Control device applied to unmanned aerial vehicle

Abstract

The utility model discloses a control device applied to an unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicle control equipment, and the device comprises a bearing structure which comprises a first bearing section and a second bearing section; the interior of the first bearing section is hollow to form a first mounting cavity, and the interior of the second bearing section is hollow to form a second mounting cavity; the first adjusting assembly is mounted in the first mounting cavity, and the second adjusting assembly is mounted in the second mounting cavity; each of the first adjusting assembly and the second adjusting assembly comprises a driving part, and a driving end of the driving part is provided with a transmission structure; the transmission structure of the first adjusting assembly is connected with the unmanned aerial vehicle through the quick release assembly, and the transmission structure of the second adjusting assembly is connected with the clamping assembly. The shooting structure is arranged on the clamping assembly, the pitching state of the shooting structure is adjusted through a first adjusting assembly, and the shooting direction of the shooting structure is adjusted through a second adjusting assembly, so that the shooting structure collects a target object; therefore, strict requirements of various operation scenes on the shooting angle are met.

Description

TECHNICAL FIELD

[0001] The present application generally relates to the technical field of unmanned aerial vehicle control devices, and particularly relates to a control device applied to an unmanned aerial vehicle. BACKGROUND

[0002] At present, unmanned aerial vehicles are widely used in many fields, such as aerial photography, surveying and mapping, agricultural plant protection, logistics distribution, etc. In these application scenarios, the performance of the control device of the unmanned aerial vehicle is crucial. The existing unmanned aerial vehicle controllers have many deficiencies in structural design and functional integration. For example, the adjustment function of some controllers is not flexible enough, and cannot meet the diversified needs for shooting angles or other operation angles in different operating environments. Therefore, we provide a control device applied to an unmanned aerial vehicle to solve the above problems. CONTENT OF THE UTILITY MODEL

[0003] In view of the above defects or deficiencies in the prior art, it is desirable to provide a control device applied to an unmanned aerial vehicle which has strong universality and can meet the shooting needs of different operating environments.

[0004] The present application provides a control device applied to an unmanned aerial vehicle, comprising:

[0005] A bearing structure, comprising a first bearing segment and a second bearing segment connected to each other and arranged vertically; the first bearing segment is hollow inside to form a first mounting chamber, and the second bearing segment is hollow inside to form a second mounting chamber;

[0006] A first adjustment assembly and a second adjustment assembly, the first adjustment assembly is installed in the first mounting chamber, and the second adjustment assembly is installed in the second mounting chamber; the first adjustment assembly and the second adjustment assembly each comprise a driving member, the driving end of the driving member is provided with a transmission structure; the transmission structure of the first adjustment assembly is connected with the unmanned aerial vehicle through a quick release assembly, and the transmission structure of the second adjustment assembly is connected with a clamping assembly, and the clamping assembly is used for installing an operating device;

[0007] A shooting structure, arranged on the clamping assembly, for collecting a target object;

[0008] The first adjustment assembly drives the control device to rotate relative to the unmanned aerial vehicle, thereby adjusting the pitch state of the shooting structure, and the second adjustment assembly drives the clamping assembly to rotate, thereby adjusting the shooting direction of the shooting structure, so that the shooting structure collects the target object.

[0009] According to the technical scheme provided by the embodiment of the present application, the clamping assembly comprises:

[0010] A clamping frame body, a bottom of the clamping frame body is connected with a transmission structure of the second adjusting assembly; the clamping frame body is provided with at least one bearing station for placing the working equipment;

[0011] A pressing plate, the pressing plate is bolted on a top of the clamping frame body, and the pressing plate is used in cooperation with the clamping frame body to fix the working equipment in the bearing station.

[0012] According to the technical scheme provided by the embodiment of the application, a damping structure is further arranged between the clamping frame body and the transmission structure of the second adjusting assembly;

[0013] The damping structure comprises:

[0014] A bottom plate, the bottom plate is connected with the transmission structure of the second adjusting assembly; at least two groups of guide rods arranged in parallel are arranged on the bottom plate, and the extension direction of the guide rods is arranged in parallel with the emission direction of the working equipment;

[0015] A sliding block, the sliding block is installed on the two groups of guide rods and is in sliding connection with the guide rods;

[0016] An elastic element, the elastic element is installed between the sliding block and one end of the guide rod.

[0017] According to the technical scheme provided by the embodiment of the application, the clamping assembly further comprises:

[0018] A limiting structure, the limiting structure is arranged on the clamping frame body and is used for limiting the relative position of the working equipment in the bearing station.

[0019] According to the technical scheme provided by the embodiment of the application, the quick release assembly comprises:

[0020] A first quick release part and a second quick release part used in cooperation, the first quick release part is installed on the unmanned aerial vehicle, and the second quick release part is connected through the transmission structure and the first adjusting assembly;

[0021] The first adjusting assembly is connected with the unmanned aerial vehicle through the clamping of the first quick release part and the second quick release part.

[0022] According to the technical scheme provided by the embodiment of the application, the shooting structure is a camera structure provided with a visible light camera, a laser ranging camera and a night vision camera.

[0023] According to the technical scheme provided in the embodiment of the present application, the work equipment, the first adjusting assembly and the second adjusting assembly are in communication connection with a control panel, the control panel comprises a plurality of control buttons, and the control panel is used for controlling the control buttons to emit corresponding instructions, so as to control the corresponding work equipment, the first adjusting assembly or the second adjusting assembly to perform corresponding actions.

[0024] According to the technical scheme provided in the embodiment of the present application, the control panel is in communication connection with a display module, and the display module is used for displaying the target object collected by the shooting structure in real time and the real-time state of each control button.

[0025] From the above technical scheme, the present application has at least the following beneficial effects:

[0026] The present application discloses a control device applied to a unmanned aerial vehicle, which comprises a bearing structure, a first bearing segment and a second bearing segment connected to each other and arranged vertically, a first mounting chamber formed in the first bearing segment, a second mounting chamber formed in the second bearing segment, a first adjusting assembly installed in the first mounting chamber, a second adjusting assembly installed in the second mounting chamber, a driving member, a transmission structure arranged on the driving end of the driving member, the transmission structure of the first adjusting assembly connected to the unmanned aerial vehicle through a quick release assembly, the transmission structure of the second adjusting assembly connected to a clamping assembly, the clamping assembly used for installing a work equipment, a shooting structure arranged on the clamping assembly and used for collecting a target object, the control device rotated relative to the unmanned aerial vehicle through the first adjusting assembly, the pitch state of the shooting structure adjusted, the clamping assembly rotated through the second adjusting assembly, and the shooting direction of the shooting structure adjusted, so that the shooting structure collects the target object.

[0027] The present application adjusts the pitch angle of the shooting structure through the first adjusting assembly, so that the shooting structure can vertically downwardly shoot, and adjusts the shooting direction through the second adjusting assembly, so that the shooting structure can shoot different areas. The flexible adjusting mode makes the shooting structure accurately collect the target object, improves the comprehensiveness and accuracy of shooting, and meets the strict requirements of various work scenes on the shooting angle.

[0028] In the present application, the transmission structure of the first adjusting assembly is connected to the unmanned aerial vehicle through the quick release assembly, which greatly improves the convenience of installation and disassembly of the control device. When the control device needs to be replaced for maintenance or upgrading, or the same control device is used on different unmanned aerial vehicles, the installation and disassembly operations can be quickly completed. Compared with the traditional fixed connection mode, a large amount of time and labor cost is saved, and the use efficiency and universality of the equipment are improved.

[0029] The clamping assembly designed in the application is used for installing a working device, and the design ensures the stability of the working device during flight. The clamping frame body is connected with the transmission structure of the second adjusting assembly, and the working device is fixed by the pressing plate and the clamping frame body, so as to ensure that the working device does not shake or fall off during flight of the unmanned aerial vehicle. When performing a special task, the stable working device can ensure the accuracy of shooting and improve the success rate of task performance. BRIEF DESCRIPTION OF DRAWINGS

[0030] Other features, objects and advantages of the application will become more apparent from the following detailed description of non-limiting embodiments made with reference to the accompanying drawings.

[0031] Figure 1 The structure diagram of the control device applied to the unmanned aerial vehicle.

[0032] Figure 2 The structure diagram of the guide rod and the sliding block.

[0033] Figure 3 The schematic diagram of the limiting structure.

[0034] Figure 4 The structure diagram of the first adjusting assembly.

[0035] Figure 5 The structure diagram of the second adjusting assembly.

[0036] Figure 6 The control principle diagram of the control panel.

[0037] Reference signs in the drawings: 1, first bearing section; 2, second bearing section; 3, driving piece; 4, transmission structure; 5, shooting structure; 6, clamping frame body; 7, pressing plate; 8, bottom plate; 9, guide rod; 10, sliding block; 11, limiting structure; 12, second quick release piece; 13, control panel; 14, display module. DETAILED DESCRIPTION

[0038] The application will be further described in detail below with reference to the drawings and embodiments. It can be understood that the specific embodiments described herein are only used to explain the related application, and not to limit the application. In addition, it should be noted that only parts related to the application are shown in the drawings for ease of description.

[0039] It should be noted that the embodiments in the application and the features in the embodiments can be combined with each other without conflict. The application will be described in detail below with reference to the drawings and embodiments.

[0040] As Figure 1 shown, the application provides a control device applied to an unmanned aerial vehicle, which comprises:

[0041] The bearing structure comprises a first bearing section 1 and a second bearing section 2 which are connected to each other and arranged vertically; the first bearing section 1 is internally hollow to form a first mounting chamber, and the second bearing section 2 is internally hollow to form a second mounting chamber;

[0042] The first adjusting assembly and the second adjusting assembly are as shown in the drawings, the first adjusting assembly is mounted in the first mounting chamber, and the second adjusting assembly is mounted in the second mounting chamber; Figure 4 The first adjusting assembly and the second adjusting assembly are as shown in the drawings, the first adjusting assembly is mounted in the first mounting chamber, and the second adjusting assembly is mounted in the second mounting chamber; Figure 5 The first adjusting assembly and the second adjusting assembly each comprise a driving member 3, and a transmission structure 4 is arranged at a driving end of the driving member 3; the transmission structure 4 of the first adjusting assembly is connected with the unmanned aerial vehicle through a quick release assembly, and the transmission structure of the second adjusting assembly is connected with a clamping assembly, and the clamping assembly is used for mounting the working equipment;

[0043] A shooting structure 5 is arranged on the clamping assembly and is used for collecting the target object; here, the shooting structure 5 is a camera structure which comprises a visible light camera, a laser ranging camera and a night vision camera.

[0044] The first adjusting assembly drives the control device to rotate relative to the unmanned aerial vehicle, so as to adjust the pitch state of the shooting structure 5, and the second adjusting assembly drives the clamping assembly to rotate, so as to adjust the shooting direction of the shooting structure 5, so that the shooting structure 5 collects the target object.

[0045] It should be noted that the bearing structure is the basic framework of the entire control device and is composed of the first bearing section 1 and the second bearing section 2 which are connected to each other vertically. The vertically arranged structure design can make full use of the space and provide reasonable mounting positions for subsequent assemblies. The first mounting chamber formed in the first bearing section 1 and the second mounting chamber formed in the second bearing section 2 not only provide mounting spaces for the first adjusting assembly and the second adjusting assembly, but also protect these assemblies from interference and damage from the external environment during the flight of the unmanned aerial vehicle. At the same time, the material selection of the bearing structure usually needs to consider the strength and weight factors, and light and high-strength materials such as aluminum alloy are generally used to ensure the stability of the structure while reducing the overall load of the unmanned aerial vehicle and improving the flight performance.

[0046] The first adjusting assembly and the second adjusting assembly are respectively installed in the mounting cavities of the first bearing segment 1 and the second bearing segment 2, and are key components for achieving flexible adjustment of the shooting structure. Both the two assemblies comprise a driving member 3 and a transmission structure 4; the driving member 3 is the core of power supply, and its type is various, for example, a motor (such as a direct current motor, a stepping motor, etc.), a hydraulic driving device or a pneumatic driving device. Taking the motor as an example, the direct current motor has low cost and simple structure, and is suitable for scenes with relatively low precision requirements; while the stepping motor can achieve precise angle control, and can meet the demand for high-precision adjustment of the shooting angle. The transmission structure 4 is responsible for transmitting the power of the driving member 3, for example, gear transmission, screw transmission, etc.; the gear transmission has high efficiency, and can achieve transmission of large torque; the screw transmission has the advantages of high precision and stable transmission.

[0047] The transmission structure 4 of the first adjusting assembly is connected with the unmanned aerial vehicle through the quick release assembly. The quick release design structure facilitates the quick mounting and dismounting of the control device between different unmanned aerial vehicles, and improves the universality and use convenience of the equipment.

[0048] For example, as shown in Figure 1 and Figure 2 , the quick release assembly comprises a first quick release member and a second quick release member 12 used in cooperation, the first quick release member is installed on the unmanned aerial vehicle, and the second quick release member 12 is connected with the transmission structure of the first adjusting assembly; the first adjusting assembly is connected with the unmanned aerial vehicle by clamping the first quick release member and the second quick release member 12; that is, the quick connection is achieved by clamping the two.

[0049] The clamping assembly is used for mounting the working equipment, and is connected with the connecting plate of the second adjusting assembly, and moves under the driving of the second adjusting assembly. As shown in Figure 1 and Figure 2 , the clamping assembly mainly comprises a clamping frame body 6 and a pressing plate 7; the clamping frame body 6 is connected with the connecting plate of the second adjusting assembly at the bottom, and has at least one bearing station, which is customized according to the shape and size of the working equipment to ensure that the working equipment can be stably placed thereon. The pressing plate 7 is connected with the top of the clamping frame body 6 through bolts, and when the working equipment is installed, tightening the bolts can press the working equipment downward by the pressing plate 7, so that the working equipment is fixed firmly by the cooperation of the pressing plate 7 and the clamping frame body 6, preventing the working equipment from shaking or moving during the flight of the unmanned aerial vehicle, and affecting the normal use of the equipment and the shooting effect. In addition, in order to further improve the stability and safety of the installation of the working equipment, the clamping assembly is also provided with some auxiliary structures, such as a limiting structure 11, as shown in Figure 3 , the limiting structure 11 is arranged on the clamping frame body 6, and is used for limiting the relative position of the working equipment in the bearing station, so as to ensure that the working equipment is always in the correct installation state.

[0050] Here, the work equipment is, for example, a mounting gun, a capture gun, a fire-fighting water gun, etc.

[0051] The application is described by taking a gear transmission as an example. The transmission structure 4 includes a first bevel gear and a second bevel gear connected in meshing. The first bevel gear is connected with the driving end of the corresponding driving member 3. The second bevel gear of the first adjusting assembly is connected with the second quick-release member 12 of the quick-release assembly. The second bevel gear of the second adjusting assembly is connected with the clamping assembly. For example, the first adjusting assembly is described. The driving member is a motor. The driving shaft of the motor is arranged perpendicularly to the length direction of the second bearing section 2. The first bevel gear rotates around the driving shaft of the motor. The rotation shaft of the second bevel gear is arranged perpendicularly to the driving shaft of the motor. The rotation shaft of the second bevel gear is arranged in parallel to the length direction of the second bearing section 2.

[0052] The shooting structure 5 is arranged on the clamping assembly and is a key component for collecting information of the target object. Here, the shooting structure 5 is a camera structure integrating a visible light camera, a laser ranging camera, and a night vision camera, which has multiple functions. The visible light camera is used to collect images of the target object under normal lighting conditions, which can provide clear and intuitive visual information and meet most conventional shooting needs. The laser ranging camera is mainly used to measure the distance between the target object and the unmanned aerial vehicle. The distance is calculated by emitting a laser beam and receiving the reflected light. This function is crucial for accurately adjusting the shooting angle and focal length and can ensure that the images are clear and accurate. The night vision camera is designed for night or low-light environments. It uses infrared technology or other low-light enhancement technology to enable the unmanned aerial vehicle to obtain image information of the target object in dark environments, greatly expanding the use scenarios and working time of the unmanned aerial vehicle.

[0053] Through the cooperative work of the first adjusting assembly and the second adjusting assembly, the shooting structure 5 can be adjusted in all directions, so that the shooting structure 5 can accurately collect the target object. The first adjusting assembly is mainly responsible for adjusting the pitch state of the shooting structure 5, that is, controlling the angle change of the shooting structure 5 in the vertical direction. For example, when shooting a target object at a high place, the first adjusting assembly can drive the shooting structure 5 to lift up to a certain angle. If you want to shoot the target object below, you can control the shooting structure 5 to tilt downward. The second adjusting assembly is used to adjust the shooting direction of the shooting structure 5, that is, to rotate or swing in the horizontal direction, so that the shooting structure 5 can be aligned with the target object in different directions. Through the flexible cooperation of the two adjusting assemblies, the shooting structure 5 can quickly and accurately adjust to the appropriate shooting angle under different environmental and task requirements, thereby effectively collecting the image, distance, and other information of the target object, and providing strong support for subsequent data analysis and task execution.

[0054] Further, a damping structure is arranged between the clamping frame body 6 and the transmission structure 4 of the second adjusting assembly.

[0055] As Figure 2 shown, the damping structure comprises:

[0056] a bottom plate 8 connected with the transmission structure 4 of the second adjusting assembly; the bottom plate 8 is provided with at least two groups of parallel guide rods 9, the extension direction of the guide rods 9 is parallel to the launching direction of the working equipment;

[0057] a sliding block 10 installed on the two groups of guide rods 9 and in sliding connection with the guide rods 9;

[0058] a elastic element installed between the sliding block 10 and one end of the guide rod 9.

[0059] It should be noted that some working equipment will produce strong recoil force when launching, which will cause severe vibration. If not effectively handled, these vibrations will be transmitted to the second adjusting assembly through the clamping frame body 6, thereby affecting the stability of the shooting structure 5, resulting in blurred and shaking shooting pictures, and seriously affecting the shooting quality. At the same time, the continuous vibration may also cause damage to the connecting parts of the equipment, shortening the service life of the equipment. The existence of the damping structure is to relieve and absorb these vibrations and ensure the normal operation of the control device.

[0060] The bottom plate 8 is the basic component of the damping structure, which is closely connected with the transmission structure 4 of the second adjusting assembly, providing an installation carrier for the entire damping structure. This connection mode ensures that the damping structure can move with the movement of the second adjusting assembly, while effectively isolating the vibration generated when the working equipment is launched from being transmitted to the second adjusting assembly.

[0061] The bottom plate 8 is provided with at least two groups of parallel guide rods 9, the extension direction of the guide rods 9 is parallel to the launching direction of the working equipment, the parallel guide rods 9 provide a stable sliding track for the sliding block 10, so that the sliding block 10 can only move linearly along the direction of the guide rods 9, thereby ensuring the stability and directionality of the damping structure during operation. The parallel arrangement with the launching direction of the working equipment can maximize the buffering and absorption of the vibration along the launching direction generated when the working equipment is launched.

[0062] The sliding block 10 is installed on the two groups of guide rods 9 and in sliding connection with the guide rods 9; this connection mode allows the sliding block 10 to slide freely on the guide rods 9, providing the necessary movement space for the work of the elastic element. When the working equipment is launched to generate vibration, the sliding block 10 will slide on the guide rods 9, converting the vibration into its own sliding kinetic energy. The sliding block 10 plays a key role in the damping process. It not only connects one end of the elastic element with the guide rod 9 as an installation carrier of the elastic element, but also adjusts the stress state of the elastic element through its sliding during vibration transmission, so that the elastic element can more effectively absorb and buffer the vibration energy.

[0063] The elastic element is mounted between the sliding block 10 and one end of the guide rod 9, and is a core component of the damping structure. The elastic element is, for example, a spring, a rubber pad, etc. Taking the spring as an example, when the operating device is launched to generate vibration, the sliding block 10 will slide on the guide rod 9 and press the spring, and the spring will be elastically deformed after being pressed, converting the kinetic energy of the vibration into its own elastic potential energy and storing it. When the vibration weakens, the spring will release the stored elastic potential energy to push the sliding block 10 back to its original position, thereby achieving the buffering and absorption of the vibration.

[0064] Here, the selection of the elastic element is crucial, and its elastic coefficient, size, and other parameters need to be determined according to the launch characteristics of the operating device (such as the size of the recoil force) and the overall structure and stability requirements of the unmanned aerial vehicle control device.

[0065] Further, as shown in Figure 6 The control panel 13 is in communication connection with the operating device, the first adjusting assembly, and the second adjusting assembly, and the control panel 13 includes a plurality of control keys. The control panel 13 is used to control the control keys to transmit corresponding instructions, thereby controlling the corresponding operating device, first adjusting assembly, or second adjusting assembly to perform corresponding actions.

[0066] It should be noted that the control panel 13 is in wireless communication connection with the operating device, the first adjusting assembly, and the second adjusting assembly. For example, wireless technologies such as Bluetooth, Wi-Fi, ZigBee, etc. are used. For example, using Bluetooth technology, the control panel 13 and each component can perform wireless data transmission within a certain distance, greatly improving the freedom of the unmanned aerial vehicle, allowing the operator to control the unmanned aerial vehicle more flexibly.

[0067] The control panel 13 is provided with a plurality of control keys, and the layout and function design of these keys are carefully planned according to actual operation needs. For the control of the operating device, a shooting key can be provided, and the operator presses the shooting key to send a shooting instruction to the operating device through the control panel 13, and the operating device executes the shooting action after receiving the instruction. There can also be an ammunition switching key to facilitate the operator to switch the ammunition type of the operating device according to different task requirements. For the first adjusting assembly and the second adjusting assembly, corresponding adjusting keys are respectively provided. For example, "upward pitch" and "downward pitch" keys are provided to control the first adjusting assembly to achieve the pitch adjustment of the shooting structure 5 in the vertical direction; "left rotation" and "right rotation" keys are provided to control the second adjusting assembly to adjust the shooting direction of the shooting structure 5. In addition, some function composite keys or combination keys can also be provided to achieve more complex operation functions, such as pressing multiple keys at the same time to execute a specific preset action.

[0068] When an operator presses a control button on the control panel 13, the internal circuitry of the control panel 13 recognizes the button press and converts it into a corresponding electrical signal command. These commands, after being encoded, are sent out through the previously established communication connection. Taking the control of the first adjustment component to adjust the pitch of the shooting structure 5 as an example, after the command is sent to the first adjustment component, its internal receiving module receives the command and then transmits it to the drive component 3 and the transmission structure 4. The drive component 3 starts according to the command and drives the transmission structure 4 to move, thereby achieving the pitch adjustment of the shooting structure 5. Similarly, the operating equipment and the second adjustment component follow a similar process, receiving commands and executing corresponding actions. In this process, the control panel 13 plays a crucial role, bridging the gap between the operator's intentions and the control system. It transforms the operator's intentions into executable commands and ensures that these commands are accurately transmitted to the corresponding components, achieving effective control of the entire control device.

[0069] In addition, such as Figure 6 As shown, the control panel 13 is connected to a display module 14. The display module 14 is connected to the control panel 13 and is used to display the target object acquired in real time by the shooting structure 5 and the real-time status of each control button.

[0070] It should be noted that the display module 14 and the control panel 13 transmit data through a specific communication protocol. The communication methods here include serial communication protocols such as SPI (Serial Peripheral Interface) and I2C (Integrated Circuit Bus), or a higher-speed parallel communication method.

[0071] Since the shooting structure 5 integrates a visible light camera, a laser rangefinder camera, and a night vision camera, the display module 14 switches between displaying images captured by the corresponding camera based on different shooting environments and needs. Under normal lighting conditions, the display module 14 primarily displays high-definition images captured by the visible light camera, allowing operators to clearly observe the details, colors, and surrounding environment of the target object. When it is necessary to measure the distance to the target object, the data from the laser rangefinder camera is overlaid on the image in graphical or digital form, such as displaying the outline of the target object in the image and marking the distance value, facilitating distance judgment by the operator. In nighttime or low-light environments, the display module 14 switches to displaying images captured by the night vision camera, using night vision technology to clearly display scenes in darkness, ensuring the drone's operational capabilities under complex lighting conditions. In addition, the display module 14 also has functions such as image scaling and contrast adjustment, allowing operators to adjust the displayed image according to actual needs for better observation of the target object.

[0072] The display module 14 also displays the status of each control button on the control panel 13 in real time, providing operational feedback to the operator and preventing misoperation. Each control button has a corresponding display indicator on the display module 14 for different operational states such as pressed, released, and long-press. For example, when the firing button is pressed, the corresponding button icon on the display module 14 will change color or flash, indicating to the operator that the button has been activated and the equipment is about to fire. When the button for adjusting the pitch angle of the shooting structure 5 is pressed, the display module 14 will not only display the button's operational status but also simultaneously display the current pitch angle value of the shooting structure 5, allowing the operator to clearly understand the adjustment range and the current actual status of the shooting structure 5. For buttons with multiple function modes, the display module 14 will display the currently selected function mode in real time, such as switching between different ammunition modes of the equipment, facilitating operator confirmation and adjustment at any time. In this way, the operator can intuitively understand the working status of the control device, promptly identify and correct operational errors, and improve operational accuracy and efficiency.

[0073] The above description is merely a preferred embodiment of this application and an explanation of the technical principles employed. Those skilled in the art should understand that the scope of the invention involved in this application is not limited to technical solutions formed by specific combinations of the above-described technical features, but should also cover other technical solutions formed by arbitrary combinations of the above-described technical features or their equivalents without departing from the inventive concept. For example, technical solutions formed by substituting the above features with (but not limited to) technical features with similar functions disclosed in this application.

Claims

1. A control device applied to a UAV, characterized in that, include: The load-bearing structure includes a first load-bearing section (1) and a second load-bearing section (2) that are interconnected and arranged vertically; the first load-bearing section (1) has a hollow interior forming a first mounting chamber, and the second load-bearing section (2) has a hollow interior forming a second mounting chamber; A first adjustment component and a second adjustment component, wherein the first adjustment component is installed in the first mounting cavity and the second adjustment component is installed in the second mounting cavity; Both the first adjustment component and the second adjustment component include: a driving component (3), the driving end of the driving component (3) is provided with a transmission structure (4); the transmission structure (4) of the first adjustment component is connected to the UAV through a quick-release component, and the transmission structure (4) of the second adjustment component is connected to a clamping component, the clamping component is used to install the operating equipment; The shooting structure (5) is disposed on the clamping assembly and is used to capture the target object; The first adjustment component drives the control device to rotate relative to the drone, thereby adjusting the pitch state of the shooting structure (5). The second adjustment component drives the clamping component to rotate, thereby adjusting the shooting direction of the shooting structure (5) so that the shooting structure (5) can capture the target object.

2. The control device for unmanned aerial vehicle according to claim 1, wherein, The clamping assembly includes: The clamping frame (6) has its bottom connected to the transmission structure (4) of the second adjustment component; the clamping frame (6) has at least one bearing station for placing the working equipment. Pressure plate (7) is bolted to the top of the clamping frame (6). The pressure plate (7) is used in conjunction with the clamping frame (6) to fix the working equipment in the bearing position.

3. The control device for unmanned aerial vehicle according to claim 2, wherein, A shock-absorbing structure is also provided between the clamping frame (6) and the transmission structure (4) of the second adjustment component; The damping structure includes: The base plate (8) is connected to the transmission structure (4) of the second adjustment component; the base plate (8) is provided with at least two sets of parallel guide rods (9), the extension direction of the guide rods (9) is parallel to the firing direction of the working equipment; A slider (10) is mounted on two sets of guide rods (9) and is slidably connected to the guide rods (9); An elastic element is installed between the slider (10) and one end of the guide rod (9).

4. The control device for unmanned aerial vehicle according to claim 2, wherein, The clamping assembly further includes: A limiting structure (11) is provided on the clamping frame (6) to limit the relative position of the working equipment on the bearing station.

5. The control device for unmanned aerial vehicle according to claim 1, wherein, The quick-release assembly includes: The first quick-release component and the second quick-release component (12) are used together. The first quick-release component is installed on the UAV, and the second quick-release component (12) is connected to the first adjustment component through the transmission structure (4). The first adjustment component is connected to the UAV by engaging the first quick-release component and the second quick-release component (12).

6. The control device for unmanned aerial vehicle according to claim 1, wherein, The shooting structure (5) is a camera structure equipped with a visible light camera, a laser rangefinder camera and a night vision camera.

7. The control device for unmanned aerial vehicle according to claim 1, wherein, The work equipment, the first adjusting assembly and the second adjusting assembly are communicatively connected with a control panel (13), the control panel (13) comprises a plurality of control buttons, the control panel (13) is used for controlling the control buttons to emit corresponding instructions, thereby controlling corresponding work equipment, the first adjusting assembly or the second adjusting assembly to execute corresponding actions.

8. The control device for unmanned aerial vehicle according to claim 7, wherein, The control panel (13) is communicatively connected with a display module (14), and the display module (14) is used for displaying the target object collected by the shooting structure (5) in real time and the real-time state of each control button.

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