Omnibearing multi-band unmanned aerial vehicle interference antenna

Abstract

The invention relates to the technical field of unmanned aerial vehicle interference antennas, in particular to an omni-directional multi-band unmanned aerial vehicle interference antenna which comprises a mainframe box and a mounting disc, and the mounting disc is mounted on the mainframe box; the device further comprises a plurality of stand columns, a plurality of receiving antennas, a plurality of first servo motors, a plurality of first transmitting antennas, a plurality of second servo motors and a plurality of second transmitting antennas, the stand columns are vertically mounted on the mounting disc, the receiving antennas are circumferentially and uniformly mounted on the outer walls of the stand columns, the first servo motors are mounted at the tops of the stand columns respectively, and the second servo motors are mounted on the outer walls of the transmitting antennas. The plurality of first transmitting antennas are respectively mounted on output shafts of the plurality of first servo motors, the plurality of first transmitting antennas and the stand column are concentrically arranged, the plurality of second servo motors are respectively mounted at the tops of the plurality of first transmitting antennas, and the plurality of second transmitting antennas are respectively mounted on output shafts of the plurality of second servo motors; directional interference can be simultaneously performed on the unmanned aerial vehicle and the ground control end, the interference effect is improved, the energy consumption is reduced, and the accuracy is better.

Description

Technical Field

[0001] The present invention relates to the technical field of unmanned aerial vehicle (UAV) jamming antennas, and in particular to an omnidirectional multi-band UAV jamming antenna. Background Art

[0002] In order to control illegal drone flights and protect our targets, it is necessary to interfere with illegally flying drones, causing them to crash or be captured. Various drone jamming antennas are disclosed in the prior art, such as the Chinese invention patent publication number CN118431733B, which proposes an antenna system for a drone jamming gun and a drone jamming gun. The drone jamming gun's antenna system is layered with a top layer, a middle layer, and a bottom layer. The structure includes an omnidirectional detection antenna, a detection antenna assembly, a jamming antenna assembly, and a navigation decoy antenna. The detection antenna assembly includes a first detection antenna and a second detection antenna. The jamming antenna assembly includes a first jamming antenna, a second jamming antenna, a third jamming antenna, and a fourth jamming antenna. The first detection antenna, the navigation decoy antenna, and the third jamming antenna are sequentially arranged in an upper and lower order arrangement on the top layer. The second detection antenna and the fourth jamming antenna share a common antenna arranged in the middle layer. The first jamming antenna and the second jamming antenna are coplanarly arranged on the bottom layer. The omnidirectional detection antenna is arranged directly in front of the top and middle layers. The system can achieve direction finding, attack, and decoy of drones in the full frequency band of 300-6000MHz, and is compact, small, and easy to carry.

[0003] However, the above-mentioned jamming antenna only interferes with the drone, and does not interfere with the ground control end of the drone. As a result, the ground control end can use anti-interference technical means to rescue the drone after the drone is interfered, resulting in a decrease in the jamming effect. Moreover, the above-mentioned jamming antenna system transmits jamming signals in all directions in space, which consumes a lot of energy and may cause false interference to normal equipment, resulting in poor accuracy. Summary of the Invention

[0004] In order to solve the above technical problems, the present invention provides an omnidirectional multi-band UAV jamming antenna that can simultaneously perform directionally jamming on UAVs and ground control terminals, improve jamming effects, reduce energy consumption, improve jamming effects, and have better accuracy.

[0005] The present invention provides an omnidirectional multi-band UAV jamming antenna, comprising a main box and a mounting plate, wherein the mounting plate is mounted on the main box; further comprising a plurality of columns, a plurality of receiving antennas, a plurality of servo motors 1, a plurality of transmitting antennas 1, a plurality of servo motors 2 and a plurality of transmitting antennas 2, wherein the plurality of columns are vertically mounted on the mounting plate, the plurality of columns are arranged in a matrix, the plurality of receiving antennas are uniformly mounted on the outer walls of the plurality of columns, the plurality of servo motors 1 are respectively mounted on the tops of the plurality of columns, the plurality of transmitting antennas 1 are respectively mounted on the output shafts of the plurality of servo motors 1, the plurality of transmitting antennas 1 are respectively arranged concentrically with the plurality of columns, and the plurality of servo motors 2 are respectively mounted on the outer walls of the plurality of columns. At the top of line one, multiple transmitting antennas two are respectively installed on the output shafts of multiple servo motors two; three columns are set, and the three columns are arranged in an equilateral triangle. Thirty-six receiving antennas are installed on the columns. The thirty-six receiving antennas on the three columns receive signals in one direction respectively. When working, multiple receiving antennas receive signals sent by the drone and signals sent by the drone ground end. The multiple receiving antennas generate electrical signals of different intensities according to the strength of the signals sent by the drone. At the same time, the multiple receiving antennas generate electrical signals of different intensities according to the strength of the signals sent by the drone ground end. The controller in the main box selects the signal that generates the strongest telecommunication signal. The receiving antenna of number one and the receiving antenna that generates the strongest electrical signal two, at this time, the three receiving antennas that generate the strongest electrical signal one are all facing the direction of the drone, and the three receiving antennas that generate the strongest electrical signal two are all facing the direction of the ground end of the drone, and the three servo motors one respectively drive the three transmitting antennas one to rotate, so that the transmitting directions of the three transmitting antennas one are aligned with the three receiving antennas that generate the strongest electrical signal one, and the three transmitting antennas one emit interfering electromagnetic wave signals to interfere with the drone, and the drone is in the intersection area of the interfering electromagnetic wave signals of the three transmitting antennas one, thereby enhancing the interference effect on the drone, and at the same time, the three servo motors two respectively drive the three The transmitting antenna 2 rotates so that the transmitting directions of the three transmitting antennas 2 are aligned with the three receiving antennas that generate the strongest electrical signal 2. The three transmitting antennas 2 emit interfering electromagnetic wave signals to interfere with the ground end of the drone, and the ground end of the drone is in the intersection area of the interfering electromagnetic wave signals of the three transmitting antennas 2, thereby enhancing the interference effect on the ground end of the drone. Compared with the existing technology, it interferes with the drone and the ground control end at the same time, improves the interference effect, and has a directional function, and concentrates on transmitting interference signals in the direction of the drone and the ground control end, reducing energy consumption, improving the interference effect, reducing false interference to normal equipment, and having better accuracy.

[0006] Preferably, the main box includes a signal amplifier, a clock module, an analysis module, a storage module, a ground-end positioning module and a drone damage module. The signal amplifier is used to amplify the signals received by multiple receiving antennas, the clock module is used to modify the timestamp of the amplified signal, and the amplified signal after the timestamp is modified is transmitted through multiple transmitting antennas one and multiple transmitting antennas two, the analysis module is used to analyze the received signal information and classify the signals, the storage module is used to store the classified signals, the ground-end positioning module is used to locate the position of the ground end, and the drone damage module is used to damage the drone; after the multiple receiving antennas receive the drone signal and the ground-end signal, the signal amplifier amplifies the signal, the clock module The block modifies the timestamp of the amplified signal to generate repeated strong signals of the same type as the signals transmitted by the drone and the ground end. These strong signals will block the communication channel between the drone and the ground end, increase the amount of signals that the processors of the drone and the ground end have to process, causing the processors to overload and jam, or insert interference signals into the command list of the drone, causing the drone to execute incorrect commands, thereby interfering with the drone and the ground end. The interference signal changes at any time with the frequency hopping of the signals received by multiple receiving antennas to achieve full-band and omnidirectional interference. The ground end positioning module locates the position of the ground end, thereby countering the ground end. The drone damage module physically damages the drone to ensure a stable interference effect.

[0007] Preferably, it also includes multiple fixed electrodes and multiple moving electrodes. The upper ends of the multiple columns are circumferentially evenly installed with multiple fixed electrodes. The multiple fixed electrodes are respectively aligned with the multiple receiving antennas. The multiple moving electrodes are respectively installed at the lower end of the transmitting antenna. The multiple moving electrodes are respectively located in the transmitting direction of the multiple transmitting antennas. The multiple moving electrodes are respectively aligned with the multiple fixed electrodes. The analysis module of the main box highlights the multiple fixed electrodes aligned with the multiple receiving antennas that generate the strongest electrical signals. When the multiple servo motors drive the multiple transmitting antennas to rotate, the multiple transmitting antennas respectively drive the multiple moving electrodes to rotate synchronously. When the multiple moving electrodes are respectively aligned with the multiple fixed electrodes that are highlighted, the multiple servo motors stop rotating. At this time, the transmitting directions of the multiple transmitting antennas are all towards the direction of the drone, thereby improving the sensitivity of the multiple transmitting antennas.

[0008] Preferably, it also includes multiple brackets and multiple moving electrodes 2, the upper ends of the multiple brackets are respectively connected to the multiple transmitting antennas 2, the lower ends of the multiple brackets are installed with moving electrodes 2, and the multiple moving electrodes 2 are respectively aligned with multiple fixed electrodes; the multiple moving electrodes 2 are located on the outside of the multiple fixed electrodes to avoid collision with the moving electrode 1, the analysis module of the main box will highlight the multiple fixed electrodes aligned with the multiple receiving antennas that generate the strongest electrical signal 2, when the multiple servo motors 2 drive the multiple transmitting antennas 2 to rotate, the multiple transmitting antennas 2 respectively drive the multiple brackets and moving electrodes 2 to rotate synchronously, and when the multiple moving electrodes 2 are respectively aligned with the multiple fixed electrodes that are highlighted, the multiple servo motors 2 stop rotating. At this time, the transmission directions of the multiple transmitting antennas 2 are all towards the direction of the ground end of the drone, thereby improving the sensitivity of the multiple transmitting antennas 2.

[0009] Preferably, the ground-end positioning module is installed in the main box, and the ground-end positioning module is used to locate the geographical location of the ground end. The ground-end positioning module includes a self-positioning unit, a marking model unit, a fitting unit, a reading unit and a navigation map unit. The self-positioning unit is used to locate the geographical location of the main box, and the navigation map module is used to understand the geographical environment around the main box and cooperate with the self-positioning unit to locate the main box on the map; the marking model unit has a built-in positioning model, the positioning model numbers multiple columns, the positioning model numbers multiple receiving antennas, and the positioning model plans the area around the main box into several positioning grids, and the several positioning grids are based on the columns. and the numbers of the receiving antennas are marked, the fitting unit is used to fit several positioning grids of the marking model unit with the map, so that each positioning grid corresponds to the geographical location on the map, the reading unit is used to read the numbers of the multiple receiving antennas facing the UAV and the numbers of the multiple receiving antennas on the multiple columns facing the ground end of the UAV, and determine the numbers of the corresponding positioning grids, and the determined positioning grid is the probabilistic position of the ground end; the specific construction method of the positioning model is: three columns are set, and thirty-six receiving antennas are set on the columns, and the three columns are marked as A, B, and C respectively. The thirty-six receiving antennas on A are marked as a1, a2, and a3. a2, a3...a36, a1, a2, a3...a36 divide the space around A into 36 sectors, and mark them as A1, A2, A3...A36 in sequence; the 36 receiving antennas on B are marked as b1, b2, b3...b36, b1, b2, b3...b36 divide the space around B into 36 sectors, and mark them as B1, B2, B3...B36 in sequence; the 36 receiving antennas on C are marked as c1, c2, c3...c36, c1, c2, c3...c36 divide the space around C into 36 sectors, and mark them as C1 in sequence , C2, C3...C36; let Ax be any one of A1, A2, A3...A36; By be any one of B1, B2, B3...B36; Cz be any one of C1, C2, C3...C36, mark the area where Ax and By intersect, that is, the secondary positioning grid, as AxBy; mark the area where Ax and Cz intersect, that is, the secondary positioning grid, as AxCz; mark the area where By and Cz intersect, that is, the secondary positioning grid, as ByCz; mark the area where Ax, By and Cz intersect, that is, the main positioning grid, as AxByCz; the main positioning grid is the high-probability position of the ground end, and the secondary positioning grid is the probable position of the ground end.

[0010] The fitting unit locates the main chassis in the map provided by the navigation map unit according to the positioning information of the self-positioning unit, and fits the positioning model in the navigation map with the main chassis as the center. The reading unit reads the numbers Ax, By and Cz of the receiving antennas on the three columns A, B and C facing the ground end, thereby determining the numbers AxByCz of the main positioning grid and AxBy, AxCz and ByCz of the secondary positioning grids; the specific location areas of the corresponding main positioning grid AxByCz and the specific location areas of the secondary positioning grids AxBy, AxCz and ByCz are obtained in the navigation map to complete the probabilistic positioning of the ground end of the UAV. The method is simple and improves the positioning speed by real pre-marking.

[0011] Preferably, it also includes a communication module, which is installed on the main box. The communication module is communicatively connected to the ground positioning module, and the communication module is used to send the position data of the UAV ground terminal obtained by the ground positioning module; the communication module sends the position information of the UAV ground terminal obtained to the countermeasure unit, and the countermeasure unit first counters to the high-probability position. If the UAV ground terminal signal has not disappeared, the probabilistic position is countered, and the countermeasure range is expanded with the high-probability position as the center until the UAV ground terminal signal disappears, completely eliminating the harm of illegal UAVs.

[0012] Preferably, it also includes a radar base and multiple radar modules. The radar base is installed in the middle of the installation plate, and multiple radar modules are installed on the radar base. The radar module can be a laser radar, a phased array radar, etc. By installing the radar base and the radar module, the drone can be detected at a long distance, the drone can be discovered earlier, and multiple transmitting antennas can be guided to interfere, thereby improving accuracy.

[0013] Preferably, it also includes a middle column, a push rod, a lower support arm, an upper support arm, a ball head rod and a ball seat, and three push rods, lower support arms, upper support arms, ball head rods and ball seats are provided. The middle column is installed in the middle of the main box, and the three push rods are evenly arranged around the circumference of the middle column. The inner ends of the three push rods are rotatably connected to the middle column, and the outer ends of the three push rods are rotatably connected to multiple hinge shafts respectively. The lower ends of the multiple lower support arms are rotatably installed on the main box, and the upper ends of the three lower support arms are rotatably connected to multiple hinge shafts respectively. The lower ends of the three upper support arms are rotatably connected to the three hinge shafts respectively. Ball head rods are installed at the upper ends of the three upper arms, and the three ball head rods are movably connected to the three ball sockets respectively, and the circumferences of the three ball sockets are evenly installed on the lower end surface of the mounting plate; the three push rods are respectively extended and retracted, so that the three push rods respectively push the three lower arms and the three upper arms through the three hinge shafts to vertically push up the mounting plate, or the three lower arms and the three upper arms are folded to lower the mounting plate, thereby adjusting the pitch angle and direction of the mounting plate, thereby adjusting the angle of the interference electromagnetic waves emitted by the multiple transmitting antennas one and the multiple transmitting antennas two, and improving the interference effect.

[0014] Preferably, the drone damage module includes a microwave pulse antenna and an infrared sensor, the microwave pulse antenna is installed on the transmitting antenna one, and the infrared sensor is installed on the mounting plate; after the multiple transmitting antennas are directed towards the drone, microwaves are emitted to the drone through the microwave pulse antenna, and the microwaves heat and damage the electronic components of the drone, thereby damaging the drone, and the infrared sensor detects the temperature changes of the drone and evaluates the damage effect.

[0015] Preferably, the UAV damage module includes a cluster antenna, which is installed on the transmitting antenna one; the frequency of the electromagnetic waves emitted by the cluster antenna is the same as the natural frequency of the UAV's motor coil. The resonant frequency of the motor is determined by its parameters such as inductance and capacitance. The specific calculation formula is: resonant frequency = 1 / (2π√LC); the electromagnetic waves of the resonant frequency cause the UAV's motor coil to resonate. When the motor coil resonates, it will heat up and the power will decrease, causing the UAV to fall and be damaged.

[0016] Compared with the existing technology, the beneficial effects of the present invention are: it can interfere with the drone and the ground control end at the same time, improve the interference effect, and has a directional function, and concentrates on transmitting interference signals in the direction of the drone and the ground control end, reducing energy consumption, improving the interference effect, reducing false interference to normal equipment, and having better accuracy. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] Figure 1 It is a structural schematic diagram of the present invention; Figure 2 It is a front schematic view of the present invention; Figure 3 It is a structural diagram of the mounting plate, column, receiving antenna, transmitting antenna 1 and transmitting antenna 2; Figure 4 It is a structural diagram of the main chassis, mounting plate, column, middle column, push rod, lower support arm and upper support arm; Figure 5 It is a structural diagram of the exploded state of the column, receiving antenna, servo motor 1, transmitting antenna 1, servo motor 2 and transmitting antenna 2; Figure 6 Figure 1 Schematic diagram of the local enlarged structure at D in the middle; Figure 7 yes Figure 5 Schematic diagram of the local enlarged structure at E in the middle; Figure 8 yes Figure 5 Schematic diagram of the local enlarged structure at F in the middle; Figure 9 yes Figure 5 Schematic diagram of the local enlarged structure at G in the middle; Figure 10 is a schematic diagram of the positioning model; Figure 11 This is a schematic diagram of the main chassis; Figure 12 This is a schematic diagram of the ground-side positioning module; Figure 13 This is a schematic diagram of the drone damage module.

[0018] Markings in the accompanying drawings: 1. Main chassis; 2. Mounting plate; 3. Column; 4. Receiving antenna; 5. Servo motor 1; 6. Transmitting antenna 1; 7. Servo motor 2; 8. Transmitting antenna 2; 9. Fixed electrode; 10. Moving electrode 1; 11. Bracket; 12. Moving electrode 2; 13. Communication module; 14. Radar base; 15. Radar module; 16. Center column; 17. Push rod; 18. Lower support arm; 19. Upper support arm; 20. Ball head rod; 21. Ball seat. DETAILED DESCRIPTION

[0019] To facilitate understanding of the present invention, the present invention will be described more fully below with reference to the accompanying drawings. The present invention can be implemented in many different forms and is not limited to the embodiments described herein. On the contrary, the purpose of providing these embodiments is to make the disclosure of the present invention more thorough and comprehensive.

[0020] Example 1 like Figures 1 to 9 and Figure 11As shown, an omnidirectional multi-band UAV jamming antenna includes a main case 1 and a mounting plate 2, and the mounting plate 2 is installed on the main case 1; it also includes multiple columns 3, multiple receiving antennas 4, multiple servo motors 5, multiple transmitting antennas 6, multiple servo motors 7 and multiple transmitting antennas 8, multiple columns 3 are vertically installed on the mounting plate 2, multiple columns 3 are arranged in a matrix, multiple receiving antennas 4 are evenly installed on the outer walls of the multiple columns 3, multiple servo motors 5 are respectively installed on the top of the multiple columns 3, multiple transmitting antennas 6 are respectively installed on the output shafts of the multiple servo motors 5, multiple transmitting antennas 6 are respectively arranged concentrically with the multiple columns 3, multiple servo motors 7 are respectively installed on the top of the multiple transmitting antennas 6, and multiple transmitting antennas 8 are respectively installed on the output shafts of the multiple servo motors 7; the main case 1 includes a signal amplifier, a clock module, an analysis module, a storage module, a ground positioning module and a UAV damage module, and the signal amplifier is used to amplify the signals received by the multiple receiving antennas 4 The clock module is used to modify the timestamp of the amplified signal. After the timestamp is modified, the amplified signal is transmitted through multiple transmitting antennas 1 6 and multiple transmitting antennas 2 8. The analysis module is used to analyze the received signal information and classify the signals. The storage module is used to store the classified signals. The ground-end positioning module is used to locate the position of the ground end. The UAV damage module is used to damage the UAV; it also includes multiple fixed electrodes 9 and multiple moving electrodes 10. The upper ends of the multiple columns 3 are uniformly installed with multiple fixed electrodes 9. The multiple fixed electrodes 9 are respectively aligned with the multiple receiving antennas 4. The multiple moving electrodes 10 are respectively installed at the lower ends of the transmitting antenna 1 6. The multiple moving electrodes 10 are respectively located in the transmission direction of the multiple transmitting antennas 1 6. The multiple moving electrodes 10 are respectively aligned with the multiple fixed electrodes 9; it also includes multiple brackets 11 and multiple moving electrodes 2 12. The upper ends of the multiple brackets 11 are respectively connected to the multiple transmitting antennas 2 8. The lower ends of the multiple brackets 11 are all installed with moving electrodes 2 12. The multiple moving electrodes 2 12 are respectively aligned with the multiple fixed electrodes 9.

[0021] Three upright posts 3 are provided, and the three upright posts 3 are arranged in an equilateral triangle. Thirty-six receiving antennas 4 are installed on the upright posts 3. The thirty-six receiving antennas 4 on the three upright posts 3 receive signals in one direction respectively. When working, multiple receiving antennas 4 receive signals sent by the UAV and signals sent by the UAV ground end. The multiple receiving antennas 4 generate electrical signal 1 of different intensities according to the strength of the signals sent by the UAV received. At the same time, the multiple receiving antennas 4 generate electrical signal 2 of different intensities according to the strength of the signals sent by the UAV ground end received. The controller in the main box 1 selects the receiving antenna 4 that generates the strongest electrical signal 1 and the receiving antenna 4 that generates the strongest electrical signal 2. At this time, the three receiving antennas 4 that generate the strongest electrical signal 1 are all facing Towards the direction of the drone, the three receiving antennas 4 that generate the strongest electrical signal 2 are all facing the direction of the drone's ground end. The analysis module of the main chassis 1 highlights the multiple fixed electrodes 9 that are aligned with the multiple receiving antennas 4 that generate the strongest electrical signal 1. When the multiple servo motors 15 drive the multiple transmitting antennas 16 to rotate, the multiple transmitting antennas 16 respectively drive the multiple moving electrodes 10 to rotate synchronously. When the multiple moving electrodes 10 are respectively aligned with the multiple fixed electrodes 9 that are highlighted, the multiple servo motors 5 stop rotating. At this time, the transmission directions of the multiple transmitting antennas 6 are all facing the direction of the drone, thereby improving the sensitivity of the multiple transmitting antennas 6; the multiple moving electrodes 12 are located on the outside of the multiple fixed electrodes 9 to avoid collision with the moving electrodes 10 , the analysis module of the main box 1 highlights the multiple fixed electrodes 9 that are aligned with the multiple receiving antennas 4 that generate the strongest electrical signal 2. When the multiple servo motors 27 drive the multiple transmitting antennas 28 to rotate, the multiple transmitting antennas 28 respectively drive the multiple brackets 11 and the moving electrodes 2 12 to rotate synchronously. When the multiple moving electrodes 2 12 are respectively aligned with the multiple fixed electrodes 9 that are highlighted, the multiple servo motors 2 7 stop rotating. At this time, the transmission directions of the multiple transmitting antennas 2 8 are all towards the direction of the ground end of the drone, so that the transmission directions of the three transmitting antennas 1 6 are respectively aligned with the three receiving antennas 4 that generate the strongest electrical signal 1. The three transmitting antennas 1 6 emit interfering electromagnetic wave signals to interfere with the drone, and the drone is in the three transmitting positions. The interference electromagnetic wave signals of the three transmitting antennas 28 are in the intersection area of the interference electromagnetic wave signals of the transmitting antenna 1 6, thereby enhancing the interference effect on the UAV, and at the same time, the transmission directions of the three transmitting antennas 28 are aligned with the three receiving antennas 4 that generate the strongest electrical signal 2. The three transmitting antennas 28 send out interference electromagnetic wave signals to interfere with the ground end of the UAV, and the ground end of the UAV is in the intersection area of the interference electromagnetic wave signals of the three transmitting antennas 28, thereby enhancing the interference effect on the ground end of the UAV. Compared with the existing technology, the UAV and the ground control end are interfered with at the same time, thereby improving the interference effect, and having a directional function, and concentrating on transmitting interference signals in the direction of the UAV and the ground control end, thereby reducing energy consumption, improving the interference effect, and reducing the false interference to normal equipment.

[0022] After the multiple receiving antennas 4 receive the drone signal and the ground signal, the signal amplifier amplifies the signal, and the clock module modifies the timestamp of the amplified signal to generate a repetitive strong signal of the same type as the signal transmitted by the drone and the ground. These strong signals will block the communication channel between the drone and the ground, increase the amount of signals that the processors of the drone and the ground need to process, causing the processor to overload and freeze, or insert interference signals into the drone's command list, causing the drone to execute wrong commands, thereby interfering with the drone and the ground. The interference signal is converted at any time with the frequency hopping of the signals received by the multiple receiving antennas 4 to achieve full-band and omnidirectional interference. The ground positioning module locates the position of the ground terminal, thereby countering the ground terminal. The drone damage module physically damages the drone to ensure a stable interference effect.

[0023] Example 2 like Figure 1 、 Figure 2 、 Figure 10 and Figure 11 As shown, on the basis of Example 1, the ground-end positioning module is installed in the main box 1, and the ground-end positioning module is used to locate the geographical location of the ground end. The ground-end positioning module includes a self-positioning unit, a marking model unit, a fitting unit, a reading unit and a navigation map unit. The self-positioning unit is used to locate the geographical location of the main box 1, and the navigation map module is used to understand the geographical environment around the main box 1 and cooperate with the self-positioning unit to locate the main box 1 on the map; the marking model unit has a built-in positioning model, the positioning model numbers multiple columns 3, the positioning model numbers multiple receiving antennas 4, and the positioning model plans the area around the main box 1 into a number of positioning grids, and the multiple positioning grids are based on the columns 3. The numbers of the columns 3 and the receiving antennas 4 are marked, and the fitting unit is used to fit several positioning grids of the marking model unit with the map, so that each positioning grid corresponds to the geographical location on the map. The reading unit is used to read the numbers of the multiple receiving antennas 4 facing the drone and the numbers of the multiple receiving antennas 4 on the multiple columns 3 facing the ground end of the drone, and determine the numbers of the corresponding positioning grids. The determined positioning grids are the probabilistic positions of the ground end. It also includes a communication module 13, which is installed on the main box 1. The communication module 13 is communicatively connected to the ground end positioning module. The communication module 13 is used to send the position data of the drone ground end obtained by the ground end positioning module.

[0024] The specific construction method of the positioning model is as follows: three columns 3 are set, and thirty-six receiving antennas 4 are set on the columns 3. The three columns 3 are marked as A, B, and C respectively. The thirty-six receiving antennas 4 on A are marked as a1, a2, a3...a36, a1, a2, a3...a36 in sequence, dividing the space around A into thirty-six sectors and marking them as A1, A2, A3...A36 in sequence; the thirty-six receiving antennas 4 on B are marked as b1, b2, b3...b36, b1, b2, b3...b36 in sequence, dividing the space around B into thirty-six sectors and marking them as B1, B2, B3...B36 in sequence; the thirty-six receiving antennas 4 on C are marked as c1, c2, c3...c36, c 1. c2, c3...c36. Divide the space around C into 36 sectors and label them C1, C2, C3...C36 in sequence. Let Ax be any one of A1, A2, A3...A36; By be any one of B1, B2, B3...B36; and Cz be any one of C1, C2, C3...C36. Label the area where Ax and By intersect, i.e., the secondary positioning grid, as AxBy; label the area where Ax and Cz intersect, i.e., the secondary positioning grid, as AxCz; label the area where By and Cz intersect, i.e., the secondary positioning grid, as ByCz; label the area where Ax, By, and Cz intersect, i.e., the primary positioning grid, as AxByCz. The primary positioning grid is the high-probability position of the ground terminal, and the secondary positioning grid is the probability position of the ground terminal. The fitting unit locates the main chassis 1 in the map provided by the navigation map unit according to the positioning information of the self-positioning unit, and fits the positioning model with the main chassis 1 as the center in the navigation map. The reading unit reads the numbers Ax, By, and Cz of the receiving antennas 4 on the three columns 3 of A, B, and C facing the ground end, thereby determining the numbers AxByCz of the main positioning grid and the numbers AxBy, AxCz, and ByCz of the secondary positioning grids; the specific location area of the corresponding main positioning grid AxByCz and the specific location area of the secondary positioning grids AxBy, AxCz, and ByCz are obtained in the navigation map to complete the probabilistic positioning of the ground end of the UAV. The method is simple and improves the positioning speed by real pre-marking. The communication module 13 sends the location information of the drone ground end to the countermeasure unit. The countermeasure unit first counters the high-probability position. If the drone ground end signal has not disappeared, it counters the probable position and expands the countermeasure range with the high-probability position as the center until the drone ground end signal disappears, completely eliminating the harm of illegal drones.

[0025] Example 3 like Figure 1 、 Figure 2 、 Figure 11 、 Figure 12 and Figure 13As shown, on the basis of embodiment 1, it also includes a radar base 14 and multiple radar modules 15, the radar base 14 is installed in the middle of the mounting plate 2, and multiple radar modules 15 are installed on the radar base 14; it also includes a center column 16, a push rod 17, a lower support arm 18, an upper support arm 19, a ball head rod 20 and a ball seat 21, and three push rods 17, lower support arm 18, upper support arm 19, ball head rod 20 and ball seat 21 are provided. The center column 16 is installed in the middle of the main box 1, and the three push rods 17 are evenly arranged around the circumference of the center column 16. The inner ends of the three push rods 17 are rotatably connected to the center column 16, and the outer ends of the three push rods 17 are rotatably connected to multiple hinge shafts respectively. The lower end of each lower arm 18 is rotatably mounted on the main chassis 1, the upper ends of the three lower arms 18 are rotatably connected to multiple hinge shafts respectively, the lower ends of the three upper arms 19 are rotatably connected to three hinge shafts respectively, the upper ends of the three upper arms 19 are all installed with ball head rods 20, the three ball head rods 20 are movably connected to three ball sockets 21 respectively, and the three ball sockets 21 are evenly mounted on the lower end surface of the mounting plate 2; the UAV damage module includes a microwave pulse antenna and an infrared sensor, the microwave pulse antenna is mounted on the transmitting antenna 6, and the infrared sensor is mounted on the mounting plate 2; the UAV damage module includes a cluster antenna, and the cluster antenna is mounted on the transmitting antenna 6.

[0026] The radar module 15 can be a laser radar, a phased array radar, etc. By installing the radar base 14 and the radar module 15, the drone can be detected from a distance, the drone can be discovered earlier, and the multiple transmitting antennas 6 can be guided to interfere, thereby improving accuracy; the three push rods 17 are respectively extended and retracted, so that the three push rods 17 respectively push the three lower arms 18 and the three upper arms 19 through the three hinged shafts to vertically push the mounting plate 2 up, or the three lower arms 18 and the three upper arms 19 are folded to lower the mounting plate 2, thereby adjusting the pitch angle and direction of the mounting plate 2, thereby adjusting the angle of the multiple transmitting antennas 16 and the multiple transmitting antennas 28 to transmit interfering electromagnetic waves, thereby improving the interference effect. After the multiple transmitting antennas 6 are directed towards the drone, microwaves are emitted to the drone through the microwave pulse antenna. The microwaves heat and damage the electronic components of the drone, thereby damaging the drone. The infrared sensor detects the temperature change of the drone and evaluates the damage effect; The frequency of the electromagnetic waves emitted by the cluster antenna is the same as the natural frequency of the drone's motor coil. The resonant frequency is determined by the inductance (L) and capacitance (C) of the motor coil, and is calculated as: resonant frequency = 1 / (2π√LC). The electromagnetic waves at the resonant frequency cause the drone's motor coil to resonate. When the motor coil resonates, it heats up and loses power, causing the drone to crash and be damaged.

[0027] like Figures 1 to 13As shown, the present invention is an omnidirectional multi-band UAV jamming antenna. When it is working, first, multiple receiving antennas 4 receive signals emitted by the UAV and signals emitted by the UAV ground end. The multiple receiving antennas 4 generate electrical signals of different strengths according to the strength of the signals received by the UAV. At the same time, the multiple receiving antennas 4 generate electrical signals of different strengths according to the strength of the signals received by the UAV ground end. The controller in the main box 1 selects the receiving antenna 4 that generates the strongest electrical signal 1 and the receiving antenna 4 that generates the strongest electrical signal 2 and highlights the corresponding fixed electrodes 9. At this time, the three receiving antennas 4 that generate the strongest electrical signal 1 are all facing the direction of the UAV, and the three receiving antennas 4 that generate the strongest electrical signal 2 are all facing the direction of the UAV ground end. Then, three servo motors 15 respectively drive the three transmitting antennas 6 to rotate. When the multiple servo motors 15 drive the multiple transmitting antennas 6 to rotate, the multiple transmitting antennas 6 respectively drive the multiple moving electrodes 10 to rotate synchronously. When the multiple moving electrodes 10 are respectively aligned with the multiple fixed electrodes 9 that are highlighted, the multiple servo motors 5 stop rotating. At this time, the transmission directions of the multiple transmitting antennas 6 are all facing the direction of the UAV. When a servo motor 27 drives the multiple transmitting antennas 28 to rotate, the multiple transmitting antennas 28 respectively drive the multiple brackets 11 and the movable electrodes 212 to rotate synchronously. When the multiple movable electrodes 212 are respectively aligned with the multiple fixed electrodes 9 with prominent marks, the multiple servo motors 27 stop rotating. At this time, the transmission directions of the multiple transmitting antennas 28 are all towards the direction of the ground end of the drone. Then the three transmitting antennas 16 emit interfering electromagnetic wave signals to interfere with the drone, and the drone is in the intersection area of the interfering electromagnetic wave signals of the three transmitting antennas 16, thereby enhancing the interference effect on the drone. At the same time, the three servo motors 27 respectively drive the three transmitting antennas 28 to rotate, so that the transmission directions of the three transmitting antennas 28 are respectively aligned with the three receiving antennas 4 that generate the strongest electrical signals 2. The three transmitting antennas 28 emit interfering electromagnetic wave signals to interfere with the ground end of the drone, and the ground end of the drone is in the intersection area of the interfering electromagnetic wave signals of the three transmitting antennas 28, thereby enhancing the interference effect on the ground end of the drone. Finally, the ground end positioning module marks the position of the ground end on the map, so that the countermeasure unit can counter the ground end of the drone, and the drone damage module can physically damage the drone.

[0028] The main functions achieved by the present invention are: 1. It can simultaneously carry out directional interference on the UAV and the ground control terminal, improve the interference effect, reduce energy consumption, improve the interference effect, and have better accuracy; 2. Ability to locate the ground terminal of the drone and support countermeasure units to counter the ground terminal; 3. The pitch angle and orientation of the mounting plate 2 can be adjusted, thereby adjusting the angles at which the multiple transmitting antennas 1 6 and the multiple transmitting antennas 2 8 transmit interfering electromagnetic waves, thereby improving the interference effect; 4. It can destroy drones and interfere with and counter-interference drones such as fiber-optic drones that are resistant to interference.

[0029] The installation method, connection method or setting method of the omnidirectional multi-band UAV jamming antenna of the present invention are all common mechanical methods, and can be implemented as long as they can achieve their beneficial effects; the main box 1, installation plate 2, column 3, receiving antenna 4, servo motor 1 5, transmitting antenna 1 6, servo motor 2 7, transmitting antenna 2 8, fixed electrode 9, moving electrode 1 10, moving electrode 2 12, communication module 13, radar base 14, radar module 15, push rod 17, ball head rod 20, ball seat 21, signal amplifier, clock module, analysis module, storage module, microwave pulse antenna, infrared sensor, and cluster antenna of the omnidirectional multi-band UAV jamming antenna of the present invention are purchased on the market, and technical personnel in this industry only need to install and operate them according to the accompanying instruction manual, without the need for technical personnel in this field to pay creative labor.

[0030] The above is only a preferred embodiment of the present invention. It should be pointed out that for ordinary technicians in this technical field, several improvements and modifications can be made without departing from the technical principles of the present invention. These improvements and modifications should also be regarded as the scope of protection of the present invention.

Claims

1. An omnidirectional multi-band UAV jamming antenna, comprising a main box (1) and a mounting plate (2), wherein the mounting plate (2) is mounted on the main box (1); characterized in that: The invention also includes a plurality of columns (3), a plurality of receiving antennas (4), a plurality of servo motors (5), a plurality of transmitting antennas (6), a plurality of servo motors (7) and a plurality of transmitting antennas (8), wherein the plurality of columns (3) are vertically mounted on the mounting plate (2), the plurality of columns (3) are arranged in a matrix, the plurality of receiving antennas (4) are evenly mounted on the outer walls of the plurality of columns (3), the plurality of servo motors (5) are respectively mounted on the tops of the plurality of columns (3), the plurality of transmitting antennas (6) are respectively mounted on the output shafts of the plurality of servo motors (5), the plurality of transmitting antennas (6) are respectively arranged concentrically with the plurality of columns (3), the plurality of servo motors (7) are respectively mounted on the tops of the plurality of transmitting antennas (6), and the plurality of transmitting antennas (8) are respectively mounted on the output shafts of the plurality of servo motors (7).

2. The omnidirectional multi-band UAV jamming antenna according to claim 1, characterized in that: The main chassis (1) includes a signal amplifier, a clock module, an analysis module, a storage module, a ground terminal positioning module and a UAV damage module. The signal amplifier is used to amplify the signal received by the multiple receiving antennas (4). The clock module is used to modify the timestamp of the amplified signal. After the timestamp is modified, the amplified signal is transmitted through the multiple transmitting antennas 1 (6) and the multiple transmitting antennas 2 (8). The analysis module is used to analyze the received signal information and classify the signal. The storage module is used to store the classified signal. The ground terminal positioning module is used to locate the position of the ground terminal. The UAV interference / damage module is used to damage the UAV.

3. The omnidirectional multi-band UAV jamming antenna according to claim 2, characterized in that: The invention also includes a plurality of fixed electrodes (9) and a plurality of movable electrodes (10). The upper ends of the plurality of columns (3) are uniformly mounted with the plurality of fixed electrodes (9). The plurality of fixed electrodes (9) are aligned with the plurality of receiving antennas (4) respectively. The plurality of movable electrodes (10) are respectively mounted at the lower ends of the transmitting antennas (6). The plurality of movable electrodes (10) are respectively located in the transmitting directions of the plurality of transmitting antennas (6). The plurality of movable electrodes (10) are respectively aligned with the plurality of fixed electrodes (9).

4. The omnidirectional multi-band UAV jamming antenna according to claim 3, characterized in that: It also includes a plurality of brackets (11) and a plurality of moving electrodes (12). The upper ends of the plurality of brackets (11) are respectively connected to the plurality of transmitting antennas (8). The lower ends of the plurality of brackets (11) are all equipped with moving electrodes (12). The plurality of moving electrodes (12) are respectively aligned with the plurality of fixed electrodes (9).

5. The omnidirectional multi-band UAV jamming antenna according to claim 2, characterized in that: The ground terminal positioning module is installed in the main box (1). The ground terminal positioning module is used to locate the geographical location of the ground terminal. The ground terminal positioning module includes a self-positioning unit, a marking model unit, a fitting unit, a reading unit and a navigation map unit. The self-positioning unit is used to locate the geographical location of the main box (1). The navigation map module is used to understand the geographical environment around the main box (1) and cooperate with the self-positioning unit to locate the main box (1) on the map. The marking model unit has a built-in positioning model. The positioning model numbers a plurality of columns (3). The positioning model numbers a plurality of receiving antennas (4). The positioning model plans the area around the main box (1) into a plurality of positioning grids. The plurality of positioning grids are marked according to the numbers of the columns (3) and the receiving antennas (4). The fitting unit is used to fit the plurality of positioning grids of the marking model unit with the map, so that each positioning grid corresponds to the geographical location on the map. The reading unit is used to read the numbers of the plurality of receiving antennas (4) facing the drone and the numbers of the plurality of receiving antennas (4) on the plurality of columns (3) facing the ground terminal of the drone, and determine the numbers of the corresponding positioning grids. The determined positioning grids are the probabilistic positions of the ground terminal.

6. The omnidirectional multi-band UAV jamming antenna according to claim 5, characterized in that: It also includes a communication module (13), which is installed on the main box (1). The communication module (13) is connected to the ground-end positioning module for communication. The communication module (13) is used to send the position data of the ground end of the UAV obtained by the ground-end positioning module.

7. The omnidirectional multi-band UAV jamming antenna according to claim 2, characterized in that: It also includes a radar base (14) and a plurality of radar modules (15), wherein the radar base (14) is installed in the middle of the installation plate (2), and the plurality of radar modules (15) are installed on the radar base (14).

8. The omnidirectional multi-band UAV jamming antenna according to claim 7, characterized in that: It also includes a center column (16), a push rod (17), a lower support arm (18), an upper support arm (19), a ball head rod (20) and a ball seat (21), wherein the push rod (17), the lower support arm (18), the upper support arm (19), the ball head rod (20) and the ball seat (21) are all provided in three pieces, the center column (16) is installed in the middle of the main box (1), the three push rods (17) are evenly arranged around the circumference of the center column (16), the inner ends of the three push rods (17) are rotatably connected to the center column (16), and the three push rods (17) are connected to the center column (16). The outer ends of the lower arms (18) are rotatably connected to the plurality of hinge shafts, the lower ends of the plurality of lower arms (18) are rotatably mounted on the main chassis (1), the upper ends of the three lower arms (18) are rotatably connected to the plurality of hinge shafts, the lower ends of the three upper arms (19) are rotatably connected to the three hinge shafts, the upper ends of the three upper arms (19) are all mounted with ball rods (20), the three ball rods (20) are movably connected to the three ball seats (21), and the three ball seats (21) are evenly mounted on the lower end surface of the mounting plate (2).

9. The omnidirectional multi-band UAV jamming antenna according to claim 2, characterized in that: The UAV damage module includes a microwave pulse antenna and an infrared sensor. The microwave pulse antenna is installed on the transmitting antenna 1 (6), and the infrared sensor is installed on the mounting plate (2).

10. The omnidirectional multi-band UAV jamming antenna according to claim 2, characterized in that: The UAV damage module includes a cluster antenna, which is installed on the transmitting antenna one (6).

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