Stabilizing mechanism and remote controller

Abstract

The utility model relates to the technical field of unmanned aerial vehicle remote control equipment, in particular to a stabilizing mechanism and a remote controller, which can be used for conveniently adding a communication antenna and protecting an antenna interface when an additional antenna is not used, and comprises an external component, comprising a shell, a screen arranged at the top of the shell, a first antenna interface arranged on the side face of the shell and a second antenna interface arranged on the side face of the first antenna interface, specifically, an operator interacts with a remote controller through the screen and sends out a control instruction to remotely control the unmanned aerial vehicle, and when an antenna is inserted into the second antenna interface, the unmanned aerial vehicle can be remotely controlled. The antenna interface can be closed to prevent the interface from being polluted when the additional antenna is not connected, the remote controller can be connected with a plurality of unmanned aerial vehicle remote controllers in parallel, and multi-task collaborative operation of the unmanned aerial vehicle is achieved.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) remote control equipment technology, and in particular to a stabilization mechanism and a remote controller. Background Technology

[0002] In recent years, the application scenarios of drones have gradually expanded, covering multiple fields from agricultural plant protection and energy inspection to emergency rescue and security monitoring. To meet increasingly complex mission requirements, multi-drone collaborative operation has become a key technology. However, existing drone control methods typically involve a single remote controller for a single drone. This approach is inefficient in multi-drone collaborative tasks and struggles to meet the demands of high-efficiency operations in various scenarios. Even multi-channel systems usually only achieve basic directional control, which is insufficient for the requirements of multi-drone collaborative operation in practical applications.

[0003] The existing technology has the following shortcomings: traditional technology relies on a one-to-one connection between the remote controller and the drone, which makes it difficult to support the simultaneous control of multiple drones; when controlling multiple drones, additional antennas need to be inserted and stabilized, and when the extra antenna interfaces are not in use, it is necessary to prevent foreign objects such as dust from entering the antenna interfaces. Utility Model Content

[0004] In view of the problem that existing technologies rely on a one-to-one connection between the remote controller and the drone, making it difficult to support the simultaneous control of multiple drones, this utility model is proposed.

[0005] To solve the above-mentioned technical problems, this utility model provides the following technical solution: a stabilizing mechanism, comprising,

[0006] The external component includes a housing, a screen disposed on the top of the housing, a first antenna interface disposed on the side of the housing, and a second antenna interface disposed on the side of the first antenna interface.

[0007] In a preferred embodiment of the stabilizing mechanism of this utility model, a switch is provided on the side of the housing, a USB interface is provided on the side of the switch, and a charging hole is provided on the side of the housing away from the switch.

[0008] In a preferred embodiment of the stabilizing mechanism of this utility model, the second antenna interface includes an arc-shaped opening on the side of the housing, a lower clamping plate is provided inside the arc-shaped opening, and a sliding plate structure is provided on the top of the lower clamping plate.

[0009] In a preferred embodiment of the stabilizing mechanism of this utility model, the sliding plate structure is disposed inside the outer shell, and the sliding plate structure is provided with an upper clamping plate structure inside the sliding plate structure.

[0010] As a preferred embodiment of the stabilizing mechanism of this utility model, the slide plate structure includes a sliding plate body, a wire inlet groove is provided at the bottom of the sliding plate body, an accommodating groove is provided inside the sliding plate body, a torsion plate is provided at the top of the sliding plate body, a first elastic element is provided at the bottom of the torsion plate, and a bending plate is provided on the side of the sliding plate body, with the bending plate located below the torsion plate.

[0011] In a preferred embodiment of the stabilizing mechanism of this utility model, the upper clamping plate structure includes a sliding clamping plate disposed inside the receiving groove, and a second elastic member is disposed on the top of the sliding clamping plate, the top of the second elastic member being connected to the sliding plate body.

[0012] The beneficial effects of the stabilizing mechanism of this utility model are as follows: when the second antenna interface is inserted, it will secure the additional antenna to prevent it from becoming loose during operation and affecting the communication effect. At the same time, when the additional antenna is not connected, it will close the antenna interface to prevent the interface from being contaminated.

[0013] This utility model also discloses a remote control, which includes a stabilizing mechanism as described in any of the above claims, and further includes: built-in components, including a GPS module, a voltage regulator module, a communication module, a sensor module, and a central processing unit.

[0014] In a preferred embodiment of the remote control described in this utility model, the central processing unit includes a central processing unit and a power supply module, and the power supply module and the central processing unit are electrically connected.

[0015] In a preferred embodiment of the remote control described in this utility model, the central processing unit further includes a communication module, a monitoring module, and a distribution module. The data terminal of the communication module is connected to the central processing unit, the data terminal of the monitoring module is connected to the central processing unit, and the data terminal of the distribution module is connected to the central processing unit.

[0016] In a preferred embodiment of the remote control described in this utility model, the data terminal of the monitoring module is further connected to a human-machine interface, and the data terminal of the human-machine interface is connected to a communication module.

[0017] The beneficial effects of this utility model remote controller are: the multi-channel communication terminal, by integrating a high-performance central processing unit, a multi-channel wireless communication module and an intelligent task allocation algorithm, can connect in parallel with multiple drone remote controllers to realize multi-task collaborative operation of drones. Attached Figure Description

[0018] 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. Among them:

[0019] Figure 1 This is a schematic diagram of the external component in this utility model.

[0020] Figure 2 This is a schematic diagram of the structure of the first antenna interface in this utility model.

[0021] Figure 3 This is a schematic diagram of the second antenna interface in this utility model.

[0022] Figure 4 This is a schematic diagram of the skateboard structure in this utility model.

[0023] Figure 5 This is a schematic diagram of the structure of the first elastic element in this utility model.

[0024] Figure 6 This is a schematic diagram of the built-in components in this utility model. Detailed Implementation

[0025] To make the above-mentioned objectives, features and advantages of this utility model more apparent and understandable, the specific embodiments of this utility model will be described in detail below with reference to the accompanying drawings.

[0026] Many specific details are set forth in the following description in order to provide a full understanding of the present invention. However, the present invention may also be implemented in other ways different from those described herein. Those skilled in the art can make similar extensions without departing from the spirit of the present invention. Therefore, the present invention is not limited to the specific embodiments disclosed below.

[0027] Secondly, the term "an embodiment" or "embodiment" as used herein refers to a specific feature, structure, or characteristic that may be included in at least one implementation of the present invention. The phrase "in one embodiment" appearing in different places in this specification does not necessarily refer to the same embodiment, nor is it a single or selective embodiment that excludes other embodiments.

[0028] Example 1, referring to Figures 1 to 6This is the first embodiment of the present utility model. This embodiment provides a stabilizing mechanism that enables the convenient addition of a communication antenna and protects the antenna interface when no additional antenna is used. It includes an external component 100, which includes a housing 107, a screen 101 disposed on the top of the housing 107, a first antenna interface 105 disposed on the side of the housing 107, and a second antenna interface 106 disposed on the side of the first antenna interface 105.

[0029] Specifically, the operator interacts with the remote controller through the screen 101 and issues control commands to control the drone. The first antenna interface 105 is the main antenna interface for normal use. However, since multiple drones need to be controlled at the same time, it is often necessary to add an additional communication antenna. This antenna is connected to the remote controller through the second antenna interface 106. When the antenna is inserted, the second antenna interface 106 will secure the additional antenna to prevent it from becoming loose during operation and affecting the communication effect. At the same time, when no additional antenna is connected, this antenna interface will be turned off to prevent the interface from being contaminated.

[0030] Example 2, refer to Figures 1-6 This is the second embodiment of the present invention. Unlike the previous embodiment, a switch 102 is provided on the side of the housing 107, a USB interface 103 is provided on the side of the switch 102, and a charging hole 104 is provided on the side of the housing 107 away from the switch 102. The USB interface 103 can read and write data and can optimize the control method using external data.

[0031] Furthermore, the second antenna interface 106 includes an arc-shaped opening 106a on the side of the housing 107. An additional antenna is connected to the second antenna interface 106 through the arc-shaped opening 106a. A lower clamping plate 106b is disposed inside the arc-shaped opening 106a, and a sliding plate structure 106c is disposed on the top of the lower clamping plate 106b. When an additional antenna is inserted, the lower clamping plate 106b and the sliding plate structure 106c cooperate to clamp the antenna, preventing it from loosening during operation and ensuring communication performance. The sliding plate structure 106c is disposed inside the housing 107 and can slide up and down inside the housing 107. An upper clamping plate structure 106d is disposed inside the sliding plate structure 106c. The sliding plate structure 106c includes a sliding plate body 106c-1, and a cable inlet groove 106c-2 is provided at the bottom of the sliding plate body 106c-1. When an additional antenna is inserted, the antenna is inserted into the remote control through the inlet slot 106c-2. The sliding plate 106c-1 has an accommodating slot 106c-3 inside. The top of the sliding plate 106c-1 is provided with a torsion plate 106c-4, and the bottom of the torsion plate 106c-4 is provided with a first elastic element 106c-6. The side of the sliding plate 106c-1 is provided with a bent plate 106c-5, which is rotatably connected to the sliding plate 106c-1. The bent plate 106c-5 is located below the torsion plate 106c-4, and the top of the bent plate 106c-5 contacts the bottom of the torsion plate 106c-4. The end of the bent plate 106c-5 away from the torsion plate 106c-4 extends out of the outside of the sliding plate 106c-1. A slot is provided on the inner wall of the outer casing 107 to cooperate with the end of the bent plate 106c-5.

[0032] Furthermore, the upper clamping plate structure 106d includes a sliding clamping plate 106d-1 disposed inside the receiving groove 106c-3. The sliding clamping plate 106d-1 can slide up and down inside the receiving groove 106c-3. A second elastic member 106d-2 is disposed on the top of the sliding clamping plate 106d-1. The top of the second elastic member 106d-2 is connected to the sliding plate body 106c-1. The second elastic member 106d-2 is in a compressed state.

[0033] Specifically, when an additional antenna needs to be inserted, first press the torsion plate 106c-4 upwards. The torsion plate 106c-4 will cause the end of the bent plate 106c-5 near the torsion plate 106c-4 to rotate upwards. The end of the torsion plate 106c-4 near the slot of the outer casing 107 will disengage downwards from the slot, and then the sliding plate 106c-1 will slide upwards. At this point, the antenna can be inserted into the second antenna interface 106. Then, push the sliding plate 106c-1 downwards, and the torsion plate 106c-4 will... Under the action of the elastic element 106c-6, the bent plate 106c-5 is reset and re-engaged into the slot. At this time, the sliding clamp 106d-1 will cooperate with the lower clamp 106b to clamp the antenna under the action of the second elastic element 106d-2, preventing the antenna from loosening and affecting the communication quality. When no additional antenna is needed, the sliding clamp 106d-1 will directly contact the lower clamp 106b, completely closing the second antenna interface 106 to prevent it from contacting the outside world, thereby protecting the interface.

[0034] Example 3, referring to Figures 1-6 This is the third embodiment of the present invention. Unlike the previous embodiment, this embodiment provides a remote control, which includes a stabilizing mechanism as described above, and also includes: a built-in component 200, which includes a GPS module 201, a voltage regulator module 202, a communication module 203, a sensor module 204, and a central processing unit 205.

[0035] Furthermore, the central processing unit 205 includes a central processing unit and a power supply module, with the power supply module and the central processing unit electrically connected. The central processing unit 205 also includes a communication module, a monitoring module, and a distribution module. The data terminal of the communication module is connected to the central processing unit, the data terminal of the monitoring module is connected to the central processing unit, the data terminal of the distribution module is connected to the central processing unit, and the data terminal of the monitoring module is also connected to a human-machine interface. The data terminal of the human-machine interface is connected to the communication module.

[0036] Power management module: Provides a stable power supply for the entire device and manages battery power and charging / discharging status.

[0037] Central Processing Unit 205 (CPU): As the core of the system, it is responsible for receiving data from various modules, managing the allocation of multiple UAV tasks, executing intelligent algorithms for real-time decision-making, and scheduling the collaborative operation of multiple UAVs.

[0038] Connectivity module: Independently connects 6 remote controllers to ensure fast and stable transmission of control signals for each drone.

[0039] Data acquisition and monitoring module: Collects flight data (position, status, etc.) of the UAV in real time and transmits the information to the central processing unit 205 for status monitoring and flight trend prediction.

[0040] Task allocation module: Performs task planning and path calculation for the UAV according to the CPU's scheduling commands, and issues the task to the UAV through the communication module.

[0041] Human-Machine Interface (HMI): Provides operators with a display of tasks and status information for multiple drones and an operation interface, supporting emergency shutdown and manual task assignment.

[0042] Remote data communication module: responsible for transmitting flight status and mission data to the cloud in real time for remote monitoring and data storage and analysis.

[0043] The device's hardware is tightly connected and works collaboratively through multiple interfaces. The computer chip, acting as the central processing unit 205, is responsible for the overall system control and data processing, communicating with other hardware components via I2C and UART interfaces. The computer chip drives the display screen via an HDMI interface, providing a real-time operating interface that displays the drone's flight status and mission information. The GPS module 201 connects to the chip via a UART interface, providing the drone's positioning data; the communication module also connects via UART to transmit flight data to the cloud for remote monitoring. Sensors connect via interfaces to collect environmental data (such as temperature, humidity, and air pressure), providing auxiliary information for flight control; the sensors also provide attitude, acceleration, and angular velocity data to help monitor the drone's flight stability. Through the organic coordination of these hardware components, the central processing unit coordinates the data flow and task allocation of each module, ensuring the efficient collaborative operation of the multi-drone system.

[0044] It is important to note that the constructions and arrangements of this application shown in several different exemplary embodiments are merely illustrative. Although only a few embodiments are described in detail in this disclosure, those who consult this disclosure will readily understand that many modifications are possible (e.g., changes in the size, dimensions, structure, shape and proportion of various elements, as well as parameter values ​​(e.g., temperature, pressure, etc.), mounting arrangements, use of materials, color, orientation, etc.) without substantially departing from the novel teachings and advantages of the subject matter described in this application). For example, an element shown as integrally formed may be composed of multiple parts or elements, the position of elements may be inverted or otherwise altered, and the nature or number or position of discrete elements may be changed or altered. Therefore, all such modifications are intended to be included within the scope of this utility model. The order or sequence of any process or method steps may be changed or reordered according to alternative embodiments. In the claims, any "device plus function" clause is intended to cover the structure described herein that performs the function, and not only structural equivalents but also equivalent structures. Without departing from the scope of this invention, other substitutions, modifications, alterations, and omissions may be made in the design, operation, and arrangement of the exemplary embodiments. Therefore, this invention is not limited to the specific embodiments, but extends to various modifications that still fall within the scope of the appended claims.

[0045] Furthermore, in order to provide a concise description of exemplary embodiments, not all features of actual embodiments (i.e., those features that are not relevant to the best mode of carrying out the present invention as currently considered, or those features that are not relevant to the implementation of the present invention) may be omitted.

[0046] It should be understood that numerous specific implementation decisions can be made during the development of any practical implementation, such as in any engineering or design project. Such development efforts may be complex and time-consuming, but for those skilled in the art who benefit from this disclosure, the development effort will be a routine work of design, manufacturing, and production without requiring much experimentation.

[0047] It should be noted that the above embodiments are only used to illustrate the technical solution of this utility model and are not intended to limit it. Although this utility model has been described in detail with reference to preferred embodiments, those skilled in the art should understand that modifications or equivalent substitutions can be made to the technical solution of this utility model without departing from the spirit and scope of the technical solution of this utility model, and all such modifications or substitutions should be covered within the scope of the claims of this utility model.

Claims

1. A stabilizing mechanism characterized by: Including, The external component (100) comprises a shell (107), a screen (101) arranged at the top of the shell (107), a first antenna interface (105) arranged at the side of the shell (107), and a second antenna interface (106) arranged at the side of the first antenna interface (105); The second antenna interface (106) comprises an arc-shaped opening (106a) arranged at the side of the shell (107), and a lower clamping plate (106b) arranged inside the arc-shaped opening (106a).

2. The stabilizing mechanism of claim 1, wherein: A switch (102) is arranged at the side of the shell (107), a USB interface (103) is arranged at the side of the switch (102), and a charging hole (104) is arranged at the side of the shell (107) away from the switch (102).

3. The stabilizing mechanism of claim 2, wherein: The slide plate structure (106c) is arranged inside the shell (107), and an upper clamping plate structure (106d) is arranged inside the slide plate structure (106c).

4. The stabilizing mechanism of claim 3, wherein: The slide plate structure (106c) comprises a sliding plate body (106c-1), a wire inlet groove (106c-2) is arranged at the bottom of the sliding plate body (106c-1), a containing groove (106c-3) is arranged inside the sliding plate body (106c-1), a torsion plate (106c-4) is arranged at the top of the sliding plate body (106c-1), a first elastic member (106c-6) is arranged at the bottom of the torsion plate (106c-4), a bent plate (106c-5) is arranged at the side of the sliding plate body (106c-1), and the bent plate (106c-5) is arranged below the torsion plate (106c-4).

5. The stabilizing mechanism of claim 4, wherein: The upper clamping plate structure (106d) comprises a sliding clamping plate (106d-1) arranged inside the containing groove (106c-3), a second elastic member (106d-2) is arranged at the top of the sliding clamping plate (106d-1), and the top of the second elastic member (106d-2) is connected with the sliding plate body (106c-1).

6. A remote control, characterized by: The stabilizing mechanism comprises the internal component (200), and the internal component (200) comprises a GPS module (201), a voltage stabilizing module (202), a communication module (203), a sensor module (204), and a central processing unit (205).

7. The remote control of claim 6, wherein: The central processing unit (205) comprises a central processor and a power module, and the power module is electrically connected with the central processor.

8. The remote control of claim 7, wherein: The central processing unit (205) further comprises a communication module, a monitoring module, and a distribution module, the data end of the communication module is connected with the central processor, the data end of the monitoring module is connected with the central processor, and the data end of the distribution module is connected with the central processor.

9. The remote control of claim 8, wherein: The data end of the monitoring module is further connected with a man-machine interaction interface, and the data end of the man-machine interaction interface is connected with a communication module.

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