Net unmanned equipment load and control method

Abstract

The invention discloses a sheet net unmanned equipment load and a control method, and relates to the technical field of unmanned equipment counteracting, the sheet net unmanned equipment load comprises a main body frame structure, a plurality of ejection type killing units and a killing control unit, and the main body frame structure is provided with a plurality of killing unit mounting inner cavities; the multiple ejection type killing units are installed in the multiple killing unit installation inner cavities correspondingly, and each ejection type killing unit comprises an internal ejection driving part, a traction part and a net warhead part. The sheet net unmanned equipment load is mainly used for unmanned equipment countering, when the internal ejection driving part is started, the sheet net warhead part is driven to eject outwards out of the killing unit mounting inner cavity, the sheet net warhead part ejects out and is combined with the traction part to form killing power on an aircraft in a covered area, and the sheet net warhead part is used for a small unmanned equipment target. Compared with a traditional warhead, the warhead has a stronger structural destructive effect on fuselages, wings, paddles and the like of small unmanned equipment made of high polymer materials such as aluminum alloy, carbon fibers, composite materials and resin plastics.

Description

Technical Field

[0001] The present invention relates to the technical field of unmanned equipment countermeasures, and in particular to a sheet network unmanned equipment load and a control method. Background Art

[0002] Human-machine countermeasures include detection, tracking, identification, and countermeasures. These technologies are mainly used in military and civilian fields to mitigate the potential risks posed by drones. There are many anti-drone systems on the market, involving sensor technologies such as radar, optoelectronics, and thermal imaging, as well as active intervention technologies such as electromagnetic interference, laser systems, and radio frequency interference.

[0003] Unmanned equipment countermeasure technology has important applications in both defense and civilian fields. For example, in the low-altitude economic and military development, anti-drone technology is becoming increasingly important. With the widespread application of drone technology, anti-drone technology has also become an important part of national security and battlefield situation.

[0004] Modern anti-drone systems combine communication technology and artificial intelligence. This includes high-speed data transmission, signal coverage, high-precision positioning, dynamic frequency switching, wide bandwidth and multiple-input multiple-output (MIMO) technology. Artificial intelligence technology has also achieved remarkable results in improving the effectiveness of anti-drone, including autonomous learning, confrontational games and multi-agent collaboration.

[0005] Although anti-unmanned equipment technology has made progress, it still has limitations. Unmanned equipment anti-jamming equipment is not effective against some drones with strong anti-jamming capabilities. Summary of the invention

[0006] In order to solve the problems of existing anti-unmanned equipment technology, the present invention provides a network of unmanned equipment load and control method. The following technical solutions are adopted:

[0007] A sheet net unmanned equipment load comprises a main frame structure, a plurality of ejection-type killing units and a killing control unit, wherein the main frame structure is provided with a plurality of killing unit installation cavities, wherein the plurality of ejection-type killing units are respectively installed in the plurality of killing unit installation cavities, wherein the ejection-type killing unit comprises an internal ejection drive unit, a traction unit and a sheet net warhead, wherein the internal ejection drive unit is installed in the killing unit installation cavity, wherein the traction unit is located in the killing unit installation cavity, wherein the sheet net warhead is connected and installed at the end of the traction unit, wherein the killing control unit respectively controls the execution actions of the plurality of ejection-type killing units, wherein when the internal ejection drive unit is turned on, the sheet net warhead is driven to eject outward from the killing unit installation cavity, and after the sheet net warhead is ejected, it combines with the traction unit to form a killing force on the aircraft in the covered area;

[0008] The killing control unit includes a communication module, an instruction memory and a control chip. The communication module is used to receive external control instructions, the instruction memory is communicatively connected to the communication module, and the control chip is communicatively connected to the instruction memory. Based on the external control instructions, the execution actions of the internal ejection drive units of multiple ejection-type killing units are controlled respectively.

[0009] By adopting the above technical solution, the unmanned equipment payload of the network can be mounted on the bottom of the aircraft through a mounting structure or a tethered rope structure. When arriving at the designated mission area, the communication module of the kill control unit receives the external command signal. The kill control unit here should also consider the risk of false control signals in specific applications. A strong encryption algorithm can be used to encrypt the transmitted instructions to ensure that only the system with the correct key can decrypt and execute these instructions. This can effectively prevent unauthorized third parties from forging or tampering with instructions. Implement identity authentication and message authentication to ensure that the instructions come from a trusted and authenticated command node. This can be achieved through digital signatures, certificates or other authentication protocols. Instructions are received through independent, multi-channel communication lines. If the instructions of one channel are inconsistent with the instructions of other channels, the system can issue a warning or refuse to execute.

[0010] When the external control instruction is judged to be credible, the control chip controls the execution actions of the internal ejection drive units of multiple ejection kill units respectively. The ejection action can be executed by all ejection kill units at the same time, or by the ejection kill unit with a specified number, which can adapt to the killing needs of various aircraft.

[0011] The sheet-net unmanned equipment payload is mainly used for countering unmanned equipment. When the internal ejection drive unit is turned on, the sheet-net warhead is driven to pop out of the killing unit installation cavity. The sheet-net warhead pop-up and the traction unit combination form lethality to the aircraft in the covered area. The sheet-net warhead has a stronger structural destructive effect on small unmanned equipment targets, and on small unmanned equipment fuselages, wings, blades, etc. made of polymer materials such as aluminum alloy, carbon fiber, composite materials, resin plastics, etc. than traditional warheads.

[0012] Optionally, the main frame structure includes a main skeleton and multiple killing unit cavities, the multiple killing unit cavities are respectively installed on the main skeleton, and the killing unit cavities are provided with a killing unit installation inner cavity.

[0013] By adopting the above technical solution, the main skeleton structure can be made of lightweight and high-strength aluminum alloy material, and multiple killing unit cavities can be made of high-strength aluminum alloy material. The shape can be cylindrical or square cylindrical, and can be installed in the installation space reserved in the main skeleton by welding.

[0014] Optionally, the main frame structure is a sphere, a hemisphere or other shapes.

[0015] By adopting the above technical solution, the main frame structure can be a sphere, which can provide omnidirectional killing, or a hemispherical or other shape, which can achieve directional killing.

[0016] Optionally, the internal ejection drive unit is a controllable explosive device, which includes explosives and an electronically controlled ignition device, wherein the electronically controlled ignition device is used to detonate the explosives, and the killing control unit controls the execution action of the electronically controlled ignition device.

[0017] By adopting the above technical solution, the controllable explosive device can be an explosive structure similar to an aviation weapon delivery device, and the thrust generated by the explosion can quickly push the traction part and the web warhead out of the killing unit cavity.

[0018] Optionally, the internal ejection drive unit includes a high-pressure gas chamber and an electrically controlled valve, wherein the electrically controlled valve controls the opening and closing of the injection port of the high-pressure gas chamber, and the killing control unit controls the execution action of the electrically controlled valve.

[0019] By adopting the above technical solution, compressed gas is stored in the high-pressure gas chamber. Under the control of the electric control valve, the injection port of the compressed gas is opened, and the high-pressure gas ejected from the injection port can quickly push the traction part and the sheet-net warhead out of the killing unit cavity.

[0020] Optionally, the internal ejection drive unit is an elastic energy storage device, which includes an elastic member and an elastic member controller, wherein the elastic member controller is used to control the extension of the telescopic portion of the elastic member, and the killing control unit controls the execution action of the elastic member controller.

[0021] By adopting the above technical solution, the elastic energy storage device can be an electrically controlled spring or an elastic energy accumulator, etc., which can quickly push the traction part and the sheet-net warhead out of the killing unit cavity under the control of the elastic part controller. Quickly push the traction part and the sheet-net warhead out of the killing unit cavity.

[0022] Optionally, the traction part is a net rope woven from multiple ropes made of high-strength and high-toughness material, and the high-strength and high-toughness material refers to Kevlar material or carbon fiber.

[0023] By adopting the above technical solution, the function of the traction part is to open under the action of traction when the sheet-net warhead is ejected, and form a killing network with the sheet-net warhead, which can greatly increase the killing area of ​​the sheet-net warhead.

[0024] Optionally, one side of the sheet-net warhead is connected to the traction part, and when the internal ejection drive part is in an unfired state, the sheet-net warhead is snapped into the opening of the killing unit installation cavity, and the sheet-net warhead and the main frame structure form a complete sphere or hemisphere.

[0025] By adopting the above technical solution, the sheet-net warhead can be a ball, sheet or other object with a certain weight. When the ejection drive unit is in an unfired state, the sheet-net warhead and the main frame structure form a complete sphere or hemisphere, which can reduce the wind resistance of the sheet-net unmanned equipment load when it is mounted.

[0026] Optionally, the sheet-net warhead includes a connecting plate, multiple spring rods and an outer combat plate, one side of the connecting plate is connected to the traction part, one end of the multiple spring rods is connected and installed on the other side of the connecting plate, and the outer combat plate is connected to the other end of the multiple spring rods. When the internal ejection drive part is in an unfired state, the outer side of the outer combat plate is bonded to the opening of the killing unit installation cavity, and the multiple spring rods are in a compressed state.

[0027] When the internal ejection drive unit is fired, the connection between the outer combat plate and the inner cavity of the killing unit installation is destroyed by the impact, the web warhead is ejected, multiple spring rods return to their original state, and the outer combat plate is separated from the connecting plate.

[0028] By adopting the above technical solution, the sheet-net warhead adopts two sheet-shaped warheads, the connecting plate is the connecting part and also the first warhead, and the outer combat plate is connected to the connecting plate by multiple spring rods. When the internal ejection drive unit is in an unfired state, the multiple spring rods are in a compressed state, and the outer side of the outer combat plate is bonded to the open part of the killing unit installation cavity to form a whole on the outside. When the internal ejection drive unit is fired, the sheet-net warhead is subjected to the internal impact force, which will quickly separate the outer combat plate from the connecting plate, and then the sheet-net warhead pops out, and the multiple spring rods return to their original state, and the outer combat plate is separated from the connecting plate to form a larger killing area. In addition, due to the multiple spring rods, the entire sheet-net warhead will experience regional shaking, reducing the possibility of smaller aircraft drilling through the gap.

[0029] A control method for a sheet network unmanned equipment load is used to control a sheet network unmanned equipment load, install the sheet network unmanned equipment load on a load mounting part of an aircraft, and establish a wireless communication connection between a communication module of a kill control unit and a flight control system of the aircraft;

[0030] When it is determined that the aircraft has flown to the mission coordinates, the flight control system sends external control instructions to the communication module. The external control instructions include the ejected sheet-net warhead number and the ejection instruction. The external control instructions of the control chip respectively control the internal ejection drive unit of the corresponding numbered sheet-net warhead to start, and the corresponding numbered sheet-net warhead is ejected outward from the killing unit installation cavity. The sheet-net warhead and the traction unit are combined to form a killing net that has a lethal force on the aircraft in the covered area.

[0031] In summary, the present invention includes at least one of the following beneficial technical effects:

[0032] The present invention can provide a sheet-net unmanned equipment payload and control method. When the sheet-net unmanned equipment payload reaches the designated mission area, the communication module of the kill control unit receives an external command signal, and the control chip of the kill control unit respectively controls the execution actions of the internal ejection drive parts of multiple ejection-type kill units. The ejection action can be executed by all ejection-type kill units at the same time, or by ejection-type kill units with designated numbers, which can adapt to the killing needs of various aircraft.

[0033] The sheet-net unmanned equipment payload is mainly used for countering unmanned equipment. When the internal ejection drive unit is turned on, the sheet-net warhead is driven to pop out of the killing unit installation cavity. The sheet-net warhead pop-up and the traction unit combination form lethality to the aircraft in the covered area. The sheet-net warhead has a stronger structural destructive effect on small unmanned equipment targets, and on small unmanned equipment fuselages, wings, blades, etc. made of polymer materials such as aluminum alloy, carbon fiber, composite materials, resin plastics, etc. than traditional warheads. BRIEF DESCRIPTION OF THE DRAWINGS

[0034] Figure 1 It is a schematic diagram of the structural principle of the sheet net warheads on both sides of the sheet net unmanned equipment load in the present invention in the ejection state;

[0035] Figure 2 It is a schematic diagram of the structural principle of a sheet net unmanned equipment payload sheet net warhead in a non-ejected state of the present invention;

[0036] Figure 3 This is a schematic diagram of the main frame structure principle of a sheet network unmanned equipment load of the present invention;

[0037] Figure 4 It is a schematic diagram of the structural principle of a single sheet-net warhead of a sheet-net unmanned equipment payload of the present invention in a non-ejected state;

[0038] Figure 5 It is a schematic diagram of the structural principle of a sheet-net unmanned equipment payload of the present invention in a single sheet-net warhead ejection state;

[0039] Figure 6 It is a schematic diagram of the structural principle of a sheet-net warhead of a sheet-net unmanned equipment payload of the present invention;

[0040] Figure 7 It is a schematic diagram of the structural principle of a sheet net unmanned equipment load sheet net hung on the payload part of an unmanned aerial vehicle according to the present invention;

[0041] Figure 8 It is a schematic diagram of the communication connection between a killing control unit of a sheet network unmanned equipment payload and a UAV flight control system of the present invention.

[0042] Explanation of the reference numerals: 1. Main frame structure; 11. Main skeleton; 12. Kill unit cavity; 21. Internal ejection drive unit; 22. Traction unit; 23. Sheet-net warhead; 231. Connecting plate; 232. Spring rod; 233. External combat plate; 31. Communication module; 32. Instruction memory; 33. Control chip; 100. Kill unit installation cavity; 101. Flight control system. DETAILED DESCRIPTION

[0043] The present invention is further described in detail below in conjunction with the accompanying drawings.

[0044] The embodiment of the present invention discloses a sheet network unmanned equipment load and a control method.

[0045] Reference Figure 1-Figure 8 Embodiment 1: A sheet net unmanned equipment load comprises a main frame structure 1, a plurality of ejection killing units and a killing control unit. The main frame structure 1 is provided with a plurality of killing unit installation cavities 100. The plurality of ejection killing units are respectively installed in the plurality of killing unit installation cavities 100. The ejection killing unit comprises an internal ejection driving unit 21, a traction unit 22 and a sheet net warhead 23. The internal ejection driving unit 21 is installed in the killing unit installation cavity 100. The traction unit 22 is located in the killing unit installation cavity 100. The sheet net warhead 23 is connected and installed at the end of the traction unit 22. The killing control unit controls the execution actions of the plurality of ejection killing units respectively. When the internal ejection driving unit 21 is turned on, the sheet net warhead 23 is driven to eject out of the killing unit installation cavity 100. After the sheet net warhead 23 is ejected, it combines with the traction unit 22 to form a lethal force on the aircraft in the covered area.

[0046] The killing control unit includes a communication module 31, an instruction memory 32 and a control chip 33. The communication module 31 is used to receive external control instructions, the instruction memory 32 is communicatively connected to the communication module 31, and the control chip 33 is communicatively connected to the instruction memory 32. Based on the external control instructions, the execution actions of the internal ejection drive units 21 of multiple ejection-type killing units are controlled respectively.

[0047] The unmanned equipment payload of the sheet network can be mounted on the bottom of the aircraft through a mounting structure or a tethered rope structure. When arriving at the designated mission area, the communication module 31 of the kill control unit receives the external command signal, which can be wired communication or wireless communication. The kill control unit here should also consider the risk of false control signals in specific applications. A strong encryption algorithm can be used to encrypt the transmitted instructions to ensure that only the system with the correct key can decrypt and execute these instructions. This can effectively prevent unauthorized third parties from forging or tampering with instructions. Implement identity authentication and message authentication to ensure that the instructions come from a trusted and authenticated command node. This can be achieved through digital signatures, certificates or other authentication protocols. Instructions are received through independent, multi-channel communication lines. If the instructions of one channel are inconsistent with the instructions of other channels, the system can issue a warning or refuse to execute.

[0048] When it is determined that the external control instruction is credible, the control chip 33 controls the execution actions of the internal ejection drive units 21 of multiple ejection-type killing units respectively. The ejection action can be executed by all ejection-type killing units at the same time, or by an ejection-type killing unit with a specified number, which can adapt to the killing needs of various aircraft.

[0049] The sheet-net unmanned equipment payload is mainly used for countering unmanned equipment. When the internal ejection drive unit 21 is turned on, the sheet-net warhead 23 is driven to pop out of the killing unit installation cavity 100. The sheet-net warhead 23 is popped out and combined with the traction unit 22 to form lethality to the aircraft in the covered area. The sheet-net warhead 23 has a stronger structural destructive effect than traditional warheads on small unmanned equipment targets, and on small unmanned equipment fuselages, wings, blades, etc. made of polymer materials such as aluminum alloy, carbon fiber, composite materials, resin plastics, etc.

[0050] In embodiment 2, the main frame structure 1 includes a main skeleton 11 and a plurality of killing unit cavities 12 . The plurality of killing unit cavities 12 are respectively installed on the main skeleton 11 . The killing unit cavities 12 are provided with a killing unit installation inner cavity 100 .

[0051] The main frame 11 structure can be made of lightweight and high-strength aluminum alloy material, and multiple killing unit cavities 12 can be made of high-strength aluminum alloy material. The shape can be cylindrical or square cylindrical, and can be installed in the installation space reserved in the main frame 11 by welding.

[0052] Embodiment 3, the main frame structure is a sphere, a hemisphere or other shapes.

[0053] The main frame structure can be a sphere, which can provide omnidirectional killing, or a hemispherical or other shape, which can achieve directional killing.

[0054] In the fourth embodiment, the internal ejection drive unit 21 is a controllable explosive device, which includes explosives and an electronically controlled ignition device. The electronically controlled ignition device is used to detonate the explosives, and the killing control unit controls the execution of the electronically controlled ignition device.

[0055] The controllable explosive device may be an explosive structure similar to an aviation weapon delivery device, and the thrust generated by the explosion can quickly push the traction part 22 and the sheet-net warhead 23 out of the killing unit cavity 12.

[0056] Embodiment 5, the internal ejection drive unit 21 includes a high-pressure gas chamber and an electrically controlled valve, the electrically controlled valve controls the switch of the injection port of the high-pressure gas chamber, and the killing control unit controls the execution action of the electrically controlled valve.

[0057] Compressed gas is stored in the high-pressure gas chamber. Under the control of the electric control valve, the injection port of the compressed gas is opened, and the high-pressure gas ejected from the injection port can quickly push the traction part 22 and the sheet-net warhead 23 out of the killing unit cavity 12.

[0058] In Embodiment 6, the internal ejection drive unit 21 is an elastic energy storage device, which includes an elastic member and an elastic member controller. The elastic member controller is used to control the extension of the telescopic portion of the elastic member, and the killing control unit controls the execution action of the elastic member controller.

[0059] The elastic energy storage device can be an electrically controlled spring or an elastic energy accumulator, etc., which can quickly push the traction part 22 and the sheet-net warhead 23 out of the killing unit cavity 12 under the control of the elastic part controller.

[0060] In Embodiment 7, the traction part 22 is a net rope woven from a plurality of ropes made of a high-strength and high-toughness material, and the high-strength and high-toughness material refers to Kevlar material or carbon fiber.

[0061] The function of the traction part 22 is to open under the action of traction when the sheet-net warhead 23 is ejected, and form a killing network with the sheet-net warhead 23, which can greatly increase the killing area of ​​the sheet-net warhead 23.

[0062] Embodiment 8, one side of the sheet-net warhead 23 is connected to the traction part 22, when the internal ejection drive part 21 is in an unfired state, the sheet-net warhead 23 is buckled into the open part of the killing unit installation cavity 100, and the sheet-net warhead 23 and the main frame structure 1 form a complete sphere or hemisphere.

[0063] The sheet-net warhead 23 can be a ball, sheet or other object with a certain weight. When the ejection drive unit 21 is in an unfired state, the sheet-net warhead 23 and the main frame structure 1 form a complete sphere or hemisphere, which can reduce the wind resistance of the sheet-net unmanned equipment load when it is mounted.

[0064] Example 9, the sheet-net warhead 23 includes a connecting plate 231, a plurality of spring rods 232 and an outer combat plate 233, one side of the connecting plate 231 is connected to the traction part 22, one end of the plurality of spring rods 232 is connected and installed on the other side of the connecting plate 231, and the outer combat plate 233 is connected to the other end of the plurality of spring rods 232. When the internal ejection drive part 21 is in an unfired state, the outer side of the outer combat plate 233 is bonded to the open part of the killing unit installation cavity 100, and the plurality of spring rods 232 are in a compressed state.

[0065] When the internal ejection drive unit 21 is fired, the connection between the outer combat plate 233 and the killing unit installation cavity 100 is destroyed by the impact, the sheet-net warhead 23 is ejected, the multiple spring rods 232 return to their original state, and the outer combat plate 233 is separated from the connecting plate 231.

[0066] The sheet-net warhead 23 uses two sheet-shaped warheads, the connecting plate 231 is the connecting part and also the first warhead, and the outer combat plate 233 is connected to the connecting plate 231 by multiple spring rods 232. When the internal ejection drive unit 21 is in an unfired state, the multiple spring rods 232 are in a compressed state, and the outer side of the outer combat plate 233 is bonded to the open part of the killing unit installation cavity 100 to form a whole on the outside. When the internal ejection drive unit 21 is fired, the sheet-net warhead 23 is subjected to the internal impact force, which will quickly separate the outer combat plate 233 from the connecting plate 231, and then the sheet-net warhead 23 is ejected, and the multiple spring rods 232 return to their original state, and the outer combat plate 233 is separated from the connecting plate 231 to form a larger killing area. In addition, due to the multiple spring rods 232, the entire sheet-net warhead 23 will have regional shaking, reducing the possibility of smaller aircraft drilling through the gap.

[0067] Embodiment 10, a control method for a web-based unmanned equipment payload, for controlling a web-based unmanned equipment payload, installing the web-based unmanned equipment payload on a payload mounting portion of an aircraft, and establishing a wireless communication connection between a communication module 31 of a kill control unit and a flight control system 101 of the aircraft;

[0068] When it is determined that the aircraft has flown to the mission coordinates, the flight control system 101 sends an external control instruction to the communication module 31. The external control instruction includes the number of the pop-up sheet net warhead 23 and the pop-up instruction. The external control instruction of the control chip 33 controls the internal ejection drive unit 21 of the corresponding numbered sheet net warhead 23 to start, and the corresponding numbered sheet net warhead 23 pops outward from the killing unit installation cavity 100. The sheet net warhead 23 and the traction part 22 are combined to form a killing net to form a lethal force on the aircraft in the covered area.

[0069] The above are all preferred embodiments of the present invention, and are not intended to limit the protection scope of the present invention. Therefore, any equivalent changes made based on the structure, shape, and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. A sheet network unmanned equipment payload, characterized by: The invention comprises a main frame structure (1), a plurality of ejection-type killing units and a killing control unit. The main frame structure (1) is provided with a plurality of killing unit installation cavities (100). The plurality of ejection-type killing units are respectively installed in the plurality of killing unit installation cavities (100). The ejection-type killing unit comprises an internal ejection drive unit (21), a traction unit (22) and a sheet-net warhead (23). The internal ejection drive unit (21) is installed in the killing unit installation cavity (100). The traction unit (22) is located in the killing unit installation cavity (100). The sheet-net warhead (23) is connected and installed at the end of the traction unit (22). The killing control unit controls the execution actions of the plurality of ejection-type killing units respectively. When the internal ejection drive unit (21) is turned on, the sheet-net warhead (23) is driven to eject outward from the killing unit installation cavity (100). After the sheet-net warhead (23) ejects, it combines with the traction unit (22) to form a killing force on the aircraft in the covered area. The killing control unit comprises a communication module (31), an instruction memory (32) and a control chip (33), wherein the communication module (31) is used to receive external control instructions, the instruction memory (32) is communicatively connected to the communication module (31), and the control chip (33) is communicatively connected to the instruction memory (32), and the execution actions of the internal ejection drive units (21) of the plurality of ejection-type killing units are respectively controlled based on the external control instructions.

2. A sheet network unmanned equipment payload according to claim 1, characterized in that: The main frame structure (1) comprises a main frame (11) and a plurality of killing unit cavities (12); the plurality of killing unit cavities (12) are respectively mounted on the main frame (11); and the killing unit cavities (12) are provided with a killing unit mounting inner cavity (100).

3. The sheet network unmanned equipment payload according to claim 1, characterized in that: The internal ejection drive unit (21) is a controllable explosive device, which comprises explosives and an electric-controlled ignition device, wherein the electric-controlled ignition device is used to detonate the explosives, and the killing control unit controls the execution action of the electric-controlled ignition device.

4. The sheet network unmanned equipment payload according to claim 1, characterized in that: The internal ejection drive unit (21) comprises a high-pressure gas chamber and an electric control valve, wherein the electric control valve controls the opening and closing of the ejection port of the high-pressure gas chamber, and the killing control unit controls the execution action of the electric control valve.

5. The sheet network unmanned equipment payload according to claim 1, characterized in that: The internal ejection drive unit (21) is an elastic energy storage device, which comprises an elastic member and an elastic member controller. The elastic member controller is used to control the extension of the telescopic part of the elastic member, and the killing control unit controls the execution action of the elastic member controller.

6. The sheet network unmanned equipment payload according to claim 1, characterized in that: The traction part (22) is a net rope woven from a plurality of ropes made of a high-strength and high-toughness material, wherein the high-strength and high-toughness material refers to a Kevlar material or a carbon fiber.

7. The sheet network unmanned equipment payload according to claim 1, characterized in that: One side of the web warhead (23) is connected to the traction part (22), and when the internal ejection drive part (21) is in an unfired state, the web warhead (23) is buckled into the open portion of the killing unit installation cavity (100).

8. The sheet network unmanned equipment payload according to claim 1, characterized in that: The web warhead (23) comprises a connecting plate (231), a plurality of spring rods (232) and an outer combat plate (233), one side of the connecting plate (231) is connected to the traction part (22), one end of the plurality of spring rods (232) is connected and installed on the other side of the connecting plate (231), and the outer combat plate (233) is connected to the other end of the plurality of spring rods (232). When the internal ejection drive part (21) is in an unfired state, the outer side of the outer combat plate (233) is bonded to the open part of the killing unit installation cavity (100), and the plurality of spring rods (232) are in a compressed state. When the internal ejection drive unit (21) is fired, the connection between the outer combat plate (233) and the killing unit installation cavity (100) is destroyed by the impact, the web warhead (23) is ejected, the plurality of spring rods (232) return to their original state, and the outer combat plate (233) is separated from the connecting plate (231).

9. A method for controlling the load of unmanned equipment in a network, characterized in that: Used to control a web-based unmanned equipment payload as described in any one of claims 1 to 8, install the web-based unmanned equipment payload on a payload mounting portion of an aircraft, and establish a wireless communication connection between a communication module (31) of a kill control unit and a flight control system (101) of the aircraft; When it is determined that the aircraft has flown to the mission coordinates, the flight control system (101) sends an external control instruction to the communication module (31), the external control instruction including the number of the ejected sheet net warhead (23) and the ejection instruction, the control chip (33) controls the internal ejection drive unit (21) of the corresponding numbered sheet net warhead (23) to start, the corresponding numbered sheet net warhead (23) ejects outward from the killing unit installation cavity (100), and the sheet net warhead (23) and the traction unit (22) are combined to form a killing net to form a killing force on the aircraft in the covered area.

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