Unmanned aerial vehicle key remote control device
Patent Information
- Application Number
- CN202522142196.4
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-10-10
- Publication Date
- 2026-10-09
- Estimated Expiration
- 2035-10-10
AI Technical Summary
但这类舵机模拟方案存在若干固有缺陷:首先,舵机的控制精度有限,难以精确模拟人工按键的力度、行程和触点反馈,容易因力度不足导致按键无效,或因过冲造成设备损坏,操作可靠性和一致性较差
本实用新型以微型步进电机为执行机构,控制精度高,能精确模拟按键行程与力度,避免按键无效或设备损坏。采用薄膜按键开关与光敏检测装置构成双重检测机制,实时反馈状态,形成闭环控制,提高操作成功率与系统可靠性。内置半导体冷凝片与抽风风扇的主动散热系统,结合防尘网与防水外壳设计,解决恶劣环境下性能下降或故障问题,提升环境适应性与耐用性。电路采用模块化设计,控制处理模块集成数据处理与逻辑控制,通讯模块采用标准RS485接口,结构紧凑、接线简洁,便于集成。本实用新型取代人工干预,克服舵机方案可靠性不足,与无人机机巢系统无缝集成,远程、自动、可靠完成遥控器按键操作,是实现无人机“无人化”值守和全自动作业的关键技术。
Smart Images

Figure CN224841598U_ABST
Abstract
Description
Technical Field
[0001] This utility model belongs to the field of unmanned aerial vehicle (UAV) equipment technology, specifically relating to a UAV button remote control device. Background Technology
[0002] With the rapid development of drone technology, its applications in surveying, inspection, logistics, and emergency rescue are becoming increasingly widespread. To achieve efficient and continuous operations, drone nests (or automated airports) have emerged, designed to enable drones to automatically take off, land, recharge, and transmit data. However, a crucial aspect of automated drone operations lies in how to remotely and automatically start the drone and its remote controller. Currently, this step typically still requires manual on-site operation, such as manually pressing the drone's power switch or the remote controller's start button. This manual intervention not only increases operational complexity and management costs but also fundamentally limits the application of drone systems in truly unattended scenarios.
[0003] To replace manual operation, some existing technologies employ servo motors to simulate human hand button pressing. These solutions control the rotation angle of the servo motor to drive a linkage or push rod, thereby triggering the remote control button. However, these servo motor simulation solutions have several inherent drawbacks: First, the control precision of servo motors is limited, making it difficult to accurately simulate the force, travel, and contact feedback of manual button pressing. Insufficient force can lead to button failure, or overshoot can cause equipment damage, resulting in poor operational reliability and consistency. Second, the mechanical structure of the servo motor itself is prone to wear and aging under prolonged, high-frequency operation, resulting in insufficient durability and reliability, affecting the long-term stable operation of the entire UAV system. Furthermore, servo motor control typically requires complex circuitry and meticulous programming and debugging, increasing system complexity and implementation and maintenance costs.
[0004] Therefore, there is an urgent need in this field for an automatic button operation device for UAV remote controllers that is precise, reliable, compact, and adaptable to long-term operation in harsh environments, in order to overcome the shortcomings of existing manual operation and servo motor simulation solutions and promote the further improvement of UAV fully automated operation technology. Utility Model Content
[0005] To address the shortcomings of existing technologies, this utility model discloses a button-operated remote control device for unmanned aerial vehicles (UAVs) to solve the aforementioned problems.
[0006] This utility model is achieved through the following technical solution: This utility model provides a drone button remote control device, including: a structural part and a circuit part, wherein the circuit part is fixed inside the structural part; The structural component includes a waterproof housing and a heat dissipation system disposed therein. The heat dissipation system includes a semiconductor condenser, an exhaust fan, and an air duct structure. The waterproof housing is provided with an air inlet and an air outlet, and a dustproof screen is provided at the air inlet. The cold end of the semiconductor condenser faces the circuit part, forming a cold air outlet for dissipating heat from the circuit part, and its hot end is opposite to the exhaust fan, which exhausts hot air through the air outlet. The circuit section includes a control processing module, a motor drive module, a power supply module, and a communication module; the power supply module is used to supply power to the entire device; the control processing module is electrically connected to the communication module, the power supply module, and the motor drive module respectively; the motor drive module is used to drive a motor device to operate.
[0007] Furthermore, the motor device includes a motor mounting bracket, a micro stepper motor, and a positioning detection unit; the micro stepper motor is fixedly installed via the motor mounting bracket, and its output shaft is used to simulate pressing a remote control button on a drone; the positioning detection unit is used to detect whether the pressing action of the micro stepper motor has been completed.
[0008] Furthermore, the positioning detection unit is a membrane key switch, which is located at the end of the output shaft stroke of the micro stepper motor and is used to trigger a signal and feed it back to the control processing module when the output shaft is pressed into position.
[0009] Furthermore, the motor device also includes a photosensitive detection device for detecting whether the micro stepper motor is operating.
[0010] Furthermore, the communication module adopts an RS485 bus communication interface.
[0011] Furthermore, the power module is a DC power module, used to supply power to the micro stepper motor and the various modules of the circuit section.
[0012] Furthermore, the semiconductor condenser is disposed on the back of the mounting plate of the exhaust fan, and the cold air outlet is located below the circuit section.
[0013] Furthermore, the control processing module integrates a data processing unit and a logic control unit.
[0014] The beneficial effects of this utility model are as follows: This invention uses a micro stepper motor as the actuator, achieving high control precision and accurately simulating button travel and force, thus preventing button malfunctions or equipment damage. A dual detection mechanism, employing a membrane key switch and a photosensitive detection device, provides real-time status feedback, forming a closed-loop control system that improves operational success rate and system reliability. An active cooling system with an integrated semiconductor condenser and exhaust fan, combined with a dustproof mesh and waterproof casing, solves performance degradation or malfunction issues in harsh environments, enhancing environmental adaptability and durability. The circuit adopts a modular design; the control processing module integrates data processing and logic control, while the communication module uses a standard RS485 interface, resulting in a compact structure, simple wiring, and easy integration. This invention replaces manual intervention, overcomes the reliability deficiencies of servo motor solutions, and seamlessly integrates with the UAV's nesting system, enabling remote, automatic, and reliable remote control button operations. It is a key technology for achieving unmanned operation and fully automated operation of UAVs. Attached Figure Description
[0015] To more clearly illustrate the technical solutions in the embodiments of this utility model or the prior art, the drawings used in the description of the embodiments or the prior art 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.
[0016] Figure 1 This is a schematic block diagram of the structure of the drone button remote control device of this utility model; Figure 2 This is a schematic diagram of the circuit part of the drone button remote control device of this utility model; Figure 3 This is a schematic diagram of the semiconductor condenser structure of the drone button remote control device of this utility model; Figure 4 This is a schematic diagram of the remote control button clicking structure device of this utility model; The labels in the diagram represent: 1. Waterproof housing; 2. Circuitry; 3. RS485 bus communication interface; 4. Exhaust fan; 5. Air duct structure; 6. Dustproof mesh; 7. Semiconductor condenser; 8. Membrane push-button switch; 9. Power interface; 10. Photosensitive detection device; 11. Cold air outlet; 100. Motor drive module; 200. Power supply module; 300. Control processing module; 400. Communication module. Detailed Implementation
[0017] To make the objectives, technical solutions, and advantages of the embodiments of this utility model clearer, the technical solutions of the embodiments of this utility model will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of this utility model, not all embodiments. Based on the embodiments of this utility model, all other embodiments obtained by those skilled in the art without creative effort are within the protection scope of this utility model.
[0018] like Figures 1 to 4 As shown, this utility model provides a drone button remote control device, including a structural part and a circuit part. The circuit part 2 is fixed inside the structural part and is encapsulated and protected by the waterproof shell 1 of the structural part. The specific embodiments of this utility model will be described in detail below with reference to the accompanying drawings.
[0019] Specific implementation methods for the structural components: The structural components mainly include a waterproof housing 1, a heat dissipation system, and a motor mounting structure. The waterproof housing 1 features a sealed design, effectively preventing the intrusion of external media such as rainwater and dust, ensuring the reliability of the device in harsh environments. The heat dissipation system is integrated inside the waterproof housing 1 and includes a semiconductor condenser 7, an exhaust fan 4, an air duct structure 5, and a dust filter 6.
[0020] The semiconductor condenser 7 is fixedly mounted on the back of the mounting plate of the exhaust fan 4, with its cold end facing downwards towards the circuit section 2, forming a cold air outlet 11 for active heat dissipation of the circuit section 2; its hot end is opposite to the exhaust fan 4. The exhaust fan 4 uses natural ventilation, expelling the hot air generated by the semiconductor condenser 7 from the air outlet on the device panel through the air duct structure 5. A dust filter 6 is provided at the air inlet to filter dust from the intake air and prevent dust accumulation from affecting the heat dissipation effect. The cold air outlet 11 circulates cold air to the remote control, effectively reducing the ambient temperature around the remote control and preventing performance degradation due to high temperatures.
[0021] Specific implementation of the circuit section: The circuit section 2 includes a control processing module 300, a motor drive module 100, a power supply module 200, and a communication module 400. Each module is connected and fixed inside the structural section via a circuit board.
[0022] The power supply module 200 is a 12V DC power supply module with a power interface 9, used to provide a stable power supply for the entire device. Its output terminals are connected to the control processing module 300, the motor drive module 100, the communication module 400, and the semiconductor condenser 7, respectively. The control processing module 300 integrates a data processing unit and a logic control unit, serving as the core controller of the device, responsible for receiving instructions, processing data, and outputting control signals. The communication module 400 uses an RS485 bus communication interface 3 for wireless remote data communication with an external control center, enabling instruction reception and status feedback. The motor drive module 100 receives instructions from the control processing module 300 and drives the micro stepper motor 62 in the motor device.
[0023] Specific implementation method of the motor device: The motor assembly includes a motor mounting bracket 61, a miniature 12V stepper motor 62, a membrane key switch 8, and a photosensitive detection device 10. The miniature stepper motor 62 is fixedly mounted via the motor mounting bracket 61, with its output shaft aligned with the corresponding button on the drone remote controller to simulate manual button operation. The membrane key switch 8 is located at the end of the stroke of the output shaft of the miniature stepper motor 62. When the output shaft is pressed to its full position, the membrane key switch 8 is triggered, generating a signal that is fed back to the control processing module 300 to detect whether the button has been pressed. The photosensitive detection device 10 is located near the motor assembly to detect whether the miniature stepper motor 62 is operating, further increasing the reliability of status monitoring.
[0024] The working process of this utility model is as follows: The external control center sends button operation commands to the control processing module 300 via the RS485 communication module 400. After parsing the commands, the control processing module 300 drives the micro stepper motor 62 through the motor drive module 100, causing its output shaft to press the remote control button. At the same time, the membrane key switch 8 and the photosensitive detection device 10 detect the button status and motor running status in real time and feed the signals back to the control processing module 300, forming a closed-loop control to ensure the accuracy and reliability of the button operation. During the operation of the device, the heat dissipation system runs continuously: the cold air generated by the semiconductor condenser 7 cools the circuit part 2 and the remote control environment through the cold air outlet 11, the exhaust fan 4 exhausts the hot air, the dustproof net 6 prevents dust from entering, and the waterproof shell 1 provides overall protection.
[0025] In summary, this invention uses a micro stepper motor as the actuator, which offers significantly higher control precision than traditional servo motors. It accurately simulates the travel and force of a button, effectively preventing button malfunctions or equipment damage caused by inaccurate force. Furthermore, the dual detection mechanism, comprised of a membrane key switch and a photosensitive detection device, provides real-time feedback on the button's position and the motor's operating status, forming a closed-loop control that greatly improves the success rate of single operations and the overall system reliability.
[0026] By combining an active cooling system with a built-in semiconductor condenser and an exhaust fan, and supplemented by a dustproof net and waterproof shell design, the device effectively solves the problem of performance degradation or failure caused by excessive internal temperature or external media intrusion during long-term continuous operation or in harsh environments such as high temperature, dust, and humidity. This significantly improves the device's environmental adaptability and long-term operational stability and durability.
[0027] The circuitry employs a modular design. The control processing module integrates data processing and logic control functions, while the communication module uses a standard RS485 bus interface. This results in a compact structure, simple wiring, and easy integration into existing UAV nest control systems. This modular and standardized design not only reduces system complexity and maintenance costs but also ensures the accuracy of command transmission and execution, as well as the stability of the entire control process.
[0028] This invention completely replaces manual intervention in the drone startup process and overcomes the shortcomings of insufficient reliability in existing servo motor solutions. Through seamless integration with the drone's nest system, it can remotely, automatically, and reliably complete remote control button operations, which is a key technical guarantee for realizing "unmanned" duty and fully automated operation processes for drones.
[0029] The above embodiments are only used to illustrate the technical solutions of this utility model, and are not intended to limit it. Although this utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art should understand that modifications can still be made to the technical solutions described in the foregoing embodiments, or equivalent substitutions can be made to some of the technical features. Such modifications or substitutions do not cause the essence of the corresponding technical solutions to deviate from the spirit and scope of the technical solutions of the embodiments of this utility model.
Claims
1. A button-operated remote control device for unmanned aerial vehicles, characterized in that, include: The structural part and the circuit part are fixed inside the structural part; The structural component includes a waterproof housing and a heat dissipation system disposed therein. The heat dissipation system includes a semiconductor condenser, an exhaust fan, and an air duct structure. The waterproof housing is provided with an air inlet and an air outlet, and a dustproof screen is provided at the air inlet. The cold end of the semiconductor condenser faces the circuit part, forming a cold air outlet for dissipating heat from the circuit part, and its hot end is opposite to the exhaust fan, which exhausts hot air through the air outlet. The circuit section includes a control processing module, a motor drive module, a power supply module, and a communication module; the power supply module is used to supply power to the entire device; the control processing module is electrically connected to the communication module, the power supply module, and the motor drive module respectively; the motor drive module is used to drive a motor device to operate.
2. The drone button remote control device according to claim 1, characterized in that, The motor assembly includes a motor mounting bracket, a micro stepper motor, and a positioning detection unit. The micro stepper motor is fixedly mounted via the motor mounting bracket, and its output shaft is used to simulate pressing a button on a drone's remote control. The positioning detection unit is used to detect whether the pressing action of the micro stepper motor has been completed.
3. The drone button remote control device according to claim 2, characterized in that, The positioning detection unit is a membrane key switch, which is located at the end of the output shaft stroke of the micro stepper motor. It is used to trigger a signal and feed it back to the control processing module when the output shaft is pressed into position.
4. The drone button remote control device according to claim 2 or 3, characterized in that, The motor device also includes a photosensitive detection device for detecting whether the micro stepper motor is operating.
5. The drone button remote control device according to claim 1, characterized in that, The communication module uses an RS485 bus communication interface.
6. The drone button remote control device according to claim 1, characterized in that, The power module is a DC power module, used to supply power to the micro stepper motor and the various modules of the circuit section.
7. The drone button remote control device according to claim 1, characterized in that, The semiconductor condenser is disposed on the back of the mounting plate of the exhaust fan, and the cold air outlet is located below the circuit section.
8. The drone button remote control device according to claim 1, characterized in that, The control processing module integrates a data processing unit and a logic control unit.