Space non-inductive harassment device and method

Abstract

The invention provides a space non-inductive harassment device and method, and relates to the technical field of microsatellites. The space non-inductive harassment device comprises a miniature carrying satellite and a force and current multi-field coupling driver installed on the miniature carrying satellite, the miniature carrying satellite is used for driving the force and current multi-field coupling driver to be close to a target satellite, and an injection opening of the force and current multi-field coupling driver is aligned with a detection lens of the target satellite through posture adjustment. The force-current multi-field coupling driver is used for jetting harassing liquid from the jet orifice which is aligned with the detection lens of the target satellite under the extrusion of electrostatic force so as to realize a blinding effect on the detection lens of the target satellite. The system not only has the characteristics of simple structure manufacturing, low manufacturing cost, low energy consumption and the like, but also can realize long-time effective harassment by spraying harassment liquid by using a detection lens aligned with a target satellite.

Description

Technical Field

[0001] The present invention relates to the technical field of micro-satellite, and in particular to a space imperceptible harassment device and method. Background Art

[0002] Satellite "blinding" is an anti-satellite technology, which usually refers to the use of technical means to temporarily or permanently disable the function of sensitive equipment such as satellite sensors (such as visual sensors), thereby weakening or destroying the satellite's reconnaissance, navigation, communication and other capabilities, which is crucial to satellite defense.

[0003] Existing satellite "blinding" means mainly include directed energy anti-satellite technology and parasitic satellite soft kill means. Among them, directed energy anti-satellite technology uses directed energy methods such as lasers, particle beams and microwaves, which are launched from space or land to damage various precision instruments in the opponent's space-based system. Parasitic satellite soft kill means use micro-satellites that can be dropped by the party and attached to the target satellite. According to the corresponding instructions of the party, the target satellite can be interfered with and temporarily disabled, thereby achieving the purpose of "blinding".

[0004] However, existing directed energy anti-satellite technology can directly damage the target satellite or disable its sensitive electronic components, but it cannot achieve covert operations. Parasite satellite soft kill methods (such as micro-robots and electronic jamming) temporarily disable the target satellite by interfering with it, but there are problems such as long deployment time, high energy consumption and short attack time. When non-our satellite reconnaissance activities occur, it is impossible to achieve immediate and long-term effective harassment of the target satellite. In addition, the above anti-satellite technical means all have the problems of complex structural control, high manufacturing cost and high energy consumption. Summary of the invention

[0005] The problem solved by the invention is: how to achieve low-cost, imperceptible, immediate and long-term effective harassment on a target satellite.

[0006] To solve the above problems, on the one hand, the present invention provides a space non-sensing harassment device, including a micro-carrier satellite and a force-current multi-field coupling driver installed on the micro-carrier satellite, the micro-carrier satellite is used to drive the force-current multi-field coupling driver to approach a target satellite, and adjust the attitude so that the injection port of the force-current multi-field coupling driver is aimed at the detection lens of the target satellite, and the force-current multi-field coupling driver is used to spray harassing liquid from the injection port to the detection lens of the target satellite under the extrusion of electrostatic force.

[0007] Optionally, the force-current multi-field coupling driver includes a flexible insulating film, a flexible conductive electrode and a dielectric fluid, the flexible conductive electrode is used to be electrically connected to a power supply device, the dielectric fluid is stored in a cavity formed by the flexible insulating film, and the flexible conductive electrode is coated on the outer surface of the cavity formed by the flexible insulating film.

[0008] Optionally, the force-current multi-field coupling drivers are arranged in multiple rows in parallel.

[0009] Optionally, a drainage tube is further included, and the drainage tube is installed at the top of the cavity.

[0010] Optionally, a film or solid particles are provided on the drainage tube to achieve sealing of the drainage tube.

[0011] Optionally, the force-current multi-field coupling driver and the micro-launch satellite are detachably connected via threaded fasteners or a mortise and tenon structure.

[0012] Optionally, a plurality of cavities formed by the flexible insulating film are arranged side by side, and the flexible conductive electrode is provided on the outer surface of any cavity.

[0013] Optionally, a plurality of the flexible conductive electrodes on the outer surface of the same side of the cavity are connected in series.

[0014] Optionally, it also includes a visual recognition system, a control center and a power control system, the visual recognition system is communicatively connected to the control center, the control center is communicatively connected to the power control, the power control system is used to be electrically connected to the power supply device, the visual recognition system is used to feedback the blinding condition of the reconnaissance lens, and the control center is used to control the output voltage of the power supply device through the power control system according to the feedback from the visual recognition system.

[0015] Compared with the prior art, the space senseless harassment device of the present invention utilizes a force-current multi-field coupling driver to be installed on a micro-carrier satellite, and can utilize the advantages of light weight and small size of the micro-carrier satellite to reduce the use cost and realize senseless harassment. The micro-carrier satellite is used to drive the force-current multi-field coupling driver to approach the target satellite, and the injection port of the force-current multi-field coupling driver is aligned with the detection lens of the target satellite through attitude adjustment. The force-current multi-field coupling driver is used to squeeze the electrostatic force to spray harassing liquid from the injection port to the detection lens of the target satellite, and can achieve a "blinding" effect on the detection lens of the target satellite. Compared with the existing directed energy anti-satellite technology or parasitic star soft killing means, it not only has the characteristics of simple structure, low manufacturing cost, low energy consumption, and instant, but also can realize long-term effective harassment by spraying harassing liquid at the detection lens of the target satellite.

[0016] On the other hand, the present invention further provides a space-undetectable harassment method, based on the space-undetectable harassment device as described above, characterized in that it comprises the following steps:

[0017] Confirm the target satellite position;

[0018] Launching a micro-carrier satellite, wherein the micro-carrier satellite jets toward the target satellite;

[0019] Adjusting the attitude of the micro-launch satellite so that the jet port of the force-current multi-field coupling driver is aligned with the target satellite reconnaissance lens;

[0020] The force-current multi-field coupling driver is powered on to spray the harassing liquid to the reconnaissance lens of the target satellite;

[0021] The force-current multi-field coupling driver is powered off, and the micro-launch satellite returns.

[0022] Compared with the prior art, the space senseless harassment method of the present invention confirms the position of the target satellite; launches a micro-carrier satellite, and sprays jets close to the target satellite; enables the micro-carrier satellite to transport the force-current multi-field coupling driver to the position of the target satellite, and adjusts the posture of the micro-carrier satellite to approach the detection lens of the target satellite; thereby, the force-current multi-field coupling driver can be aimed at the detection lens of the target satellite, and then the force-current multi-field coupling driver is powered on to spray the harassment liquid to the detection lens of the target satellite; the force-current multi-field coupling driver is powered off, and the micro-carrier satellite returns, thereby achieving a "blinding" effect on the detection lens of the target satellite, and can achieve a senseless, immediate, and long-term effective attack on the detection lens of the opponent's satellite. BRIEF DESCRIPTION OF THE DRAWINGS

[0023] Figure 1 Schematic diagram of the structure of a space-undetectable harassment device in an embodiment of the present invention;

[0024] Figure 2 Schematic diagram of the structure of the force-current multi-field coupling driver in an embodiment of the present invention;

[0025] Figure 3 It is a structural schematic diagram of a case where a thin film is provided at the tube opening of the drainage tube in an embodiment of the present invention;

[0026] Figure 4 This is a schematic diagram of the structure in which solid particles are arranged inside the drainage tube in an embodiment of the present invention;

[0027] Figure 5 is a schematic diagram of the harassing liquid being sprayed in an embodiment of the present invention;

[0028] Figure 6It is a schematic diagram of the space non-sensing harassment device in an embodiment of the present invention spraying harassment liquid on the detection lens of the target satellite;

[0029] Figure 7 The figure is a flow chart of a space imperceptible harassment method in an embodiment of the present invention.

[0030] Description of reference numerals:

[0031] 1-force-current multi-field coupling driver; 11-power supply; 12-flexible insulating film; 13-flexible conductive electrode; 14-dielectric fluid; 15-drainage tube; 151-solid particles; 2-micro-carrier satellite; 3-reconnaissance lens. DETAILED DESCRIPTION

[0032] In order to make the above-mentioned objects, features and advantages of the present invention more obvious and easy to understand, specific embodiments of the present invention are described in detail below with reference to the accompanying drawings.

[0033] In the accompanying drawings, the Z axis represents the vertical position, and the positive direction of the Z axis (that is, the direction in which the arrow of the Z axis points) represents the upper side, and the negative direction of the Z axis (that is, the direction opposite to the positive direction of the Z axis) represents the lower side; in the accompanying drawings, the X axis represents the horizontal position, and the positive direction of the X axis (that is, the direction in which the arrow of the X axis points) represents the right side, and the negative direction of the X axis (that is, the direction opposite to the positive direction of the X axis) represents the left side; in the accompanying drawings, the Y axis represents the front and rear positions, and the positive direction of the Y axis (that is, the direction in which the arrow of the Y axis points) represents the front side, and the negative direction of the Y axis (that is, the direction opposite to the positive direction of the Y axis) represents the rear side. It should also be noted that the aforementioned Z axis, Y axis, and X axis are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation to the present invention.

[0034] It should be noted that the terms "first", "second", etc. in the specification and claims of the present invention and the above-mentioned drawings are used to distinguish similar objects, and are not necessarily used to describe a specific order or sequence. It should be understood that the numbers used in this way can be interchanged where appropriate, so that the embodiments of the present invention described herein can be implemented in an order other than those illustrated or described herein.

[0035] Satellite "blinding" is an anti-satellite technology, which usually refers to the use of technical means to temporarily or permanently disable the function of sensitive equipment such as satellite sensors (such as visual sensors), thereby weakening or destroying the satellite's reconnaissance, navigation, communication and other capabilities, which is crucial to satellite defense. Existing "blinding" means mainly include directed energy anti-satellite technology and parasitic satellite soft kill means. Among them, directed energy anti-satellite technology uses directed energy methods such as lasers, particle beams and microwaves, which are launched from space or land to damage various precision instruments in the opponent's space-based system. Parasitic satellite soft kill means use micro-satellites that can be dropped by the party and attached to the target satellite. According to the corresponding instructions of the party, the target satellite can be interfered with and temporarily disabled, thereby achieving the purpose of "blinding".

[0036] However, although laser technology has the advantages of fast speed, high precision and no pollution, the laser beam needs to pass through the atmosphere to enter space, which is accompanied by energy attenuation and decreased target aiming rate, and is also seriously affected by the weather; particle beams are not affected by the atmosphere and weather, but there are problems such as large particle accelerators, inability to focus, and difficulty in fire control; microwaves have the characteristics of large irradiation range and long range, but there are problems such as high power and difficulty in focusing and controlling microwave beams. In addition, directed energy anti-satellite technologies such as lasers, particle beams and microwaves cannot achieve covert operations. Parasitic satellites can be deployed covertly and accurately due to their small size. However, existing parasitic satellite soft kill methods (such as micro-robots and electronic interference) temporarily disable target satellites by interfering with them, but there are problems such as long deployment time, high energy consumption and short attack time. When non-our satellite reconnaissance activities occur, it is impossible to achieve immediate and long-term effective harassment of target satellites. In addition, the above anti-satellite technical means all have problems such as complex structural control, high manufacturing cost and high energy consumption.

[0037] Combination Figure 1 and Figure 6 As shown, the present invention provides a space non-sensing harassment device, including a micro-carrier satellite 2 and a force current multi-field coupling driver 1 installed on the micro-carrier satellite 2, the micro-carrier satellite 2 is used to drive the force current multi-field coupling driver 1 to approach a target satellite, and adjust the attitude so that the injection port of the force current multi-field coupling driver 1 is aimed at the detection lens 3 of the target satellite, and the force current multi-field coupling driver 1 is used to spray harassment liquid from the injection port to the detection lens 3 of the target satellite under the extrusion of electrostatic force.

[0038] Specifically, microsatellites are a new generation of satellites with clear purposes, with high new technology content, short development cycle (about one year), low development cost (tens of millions of RMB) and the ability to further network. The advantages of light weight and small size of microsatellites make them play an important role in military aspects such as reconnaissance, communication, command, decision-making, logistics and weapons and equipment. The harassment device based on microsatellites has the advantages of concealed deployment, on-demand mobility and controllable intensity, and can achieve non-sensing harassment of target satellites. Micro-carrier satellite 2 is a microsatellite, and micro-carrier satellite 2 includes structures such as identification camera, antenna, attitude adjuster, star sensor and thruster. The force current multi-field coupling driver 1 is installed on micro-carrier satellite 2, and the injection port of micro-carrier satellite 2 with power current multi-field coupling driver 1 is aimed at the detection lens 3 of the target satellite to spray harassing liquid at the detection lens 3 of the target satellite. Among them, force current multi-field coupling is the coupling of force field, electric field and fluid field. Force current multi-field coupling driver 1 refers to a driver that realizes driving through multi-field coupling of force field, electric field and fluid field. Specifically, the position of the target satellite can be confirmed by means of space positioning technology or visual capture. After the position of the target satellite is confirmed, the micro-carrier satellite 2 is launched. The micro-carrier satellite 2 uses its own thrusters to jet air to approach the target satellite. In the process of approaching the target satellite, the posture of the micro-carrier satellite 2 is continuously adjusted to gradually approach the detection lens 3 of the target satellite, so that the injection port of the force-current multi-field coupling driver 1 is aligned with the detection lens 3 of the target satellite. Then, the force-current multi-field coupling driver 1 is powered on, and through the squeezing of electrostatic force, the force-current multi-field coupling driver 1 sprays the harassing liquid to the detection lens 3 of the target satellite, as shown in FIG. Figure 6 As shown, after the detection lens 3 of the target satellite is shielded, the force-current multi-field coupling driver 1 is powered off, and the micro-carrier satellite 2 returns.

[0039] Therefore, in this embodiment, the force current multi-field coupling driver 1 is installed on the micro-carrier satellite 2, and the advantages of the micro-carrier satellite 2 of light weight and small size can be used to reduce the use cost and realize non-sensing harassment. The micro-carrier satellite 2 is used to drive the force current multi-field coupling driver 1 to approach the target satellite, and the injection port of the force current multi-field coupling driver 1 is aimed at the detection lens 3 of the target satellite by adjusting the attitude. The force current multi-field coupling driver 1 is used to squeeze the electrostatic force to spray the harassing liquid from the injection port to the detection lens 3 of the target satellite, which can achieve the "blinding" effect on the detection lens 3 of the target satellite. Compared with the existing directed energy anti-satellite technology or parasitic star soft killing means, it not only has the characteristics of simple structure, low manufacturing cost, low energy consumption, and instant, but also can realize long-term effective harassment by spraying the harassing liquid towards the detection lens 3 of the target satellite.

[0040] Optionally, combined Figures 1 to 5As shown, the force-current multi-field coupling driver 1 includes a flexible insulating film 12, a flexible conductive electrode 13 and a dielectric liquid 14. The flexible conductive electrode 13 is used to be electrically connected to the power supply device 11. The dielectric liquid 14 is stored in a cavity formed by the flexible insulating film 12, and the flexible conductive electrode 13 is coated on the outer surface of the cavity.

[0041] Specifically, the dielectric liquid 14 is the harassing liquid, and the dielectric liquid 14 can be a non-transparent liquid such as black ink to physically cover the opponent's detection lens 3, or it can be a chemical liquid that can react with the opponent's detection lens 3 to chemically destroy the opponent's detection lens 3. The dielectric liquid 14 is sprayed on the detection lens 3 to achieve "blinding" of the detection lens 3. The flexible insulating film 12 can be made of any flexible insulating material, and the flexible insulating film 12 is non-conductive and can be deformed, and there is no chemical reaction between the flexible insulating film 12 and the dielectric liquid 14. The flexible insulating film 12 can form cavities of different shapes according to needs, such as Figure 5 As shown, the flexible insulating film 12 is surrounded by a columnar structure, and the space surrounded by the flexible insulating film 12 forms a columnar cavity to store the dielectric liquid 14 in the cavity. The cavity prepared by the flexible insulating film 12 is installed on the micro-launch satellite 2. The flexible conductive electrode 13 can be any flexible conductive material. The outer surface of the cavity formed by the flexible insulating film 12 refers to the surface of the flexible insulating film 12 located outside the cavity. The flexible conductive electrode 13 is coated on the outer surface of the cavity (the flexible conductive electrode 13 can also be installed on the outer surface of the cavity by screen printing, electroplating, chemical etching / deposition or inkjet printing, and the shape of the flexible conductive electrode 13 can be adaptively adjusted according to actual needs). Two flexible conductive electrodes 13 are respectively coated on the outer surfaces of the front and rear sides of the cavity, and the two flexible conductive electrodes 13 are not conductive. The power supply device 11 is a power supply device capable of outputting high voltage, including a low-voltage power supply and a high-voltage module (high-voltage amplifier). The positive and negative voltage output ends of the low-voltage power supply are converted into high-voltage outputs through the high-voltage module (high-voltage amplifier), that is, the voltage is boosted from a few volts to several thousand volts and then the two flexible conductive electrodes 13 are powered, so that the positive and negative charges on the two flexible conductive electrodes 13 attract each other to generate electrostatic adsorption force. Under the action of the electrostatic adsorption force, the two flexible conductive electrodes 13 approach each other, so that the cavity is gradually compressed, and the dielectric fluid 14 inside the cavity is sprayed out.

[0042] In this way, the flexible conductive electrode 13 is used to be electrically connected to the power supply device 11, the dielectric liquid 14 is stored in the cavity formed by the flexible insulating film 12, and the flexible conductive electrode 13 is used to coat the outer surface of the cavity, so that after the power supply device 11 passes high voltage to the flexible conductive electrode 13, the positive and negative charges on the two flexible conductive electrodes 13 can attract each other to generate electrostatic adsorption force, so that under the action of the electrostatic adsorption force, the two flexible conductive electrodes 13 are close to each other, so that the cavity formed by the flexible insulating film 12 is gradually compressed, and then the concentrated injection of the dielectric liquid 14 is realized, so that the dielectric liquid 14 can quickly "blind" the detection lens 3, thereby improving the "blinding" efficiency of the dielectric liquid 14.

[0043] Optionally, combined Figure 1 As shown, the force-current multi-field coupling driver 1 is arranged in multiple rows in parallel.

[0044] Specifically, five force-current multi-field coupling drivers 1 are provided, and the five force-current multi-field coupling drivers 1 are arranged side by side along the length direction of the micro-carrier satellite 2 .

[0045] In this way, by using the force-current multi-field coupling drivers 1 to be arranged in multiple rows in parallel, the detection lens 3 or even multiple detection lenses 3 can be contaminated more thoroughly.

[0046] Optionally, combined Figures 1 to 5 As shown, the force-current multi-field coupling driver 1 further includes a drainage tube 15 , which is installed at the top of the cavity.

[0047] Specifically, in combination with the foregoing, the drainage tube 15 is located at the upper end of the cavity formed by the flexible insulating film 12, the drainage tube 15 is connected to the cavity, and the upper end of the drainage tube 15 is the injection port of the force-current multi-field coupling driver 1. In this way, by vertically installing the drainage tube 15 at the top of the cavity, the drainage tube 15 can spray and guide the dielectric liquid 14, thereby improving the accuracy of the injection.

[0048] Optionally, combined Figure 3 and Figure 4 As shown, a film or solid particles 151 is provided on the drainage tube 15 to achieve sealing of the cavity formed by the flexible insulating film 12 .

[0049] Specifically, a film may be provided at the connection between the drainage tube 15 and the cavity formed by the flexible insulating film 12. When not spraying, the film seals the cavity formed by the flexible insulating film 12. When spraying, the harassing liquid can flush the film open for spraying. Alternatively, solid particles 151 are provided in the drainage tube 15. When not spraying, the solid particles 151 seal the cavity formed by the flexible insulating film 12. When spraying, the harassing liquid can flush the solid particles 151 out of the drainage tube 15 for spraying.

[0050] In this way, a film or solid particles 151 is provided on the drainage tube 15 to achieve the sealing of the cavity formed by the flexible insulating film 12, so that when there is no need to spray the harassing liquid, the film or solid particles 151 can seal the cavity formed by the flexible insulating film 12, thereby improving the storage stability of the harassing liquid in the cavity formed by the flexible insulating film 12.

[0051] Optionally, the force-current multi-field coupling driver 1 and the micro-launch satellite 2 are detachably connected.

[0052] Specifically, for example, the force-current multi-field coupling driver 1 and the micro-launch satellite 2 are connected by threaded fasteners such as bolts made by 3D printing or a mortise and tenon structure.

[0053] In this way, the detachable connection between the force current multi-field coupling driver 1 and the micro-launch satellite 2 can not only improve the stability of the connection between the force current multi-field coupling driver 1 and the micro-launch satellite 2, but also facilitate the replacement of the force current multi-field coupling driver 1.

[0054] Optionally, combined Figure 1 As shown, a plurality of cavities formed by the flexible insulating film 12 are arranged side by side, and a flexible conductive electrode 13 is arranged on the outer surface of any cavity.

[0055] It should be noted that, when a plurality of cavities formed by the flexible insulating film 12 are arranged side by side, the drainage tube 15 may be provided on only one cavity located in the middle.

[0056] Specifically, five cavities formed by the flexible insulating films 12 are arranged side by side, and the cavities formed by the five flexible insulating films 12 are arranged in a row along the width direction of the micro-launch satellite 2. The cavities formed by the five flexible insulating films 12 are connected in sequence, and the flexible conductive electrodes 13 on the two front cavities and the flexible conductive electrodes 13 on the two rear cavities are symmetrical about the axis of the drainage tube 15, so that the dielectric fluid 14 in the four front and rear cavities flows toward the middle cavity.

[0057] In this way, multiple cavities formed by the flexible insulating film 12 are arranged side by side, and a flexible conductive electrode 13 is arranged on the outer surface of any cavity, which can increase the carrying capacity of the dielectric liquid 14, thereby being able to more thoroughly contaminate the detection lens 3 or even multiple detection lenses 3.

[0058] Optionally, combined Figure 1 and Figure 5 As shown, the flexible conductive electrodes 13 on the outer surfaces of the same side of the multiple cavities are connected in series.

[0059] Specifically, in combination with the foregoing, the flexible conductive electrodes 13 on the outer surface of the same side of the five cavities (the five flexible conductive electrodes 13 on the left side of the five cavities are connected in series, and the five flexible conductive electrodes 13 on the right side of the five cavities are connected in series) can be connected in series in sequence through wires.

[0060] In this way, by connecting the flexible conductive electrodes 13 on the outer surfaces of the multiple cavities in series, only one power supply device 11 is needed to achieve synchronous compression of the multiple cavities, thereby significantly improving the flow efficiency of the dielectric liquid 13 and further improving the injection efficiency of the harassing liquid.

[0061] Optionally, the space-undetectable harassment device also includes a visual recognition system, a control center and a power control system. The visual recognition system is communicatively connected to the control center, the control center is communicatively connected to the power control, the power control system is used to be electrically connected to the power supply device 11, the visual recognition system is used to feedback the blinding condition of the detection lens 3, and the control center is used to control the output power of the power supply device 11 through the power control system according to the feedback from the visual recognition system.

[0062] Specifically, the visual recognition system identifies the image after the dielectric liquid covers the detection lens 3, and transmits the image to the control center. The control center controls the output voltage of the power supply device 11 according to the image transmitted by the visual recognition system. For example, according to the image, the dielectric liquid does not completely cover the detection lens 3, then the control center increases the output voltage of the power supply device 11 through the power control system, thereby achieving further compression of the cavity, that is, spraying more dielectric liquid to cover the uncovered area on the detection lens 3; or, according to the image, the dielectric liquid has completely covered the detection lens 3, then the control center reduces the output voltage of the power supply device 11 through the power control system until it is zero, that is, the power supply device 11 no longer applies high voltage to the flexible conductive electrode 13 to reduce energy waste.

[0063] In this way, the visual recognition system is connected to the control center through communication, the control center is connected to the power control communication, the power control system is used to be electrically connected to the power supply device 11, the visual recognition system is used to feedback the blinding situation of the detection lens 3, and the control center is used to control the output voltage of the power supply device 11 through the power control system according to the feedback from the visual recognition system. The visual recognition system can capture and feedback the situation of the dielectric liquid covering the detection lens 3 in time, so that the control center can easily adjust the output voltage of the power supply device 11 through the power control system, so as to realize the adjustable output voltage of the power supply device 11, which can not only improve the use flexibility of the power supply device 11, but also reduce energy waste when the dielectric liquid completely covers the detection lens 3.

[0064] Combination Figure 7 As shown, an embodiment of the present invention further provides a space-sensing harassment method, based on the above-mentioned space-sensing harassment device, comprising the following steps:

[0065] Step 1: Confirm the target satellite position;

[0066] Step 2: launching the micro-carrier satellite 2, which jets close to the target satellite;

[0067] Step 3: Adjust the attitude of the micro-carrier satellite 2 so that the jet nozzle of the force-current multi-field coupling driver 1 is aligned with the target satellite detection lens 3;

[0068] Step 4: The force-current multi-field coupling driver 1 is powered on to spray the harassing liquid to the reconnaissance lens 3 of the target satellite;

[0069] Step 5: The force-current multi-field coupling driver 1 is powered off and the micro-launch satellite 2 returns.

[0070] Specifically, the position of the target satellite can be confirmed by means of space positioning technology or visual capture. After the position of the target satellite is confirmed, the micro-carrier satellite 2 is launched. The micro-carrier satellite 2 uses its own thrusters and other jets to approach the target satellite. In the process of approaching the target satellite, the posture of the micro-carrier satellite 2 is continuously adjusted to gradually approach the reconnaissance lens 3 of the target satellite. Then, the force-current multi-field coupling driver 1 is powered on, and the harassing liquid is sprayed onto the reconnaissance lens 3 of the target satellite. After the reconnaissance lens 3 of the target satellite is shielded, the force-current multi-field coupling driver 1 is powered off, and the micro-carrier satellite 2 returns.

[0071] In this way, the position of the target satellite is confirmed; the micro-carrier satellite 2 is launched and the jet is close to the target satellite; the micro-carrier satellite 2 can transport the force-current multi-field coupling driver 1 to the position of the target satellite, and adjust the posture of the micro-carrier satellite 2 to approach the target satellite reconnaissance lens 3; thereby, the force-current multi-field coupling driver 1 can be aimed at the reconnaissance lens 3 of the target satellite, and then the force-current multi-field coupling driver 1 is powered on to spray the harassing liquid onto the reconnaissance lens 3 of the target satellite; the force-current multi-field coupling driver 1 is powered off, and the micro-carrier satellite 2 returns, thereby achieving a "blinding" effect on the reconnaissance lens 3 of the target satellite, and being able to achieve an imperceptible, immediate, and long-term effective attack on the opponent's satellite reconnaissance lens.

[0072] Although the disclosure is disclosed as above, the protection scope of the disclosure is not limited thereto. Those skilled in the art may make various changes and modifications without departing from the spirit and scope of the disclosure, and these changes and modifications will fall within the protection scope of the present invention.

Claims

1. A space-undetectable harassment device, characterized in that: The invention comprises a micro-carrier satellite (2) and a force-current multi-field coupling driver (1) installed on the micro-carrier satellite (2). The micro-carrier satellite (2) is used to drive the force-current multi-field coupling driver (1) to approach a target satellite, and adjust the posture so that the injection port of the force-current multi-field coupling driver (1) is aligned with the detection lens (3) of the target satellite. The force-current multi-field coupling driver (1) is used to spray a harassing liquid from the injection port to the detection lens (3) of the target satellite under the pressure of electrostatic force.

2. The space-undetectable harassment device according to claim 1, characterized in that: The force-current multi-field coupling driver (1) comprises a flexible insulating film (12), a flexible conductive electrode (13) and a dielectric liquid (14); the flexible conductive electrode (13) is used to be electrically connected to a power supply device (11); the dielectric liquid (14) is stored in a cavity formed by the flexible insulating film (12); and the flexible conductive electrode (13) is coated on the outer surface of the cavity formed by the flexible insulating film (12).

3. The space-undetectable harassment device according to claim 2, characterized in that: The force-current multi-field coupling driver (1) is arranged in multiple rows in parallel.

4. The space-undetectable harassment device according to claim 2, characterized in that: It also comprises a drainage tube (15), wherein the drainage tube (15) is installed at the top end of the cavity.

5. The space-undetectable harassment device according to claim 4, characterized in that: The drainage tube (15) is provided with a film or solid particles (151) to achieve sealing of the cavity formed by the flexible insulating film (12).

6. The space-undetectable harassment device according to claim 1, characterized in that: The force-current multi-field coupling driver (1) and the micro-carrier satellite (2) are detachably connected.

7. The space-undetectable harassment device according to claim 2, characterized in that: A plurality of cavities formed by the flexible insulating film (12) are arranged side by side, and the flexible conductive electrode (13) is arranged on the outer surface of any cavity.

8. The space-undetectable harassment device according to claim 7, characterized in that: The flexible conductive electrodes (13) on the outer surface of the same side of the cavity are connected in series.

9. The space-undetectable harassment device according to claim 2, characterized in that: The system also comprises a visual recognition system, a control center and a power control system. The visual recognition system is connected to the control center for communication, the control center is connected to the power control for communication, the power control system is used to be electrically connected to the power supply device (11), the visual recognition system is used to feedback the blinding condition of the detection lens (3), and the control center is used to control the output voltage of the power supply device (11) through the power control system according to the condition fed back by the visual recognition system.

10. A space-free harassment method, based on the space-free harassment device according to any one of claims 1 to 9, characterized in that: The steps include: Confirm the target satellite position; Launching a micro-carrier satellite (2), wherein the micro-carrier satellite (2) jets toward the target satellite; Adjusting the attitude of the micro-carrier satellite (2) so that the injection port of the force-current multi-field coupling driver (1) is aligned with the target satellite reconnaissance lens (3); The force-current multi-field coupling driver (1) is powered on to spray the harassing liquid onto the reconnaissance lens (3) of the target satellite; The force-current multi-field coupling driver (1) is powered off, and the micro-carrier satellite (2) returns.

Images