Multi-mode integrated air-based AI unmanned aerial vehicle countermeasure cooperative platform

Abstract

The utility model provides a kind of multi-mode integrated air-based AI unmanned plane countermeasure cooperation platform of multi-modal fusion perception, multi-element collaborative processing capability.The utility model includes unmanned plane component, the investigation module being arranged at the bottom of the unmanned plane component, the vibration damping holder being arranged at the bottom of the investigation module and the strike and recovery module being installed on the vibration damping holder, radio reconnaissance unit, radar detection unit, photoelectric identification unit and investigation information processing unit are equipped inside the investigation module, the investigation information processing unit is respectively connected with radio reconnaissance unit, radar detection unit and photoelectric identification unit electric signal, the strike and recovery module includes laser strike unit, high pressure pneumatic net catch launch unit and the strike execution control unit being arranged in the shell of laser strike unit.The utility model relates to low-altitude safety control and anti-unmanned plane field.

Description

Technical Field

[0001] This utility model relates to the field of low-altitude safety management and anti-drone technology, and in particular to a multi-mode integrated airborne AI drone countermeasure collaborative platform. Background Technology

[0002] In recent years, with the rapid development of miniaturized and multi-rotor drone technology, the widespread application of consumer-grade and modified drones in the low-altitude domain has given rise to severe airspace security challenges. Illegal intrusions, surreptitious filming and evidence collection, airdrops, and even disguised harassment are frequent occurrences, posing potential threats to urban security, key area protection, and major events, urgently requiring efficient, intelligent, and controllable aerial sensing and countermeasures.

[0003] Traditional drone countermeasures primarily rely on radio jamming and GNSS deception. By interfering with the target drone's communication links and positioning systems, they force it to land uncontrollably or return to base. However, these "soft-kill" methods have significant limitations. On one hand, they are ineffective against drones using fiber optic wire control or those with anti-jamming designs. On the other hand, jamming technologies often involve public communication frequencies, posing a risk of impacting legitimate wireless communications and limiting their application in highly communication-sensitive environments such as airports, sporting events, and government districts. Furthermore, while some systems have introduced "hard-kill" methods such as laser strikes and physical impacts to enhance countermeasures, these methods often result in the target drone falling uncontrollably from high altitudes, potentially causing personal injury, property damage, or secondary destruction, posing significant safety hazards and failing to meet the requirements for preserving the target drone's payload and for law enforcement evidence collection.

[0004] Existing low-altitude sensing systems still lack highly integrated and collaborative systematic solutions in key aspects such as target detection, threat identification, real-time positioning, precision strike, and target recovery. Most products only have some functional modules and cannot achieve a complete closed loop of "detection-identification-positioning-strike-recovery". They suffer from problems such as slow system response, limited handling methods, and poor environmental adaptability, making it difficult to cope with the current diverse and highly concealed new drone threats.

[0005] Therefore, there is an urgent need to develop an airborne low-altitude perception platform with multimodal fusion perception and multi-element collaborative processing capabilities. This platform should integrate multiple technical approaches such as radio reconnaissance, radar detection, photoelectric identification, laser strike, and net capture and recovery to achieve integrated processing capabilities including rapid response, precise strike, and safe recovery. This would fill the capability gaps of current anti-drone systems in scenarios such as urban security and key area protection, and meet the comprehensive requirements for target integrity, security, and the integrity of the law enforcement evidence chain. Utility Model Content

[0006] To address the shortcomings of the existing technologies, this invention provides a multi-mode integrated airborne AI drone countermeasure collaborative platform, aiming to solve the problems of insufficient perception dimensions, limited strike methods, and lack of controllable target recovery in the existing technologies.

[0007] To achieve the above objectives, the technical solution adopted by this utility model is: a multi-mode integrated airborne AI drone countermeasure collaborative platform, including a drone component, a reconnaissance module disposed at the bottom of the drone component, a vibration damping gimbal bracket disposed at the bottom of the reconnaissance module, and a strike and recovery module mounted on the vibration damping gimbal bracket. The reconnaissance module internally includes a radio reconnaissance unit, a radar detection unit, an optoelectronic identification unit, and a reconnaissance information processing unit. The reconnaissance information processing unit is electrically connected to the radio reconnaissance unit, the radar detection unit, and the optoelectronic identification unit, respectively. The strike and recovery module includes a laser strike unit, a high-pressure pneumatic net capture and launch unit, and a strike execution control unit disposed within the housing of the high-pressure pneumatic net capture and launch unit. The strike execution control unit is electrically connected to the laser strike unit and the high-pressure pneumatic net capture and launch unit, respectively. The reconnaissance information processing unit is electrically connected to the strike execution control unit.

[0008] Based on the above structural design, this utility model, by placing the reconnaissance module at the bottom of the UAV components, enables stable and efficient information collection during flight, which is beneficial to improving the comprehensiveness and effectiveness of aerial detection. The reconnaissance module integrates a radio reconnaissance unit, a radar detection unit, and an optoelectronic identification unit, realizing multi-source fusion detection of electromagnetic, radar, and visible / infrared information. It has stronger perception and adaptability in complex low-altitude environments. The electrical signal connection between the reconnaissance information processing unit and various reconnaissance sub-units enables the system to quickly complete data collection and preprocessing during flight, effectively improving target identification efficiency. By introducing an autonomous identification and decision-making mechanism based on artificial intelligence algorithms into the reconnaissance information processing unit, the platform can achieve local autonomous operation based on the target status even without ground commands or when the communication link is weakened. At the same time, through the information sharing mechanism between the communication unit and the ground monitoring terminal, a collaborative linkage capability between the airborne platform and the ground countermeasure system is built. This allows the target detection, early warning judgment, and disposal strategies to form a supplementary cooperation with the ground system on the basis of the airborne priority closed loop, thereby realizing an integrated collaborative disposal mode of "airborne autonomy - ground monitoring - joint countermeasures", further improving the platform's mission continuity and countermeasure effectiveness in complex low-altitude environments.

[0009] The vibration-damping gimbal bracket is used to install the strike and recovery module. It has good vibration isolation performance and can effectively reduce the impact of vibration caused by UAV flight on strike accuracy, ensuring the stable execution of strike and capture missions. The strike and recovery module integrates a laser strike unit and a high-pressure pneumatic net capture and launch unit. It can flexibly select energy strike or physical capture methods according to different combat scenarios, realize a multi-modal strike method combining soft and hard, and improve the reliability of mission completion. The laser strike unit can be used to carry out fixed-point high-energy strikes on targets, while the high-pressure pneumatic net capture and launch unit carries out capture operations through a capture net.

[0010] In addition, the electrical connection structure between the strike execution control unit and the laser strike unit and the high-pressure pneumatic net capture and launch unit avoids functional descriptions and improves the overall control accuracy and response speed of the system. The electrical signal interaction between the reconnaissance information processing unit and the strike control unit also realizes the rapid response logic of "reconnaissance-strike" integration, which helps to improve the adaptive decision-making capability and combat efficiency of the unmanned platform. It is particularly suitable for rapid deployment and precise response in ever-changing battlefield environments.

[0011] Furthermore, the strike execution control unit is equipped with independent control boards corresponding to the laser strike unit and the high-pressure pneumatic net capture and launch unit, respectively.

[0012] Based on the above, the strike execution control unit has an independent control board corresponding to both the laser strike unit and the high-pressure pneumatic net capture and launch unit. This structure enables physical isolation and task separation between the two types of execution units at the control level, thus providing significant advantages in terms of electrical interference, fault isolation, and safety strategy implementation. On the one hand, the independent control board can respectively undertake the drive and protection functions of its respective execution unit (such as power switching, overcurrent / overvoltage protection, preheating / cooling management, and safety interlocking), reducing the risk of the entire strike capability failing due to a single point of failure. On the other hand, the decoupling between the control circuits makes the response during mode switching faster and more reliable. The strike execution control unit can achieve rapid switching between laser and net capture through parallel or serial scheduling of the independent circuits, which is beneficial for maintaining continuous operation capability in variable scenarios. Furthermore, this structure facilitates modular design and on-site maintenance. Each independent circuit can be individually debugged and replaced as a replaceable unit, reducing maintenance difficulty and improving the overall availability and scalability of the system. Overall, the setting of the above-mentioned independent control board further enhances the technical effects of this utility model in terms of control accuracy, reliability, and on-site adaptability.

[0013] Furthermore, the strike execution control unit includes a control circuit board installed inside the housing of the high-pressure pneumatic net capture and launch unit and a signal interface component connected to the control circuit board. The signal interface component is electrically connected to the reconnaissance information processing unit via a shielded cable.

[0014] Based on the above, the strike execution control unit is arranged inside the housing of the high-pressure pneumatic net capture and launch unit, which helps to realize the integrated and compact design of the strike module, improves the space utilization and overall layout rationality of the device, and completes the functional division between the control circuit board and the signal interface component through internal connection, so that the unit has good modular maintainability and interface expansion capability. The signal interface component establishes an electrical signal connection with the reconnaissance information processing unit through shielded cable, which can effectively shield electromagnetic interference, ensure the stability and reliability of information transmission, and thus enhance the platform's mission execution capability in complex electromagnetic environments.

[0015] Furthermore, the drone components include a fuselage, arms and antennas respectively mounted on the fuselage, and brushless motors and propellers mounted on the arms. The fuselage contains a flight control unit, a power management unit, an attitude measurement unit, a navigation and positioning unit, and a communication unit. The flight control unit is electrically connected to the reconnaissance information processing unit.

[0016] Based on the above, the UAV component integrates flight components such as arms, antennas, brushless motors, and propellers, providing the platform with reliable flight power and communication capabilities. This ensures the platform maintains good flight stability and maneuverability in various low-altitude environments. The internally installed flight control unit, power management unit, attitude measurement unit, navigation and positioning unit, and communication unit enable the platform to possess core capabilities such as autonomous flight, precise positioning, attitude adjustment, and stable communication. This helps improve overall mission response efficiency and system operational stability. Simultaneously, the flight control unit establishes an electrical signal connection with the reconnaissance information processing unit, enabling unified coordination and control of the reconnaissance module. This enhances the platform's response speed and collaborative combat capabilities during target identification and engagement.

[0017] Furthermore, the high-pressure pneumatic net capture and launch unit includes a launch housing, a capture net disposed within the launch housing, a launch mechanism connected to the capture net, and a high-pressure gas storage assembly for driving the launch mechanism. The launch mechanism is electrically connected to the strike execution control unit.

[0018] Based on the above, the structure of the high-pressure pneumatic net capture launch unit enables precise timing and localized management of the launch action under the electrical signal of the strike execution control unit. By integrating the high-pressure gas storage component, launch mechanism, and launch shell, and arranging the strike execution control unit within the shell, the control loop can be shortened and wiring complexity reduced, thereby improving launch response speed and reliability. At the same time, the electrical signal connection of the shielded cable and the mechanical constraint of the shell help reduce electromagnetic interference and ensure that the capture net is stably deployed along the predetermined direction, thereby improving the interception success rate. This structure also facilitates local protection and maintenance of launch energy and launch angle, facilitates modular replacement, and is conducive to the recovery of the capture net, thereby reducing the risk of secondary fall of the captured target and improving the safety and controllability of on-site disposal.

[0019] Furthermore, a landing gear assembly is provided at the bottom of the fuselage, the landing gear assembly including a support frame and foot pads fixedly connected to the end of the support frame.

[0020] Based on the above, the landing gear assembly added to the bottom of the fuselage, through the structural cooperation of the support frame and the foot pads, can effectively provide stable support and buffer protection during platform takeoff, landing and ground parking, enhance the platform's adaptability to takeoff and landing in various complex environments, and help improve the overall structure's seismic resistance and practicality. To more clearly illustrate the above-mentioned features of this utility model and the objectives it aims to achieve, the present utility model will be further described below in conjunction with the accompanying drawings and specific embodiments. Attached Figure Description

[0021] Figure 1 This is a schematic diagram of the structure of this utility model; Figure 2 This is a schematic diagram of the internal structure of the reconnaissance module; Figure 3 This is a schematic diagram of the laser strike unit. Figure 4 This is a flowchart illustrating the process of this utility model. Detailed Implementation

[0022] like Figures 1-4As shown, this utility model is a multi-mode integrated airborne AI drone countermeasure collaborative platform, including a drone component 1, a reconnaissance module 2 disposed at the bottom of the drone component 1, a vibration damping gimbal bracket 3 disposed at the bottom of the reconnaissance module 2, and a strike and recovery module 4 installed in the vibration damping gimbal bracket 3. The reconnaissance module 2 is equipped with a radio reconnaissance unit 20, a radar detection unit 21, an optoelectronic identification unit 22, and a reconnaissance information processing unit 23. The reconnaissance information processing unit 23 is electrically connected to the radio reconnaissance unit 20, the radar detection unit 21, and the optoelectronic identification unit 22 respectively. The strike and recovery module 4 includes a laser strike unit 40, a high-pressure pneumatic net capture and launch unit 41, and a strike execution control unit 42 disposed in the housing of the high-pressure pneumatic net capture and launch unit 41. The strike execution control unit 42 is electrically connected to the laser strike unit 40 and the high-pressure pneumatic net capture and launch unit 41 respectively. The reconnaissance information processing unit 23 is electrically connected to the strike execution control unit 42.

[0023] The strike execution control unit 42 is equipped with an independent control board corresponding to the laser strike unit 40 and the high-pressure pneumatic net capture and launch unit 41, respectively.

[0024] The strike execution control unit 42 includes a control circuit board installed inside the housing of the high-pressure pneumatic net capture and launch unit 41 and a signal interface component connected to the control circuit board. The signal interface component is electrically connected to the reconnaissance information processing unit 23 via a shielded cable.

[0025] The UAV component 1 includes a fuselage 10, an arm 11 and an antenna 12 respectively mounted on the fuselage 10, and a brushless motor and a propeller 13 mounted on the arm 11. The fuselage 10 is equipped with a flight control unit, a power management unit, an attitude measurement unit, a navigation and positioning unit, and a communication unit. The flight control unit is electrically connected to the reconnaissance information processing unit 23.

[0026] The high-pressure pneumatic net capture and launch unit 41 includes a launch housing, a capture net disposed in the launch housing, a launch mechanism connected to the capture net, and a high-pressure gas storage assembly for driving the launch mechanism. The launch mechanism is electrically connected to the strike execution control unit 42.

[0027] The bottom of the fuselage 10 is provided with a landing gear assembly 5, which includes a support frame 50 and foot pads 51 fixedly connected to the end of the support frame 50.

[0028] In summary, the specific embodiments of this utility model are as follows: In practical applications, the UAV component 1 works in concert with the flight control unit, power management unit, navigation and positioning unit and attitude measurement unit to receive flight commands from the host computer or ground control station and make real-time adjustments to the current flight status to achieve precise hovering or cruising. The communication unit on the fuselage 10 ensures stable data interaction between the platform and the ground, and the power management unit provides distributed and stable power supply for the entire platform.

[0029] When the platform enters the target reconnaissance area, the reconnaissance module 2 located at the bottom of the UAV component 1 starts working. The radio reconnaissance unit 20, radar detection unit 21 and photoelectric identification unit 22 in the reconnaissance module 2 collect the corresponding multimodal target information and transmit the perception data to the reconnaissance information processing unit 23 in real time. The reconnaissance information processing unit 23 performs fusion analysis and identification judgment on the multi-source information. Once a suspected target to be attacked is detected, the reconnaissance information processing unit 23 sends the corresponding control command to the strike execution control unit 42 through an electrical signal.

[0030] Upon receiving the control command, the independent control board in the strike execution control unit 42 judges and issues the execution strategy. If the net capture mode is selected, the strike execution control unit 42 drives the high-pressure gas storage component and controls the launching mechanism to make the capture net pop out from the launching shell and unfold to carry out non-lethal interception of the target. At the same time, the capture net and the recovery mechanism cooperate to realize the target recovery. If the energy strike mode is selected, the strike execution control unit 42 controls the laser strike unit 40 to start high-energy emission and carry out targeted damage to the target. The electrical connection between the strike execution control unit 42, the laser strike unit 40 and the high-pressure pneumatic net capture launching unit 41, and the electrical signal connection with the reconnaissance information processing unit 23 ensure the timeliness of command transmission and the reliability of execution.

[0031] To ensure strike accuracy and system response time, the strike and recovery module 4 is structurally isolated from the UAV component 1 through the vibration damping gimbal bracket 3. This reduces load vibration when the platform moves or encounters disturbances, thereby improving the stability of the sensing and strike process. During platform takeoff and landing, the landing gear component 5 at the bottom of the fuselage 10 provides stable support and buffer protection through the structural cooperation of the support frame 50 and the foot pads 51, ensuring the safety of the entire platform structure.

[0032] To enhance autonomy in real-world scenarios, this invention integrates a deep learning-based feature extraction unit and a target status assessment unit within the reconnaissance information processing unit. Through algorithmic models, it fuses radio spectrum features, radar echo features, and photoelectric image features to achieve adaptive judgment of suspected target categories, trajectories, and threat levels. When the platform is without a ground control link or in a communication-restricted state, the reconnaissance information processing unit can generate local autonomous handling instructions according to preset operational strategies and directly link with the strike execution control unit to complete the interception process, forming a closed-loop autonomous operation capability of "detection-discrimination-handling," thereby improving the platform's response efficiency in dynamic and sudden environments.

[0033] When a ground station communication link is available, the communication unit can push real-time target information, location data, and threat level to the ground monitoring terminal. The ground command terminal can then coordinate and schedule the operation according to the regional control strategy, enabling task linkage between the airborne reconnaissance platform and the ground control system. The platform can dynamically adjust its operation mode based on the disposal authorization or no-fly zone situation information transmitted back from the ground. When a target enters a designated airspace or poses a substantial threat, the platform can also work with ground radar arrays or electronic blockade equipment to improve the interception success rate on the basis of "airborne advance and autonomous interception," thereby forming an integrated joint response mode of "airborne perception + ground support + autonomous countermeasure."

[0034] In summary, by integrating multimodal reconnaissance and composite strike methods, this platform has constructed an integrated process from target detection, identification, decision-making to disposal, significantly improving the autonomy and combat effectiveness of low-altitude perception missions.

[0035] The above description is only the optimal solution embodiment of this utility model and is not intended to limit this utility model. Various modifications or substitutions made by those skilled in the art to this utility model without departing from the essence and protection scope of this utility model should also be within the protection scope of this utility model.

Claims

1. A multi-mode integrated airborne AI drone countermeasure collaborative platform, comprising a drone component (1), a reconnaissance module (2) disposed at the bottom of the drone component (1), a vibration damping gimbal bracket (3) disposed at the bottom of the reconnaissance module (2), and a strike and recovery module (4) mounted on the vibration damping gimbal bracket (3), characterized in that: The reconnaissance module (2) is equipped with a radio reconnaissance unit (20), a radar detection unit (21), an optoelectronic identification unit (22), and a reconnaissance information processing unit (23). The reconnaissance information processing unit (23) is electrically connected to the radio reconnaissance unit (20), the radar detection unit (21), and the optoelectronic identification unit (22). The strike and recovery module (4) includes a laser strike unit (40), a high-pressure pneumatic net capture and launch unit (41), and a strike execution control unit (42) disposed in the housing of the laser strike unit (40). The strike execution control unit (42) is electrically connected to the laser strike unit (40) and the high-pressure pneumatic net capture and launch unit (41), and the reconnaissance information processing unit (23) is electrically connected to the strike execution control unit (42).

2. The multi-mode integrated airborne AI drone countermeasure collaborative platform according to claim 1, characterized in that: The strike execution control unit (42) is equipped with an independent control board corresponding to the laser strike unit (40) and the high-pressure pneumatic net capture and launch unit (41), respectively.

3. The multi-mode integrated airborne AI UAV countermeasure collaborative platform according to claim 1, characterized in that: The strike execution control unit (42) includes a control circuit board installed inside the housing of the high-pressure pneumatic net capture and launch unit (41) and a signal interface component connected to the control circuit board. The signal interface component is electrically connected to the reconnaissance information processing unit (23) via a shielded cable.

4. The multi-mode integrated airborne AI drone countermeasure collaborative platform according to claim 1, characterized in that: The unmanned aerial vehicle (UAV) component (1) includes a fuselage (10), an arm (11) and an antenna (12) respectively mounted on the fuselage (10), and a brushless motor and a propeller (13) mounted on the arm (11). The fuselage (10) is equipped with a flight control unit, a power management unit, an attitude measurement unit, a navigation and positioning unit and a communication unit. The flight control unit is electrically connected to the reconnaissance information processing unit (23).

5. The multi-mode integrated airborne AI drone countermeasure collaborative platform according to claim 1, characterized in that: The high-pressure pneumatic net capture and launch unit (41) includes a launch housing, a capture net disposed in the launch housing, a launch mechanism connected to the capture net, and a high-pressure gas storage component for driving the launch mechanism. The launch mechanism is electrically connected to the strike execution control unit (42).

6. The multi-mode integrated airborne AI UAV countermeasure collaborative platform according to claim 4, characterized in that: The bottom of the fuselage (10) is provided with a landing gear assembly (5), which includes a support frame (50) and foot pads (51) fixedly connected to the end of the support frame (50).

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