6 takeoff and landing system provided in this embodiment solves the problems of large ground footprint, difficulty in deployment, immobility, and limited applicability of the UAV 6 takeoff and landing platform 2. It integrates the UAV 6 integrated unit 3 and the takeoff and landing platform 2 onto the top of the space capsule 1, forming a complete UAV 6 operation and management system. This system achieves efficient resource utilization, while also offering convenience and flexibility. It can be deployed quickly, occupies a small area, is easy to transport, and is suitable for various environments and scenarios, such as scenic spots, islands, grasslands, and other natural environments, greatly expanding the application scope of the UAV 6.

[0048] The embodiment is merely a special case and does not indicate that this utility model is implemented in such a way.

[0049] The above description is merely a preferred embodiment of the present utility model. Those skilled in the art will understand that various changes or equivalent substitutions can be made to these features and embodiments without departing from the spirit and scope of the present utility model. Furthermore, under the teachings of the present utility model, these features and embodiments can be modified to adapt to specific situations and materials without departing from the spirit and scope of the present utility model. Therefore, the present utility model is not limited to the specific embodiments disclosed herein, and all embodiments falling within the scope of the claims of this application are within the protection scope of the present utility model.

Claims

1. An unmanned aerial vehicle (6) take-off and landing system integrated with artificial intelligence, characterized by, The utility model provides a space cabin (1), landing platform (2), integrated machine (3) and control box (4) are included, landing platform (2) sets up at the top of space cabin (1), is used to provide the place of takeoff and landing for unmanned aerial vehicle (6), integrated machine (3) sets up at the top of space cabin (1), is used for monitoring the takeoff and landing environment of landing platform (2), control box (4) sets up in the inside of space cabin (1) with integrated machine (3) electric connection, is used to provide power supply and network connection for integrated machine (3), space cabin (1) is used to bear landing platform (2), integrated machine (3) and control box (4), still be used to provide the place of office for user and the storage and charging site for unmanned aerial vehicle (6).

2. An unmanned aerial vehicle (6) take-off and landing system integrated with a general artificial intelligence according to claim 1, characterized in that, The utility model provides a space cabin (1), landing platform (2), integrated machine (3) and control box (4) are included, landing platform (2) sets up at the top of space cabin (1), is used to provide the place of takeoff and landing for unmanned aerial vehicle (6), integrated machine (3) sets up at the top of space cabin (1), is used for monitoring the takeoff and landing environment of landing platform (2), control box (4) sets up in the inside of space cabin (1) with integrated machine (3) electric connection, is used to provide power supply and network connection for integrated machine (3), space cabin (1) is used to bear landing platform (2), integrated machine (3) and control box (4), still be used to provide the place of office for user and the storage and charging site for unmanned aerial vehicle (6).

3. An unmanned aerial vehicle (6) take-off and landing system integrated with a general artificial intelligence according to claim 2, characterized in that, The utility model provides a space cabin (1), landing platform (2), integrated machine (3) and control box (4) are included, landing platform (2) sets up at the top of space cabin (1), is used to provide the place of takeoff and landing for unmanned aerial vehicle (6), integrated machine (3) sets up at the top of space cabin (1), is used for monitoring the takeoff and landing environment of landing platform (2), control box (4) sets up in the inside of space cabin (1) with integrated machine (3) electric connection, is used to provide power supply and network connection for integrated machine (3), space cabin (1) is used to bear landing platform (2), integrated machine (3) and control box (4), still be used to provide the place of office for user and the storage and charging site for unmanned aerial vehicle (6).

4. An unmanned aerial vehicle (6) take-off and landing system integrated with a general artificial intelligence according to claim 3, characterized in that, The utility model provides a space cabin (1), landing platform (2), integrated machine (3) and control box (4) are included, landing platform (2) sets up at the top of space cabin (1), is used to provide the place of takeoff and landing for unmanned aerial vehicle (6), integrated machine (3) sets up at the top of space cabin (1), is used for monitoring the takeoff and landing environment of landing platform (2), control box (4) sets up in the inside of space cabin (1) with integrated machine (3) electric connection, is used to provide power supply and network connection for integrated machine (3), space cabin (1) is used to bear landing platform (2), integrated machine (3) and control box (4), still be used to provide the place of office for user and the storage and charging site for unmanned aerial vehicle (6).

5. An integrated unmanned aerial vehicle (6) take-off and landing system with sensing and intelligence according to claim 3, characterized in that, The utility model provides a space cabin (1), landing platform (2), integrated machine (3) and control box (4) are included, landing platform (2) sets up at the top of space cabin (1), is used to provide the place of takeoff and landing for unmanned aerial vehicle (6), integrated machine (3) sets up at the top of space cabin (1), is used for monitoring the takeoff and landing environment of landing platform (2), control box (4) sets up in the inside of space cabin (1) with integrated machine (3) electric connection, is used to provide power supply and network connection for integrated machine (3), space cabin (1) is used to bear landing platform (2), integrated machine (3) and control box (4), still be used to provide the place of office for user and the storage and charging site for unmanned aerial vehicle (6).

6. An unmanned aerial vehicle (6) take-off and landing system integrated with a general-purpose computer according to claim 5, characterized in that, The control box (4) comprises a power supply (41), an exchange (42), a main network router (43), a wireless router (44), a server (45), a network video recorder (46) and a gateway (47) arranged on the control board; the power supply (41) is used to convert the mains into 48V power supply and 12V power supply, and provide 48V power supply for the exchange (42), and provide 12V power supply for the gateway (47), the main network router (43), the weather station (31) and the rain gauge (32); the server (45), the wireless router (44) and the network video recorder (46) are connected with the mains through the extension socket (410).

7. An unmanned aerial vehicle (6) take-off and landing system integrated with a general artificial intelligence according to claim 6, characterized in that, The WAN interface of the main network router (43) is connected with the main network; the four LAN interfaces of the main network router (43) are connected with the exchange (42), the wireless router (44), the server (45) and the network video recorder (46) respectively; the exchange (42) is connected with the network port in the space cabin (1), and is used to support the data transmission in the space cabin (1); the wireless router (44) is connected with the network port in the space cabin (1), and is used to provide wireless network for the space cabin (1); the exchange (42) is further connected with the weather station (31) and the rain gauge (32) through the gateway (47), and is used to support the data exchange of the weather station (31) and the rain gauge (32); the server (45) is connected with the loudspeaker (36) through the audio lotus head, and is used to transmit audio signals to the loudspeaker (36).

8. An integrated unmanned aerial vehicle (6) take-off and landing system with sensing and intelligence according to claim 6, characterized in that, The control box (4) further comprises an air circuit breaker (48) arranged between the mains and the power supply (41), the exchange (42), the main network router (43), the wireless router (44), the server (45), the network video recorder (46) and the gateway (47), and is used to automatically cut off the current when the control box (4) is overloaded or short-circuited.

9. The unmanned aerial vehicle (6) take-off and landing system integrated with a general artificial intelligence according to claim 6, characterized in that, The control box (4) further comprises a control switch (49); the projection lamp (35) is connected with the mains through the control switch (49).

10. The unmanned aerial vehicle (6) take-off and landing system integrated with a general artificial intelligence according to claim 1, characterized in that, The space cabin (1) is provided with a ladder (5) on the side, and the ladder (5) is used to assist the user to go to the top of the space cabin (1) from the ground.

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