A sheet web unmanned equipment load and control method

Abstract

The application discloses a kind of sheet net unmanned equipment load and control method, it is related to unmanned equipment countermeasure technical field, including main frame structure, multiple ejection type killing units and killing control unit, main frame structure is provided with multiple killing unit installation inner cavity, multiple ejection type killing units are respectively installed in multiple killing unit installation inner cavity, ejection type killing unit includes internal ejection drive part, traction part and sheet net warhead.The present application sheet net unmanned equipment load is mainly used for unmanned equipment countermeasure, when internal ejection drive part is opened, drive sheet net warhead and eject killing unit installation inner cavity, sheet net warhead ejects and traction part combination to the aircraft of the covered area forms killing power, sheet net warhead for small unmanned equipment target, for aluminum alloy, carbon fiber, composite material, resin plastic and other polymer materials made small unmanned equipment fuselage, wing, paddle etc., have stronger structural damage effect compared with traditional warhead.

Description

TECHNICAL FIELD

[0001] The present application relates to the field of unmanned equipment countermeasure technology, and in particular to a sheet net unmanned equipment load and control method. BACKGROUND

[0002] Unmanned aircraft countermeasure technology includes detection, tracking, identification, and countermeasure measures. These technologies are mainly used in military and civilian fields to mitigate potential risks posed by unmanned aircraft. There are various anti-unmanned aircraft systems on the market, involving radar, photoelectric, thermal imaging, and other sensor technologies, 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 low-altitude economic and military development, anti-unmanned aircraft technology is becoming increasingly important. As unmanned aircraft technology is widely used, anti-unmanned aircraft technology has become an important part of national security and battlefield situation.

[0004] Modern anti-unmanned aircraft systems combine communication technology and artificial intelligence. This includes high-speed data transmission, signal coverage, high-precision positioning, dynamic frequency switching, wideband, and multiple-input multiple-output (MIMO) technology. Artificial intelligence technology has also made significant contributions to improving the effectiveness of anti-unmanned aircraft systems, including autonomous learning, adversarial games, and multi-agent collaboration.

[0005] Although anti-unmanned equipment technology has made progress, there are still limitations. Anti-unmanned equipment jamming devices are not stable for some anti-jamming unmanned aircraft. SUMMARY

[0006] To solve the problem of existing anti-unmanned equipment technology, the present application provides a sheet net unmanned equipment load and control method. The technical scheme adopted is as follows:

[0007] A sheet net unmanned equipment load includes a main frame structure, a plurality of ejection-type killing units, and a killing control unit. The main frame structure has a plurality of killing unit installation cavities, and the plurality of ejection-type killing units are installed in the killing unit installation cavities. The ejection-type killing unit includes an internal ejection drive part, a traction part, and a sheet net warhead. The internal ejection drive part is installed in the killing unit installation cavity, the traction part is located in the killing unit installation cavity, and the sheet net warhead is connected and installed at the end of the traction part. The killing control unit controls the execution action of the plurality of ejection-type killing units. When the internal ejection drive part is turned on, it drives the sheet net warhead to pop out of the killing unit installation cavity. After the sheet net warhead pops out, it combines with the traction part to form a killing force on the aircraft in the covered area.

[0008] The killing control unit comprises a communication module for receiving external control instructions, an instruction memory connected in communication with the communication module, and a control chip connected in communication with the instruction memory, which controls the execution of the internal ejection driving part of the plurality of ejection killing units based on the external control instructions.

[0009] By adopting the above technical solution, the sheet net unmanned equipment load can be mounted on the bottom of the aircraft through the mounting structure or the tethered rope structure. When reaching the designated task area, the communication module of the killing control unit receives external instruction signals. In specific applications, the risk of false control signals should also be considered. Strong encryption algorithms can be used to encrypt the transmitted instructions to ensure that only systems with the correct key can decrypt and execute these instructions. This can effectively prevent unauthorized third parties from falsifying 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. Receive instructions through independent, multi-channel communication lines. If the instructions from one channel are inconsistent with those from other channels, the system can issue a warning or refuse to execute.

[0010] When it is determined that the external control instruction is authentic, the control chip controls the execution of the internal ejection driving part of the plurality of ejection killing units. The execution of the ejection action can be simultaneous execution of all ejection killing units or execution of a specified number of ejection killing units, which can adapt to various aircraft killing requirements.

[0011] The sheet net unmanned equipment load is mainly used for unmanned equipment countermeasures. When the internal ejection driving part is turned on, the driving sheet net warhead ejects the killing unit installation inner cavity. The sheet net warhead ejects and combines with the traction part to form a killing force on the aircraft in the covered area. The sheet net warhead has a stronger structural damage effect on small unmanned equipment targets made of high molecular materials such as aluminum alloy, carbon fiber, composite material, and resin plastic.

[0012] Optionally, the main frame structure comprises a main skeleton and a plurality of killing unit cavities, the plurality of killing unit cavities are respectively mounted on the main skeleton, and the killing unit cavity is provided with a killing unit installation inner cavity.

[0013] By adopting the above technical solution, the main skeleton structure can be made of lightweight high-strength aluminum alloy material, and the plurality of 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 reserved mounting space of the main skeleton by welding.

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

[0015] By adopting the technical scheme, the main body frame structure can be a sphere, omnidirectional killing can be provided, or can be a hemisphere or other shape, and directional killing can be achieved.

[0016] Optionally, the internal ejection driving part is a controllable explosion device, the controllable explosion device comprises an explosive and an electric control ignition device, the electric control ignition device is used for detonating the explosive, and the killing control unit controls the execution action of the electric control ignition device.

[0017] By adopting the technical scheme, the controllable explosion device can be an explosion structure similar to an aerial weapon launching device, and the thrust generated by explosion can rapidly push the traction part and the sheet net warhead out of the killing unit cavity.

[0018] Optionally, the internal ejection driving part comprises a high-pressure gas cavity and an electric control valve, the electric control valve controls the opening and closing of a jet port of the high-pressure gas cavity, and the killing control unit controls the execution action of the electric control valve.

[0019] By adopting the technical scheme, compressed gas is stored in the high-pressure gas cavity, under the control of the electric control valve, the jet port of the compressed gas is opened, and the high-pressure gas sprayed out of the jet port can rapidly push the traction part and the sheet net warhead out of the killing unit cavity.

[0020] Optionally, the internal ejection driving part is an elastic energy storage device, the elastic energy storage device comprises an elastic member and an elastic member controller, the elastic member controller is used for controlling the extension of the elastic member, and the killing control unit controls the execution action of the elastic member controller.

[0021] By adopting the technical scheme, the elastic energy storage device can be an electric control spring or an elastic accumulator, etc., and under the control of the elastic member controller, the traction part and the sheet net warhead can be rapidly pushed out of the killing unit cavity.

[0022] Optionally, the traction part is a net rope woven by a plurality of 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 technical scheme, the traction part functions to be stretched under the traction force when the sheet net warhead is ejected, and forms a killing network with the sheet net warhead, so that the killing area of the sheet net warhead can be greatly improved.

[0024] Optionally, one side of the sheet net warhead is connected with the traction part, when the internal ejection driving part is in an uncocked state, the sheet net warhead is buckled at an open end of the killing unit installation inner cavity, and the sheet net warhead and the main body frame structure form a complete sphere or hemisphere.

[0025] By adopting the technical scheme, the slice net warhead can be a ball, a slice or other objects with a certain weight, when the main body is in an un-fired state, the slice net warhead and the main frame structure form a complete ball or a semi-ball, so that the wind resistance of the slice net unmanned equipment load during hanging is reduced.

[0026] Optionally, the slice net warhead comprises a connecting plate, a plurality of spring rods and an outer warhead plate, one side of the connecting plate is connected with the traction part, one end of the plurality of spring rods is connected and installed on the other side of the connecting plate, and the outer warhead plate is connected at the other end of the plurality of spring rods, when the internal ejection driving part is in an un-fired state, the outer side of the outer warhead plate is bonded with the open end of the killing unit installation inner cavity, and the plurality of spring rods are in a compressed state.

[0027] When the internal ejection driving part is fired, the connection between the outer warhead plate and the killing unit installation inner cavity is impacted and destroyed, the slice net warhead is ejected, the plurality of spring rods return to the original state, and the outer warhead plate is separated from the connecting plate.

[0028] By adopting the technical scheme, the slice net warhead adopts two slice warheads, the connecting plate is a connecting part and a first warhead, and the outer warhead plate is connected with the connecting plate through the plurality of spring rods, when the internal ejection driving part is in an un-fired state, the plurality of spring rods are in a compressed state, the outer side of the outer warhead plate is bonded with the open end of the killing unit installation inner cavity, and the outer warhead plate forms an integral whole on the outer surface, when the internal ejection driving part is fired, the slice net warhead is subjected to an internal impact force, the outer warhead plate is quickly separated from the connecting plate, then the slice net warhead is ejected, the plurality of spring rods return to the original state, the outer warhead plate is separated from the connecting plate, a larger killing area is formed, and due to the plurality of spring rods, the slice net warhead shakes in the area, so that the possibility of a smaller aircraft passing through the gap is reduced.

[0029] A control method of a slice net unmanned equipment load is used for controlling a slice net unmanned equipment load, the slice net unmanned equipment load is installed on a load hanging part of an aircraft, a communication module of a killing control unit is wirelessly connected with a flight control system of the aircraft.

[0030] When it is judged that the aircraft flies to a task coordinate, the flight control system sends an external control instruction to the communication module, the external control instruction comprises a slice net warhead number and an ejection instruction, and the control chip controls the internal ejection driving part of the corresponding slice net warhead to start according to the external control instruction, the corresponding slice net warhead ejects the killing unit installation inner cavity, and the slice net warhead and the traction part form a killing net to form a killing force on the aircraft in the covered area.

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

[0032] The present application can provide a slice net unmanned equipment load and control method, when the slice net unmanned equipment load reaches the designated task area, the communication module of the killing control unit receives the external instruction signal, the control chip of the killing control unit controls the execution action of the internal ejection driving part of the plurality of ejection killing units respectively, and the execution action of the ejection can be simultaneous execution of all ejection killing units or execution of the ejection killing units with specified numbers, which can adapt to various aircraft killing requirements.

[0033] The slice net unmanned equipment load is mainly used for unmanned equipment countermeasures, when the internal ejection driving part is opened, the driving slice net warhead ejects the killing unit installation inner cavity outward, the slice net warhead ejects and combines with the traction part to form the killing force to the aircraft in the covered area, and the slice net warhead has stronger structural damage effect on the small unmanned equipment target made of high molecular materials such as aluminum alloy, carbon fiber, composite material and resin plastic, and the small unmanned equipment fuselage, wing and paddle. BRIEF DESCRIPTION OF DRAWINGS

[0034] Figure 1 is a slice net unmanned equipment load two-side slice net warhead ejection state structure principle schematic diagram of the present application;

[0035] Figure 2 is a slice net unmanned equipment load slice net warhead non-ejection state structure principle schematic diagram of the present application;

[0036] Figure 3 is a main frame structure principle schematic diagram of the slice net unmanned equipment load of the present application;

[0037] Figure 4 is a single slice net warhead non-ejection state structure principle schematic diagram of the slice net unmanned equipment load of the present application;

[0038] Figure 5 is a single slice net warhead ejection state structure principle schematic diagram of the slice net unmanned equipment load of the present application;

[0039] Figure 6 is a slice net unmanned equipment load slice net warhead structure principle schematic diagram of the present application;

[0040] Figure 7 is a slice net unmanned equipment load slice net hanging in the load part of the unmanned aerial vehicle structure principle schematic diagram of the present application;

[0041] Figure 8 is a killing control unit and unmanned aerial vehicle flight control system communication connection schematic diagram of the slice net unmanned equipment load of the present application.

[0042] Explanation of reference signs: 1, main frame structure; 11, main skeleton; 12, killing unit cavity; 21, internal ejection driving part; 22, traction part; 23, sheet net warhead; 231, connecting plate; 232, spring rod; 233, outer combat plate; 31, communication module; 32, instruction memory; 33, control chip; 100, killing unit installation inner cavity; 101, flight control system. DETAILED DESCRIPTION

[0043] The application will be further described in detail below with reference to the accompanying drawings.

[0044] The embodiment of the application discloses a sheet net unmanned equipment load and control method.

[0045] Reference Figures 1-8 , embodiment 1, a sheet net unmanned equipment load, comprising 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 inner cavities 100, a plurality of ejection killing units are respectively installed in the plurality of killing unit installation inner cavities 100, the ejection killing unit comprises an internal ejection driving part 21, a traction part 22 and a sheet net warhead 23, the internal ejection driving part 21 is installed in the killing unit installation inner cavity 100, the traction part 22 is located in the killing unit installation inner cavity 100, the sheet net warhead 23 is connected and installed at the end of the traction part 22, the killing control unit controls the execution action of the plurality of ejection killing units respectively, when the internal ejection driving part 21 is started, the sheet net warhead 23 is driven to pop out of the killing unit installation inner cavity 100, after the sheet net warhead 23 pops out, the sheet net warhead 23 and the traction part 22 combine to form a killing force to the aircraft in the covered area;

[0046] The killing control unit comprises a communication module 31, an instruction memory 32 and a control chip 33, the communication module 31 is used for receiving an external control instruction, the instruction memory 32 is in communication connection with the communication module 31, the control chip 33 is in communication connection with the instruction memory 32, and the execution action of the internal ejection driving part 21 of the plurality of ejection killing units is controlled based on the external control instruction.

[0047] The slice net unmanned equipment load can be mounted on the bottom of the aircraft through the mounting structure or tethered rope structure. When reaching the designated task area, the communication module 31 of the killing control unit receives external instruction signals, which can use wired communication or wireless communication. In specific applications, the killing control unit should also consider the risk of false control signals. Strong encryption algorithms can be used to encrypt the transmitted instructions to ensure that only systems with the correct key can decrypt and execute the instructions. This can effectively prevent unauthorized third parties from falsifying 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. Receive instructions through independent, multi-channel communication lines. If the instructions from one channel are inconsistent with those from other channels, the system can issue a warning or refuse to execute.

[0048] When it is determined that the external control instruction is reliable, the control chip 33 controls the execution action of the internal ejection driving part 21 of the plurality of ejection type killing units respectively. The execution action of the ejection can be simultaneous execution of all ejection type killing units, or execution of ejection type killing units with specified numbers, which can adapt to various aircraft killing requirements.

[0049] The slice net unmanned equipment load is mainly used for unmanned equipment countermeasures. When the internal ejection driving part 21 is turned on, the driving slice net warhead 23 is ejected to the outside of the killing unit installation inner cavity 100. The combination of the slice net warhead 23 and the traction part 22 forms a killing force on the aircraft in the covered area. The slice net warhead 23 has a stronger structural damage effect on small unmanned equipment targets made of high molecular materials such as aluminum alloy, carbon fiber, composite material and resin plastic for small unmanned equipment fuselage, wings and blades, etc., compared with traditional warheads.

[0050] Embodiment 2, the main body 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, and the killing unit cavity 12 is provided with a killing unit installation inner cavity 100.

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

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

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

[0054] The embodiment 4, the internal ejection driving part 21 is a controllable explosive device, the controllable explosive device includes explosive and electric control ignition device, the electric control ignition device is used for detonating the explosive, the killing control unit controls the execution action of the electric control ignition device.

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

[0056] The embodiment 5, the internal ejection driving part 21 includes a high-pressure gas cavity and an electric control valve, the electric control valve controls the opening and closing of the jet port of the high-pressure gas cavity, and the killing control unit controls the execution action of the electric control valve.

[0057] The high-pressure gas cavity stores compressed gas, under the control of the electric control valve, the jet port of the compressed gas is opened, and the high-pressure gas sprayed out of the jet port can quickly push the traction part 22 and the sheet net warhead 23 out of the killing unit cavity 12.

[0058] The embodiment 6, the internal ejection driving part 21 is an elastic energy storage device, the elastic energy storage device includes an elastic member and an elastic member controller, the elastic member controller is used for controlling the extension 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 electric control spring or an elastic accumulator, etc., under the control of the elastic member controller, the traction part 22 and the sheet net warhead 23 can be quickly pushed out of the killing unit cavity 12. Quickly push the traction part 22 and the sheet net warhead 23 out of the killing unit cavity 12.

[0060] The embodiment 7, the traction part 22 is a net rope woven by 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.

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

[0062] The embodiment 8, one side of the sheet net warhead 23 is connected with the traction part 22, when the internal ejection driving part 21 is in an uncocked state, the sheet net warhead 23 is buckled at the open end of the killing unit installation inner cavity 100, and the sheet net warhead 23 and the main frame structure 1 form a complete sphere or a hemisphere.

[0063] The sheet net warhead 23 can be a ball, a sheet, etc. with a certain weight, when the internal ejection driving part 21 is in an uncocked state, the sheet net warhead 23 and the main frame structure 1 form a complete sphere or a hemisphere, which can reduce the wind resistance of the sheet net unmanned equipment load when hanging.

[0064] The sheet net combat unit 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 with the traction unit 22. One end of the plurality of spring rods 232 is connected with the other side of the connecting plate 231. The outer side of the outer combat plate 233 is adhered to the opening of the killing unit installation inner cavity 100 when the internal ejection driving unit 21 is in the un-fired state. The plurality of spring rods 232 are in the compressed state.

[0065] When the internal ejection driving unit 21 is fired, the connection between the outer combat plate 233 and the killing unit installation inner cavity 100 is impacted and destroyed. The sheet net combat unit 23 is ejected. The plurality of spring rods 232 return to the original state. The outer combat plate 233 is separated from the connecting plate 231.

[0066] The sheet net combat unit 23 adopts two sheet-shaped combat units. The connecting plate 231 is the connecting unit and the first combat unit. The outer combat plate 233 is connected with the connecting plate 231 through the plurality of spring rods 232. When the internal ejection driving unit 21 is in the un-fired state, the plurality of spring rods 232 are in the compressed state. The outer side of the outer combat plate 233 is adhered to the opening of the killing unit installation inner cavity 100 to form an integral whole on the outer surface. When the internal ejection driving unit 21 is fired, the sheet net combat unit 23 is subjected to the internal impact force. The outer combat plate 233 is quickly separated from the connecting plate 231. Then the sheet net combat unit 23 is ejected. The plurality of spring rods 232 return to the original state. The outer combat plate 233 is separated from the connecting plate 231 to form a larger killing area. Due to the plurality of spring rods 232, the entire sheet net combat unit 23 will appear regional shaking to reduce the possibility of smaller aircrafts drilling through the gap.

[0067] The sheet net unmanned equipment load control method is used for controlling a sheet net unmanned equipment load. The sheet net unmanned equipment load is installed on the load hanging unit of an aircraft. The communication module 31 of the killing control unit is wirelessly connected with the flight control system 101 of the aircraft.

[0068] When it is judged that the aircraft flies to the task coordinates, the flight control system 101 sends an external control instruction to the communication module 31. The external control instruction comprises the number of the ejected sheet net combat unit 23 and the ejection instruction. The external control instruction of the control chip 33 controls the start of the internal ejection driving unit 21 of the corresponding number of sheet net combat units 23. The corresponding number of sheet net combat units 23 eject the killing unit installation inner cavity 100 outward. The sheet net combat unit 23 and the traction unit 22 are combined to form a killing net to form a killing force on the aircrafts in the covered area.

[0069] The above are preferred embodiments of the present application, and do not limit the protection scope of the present application, so that: any equivalent changes made according to the structure, shape, principle of the present application should be covered within the protection scope of the present application.

Claims

1. A sheet web unmanned equipment payload, characterized by: The application relates to a main body frame structure (1), a plurality of ejection type killing units and a killing control unit, the main body frame structure (1) is provided with a plurality of killing unit mounting cavities (100), the plurality of ejection type killing units are respectively mounted in the plurality of killing unit mounting cavities (100), the ejection type killing unit comprises an internal ejection driving part (21), a traction part (22) and a sheet net warhead (23), the internal ejection driving part (21) is mounted in the killing unit mounting cavity (100), the traction part (22) is located in the killing unit mounting cavity (100), the sheet net warhead (23) is connected and mounted at the end of the traction part (22), the killing control unit controls the execution action of the plurality of ejection type killing units, when the internal ejection driving part (21) is opened, the sheet net warhead (23) is driven to pop out of the killing unit mounting cavity (100), after the sheet net warhead (23) is popped out, the sheet net warhead (23) and the traction part (22) are combined to form a killing force on the aircraft in a covered area. The killing control unit comprises a communication module (31), an instruction storage (32) and a control chip (33), the communication module (31) is used for receiving an external control instruction, the instruction storage (32) is in communication connection with the communication module (31), the control chip (33) is in communication connection with the instruction storage (32), and the execution action of the internal ejection driving part (21) of the plurality of ejection type killing units is controlled based on the external control instruction. The sheet net warhead (23) comprises a connecting plate (231), a plurality of spring rods (232) and an outer warhead plate (233), one side of the connecting plate (231) is connected with the traction part (22), one end of the plurality of spring rods (232) is connected and mounted on the other side of the connecting plate (231), and the outer warhead plate (233) is connected at the other end of the plurality of spring rods (232); when the internal ejection driving part (21) is in an unfired state, the outer side of the outer warhead plate (233) is bonded with the opening of the killing unit mounting cavity (100), and the plurality of spring rods (232) are in a compressed state. When the internal ejection driving part (21) is fired, the connection between the outer warhead plate (233) and the killing unit mounting cavity (100) is impacted and damaged, the sheet net warhead (23) is popped out, the plurality of spring rods (232) return to the original state, and the outer warhead plate (233) is separated from the connecting plate (231).

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

3. A sheet web unmanned equipment payload according to claim 1, characterized in that: The internal ejection driving part (21) is a controllable explosion device, the controllable explosion device comprises an explosive and an electric control ignition device, the electric control ignition device is used for detonating the explosive, and the killing control unit controls the execution action of the electric control ignition device.

4. A sheet web unmanned equipment payload according to claim 1, wherein: The internal ejection driving part (21) comprises a high-pressure gas cavity and an electric control valve, the electric control valve controls the opening and closing of a jet port of the high-pressure gas cavity, and the killing control unit controls the execution action of the electric control valve.

5. A sheet web unmanned equipment payload according to claim 1, wherein: The internal ejection driving part (21) is an elastic energy storage device, which comprises an elastic member and an elastic member controller for controlling the extension of the elastic member.

6. A sheet web unmanned equipment payload according to claim 1, wherein: The traction part (22) is a net rope woven by multiple ropes made of high-strength and high-toughness material, which refers to Kevlar material or carbon fiber.

7. A method of controlling an unattended equipment payload of a sheet web, characterized by, The application relates to a kind of sheet net unmanned equipment loads for controlling the load of any one of claims 1-6, the sheet net unmanned equipment load is installed in the load hanging part of aircraft, the communication module (31) of killing control unit is connected with the wireless communication of flight control system (101) of aircraft; When judging that the aircraft flies to the task 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 ejected sheet net warhead (23) and the ejection instruction, the control chip (33) controls the internal ejection driving part (21) of the corresponding number sheet net warhead (23) to start based on the external control instruction, the corresponding number sheet net warhead (23) ejects the killing unit installation inner cavity (100) outward, the sheet net warhead (23) and the traction part (22) are combined to form a killing net, which forms a killing force on the aircraft in the covered area.

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