Air defense multifunctional comprehensive drive vehicle based on partition isolation and integrated hardware cooperation method

Abstract

The application discloses an air defense multifunctional comprehensive expelling vehicle based on partition isolation, and the vehicle body is sequentially divided into a front sensing area, a middle processing area and a rear disposal area in the longitudinal direction. The application comprises a multi-source sensing hardware group arranged in the front sensing area, a three-layer heterogeneous detection system constructed by a mast, a holder and a base, a central processing unit covered by a metal shielding shell in the middle processing area, a comprehensive expelling hardware group and a standardized quick-release base arranged in the rear disposal area, and the rear disposal area supports plugging and replacing different physical attack modules. Metal isolation rib plates with a height not less than one half of a launching caliber are vertically fixed between the front and rear areas, and the internal strong and weak electric wire grooves of the vehicle body are physically separated and are provided with shielding tubes. The application can block the electromagnetic blinding of high-power expelling operation to the radar from the hardware bottom layer, and guarantees the continuous situation awareness. In combination with the modular expansion and the electromechanical anti-collision scheduling strategy, the attack adaptability and the system operation safety in a complex multi-target scene are significantly improved.

Description

Technical Field

[0001] This invention relates to the field of airport protection and security equipment technology, and more specifically, to a multi-functional air defense vehicle based on zoned isolation and an integrated hardware coordination method. Background Technology

[0002] With the rapid development of civil aviation, the environmental safety of airport airspace is directly related to the safety of aircraft takeoff and landing. In recent years, bird strikes and unauthorized drone flights ("black flights") have frequently intruded into airport airspace, posing serious safety hazards to normal flight operations. To maintain low-altitude safety around airports, various air defense and deterrence equipment have been widely used. In the current airport protection system, traditional deterrence methods are generally divided into two relatively independent camps: equipment specifically for dispersing birds (such as fixed gas cannons, bird deterrent vehicles, etc.) and systems specifically for countering drones (such as fixed electromagnetic interference sites). In actual operation, these devices often require manual scheduling and control based on the on-site situation. Some equipment attempts to integrate different functions onto vehicles, but hardware integration of multi-source equipment, electromagnetic compatibility, and multi-task concurrent control are still in the initial stages. Existing integrated deterrence technologies and related equipment mainly have the following defects and shortcomings: First, the hardware is redundantly stacked and is prone to generating electromagnetic interference. Existing attempts mostly combine the detection radar and high-powered expulsion device on the same vehicle body, lacking a scientific physical space isolation and shielding design. When the high-powered electromagnetic interference device is working, it can easily cause electromagnetic "blinding" to its own highly sensitive detection radar, causing the system to lose its ability to continuously perceive the target during the expulsion process.

[0003] Second, there is a lack of electromechanical scheduling mechanisms to prevent conflicts. When faced with complex multi-target intrusion scenarios (such as the simultaneous appearance of flocks of birds and drones), existing equipment lacks the ability to prioritize scheduling based on hardware status. If multiple high-power drive-away loads such as sound, light, and electricity are activated concurrently, it can easily lead to overload of the vehicle power supply system and conflicts in hardware execution timing.

[0004] Third, the adaptability to different scenarios and the ability to expand physical capabilities are poor. The strike payloads of existing anti-tank vehicles mostly use fixed, dead-connected configurations, making it difficult to quickly modularize and replace them according to the specific needs of different seasons at the airport or sudden irregular targets (such as balloons, sky lanterns, large kites, etc.). This results in a limited range of physical strike methods and a low equipment reuse rate. Summary of the Invention

[0005] The purpose of this invention is to provide a multi-functional air defense vehicle based on zoned isolation and an integrated hardware coordination method. It can utilize the spatial movement capabilities of the automatic lifting mast and the second robotic arm. In mission mode, it can quickly extend and accurately point to the target according to the sensing command. Combined with the high mobility of the chassis, it breaks through the geographical limitations of traditional fixed defense lines, thereby effectively enhancing the comprehensive security level of the low-altitude area of ​​the airport.

[0006] To achieve the above objectives, in a first aspect of the present invention, a multi-functional air defense integrated destroyer vehicle based on partitioned isolation and an integrated hardware coordination method are provided, comprising: The vehicle has an autonomous driving chassis with both autonomous driving and manual control modes and a vehicle body mounted on the chassis. The top of the vehicle body is divided into a front perception area, a middle processing area and a rear processing area along the longitudinal space. The front of the vehicle body is equipped with a driver's cab, which is equipped with a personnel electromagnetic shielding structure to block high-power electromagnetic radiation. Multi-source sensing hardware group: physically deployed in the front sensing area, including a phased array radar installed on the top of the lifting mast, a polarized lidar installed on the rotating gimbal, and an ultra-high-definition zoom camera installed on the fixed base on the vehicle roof. Central processing unit: Physically deployed in the central processing area, the central processing unit is covered by a metal shielding shell, and the internal signal cable trays are connected to the power cable trays through physically separated cable trays; Integrated expulsion hardware group: Physically deployed in the post-processing area, it adopts a clustered arrangement, including an acoustic transmitter array, a multi-level laser transmitter, and an interference transmitting antenna installed on the second robotic arm; Physical isolation module: Deployed between the front sensing area and the rear processing area, including a metal isolation rib plate vertically fixed between the jamming transmitting antenna and the phased array radar. The height of the metal isolation rib plate is determined according to the half wavelength corresponding to the lower limit frequency of the jamming transmitting antenna's operating frequency band, and is not less than half of the transmitting aperture. The central processing unit is configured with hardware anti-collision scheduling logic, including: in a multi-target intrusion scenario, based on the threat score and current location of each target, controlling different handling hardware to physically point at different spatial targets, and executing the following timing control: prioritizing the activation of the acoustic transmitter array to issue an acoustic warning to the first threat target; if the target threat is not eliminated after the warning has lasted for a preset time, activating the multi-level laser transmitter or the jamming transmitting antenna to suppress the target, and at the same time only outputting a full-power drive signal to one expulsion hardware.

[0007] In one embodiment of the present invention, the sensing hardware of the front sensing region adopts a gradient space layout: The far-field sensing submodule includes the phased array radar and wide-angle infrared scanner for wide-area search of targets at the first distance. The mid-level perception submodule includes the polarization lidar and mid-wave infrared thermal imager, used for feature extraction of the second-range target; Near-field perception submodule: includes the ultra-high-definition zoom camera, ultraviolet flame detector and radio direction finding array, used for detailed identification of targets at third distance.

[0008] In one embodiment of the present invention, the phased array radar has a specific anti-interference mounting structure: the radar is installed in a first robotic arm with a multi-degree-of-freedom joint design. The first robotic arm achieves flexible adjustment in three dimensions (front, back, left, right, and up and down) through built-in joint drive, and is internally configured with a sealed wiring cavity to accommodate power supply and signal wires.

[0009] In one embodiment of the present invention, the electromagnetic compatibility structure of the central processing area is specifically as follows: the signal cable tray is covered with a metal braided mesh shielding tube throughout, and the physical distance between the signal cable tray and the power cable tray inside the vehicle body is maintained at a certain distance.

[0010] In one embodiment of the present invention, the hardware connection of the post-processing area includes a shock-absorbing and stabilizing platform: the base of the multi-stage laser emitter is connected to the vehicle body through a steel wire rope shock absorber; the acoustic transmitter array is fixed by a flexible suspension structure to isolate the mechanical resonance caused by the vehicle's movement.

[0011] In one embodiment of the present invention, the expulsion device of the post-disposal area has a telescopic storage function: the bottom of the multi-stage laser emitter is connected to an automatic lifting mechanism, which is configured to be stored within the outline of the top of the vehicle body in the non-mission state, and to be raised and exposed to the emission aperture in the mission state.

[0012] In one embodiment of the present invention, the post-processing area is further provided with a standardized quick-release base: the standardized quick-release base integrates a power supply copper bus, a high-speed data bus interface and mechanical positioning pin holes, for plug-and-play replacement of different physical impact modules.

[0013] In one embodiment of the present invention, the quick-release base supports the expansion installation of any of the following modules: Interception net capture module: Net gun mechanism driven by compressed air or gunpowder; High-power microwave heating module: Equipped with a microwave emitting array, used to generate a thermal effect on metal-coated balloons; Evidence collection lighting composite module: integrates a high-magnification zoom camera and a high-power LED array light.

[0014] In one embodiment of the present invention, the central processing unit is configured with hardware anti-collision scheduling logic: in a multi-target intrusion scenario, the central processing unit controls different processing hardware to physically point to different spatial targets, and forces the execution of a hardware power-on sequence that first activates acoustic warnings and then activates high-power electromagnetic or laser suppression.

[0015] In one embodiment of the present invention, the chassis is equipped with a power battery system, the power battery system supports a fast charging mode and is equipped with a quick-release battery pack; the battery pack integrates a liquid cooling / air cooling system and a thermal runaway management system.

[0016] In one embodiment of the present invention, the personnel electromagnetic shielding structure of the cockpit includes: an observation window with an embedded metal shielding mesh, a conductive absorbing coating applied to the surface of the cabin, and a conductive sealing structure disposed at the seam of the cabin door.

[0017] In a second aspect of the present invention, an integrated hardware coordination method based on any one of the above-described air defense multi-functional destroyer vehicle is provided, comprising the steps of: S1: The autonomous driving chassis performs patrols, acquiring target feature data through the lifting mast, rotating gimbal, and sensing hardware group on the fixed base within the perception area; S2: The central processing unit in the middle processing area classifies and interprets the feature data, and generates hardware scheduling instructions based on the target's threat score and current location; S3: The second robotic arm or automatic lifting mechanism in the post-processing area moves to drive the corresponding expulsion hardware to align with the target. When performing physical expulsion or suppression actions, it strictly follows the sequence of prioritizing acoustic warnings and then suppressing the target after the warnings are ineffective. At the same time, it only outputs a full-power drive signal to one expulsion hardware.

[0018] The present invention has the following beneficial effects: First, this invention significantly reduces the risk of electromagnetic interference between onboard equipment by constructing a three-zone physical architecture on the vehicle body, longitudinally divided into a sensing zone, a processing zone, and a rear zone, and by installing metal isolation ribs and shielded cable trays. This hardware-level spatial isolation and electromagnetic protection structure allows the high-power jamming antenna in the rear zone to effectively avoid the "blinding" effect on the radar echo receiving link in the front sensing zone when performing suppression tasks, thereby ensuring the stability of the situational awareness of the vehicle throughout the entire mission cycle.

[0019] Secondly, by introducing a standardized quick-release base and a three-layer heterogeneous sensing hardware cluster, this invention effectively overcomes the shortcomings of traditional equipment, such as poor scalability and large detection blind spots. The three-layer sensing sub-modules (far, medium, and near range) can accurately cover the full range of needs, from large-scale early warning to close-range detail identification. Simultaneously, the quick-release base supports rapid plug-and-play replacement of different physical loads, such as interception net capture modules and high-power microwave heating modules, enabling a single vehicle to flexibly configure corresponding strike hardware for different types of low-altitude intrusions, significantly improving the system's scenario adaptability and equipment utilization.

[0020] Furthermore, this invention effectively mitigates power supply and timing crises in multi-target concurrent scenarios by incorporating an anti-collision hardware scheduling strategy within the central processing unit. This strategy allocates expulsion hardware with different spatial orientations based on the priority of the targets and strictly adheres to the power-on sequence of activating audible and visual warnings first, followed by activating high-power suppression, preventing system downtime caused by the simultaneous activation of high-load devices throughout the vehicle and ensuring the reliability of collaborative operation of complex electromechanical systems.

[0021] Finally, this invention achieves a highly efficient closed loop from target detection to differentiated handling through deep collaboration between multi-source sensing hardware and electromechanical actuators. Relying on the spatial mobility of the automatic lifting mast and the second robotic arm, various deflection hardware components can be safely stored in non-missionary states and can quickly extend and accurately point to the target according to sensing commands in mission states. Combined with the high mobility of the chassis, this breaks through the geographical limitations of traditional fixed defense lines, thereby effectively enhancing the comprehensive security level of the airport's low-altitude area. Attached Figure Description

[0022] Figure 1 The overall vehicle architecture and three-zone physical layout diagram of the air defense multi-functional integrated destroyer vehicle of the present invention are disclosed. Figure 2 A structural diagram of the multi-source sensing hardware group in the front sensing zone of the air defense multi-functional integrated destroyer vehicle of the present invention is disclosed. Figure 3 A structural diagram of the central processing unit of the air defense multi-functional integrated destroyer vehicle of the present invention is disclosed; Figure 4 A structural diagram of the integrated anti-aircraft hardware group in the rear disposal area of ​​the multi-functional anti-aircraft vehicle of the present invention is disclosed. Figure 5 A cross-sectional view of the standardized quick-release system of the air defense multi-functional integrated destroyer vehicle of the present invention is shown; Figure 6 The diagrams reveal the power battery system, battery swapping structure, and replaceable modules of the air defense multi-functional integrated destroyer vehicle of the present invention; Figure 7 The mechanical arm structure diagram of the air defense multi-functional integrated destroyer vehicle of the present invention is disclosed.

[0023] Figure Labels

[0024] 100. Chassis; 110. Manned cab; 111. Electromagnetic shielding structure for personnel; 120. Power battery system; 121. Quick-release battery pack; 200. Vehicle body; 210. Front sensing area; 220. Middle processing area; 230. Rear processing area; 300. Multi-source sensing hardware cluster; 310. Far-layer sensing submodule; 311. Lifting mast; 312. First robotic arm; 313. Phased array radar; 314. Wide-angle infrared scanner; 315. Wiring cavity; 320. Mid-layer sensing submodule; 321. Rotating gimbal; 322. Dual-frequency radar; 323. Polarized lidar; 324. Mid-wave infrared thermal imager; 330. Near-layer sensing submodule; 331. Fixed base; 332. Ultra-high-definition zoom camera; 333. Ultraviolet flame detector; 334. Radio direction finding array; 400. Central processing unit; 410. Metal shielding housing; 420. Physical isolation module; 421. Metal isolation stiffener; 430. Internal cable tray; 431. Signal cable tray; 432. Power cable tray; 433. Metal braided shielding tube; 500. Integrated expulsion hardware cluster; 510. Jamming transmitting antenna; 511. Second robotic arm; 520. Multi-stage laser emitter; 521. Automatic lifting mechanism; 522. Steel wire rope shock absorber; 530. Acoustic transmitter array; 531. Flexible suspension structure; 600. Standardized quick-release system; 610. Standardized quick-release base; 611. Power supply copper busbar; 612. High-speed data bus interface; 613. Mechanical positioning pin hole; 620. Replaceable ejection hardware. Detailed Implementation

[0025] To make the objectives, technical solutions, and advantages of this invention clearer, the invention will be further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are for illustrative purposes only and are not intended to limit the invention.

[0026] In a first embodiment of the present invention, a multi-functional air defense vehicle based on partitioned isolation is provided, such as... Figure 1 As shown, it includes an autonomous driving chassis 100 with dual modes of autonomous driving and manual takeover, and a vehicle body 200 mounted on the chassis 100. The top of the vehicle body 200 is divided into a front perception area 210, a middle processing area 220 and a rear processing area 230 along the longitudinal space. A manned driver's cab 110 is provided at the front of the vehicle body 200. The driver's cab 110 is equipped with a personnel electromagnetic shielding structure 111 to block high-power electromagnetic radiation. Multi-source sensing hardware group 300: physically deployed in the front sensing area 210, including a phased array radar 313 installed on the top of the lifting mast 311, a polarized lidar 323 installed on the rotating gimbal 321, and an ultra-high-definition zoom camera 332 installed on the fixed base 331 on the vehicle roof. Central processing unit 400: Physically deployed in central processing area 220, the central processing unit 400 is covered by a metal shielding shell 410, and internally connected to power supply cable tray 432 through physically separated signal cable tray 431; Integrated expulsion hardware group 500: Physically deployed in the post-disposal area 230, it adopts a clustered arrangement and includes an acoustic transmitter array 530, a multi-stage laser emitter 520, and an interference transmitting antenna 510 mounted on the second robotic arm 511; Physical isolation module 420: Deployed between the front sensing area 210 and the rear processing area 230, including a metal isolation rib plate 421 vertically fixed between the jamming transmitting antenna 510 and the phased array radar 313. The height of the metal isolation rib plate 421 is determined according to the half wavelength corresponding to the lower limit frequency of the operating frequency band of the jamming transmitting antenna 510, and is not less than half of the transmitting aperture. The central processing unit 400 controls the second robotic arm 511 of the post-processing area 230 to unfold based on the heterogeneous features acquired by the multi-source sensing hardware group 300. The central processing unit 400 is equipped with hardware anti-conflict scheduling logic. In the multi-target intrusion scenario, based on the threat score and current position of each target, it controls different processing hardware to physically point to different spatial targets and forcibly executes the hardware power-up sequence of prioritizing the activation of acoustic warnings and activating high-power electromagnetic or laser suppression after the warnings are ineffective. At the same time, it only outputs a full-power drive signal to one expulsion hardware.

[0027] In this embodiment, the sensing hardware of the front sensing area 210 adopts a gradient spatial layout: Far-field sensing submodule 310: includes phased array radar 313 and wide-angle infrared scanner 314, used for wide-area search of targets at first distance; The mid-level perception submodule 320 includes a polarized lidar 323 and a mid-wave infrared thermal imager 324, used for feature extraction of targets at a second distance. Near-field sensing submodule 330: includes an ultra-high-definition zoom camera 332, an ultraviolet flame detector 333, and a radio direction finding array 334, for detailed identification of targets at third distance.

[0028] In this embodiment, the phased array radar 313 has a specific anti-interference mounting structure: the radar 313 is installed in a first robotic arm 312 with a multi-degree-of-freedom joint design. The first robotic arm 312 achieves flexible adjustment in three dimensions (front, back, left, right, and up and down) through built-in joint drive, and is internally configured with a sealed wiring cavity 315 to accommodate power supply and signal wires.

[0029] In this embodiment, the electromagnetic compatibility structure of the central processing area 220 is as follows: the signal cable tray 431 is covered with a metal braided mesh shielding tube 433 throughout, and the physical distance between the signal cable tray 431 and the power cable tray 432 inside the vehicle body 200 is maintained at a certain distance.

[0030] In this embodiment, the hardware connection of the post-processing area 230 includes a shock-absorbing and stabilizing platform: the base of the multi-stage laser emitter 520 is connected to the vehicle body 200 through a steel wire rope shock absorber 522; the acoustic transmitter array 530 is fixed through a flexible suspension structure 531 to isolate the mechanical resonance caused by the movement of the vehicle body 200.

[0031] In this embodiment, the expulsion device of the post-processing area 230 has a telescopic storage function: the bottom of the multi-stage laser emitter 520 is connected to an automatic lifting mechanism 521, which is configured to be stored within the top outline of the vehicle body 200 in the non-mission state, and to be raised and exposed to the emission aperture in the mission state.

[0032] In this embodiment, the post-processing area 230 is also provided with a standardized quick-release base 610: the standardized quick-release base 610 integrates a power supply copper bus 611, a high-speed data bus interface 612, and a mechanical positioning pin hole 613, for plug-and-play replacement of different physical impact modules. The expulsion hardware 620 can be replaced by plug-and-play replacement of different physical impact modules.

[0033] In this embodiment, the standardized quick-release base 610 supports the expansion installation of any of the following modules: Interception net capture module: Net gun mechanism driven by compressed air or gunpowder; High-power microwave heating module: Equipped with a microwave emitting array, used to generate a thermal effect on metal-coated balloons; Evidence collection lighting composite module: integrates a high-magnification zoom camera and a high-power LED array light.

[0034] In this embodiment, the central processing unit 400 is configured with hardware anti-conflict scheduling logic: in a multi-target intrusion scenario, the central processing unit 400 controls different processing hardware to physically point to different spatial targets, and forces the execution of a hardware power-on sequence that first activates acoustic warnings and then activates high-power electromagnetic or laser suppression.

[0035] In this embodiment, the chassis 100 is equipped with a power battery system 120, which supports fast charging mode and is equipped with a quick-release battery pack 121; the quick-release battery pack 121 integrates a liquid cooling / air cooling system and a thermal runaway management system.

[0036] In this embodiment, the personnel electromagnetic shielding structure 111 of the cockpit 110 includes: an observation window embedded with a metal shielding mesh, a conductive wave-absorbing coating applied to the surface of the cabin, and a conductive sealing structure disposed at the cabin door seam.

[0037] The first embodiment of the present invention also provides an integrated hardware collaboration method for a multi-functional air defense vehicle based on partitioned isolation, as described above, comprising the following steps: S1: The autonomous driving chassis 100 performs a patrol, acquiring the target's feature data through the lifting mast 311, rotating gimbal 321 and multi-source sensing hardware group 300 on the fixed base 331 in the front perception area 210. S2: The central processing unit 400 in the central processing area 220 classifies and interprets the feature data, and generates hardware scheduling instructions based on the target's threat score and current location. S3: The second robotic arm 511 or automatic lifting mechanism 521 of the post-processing area 230 moves to drive the corresponding expulsion hardware to align with the target, and when performing the suppression action, it strictly follows the timing sequence of priority acoustic warning and invalid suppression, and only outputs a single full-power signal at the same time.

[0038] In the second embodiment of the present invention, this embodiment provides a multi-functional air defense vehicle based on zone isolation, focusing on its overall vehicle architecture based on three-zone physical isolation, personnel electromagnetic safety protection, and electromagnetic interference and electromagnetic compatibility (EMC) underlying design.

[0039] The air defense multi-functional integrated destroyer vehicle in this embodiment includes an autonomous driving chassis 100 with both autonomous and manual control modes, and a vehicle body 200 mounted on top of the chassis 100. 1. Top-floor spatial layout and personnel protection zone The top of the vehicle body 200 is strictly divided into three independent working areas along the longitudinal direction from front to back: the front sensing area 210, the middle processing area 220, and the rear processing area 230. Meanwhile, a manned driver's cab 110 is located at the front of the vehicle body 200, serving as a standby and operating space for the observer or driver. To prevent electromagnetic radiation damage to personnel during high-power expulsion operations, the driver's cab 110 is equipped with a dedicated personnel electromagnetic shielding structure 111: the observation window glass of the driver's cab 110 has a microporous metal shielding mesh embedded inside; the surface of the cabin shell is coated with a highly conductive wave-absorbing coating; and all mechanical joints between the cabin door and the vehicle body 200 are fitted with conductive rubber sealing strips to form a complete Faraday cage effect.

[0040] Front sensing area 210: Deployed with a lifting mast 311 and a multi-source sensing hardware group 300 (including phased array radar 313, photoelectric detectors, etc.). This area adopts the lifting mast 311 design to compactly integrate various detection antennas, avoid cluttered external wiring, and improve the overall aesthetics of the vehicle.

[0041] Central processing area 220: Deployed with central processing unit 400, which serves as the control hub of the entire vehicle and is responsible for receiving data from the front area and issuing instructions to the rear area.

[0042] Post-processing zone 230: Deployed with a clustered integrated anti-jamming hardware group 500 (including high-power jamming transmitting antenna 510, multi-stage laser emitter 520, acoustic transmitter array 530, etc.), serving as a high-power output zone. By arranging the phased array radar 313 and strong jamming sources at the front and rear ends of the vehicle body 200 respectively, and combining this with the specialized shielding design of the manned cab 110, a spatial distance foundation is laid for the entire vehicle's electromagnetic interference protection.

[0043] 2. Core physical isolation structure

[0044] like Figure 3 As shown, in this embodiment, a physical isolation module 420 is provided between the front sensing area 210 and the rear processing area 230. Specifically, a metal isolation rib plate 421 is vertically fixed on the top of the vehicle body 200 between the jamming transmitting antenna 510 and the phased array radar 313. In order to achieve the effect of shielding the radiation leakage of the rear lobe and side lobe, the height of the metal isolation rib plate 421 is strictly limited to the half wavelength corresponding to the lower limit frequency of the operating frequency band (such as L, S, X band) of the jamming transmitting antenna 510, and is not less than half of the transmitting aperture of the jamming transmitting antenna 510. The metal isolation rib plate 421 utilizes the reflection and absorption characteristics of electromagnetic waves by the metal material to form a physical blocking barrier, thereby blocking the spatial path of electromagnetic waves directly reaching the receiving end of the phased array radar 313 and the driver's cab 110 at the hardware level.

[0045] To verify the effectiveness of this design, system-level electromagnetic compatibility (EMC) measurements showed that, under different operating frequency bands such as the L-band and X-band, after installing the metal isolation rib plate 421, the interference signal strength measured at the phased array radar 313 receiver was reduced by an average of more than 45 dB compared to the uninstalled state, achieving a highly significant electromagnetic shielding effect. Compared with existing technologies, this invention, through single-vehicle integration and physical longitudinal partitioning with rib plate isolation, not only significantly reduces communication latency, space occupation, and scheduling complexity during multi-vehicle platooning deployment, but also achieves an EMC performance equal to or even higher than that of multiple vehicles with physical spacing, breaking through the technical bottleneck of electromagnetic interference in traditional single-vehicle platforms.

[0046] 3. Shielding protection of the central computing unit

[0047] The central processing unit 400, located in the central processing area 220, integrates core computing chips such as CPU, GPU, and signal processing FPGA, which are susceptible to electromagnetic interference. To prevent electromagnetic pulses from causing flip-flops or system crashes in the computing logic, this embodiment completely encloses the central processing unit 400 with a metal shielding shell 410. This metal shielding shell 410 completely isolates high-frequency electromagnetic radiation from the external space, ensuring high stability in the signal fusion computing and hardware electromechanical collaborative scheduling command issuance process.

[0048] 4. Internal isolation between low-voltage and high-voltage wiring

[0049] Besides external space radiation, crosstalk between cables is also a key factor causing system instability. Inside the vehicle body 200, the wiring system connecting the front, middle, and rear zones employs a 430-degree internal cable tray design with deep separation of strong and weak current. Line spacing isolation: The physical parallel spacing between the signal cable tray 431 for transmitting radar and photoelectric weak signals and the power cable tray 432 for transmitting current of drive motor and high-power transmitting equipment inside the vehicle body 200 shall be more than 10 cm, and it is strictly forbidden for the two to cross or bundle the cables.

[0050] Cable shielding cover: The signal cable tray 431 is fully covered with a metal braided mesh shielding tube 433, and the metal braided mesh shielding tube 433 is connected to the vehicle body beam at multiple points of equipotential grounding. This structure can quickly conduct and discharge the parasitic induced electromagnetic field generated by the sudden change of large power current, thereby completely cutting off the path of conducted electromagnetic interference.

[0051] Through the above design of this embodiment, the integrated destroyer can ensure the electromagnetic radiation safety of the personnel in the driver's cab 110 while the electromagnetic suppression load in the rear area is activated at full power, and maintain high-precision continuous tracking of the radar and optoelectronic equipment in the front sensing area 210.

[0052] In the third embodiment of the present invention, this embodiment further discloses a layered mounting structure for a multi-source sensing hardware group 300. Traditional decoy devices typically use only a single detection radar, which suffers from large detection blind spots and low resolution for slow-moving or small targets (such as Kongming lanterns or floating objects). Therefore, as... Figure 2 As shown, in this embodiment, a three-layer perception architecture with a gradient spatial layout is constructed in the front perception area 210 of the vehicle body 200. Through a highly integrated mechanical mounting platform, seamless situational awareness in the far, medium and near airspace is achieved.

[0053] 1. Remote sensing submodule 310 and multi-degree-of-freedom robotic arm structure

[0054] The far-field sensing submodule 310 is mainly used for wide-area search and coarse classification of airspace beyond 500 meters. This module includes a phased array radar 313 and a wide-angle infrared scanner 314. The phased array radar 313 is preferably an S / X dual-frequency phased array radar.

[0055] In terms of mechanical installation structure, to overcome obstruction from the vehicle's surroundings and to achieve an aesthetically pleasing overall vehicle design, the aforementioned sensors are mounted on the top of the roof-mounted lifting mast 311. The lifting mast 311 features an optimized antenna layout, housing all feed lines and control cables inside the mast, thus avoiding cluttered external wiring.

[0056] In particular, such as Figure 7 As shown, to achieve all-dimensional detection of the phased array radar 313 in complex dynamic environments, this embodiment employs a multi-degree-of-freedom robotic arm with a scientifically designed joint. The phased array radar 313 is mounted at the end of the first robotic arm 312. Through the precision servo joints configured inside the first robotic arm 312, the radar can not only perform 360-degree horizontal rotation and vertical pitch, but also has flexible movement capabilities such as left-right offset and forward-backward extension. This scientific joint structure design relies entirely on internal drive mechanisms to achieve multi-dimensional movement, avoiding the need for complex and unsightly auxiliary structures such as additional external pressure devices or support rods. While ensuring structural strength, it greatly improves the flexibility and visual appeal of the first robotic arm 312. The first robotic arm 312 also has a sealed wiring cavity 315 inside, through which power supply wires and high-speed data lines pass, ensuring that the cables do not become tangled or fatigued during all-dimensional movement. Furthermore, both the first robotic arm 312 and the second robotic arm 511 are multi-degree-of-freedom robotic arms.

[0057] 2. Mid-layer perception submodule 320 and stable platform structure

[0058] The mid-level sensing submodule 320 is mainly used for precise tracking and micro-motion feature extraction of targets in the 50-meter to 500-meter range. This module includes a dual-frequency radar 322 (such as Ku / Ka band), a polarized lidar 323, and a mid-wave infrared thermal imager 324.

[0059] Because devices such as the polarization lidar 323 have extremely narrow beams, they require extremely high platform stability. In this embodiment, they are mounted entirely on a rotating gimbal 321 at the front of the vehicle roof. This rotating gimbal 321 incorporates a gyroscope and a shock absorber, enabling it to acquire the pitch and roll angles of the autonomous driving chassis 100 in real time when driving on uneven roads, and to perform reverse attitude compensation via servo motors. This mechanical decoupling design allows the mid-level perception submodule 320 to firmly lock onto small targets in the sky and acquire high-quality micro-motion spectral characteristics even when the vehicle is patrolling at speeds between 20 km / h and 40 km / h.

[0060] 3. Near-layer sensing submodule 330 and dead-angle-free base

[0061] The near-space sensing submodule 330 is mainly used for detailed identification, evidence collection, and final-stage handling guidance of near-space targets within 50 meters. This module includes an ultra-high-definition zoom camera 332, an ultraviolet flame detector 333, and a radio direction-finding array 334.

[0062] The aforementioned three-layer perception distance thresholds—over 500 meters, 50-500 meters, and within 50 meters—are derived from comprehensive statistical data on the airspace protection zones of large international airports and small regional airports. This is based on theoretical modeling and derivation using common intruders (such as the maximum flight speed of drones) and the required security response buffer time for security systems, demonstrating high versatility across all scenarios. Based on this three-layer perception hardware system and multi-source information fusion algorithm, system-level verification and testing have shown that the multi-source perception fusion system of this invention exhibits excellent target recognition accuracy in complex backgrounds: the accuracy rate for bird recognition reaches over 96.5%, the accuracy rate for "black flight" drones reaches 98.2%, and the accuracy rate for low radar cross-section (RCS) floating targets such as balloons and sky lanterns also reaches over 91.5%, providing precise data support for subsequent conflict prevention and control.

[0063] To counter high-angular-velocity maneuvers of close-range targets (such as small racing drones speeding across the roof), the rotation of the mechanical gimbal often suffers from physical delay. Therefore, in this embodiment, the near-field sensing hardware is mounted in an array on fixed bases 331 on the front edge and sides of the roof. Multiple ultra-high-definition zoom cameras 332 and ultraviolet flame detectors 333 are arranged at a certain angle to form a wide-angle staring field of view. This static mounting method, which uses an array instead of rotation, eliminates mechanical tracking delays, ensuring that sudden threats at close range can be detected instantly.

[0064] Through the three-layer mechanical mounting design of the first robotic arm 312 with scientifically designed joints and the lifting mast 311, this embodiment maximizes the physical potential of various heterogeneous sensors, providing a high-quality data source guarantee for subsequent accurate classification and identification.

[0065] In the fourth embodiment of the present invention, as Figure 4 As shown, the mechanical mounting and storage mechanism and standardized expansion structure of the integrated destructive hardware cluster 500 in the post-disposal area 230 are further disclosed. The core of this embodiment lies in achieving a high degree of integration of various destructive hardware through clustered arrangement, improving disposal efficiency while maintaining the vehicle's aesthetic appearance and avoiding cluttered external wiring. Because the integrated destructive hardware cluster 500 includes various physical characteristics of attack and suppression equipment, and the vehicle experiences a complex force environment during driving and launch, such as... Figure 5 As shown, this embodiment is equipped with a specific shock-absorbing stabilizing platform, a deployment protection mechanism, a standardized quick-release base 610, and a standardized quick-release system 600 in the post-processing area 230.

[0066] 1. Hardware-connected shock-absorbing and stabilizing platform structure

[0067] In response to the extremely high beam pointing accuracy requirements of the multi-stage laser emitter 520, in this embodiment, the base of the multi-stage laser emitter 520 is connected to the vehicle body 200 via a wire rope shock absorber 522. The wire rope shock absorber 522 is configured to isolate the high-frequency vibrations generated by the vehicle chassis 100 during driving and engine operation, to prevent the high-frequency vibrations from being transmitted upwards and causing physical deviation of the laser spot.

[0068] Meanwhile, to address the issue of resonance in the vehicle body 200 caused by the acoustic transmitter array 530 under high power output, the acoustic transmitter array 530 is fixed to the rear treatment area 230 via a flexible suspension structure 531. This flexible suspension structure 531 is configured to sever the rigid mechanical connection between the acoustic transmitter array 530 and the vehicle frame. Through this optimized arrangement of the vibration damping structure, multiple loads can be compactly clustered in the rear treatment area 230 without interfering with each other's mechanical stability.

[0069] 2. Deployment and Retraction Protection Mechanism of the Destroyer Device

[0070] To reduce air resistance during patrol operations, this embodiment features a dynamically retractable storage structure in the rear handling area 230. This ensures that all core launch hardware is stored within the vehicle body 200's outline when not on mission, avoiding a cluttered visual appearance caused by stacked external components. The multi-stage laser emitter 520 is mechanically connected to an automatic lifting mechanism 521 at its bottom. In non-mission mode, control commands drive the automatic lifting mechanism 521 to retract, allowing the multi-stage laser emitter 520 to be stored entirely within the top outline of the vehicle body 200. Upon entering mission mode and receiving a launch preparation command, the automatic lifting mechanism 521 extends upwards, raising the multi-stage laser emitter 520 to expose its launch aperture, thus obtaining an unobstructed launch field of view.

[0071] Simultaneously, the jamming transmitting antenna 510 is mounted on the second robotic arm 511. When performing a suppression mission, the second robotic arm 511 is controlled to extend outwards from the roof to a preset working position; in non-mission mode, it folds and retracts, coordinating with the multi-stage laser emitter 520 and other strike modules for storage, thereby achieving structural integration in terms of physical appearance.

[0072] 3. Standardized quick-release base 610 and replaceable expulsion hardware 620

[0073] like Figure 5As shown, in order to achieve differentiated physical strikes against different low-altitude intrusion interference objects (such as drones, metal-coated balloons, etc.), this embodiment has a clustered standardized quick-release base 610 fixedly installed in the post-disposal area 230 to support plug-and-play replacement of hardware devices.

[0074] In terms of physical construction, the standardized quick-release base 610 integrates a power supply copper busbar 611, a high-speed data bus interface 612, and mechanical positioning pin holes 613. The mechanical positioning pin holes 613 facilitate the structural alignment and physical locking of the replaceable ejector hardware 620. When locked in place, the power supply copper busbar 611 is simultaneously connected to the communication link of the high-speed data bus interface 612. Furthermore, the standardized quick-release base 610 is designed with concealment and integration in mind. All power and data links are coupled internally through the base, eliminating the need for any external exposed wiring. This completely solves the technical pain points of tangled and visually cluttered external wiring in traditional equipment, meeting both aesthetic and reliable design requirements.

[0075] Based on the standardized quick-release base 610, the air defense multi-functional integrated destroyer vehicle of this embodiment supports the plug-and-play expansion installation of the following physical attack modules in the rear cluster, which can replace the destroyer hardware 620: Interception net capture module: A net gun mechanism driven by compressed air or gunpowder, used to physically intercept low-altitude targets with a net. High-power microwave heating module: It is equipped with a microwave transmitting array, which is configured to output high-power microwaves in a directional manner, and uses the eddy current heating effect to detonate the metal-coated target; Evidence collection lighting composite module: mechanically integrated with a high-magnification zoom camera, infrared thermal imager and high-power LED array lights.

[0076] When any of the aforementioned replaceable expulsion hardware 620 is physically inserted and locked onto the standardized quick-release base 610, the central processing unit 400 located in the central processing area 220 is configured to read the load identification code via the high-speed data bus interface 612 and automatically load the underlying control driver that matches the physical strike module.

[0077] Through the coordinated arrangement of the aforementioned clustered layout and the standardized quick-release system 600, this invention not only achieves visual uniformity and aesthetic enhancement of the hardware in the post-processing area 230, but also ensures that various anti-interference devices can operate in an orderly and efficient manner. Preferably, the anti-interference devices include an interception net, a multi-stage laser emitter 520, and an interference transmitting antenna 510, etc.

[0078] Regarding the feasibility of practical deployment, the vehicle and integrated anti-ship hardware group 500 of this invention has undergone rigorous environmental adaptability design, with an overall protection level of IP65 (protection rating), fully adaptable to harsh operating conditions such as high temperature, extreme cold, wind, rain, and sandstorms in airport environments. Simultaneously, to meet legal and regulatory compliance requirements, the central processing unit 400 is pre-installed with an electronic fence and transmission compliance control protocol: its interference transmitting antenna 510 has a frequency band dynamic avoidance function, strictly isolating the civil aviation navigation and communication frequency bands stipulated in the "Regulations on Radio Management of the People's Republic of China" and the "Civil Aviation Law of the People's Republic of China"; high-power equipment such as the multi-level laser transmitter 520 is equipped with physical elevation angle limits and ground personnel safety distance sensors to ensure that high-power output does not pose a threat to off-site personnel or takeoff and landing flights.

[0079] In the fifth embodiment of the present invention, this embodiment discloses an integrated hardware coordination method based on an air defense multi-functional integrated anti-aircraft vehicle, focusing on the hardware anti-collision scheduling logic and electromechanical linkage execution process of the system in a multi-target intrusion scenario. The coordination method of this embodiment specifically includes the following steps: S1: Hardware Situation Awareness and Layered Feature Acquisition During the automatic or manual patrol of the airport protection area by the autonomous driving chassis 100, which has both autonomous driving and manual takeover modes, the multi-source sensing hardware group 300 of the forward sensing zone 210 performs layered detection according to preset spatial distance thresholds. Specifically, the far-layer sensing submodule 310 installed at the top of the lifting mast 311 first transmits a detection signal to perform a search task in a wide airspace beyond 500 meters; when a target is detected to have entered the mid-layer threshold range of 50 to 500 meters, the mid-layer sensing submodule 320 installed on the rotating gimbal 321 is triggered to extract the micro-motion spectrum physical characteristics of the target using a dual-frequency radar 322 and a polarized lidar 323; when the target enters the near-layer threshold range of less than 50 meters, the near-layer sensing submodule 330 installed on the fixed base 331 is activated to acquire the target's radio frequency and image physical data through an ultraviolet flame detector 333 or a radio direction finding array 334.

[0080] S2: Signal Fusion and Priority Hardware-Level Analysis

[0081] The multi-source heterogeneous sensing signals acquired by the front sensing zone 210 are transmitted unidirectionally to the central processing unit 400 in the middle processing zone 220 via signal cable trays 431 covered with metal braided mesh shielding tubes 433. Because the central processing unit 400 is encased in a metal shielding shell 410, the signal transmission and fusion calculation process is protected from electromagnetic radiation interference from the external space. The central processing unit 400 extracts the physical features of the target and determines the target's attributes (covering birds, drones, balloons, sky lanterns, kites, or environmental floating objects) based on a preset feature library. Simultaneously, according to preset threat level rules, it outputs priority classification instructions for multiple simultaneously detected targets.

[0082] The central processing unit 400 incorporates specific scheduling algorithms and priority determination rules: by extracting four dimensions of target characteristics—intrusion distance, approach rate, target size, and heading angle—a real-time threat score is calculated (e.g., a high-speed approaching drone scores significantly higher than a slowly drifting Kongming lantern), thereby quantifying the absolute priority of multiple concurrent targets. For false alarm targets identified as environmental floating objects, the central processing unit 400 locks the corresponding hardware driver port at the underlying level, prohibiting any hardware actions in the post-processing area 230. For targets identified as high threats (such as approaching drones), the central processing unit 400 simultaneously sends warning information to the electromagnetically shielded control terminal in the front-end manned cockpit 110, reminding the waiting observer or pilot to conduct manual verification or prepare for manual takeover.

[0083] S3: Hardware anti-collision timing allocation and electromechanical linkage

[0084] To prevent the onboard power supply system from overloading and voltage drops due to the instantaneous concurrent activation of high-power expulsion hardware across the entire vehicle, the central processing unit 400, upon receiving priority classification instructions, strictly implements hardware anti-collision scheduling and power-on timing control mechanisms. Specifically, this includes: multi-channel hardware space allocation: When facing simultaneous intrusions by multiple targets, the central processing unit 400, based on the principle of independent physical channels, controls different mechanical servo mechanisms to point towards different targets. For example, it drives the servo motor of the multi-stage laser emitter 520 to operate and point it towards the Kongming lantern target, while simultaneously driving the acoustic transmitter array 530 to point it towards the bird flock target, avoiding frequent back-and-forth switching of the mechanical gimbal.

[0085] Forced interlocking power-on sequence and timeout handling mechanism: The central processing unit 400 executes a hardware startup sequence of low-power warning first, followed by high-power suppression. The system first outputs a low-current drive signal to the acoustic transmitter array 530 or the multi-level laser transmitter 520 to perform a non-contact physical warning; if the target does not deviate from its course and a high-power electromagnetic suppression action is required, the system must wait for the authorization command issued manually by the front-end manned cab 110 (or after the set automatic takeover timeout); after obtaining the redundant power data of the reserved quick-release battery pack 121 and the safety status of the thermal runaway management system, and determining that the high-frequency discharge threshold requirement is met, a high-current conduction command can be output to the interference transmitting antenna 510 installed on the deploying arm (second robotic arm 511) or the high-power microwave heating module on the standardized quick-release base 610. Meanwhile, in order to completely solve the problem of power supply capacity overload, the hardware anti-collision scheduling algorithm sets a forced interlocking procedure at the underlying logic through a real-time power supply capacity monitoring method: even if there are multiple high-risk targets, the system can only output a full-power drive signal to one high-power load (such as a single-channel interference antenna or a single-channel microwave module) in the integrated expulsion hardware group 500 at the same time, while the other loads are in standby or low-power tracking state.

[0086] Electromechanical linkage execution: Under the aforementioned timing control, the automatic lifting mechanism 521 of the post-processing area 230 extends upward to a predetermined height, and the second robotic arm 511 extends outward to the working range. The standardized quick-release base 610, based on the internally identified load type, distributes independent power and control signals to the clustered interception net capture module or microwave heating module to complete the predetermined physical removal, net gun capture, or electromagnetic isolation actions. After execution, the high-power power supply circuit is cut off, and the mechanical storage mechanism is driven to reset.

[0087] In the sixth embodiment of the present invention, a power battery system 120 is disclosed that supports the high-power load of the entire vehicle and the operation of the autonomous driving chassis 100.

[0088] like Figure 6 As shown, to meet the stringent endurance requirements of high-frequency patrols and high-power concurrent expulsion operations, the autonomous driving chassis 100 is equipped with a power battery system 120 that supports fast charging and innovatively adopts a quick-release battery pack 121 design. Referring to mature quick-change solutions for industrial forklifts, this quick-release battery pack 121 is connected to the vehicle body 200 via a bottom slide rail and a high-voltage quick-connect interface, enabling convenient plugging and unplugging and rapid replacement of the entire pack during task breaks. This significantly shortens recharging time and ensures the all-weather, high-frequency deployment of the expulsion vehicle.

[0089] Furthermore, to address the challenge of instantaneous high-rate discharge caused by the simultaneous activation of multiple high-power suppression loads (such as microwaves and lasers), the quick-release battery pack 121 integrates a unified cooling system and incorporates a thermal runaway management system. This management system can monitor the temperature rise and voltage status of each cell group in real time. Upon detecting an abnormal thermal surge, it can instantly cut off the high-power power supply circuit and force the cooling system to operate at full power, fundamentally ensuring the power supply reliability and physical safety of the entire vehicle under extreme suppression conditions.

[0090] The present invention has the following beneficial effects: First, this invention significantly reduces the risk of electromagnetic interference between onboard equipment by constructing a three-zone physical architecture on the vehicle body, longitudinally divided into a front sensing zone, a middle processing zone, and a rear processing zone, and by installing metal isolation ribs and shielded cable trays. This hardware-level spatial isolation and electromagnetic protection structure allows the high-power jamming antenna in the rear zone to effectively avoid the "blinding" effect on the radar echo receiving link in the front sensing zone when performing suppression tasks, thereby ensuring the stability of the situational awareness of the vehicle throughout the entire mission cycle.

[0091] Secondly, by introducing a standardized quick-release base and a three-layer heterogeneous sensing hardware cluster, this invention effectively overcomes the shortcomings of traditional equipment, such as poor scalability and large detection blind spots. The three-layer sensing sub-modules (far, medium, and near range) can accurately cover the full range of needs, from large-scale early warning to close-range detail identification. Simultaneously, the quick-release base supports rapid plug-and-play replacement of different physical loads, such as interception net capture modules and high-power microwave heating modules, enabling a single vehicle to flexibly configure corresponding strike hardware for different types of low-altitude intrusions, significantly improving the system's scenario adaptability and equipment utilization.

[0092] Furthermore, this invention effectively mitigates power supply and timing crises in multi-target concurrent scenarios by incorporating an anti-collision hardware scheduling strategy within the central processing unit. This strategy allocates expulsion hardware with different spatial orientations based on the priority of the targets and strictly adheres to the power-on sequence of activating audible and visual warnings first, followed by activating high-power suppression, preventing system downtime caused by the simultaneous activation of high-load devices throughout the vehicle and ensuring the reliability of collaborative operation of complex electromechanical systems.

[0093] Finally, this invention achieves a highly efficient closed loop from target detection to differentiated handling through deep collaboration between multi-source sensing hardware and electromechanical actuators. Relying on the spatial mobility of the automatic lifting mast and the second robotic arm, various deflection hardware components can be safely stored in non-missionary states and can quickly extend and accurately point to the target according to sensing commands in mission states. Combined with the high mobility of the chassis, this breaks through the geographical limitations of traditional fixed defense lines, thereby effectively enhancing the comprehensive security level of the airport's low-altitude area.

[0094] The embodiments described above are merely further illustrations of the present invention and are not intended to limit the present invention in any other way. The present invention may have many other embodiments. Without departing from the spirit and essence of the present invention, those skilled in the art can make various corresponding modifications and changes based on the present invention, but all such modifications and changes should fall within the protection scope of the present invention.

Claims

1. A multi-functional air defense vehicle based on zoned isolation, characterized in that, It includes an autonomous driving chassis with dual modes of autonomous driving and manual takeover, and a vehicle body installed on the chassis. The top of the vehicle body is divided into a front perception area, a middle processing area and a rear processing area in a longitudinal space. A manned driver's cab is provided at the front of the vehicle body. The driver's cab is equipped with a personnel electromagnetic shielding structure to block high-power electromagnetic radiation. Multi-source sensing hardware group: physically deployed in the front sensing area, including a phased array radar installed on the top of the lifting mast, a polarized lidar installed on the rotating gimbal, and an ultra-high-definition zoom camera installed on the fixed base on the vehicle roof. Central processing unit: Physically deployed in the central processing area, the central processing unit is covered by a metal shielding shell, and the internal signal cable trays are connected to the power cable trays through physically separated cable trays; Integrated expulsion hardware group: Physically deployed in the post-processing area, it adopts a clustered arrangement, including an acoustic transmitter array, a multi-level laser transmitter, and an interference transmitting antenna installed on the second robotic arm; Physical isolation module: Deployed between the front sensing area and the rear processing area, including a metal isolation rib plate vertically fixed between the jamming transmitting antenna and the phased array radar. The height of the metal isolation rib plate is determined according to the half wavelength corresponding to the lower limit frequency of the jamming transmitting antenna's operating frequency band, and is not less than half of the transmitting aperture. The central processing unit is configured with hardware anti-collision scheduling logic, including: in a multi-target intrusion scenario, based on the threat score and current location of each target, controlling different handling hardware to physically point at different spatial targets, and executing the following timing control: prioritizing the activation of the acoustic transmitter array to issue an acoustic warning to the first threat target; if the target threat is not eliminated after the warning has lasted for a preset time, activating the multi-level laser transmitter or the jamming transmitting antenna to suppress the target, and at the same time only outputting a full-power drive signal to one expulsion hardware.

2. The multi-functional air defense vehicle based on zoned isolation according to claim 1, characterized in that, The sensing hardware in the front sensing area adopts a gradient space layout: The far-field sensing submodule includes the phased array radar and wide-angle infrared scanner for wide-area search of targets at the first distance. The mid-level sensing submodule includes the polarization lidar and mid-wave infrared thermal imager, used for feature extraction of targets at the second distance; Near-field perception submodule: includes the ultra-high-definition zoom camera, ultraviolet flame detector and radio direction finding array, used for detailed identification of targets at third distance.

3. The multi-functional air defense vehicle based on zoned isolation according to claim 2, characterized in that, The phased array radar has a specific anti-interference mounting structure: the radar is installed in a first robotic arm with a multi-degree-of-freedom joint design. The first robotic arm achieves flexible adjustment in three dimensions (front, back, left, right, and up and down) through built-in joint drive, and is internally equipped with a sealed wiring cavity to accommodate power supply and signal wires.

4. The multi-functional air defense vehicle based on zoned isolation according to claim 1, characterized in that, The electromagnetic compatibility structure of the intermediate processing area is as follows: the signal cable tray is covered with a metal braided mesh shielding tube throughout, and the physical distance between the signal cable tray and the power cable tray inside the vehicle body is maintained at a certain distance.

5. The multi-functional air defense vehicle based on zoned isolation according to claim 1, characterized in that, The hardware connection of the post-processing area includes a shock-absorbing and stabilizing platform: the base of the multi-level laser emitter is connected to the vehicle body through a steel wire rope shock absorber; the acoustic transmitter array is fixed by a flexible suspension structure to isolate the mechanical resonance caused by the vehicle's movement.

6. The multi-functional air defense vehicle based on zoned isolation according to claim 1, characterized in that, The expulsion device in the post-processing area has a telescopic storage function: the bottom of the multi-stage laser emitter is connected to an automatic lifting mechanism, which is configured to be stored within the outline of the top of the vehicle body when not in mission mode, and to be raised and expose the emission aperture when in mission mode.

7. The multi-functional air defense vehicle based on zoned isolation according to claim 1, characterized in that, The post-processing area is also equipped with a standardized quick-release base: the standardized quick-release base integrates a power supply copper bus, a high-speed data bus interface and mechanical positioning pin holes, for plug-and-play replacement of different physical impact modules.

8. The multi-functional air defense vehicle based on zoned isolation according to claim 7, characterized in that, The quick-release base supports the expansion installation of any of the following modules: Interception net capture module: Net gun mechanism driven by compressed air or gunpowder; High-power microwave heating module: Equipped with a microwave emitting array, used to generate a thermal effect on metal-coated balloons; Evidence collection lighting composite module: integrates a high-magnification zoom camera and a high-power LED array light.

9. The multi-functional air defense vehicle based on zoned isolation according to claim 1, characterized in that, The central processing unit is equipped with hardware anti-collision scheduling logic: in a multi-target intrusion scenario, the central processing unit controls different processing hardware to physically point to different spatial targets, and forces the execution of a hardware power-on sequence that first activates acoustic warnings and then activates high-power electromagnetic or laser suppression.

10. The multi-functional air defense vehicle based on zoned isolation according to claim 1, characterized in that, The chassis is equipped with a power battery system that supports fast charging and features a quick-release battery pack. The battery pack integrates a liquid / air cooling system and a thermal runaway management system.

11. The multi-functional air defense vehicle based on partitioned isolation according to claim 1, characterized in that, The electromagnetic shielding structure for personnel in the cockpit includes: an observation window with an embedded metal shielding mesh, a conductive wave-absorbing coating applied to the surface of the cabin, and a conductive sealing structure located at the seam of the cabin door.

12. An integrated hardware collaboration method for a multi-functional air defense destroyer based on partitioned isolation as described in any one of claims 1 to 11, characterized in that, Including the following steps: S1: The autonomous driving chassis performs patrols, acquiring target feature data through the lifting mast, rotating gimbal, and sensing hardware group on the fixed base within the perception area; S2: The central processing unit in the middle processing area classifies and interprets the feature data, and generates hardware scheduling instructions based on the target's threat score and current location; S3: The second robotic arm or automatic lifting mechanism in the post-processing area moves to drive the corresponding expulsion hardware to align with the target. When performing physical expulsion or suppression actions, it strictly follows the sequence of prioritizing acoustic warnings and then suppressing the target after the warnings are ineffective. At the same time, it only outputs a full-power drive signal to one expulsion hardware.

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