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WO2017197939A1 - Anti-unmanned aerial vehicle method and system - Google Patents

Anti-unmanned aerial vehicle method and system Download PDF

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Publication number
WO2017197939A1
WO2017197939A1 PCT/CN2017/073895 CN2017073895W WO2017197939A1 WO 2017197939 A1 WO2017197939 A1 WO 2017197939A1 CN 2017073895 W CN2017073895 W CN 2017073895W WO 2017197939 A1 WO2017197939 A1 WO 2017197939A1
Authority
WO
WIPO (PCT)
Prior art keywords
drone
navigation
simulation
signal
navigation signal
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/CN2017/073895
Other languages
French (fr)
Chinese (zh)
Inventor
刘志俭
刘春阳
陈致福
张明
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hunan Matrix Electronic Technology Co Ltd
Original Assignee
Hunan Matrix Electronic Technology Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hunan Matrix Electronic Technology Co Ltd filed Critical Hunan Matrix Electronic Technology Co Ltd
Publication of WO2017197939A1 publication Critical patent/WO2017197939A1/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S19/00Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/38Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
    • G01S19/39Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S19/00Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/01Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/13Receivers
    • G01S19/21Interference related issues ; Issues related to cross-correlation, spoofing or other methods of denial of service
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04KSECRET COMMUNICATION; JAMMING OF COMMUNICATION
    • H04K3/00Jamming of communication; Counter-measures
    • H04K3/80Jamming or countermeasure characterized by its function
    • H04K3/90Jamming or countermeasure characterized by its function related to allowing or preventing navigation or positioning, e.g. GPS

Definitions

  • the present invention relates to the field of anti-UAV technology, and more particularly to a method and system for an anti-UAV.
  • domestic anti-UAVs mainly focus on capturing and destroying drones.
  • the means of implementation include the use of microwave weapons to shoot down, destroy drones and low-altitude interception, such as low-altitude interception using fixed launchers or mobile launchers.
  • the "cannonball” that was fired flew near the target drone, and the magnified net entangled the target, causing its control and power system to fail, and snoring the parachute to ensure that the drone landed smoothly.
  • the system cost of these two methods is very high, the application range is narrow, and the hit rate is not high. Therefore, the economic security of suppressing the "black fly” and counter-production of the drone is an urgent problem to be solved.
  • the present invention provides a method and system for an anti-hand drone that can accurately improve the security of an unattended/manned security zone against the precise induction and counterattack of the black-flying drone.
  • a method of anti-UAV comprising the following steps:
  • S1 a preset safety area, and an antenna is arranged according to the area;
  • S2 a simulation scenario, forming an anti-navigation signal received by the drone by generating simulation location information of the security area
  • S3 The drone enters the edge of the safe area, and replaces the real satellite signal received by the drone by the anti-navigation signal, so that the drone is located outside the safe area.
  • a further improvement to the above technical solution is that, in the S2, the simulation scene is generated based on a high-precision enthalpy of the satellite navigation authorization technology and a corresponding second pulse, and the simulation scenario is Synchronization between the daytime and the real environment.
  • the simulation position information is a position point or a dynamic track deviating from the security area.
  • step S4 the drone re-receives the real satellite signal, drives to the edge of the safe area, and repeats step S3 to cycle.
  • the satellite navigation system includes at least one of BDS, GPS, GLON ASS, GALILEO, QZSS, and GAGAN.
  • the present invention also provides a system for an anti-UAV, comprising a simulation control computer and an anti-navigation signal simulation subsystem, an authorization subsystem, and an antenna feeder subsystem, wherein the simulation control computer provides a human-computer interaction interface, and Sending a running command to the anti-navigation signal simulation subsystem, the anti-navigation signal simulation subsystem outputs an anti-navigation signal of the security area based on a cuckoo clock reference provided by the authorization subsystem, and passes the anti-navigation signal
  • the antenna feed subsystem is transmitted to the drone, and the anti-navigation signal includes simulated position information.
  • a further improvement of the above technical solution is that the simulation position information is a position point or a dynamic track deviating from the safety area.
  • the running instruction includes at least one of setting an anti-navigation signal power magnitude, ephemeris information, a signal modulation mode, an error model, and trajectory information of the simulated security zone.
  • the anti-navigation signal simulation subsystem includes a signal generation module Block
  • the signal generating module includes a baseband unit, an up-conversion unit, and a signal power control unit
  • the baseband unit receives a clock reference of the authorization subsystem, performs vector modulation by the up-conversion unit, and then passes the The signal power control unit outputs an anti-navigation signal to the antenna feed subsystem.
  • the authorization subsystem includes an interconnected frequency processing module, a satellite navigation authorization receiving module, and an application interface module, and the frequency processing module further includes satellite navigation
  • the authorization receiving module performs a system performance monitoring processing unit for monitoring and controlling satellite navigation
  • the application interface module is connected to the baseband unit.
  • the satellite navigation system includes at least one of BDS, GPS, GLON ASS, GALILEO ⁇ QZSS, and GAGAN, or the satellite navigation system includes B DS, GPS, GLONASS, Combined satellite navigation of any two or more of GALILEO, QZSS and GAGAN, the system performance monitoring and processing unit of the satellite navigation monitors and controls the combined satellite navigation to form a hot backup technology.
  • the antenna feeder subsystem comprises a power splitter and at least one antenna, the antenna being arranged at the center and/or the edge of the security zone.
  • the antenna feeder subsystem is an anti-UAV rifle, and the anti-UAV rifle is provided with a circularly polarized antenna for transmitting an anti-navigation signal generated by the anti-navigation signal simulation subsystem.
  • the simulation scenario is based on the satellite navigation authorization technology, and outputs a high-precision ⁇ base and a corresponding second pulse, completely covering any satellite navigation system, and the simulation signal generated by the method is synchronized with the real environment, and a combination can also be established.
  • the satellite navigation system implements monitoring and monitoring of various types of satellite navigation, and uses the hot backup technology to ensure the continuity of the granting second pulse in phase, thereby ensuring the optimality of the system, and outputting high-precision daytime through the application interface module.
  • 1PPS signal improve the reliability of the license, the delay is very low, the decoy effect is good, the drone can be driven away from the safe area according to the anti-navigation signal, or the drone is out of control at the edge of the safe area, The edge of the safe area is lost, causing the drone to fly wrong, or the digital transmission link between the drone and its accusation center is invalid, causing the drone system to collapse;
  • the base station also does not need to set a low-altitude interception defense system.
  • the anti-unmanned aerial vehicle system constructed according to the present invention is economical and has no impact on the surrounding environment, and has wide application range, and is suitable not only for various static important military regions, but also for party and government.
  • the static drone no-fly zone which is built around the clock for a long time, such as the location of the government, prisons, and other major sports conferences, is also suitable for regular patrols of important important roads, regular patrols of large important facilities, and important personnel. Travel team protection, important resource escort protection areas, etc., start the system according to the task, build a dynamic drone no-fly zone, and fundamentally control and counterattack the "black fly" of the drone in the protected area;
  • the antenna or anti-UAV rifle can be flexibly configured according to the safe environment and range, and the anti-navigation signal can accurately induce and counterattack the UAV, effectively improving the unattended/manned security area. Security within;
  • the invention is simple and practical, economical and environmentally friendly, and can accurately and accurately build an accurate anti-UAV system according to the size and environment of the protection area, and output anti-navigation signal power. Linearly controllable, ensuring that it does not interfere with the normal use of the navigation system of other electronic devices around the protected area.
  • FIG. 1 is a flow chart of a method according to an embodiment of the present invention.
  • FIG. 2 is a flow chart of a method according to an embodiment of the present invention.
  • FIG. 3 is a schematic structural diagram of a system according to an embodiment of the present invention.
  • FIG. 4 is a schematic structural diagram of a system according to an embodiment of the present invention.
  • FIG. 5 is a schematic diagram of generating an anti-navigation signal according to an embodiment of the present invention.
  • FIG. 6 is a schematic diagram of a design of an authorization subsystem according to an embodiment of the present invention.
  • [0036] 10 anti-UAV system; 1, simulation control computer; 2, anti-navigation signal simulation subsystem; 21, signal generation module; 211, baseband unit; 212, up-conversion unit; 213, signal power control unit; 3, the authorization subsystem; 31, the frequency processing module; 311, the system performance monitoring and processing unit of satellite navigation; 312, ⁇ frequency standard synthesis unit 312; 32, satellite navigation authorization receiving module; 33, application interface module; 4, antenna feeder subsystem; 41, power distributor; 42, antenna; 5, drone.
  • FIG. 1 a flowchart of a method according to an embodiment of the present invention: a method for an anti-UAV, comprising the following steps: S1: preset a security area, and arranging an antenna according to the area;
  • S2 simulating the scene, forming an anti-navigation signal received by the drone by generating location information of the security area
  • a safe area range For an area that needs to improve security, set a safe area range, and arrange an antenna according to the size of the security area, for example, by setting a central coordinate point of the area, or a peripheral coordinate point, by calculating factors such as antenna gain and free space loss, A reasonable edge antenna is set; in the simulation scenario, the simulated position information in the simulation scene is a fraudulent position signal deviating from the security area, and the anti-navigation signal that can be received by the drone is transmitted through the edge antenna, and the drone enters the security area.
  • the edge switching from receiving the real satellite signal to receiving the anti-navigation signal with the location information of the simulated security zone, so that the drone can not identify the real target area, resulting in the inability to enter the security zone, always in the security zone
  • the reliable control of the drone "black fly" in a fixed security area makes the safe area a "no-fly" area.
  • This static security area can be applied to small laboratories, conference rooms, and stadiums. Important military areas such as schools, hospitals, and party and government Off the seat of important places, such as prisons, conferences and other major sports, to build a full inch long all-weather period laid drone-fly zone, to form an effective barrier against the black fly UAVs.
  • the preset safety zone is a moving safety zone, such as a running fleet driving zone
  • the antenna is installed on the fleet, and as the team moves together, the location information of the security zone in the simulation scenario is A positional information deviating from the safe area, transmitted through the antenna to the anti-navigation signal that the drone can receive, when the "black-flying" drone approaches the edge of the safe area, switching from receiving the real satellite signal to receiving the one Anti-navigation signal with simulated safety zone location information, making the drone unrecognizable
  • the real target area which leads to the inability to follow the driving team into the safe area, is always outside the safe area.
  • this dynamic safety area can be applied to regular patrols of important roads, regular patrols of large important facilities, and important personnel travel.
  • the system is started according to the mission requirements, and the dynamic drone no-fly zone is constructed.
  • the system launches anti-navigation signals to realize the deception blocking of the black fly drone navigation components on the specific exercise line. Barrier black fly drone.
  • a high-precision ⁇ basis and a corresponding second pulse generated by the satellite navigation authorization technology are generated in the simulation scenario, and the diurnal and real environment of the simulation scenario are performed. Synchronization, delay control in nanoseconds.
  • the method simulation generates an anti-navigation signal whose position actually deviates from the protection area. Due to the real synchronization with the real environment, the anti-navigation signal has a very low delay, the decoy effect is good, and the output anti-navigation signal power is linearly controllable, ensuring that it is not It will interfere with the normal use of other navigation systems in and around the protected area.
  • the simulation position information in the simulation scenario is a position point or a dynamic trajectory deviating from the security area, and may be a real simulation scene or a virtual simulation scene, for example, a real coordinate position of the security area to be protected is in a certain Xicheng District No. 100, and the location of the simulation can be set to No. 1 in Xicheng District of a certain city.
  • No. 1 of Xicheng District of a certain city can be a real point in reality, or simulate a change.
  • Dynamic trajectories or simulations based on dynamic safety zones, are dynamic trajectories or static points or locations that are constantly changing, and these location points or dynamic trajectories are transmitted through the antenna to the incoming drone in the form of anti-navigation signals.
  • a further improvement to the above technical solution is that, in the S3, the drone is located outside the security zone, including two cases, one of which is that the drone drives away from the security zone according to the anti-navigation signal, It is that the drone is out of control at the edge of the safe area, the trek at the edge of the safe area causes the drone to fly wrong, or the digital transmission link between the drone and its accusation center fails, resulting in the drone system breakdown.
  • step S4 the drone re-receives the real satellite signal, drives to the edge of the safe area, and repeats step S3 to cycle.
  • the drone flies to the edge of the security zone according to the alleged path, unintentionally switching from receiving the real satellite position signal to receiving the anti-navigation signal, and receiving the simulated scene as a position away from the safe area or the inverse of the dynamic trajectory Navigation signal ⁇ , according to allegations with him
  • the path is compared and it is found that the safe area is not the destination location to be called, and the drone re-receives the real satellite signal after relocating from the safe area, subject to the drone's alleged path flight, and enters the safe area.
  • the satellite navigation system includes at least one of BDS, GPS, GLONASS, GALILEO ⁇ QZSS and GAGAN, and can be compatible with any satellite navigation system, and has a wide application range, and can also implement any two kinds of satellite navigation. Or a combination of multiple, through the hot backup technology, to ensure the continuity of the second pulse in the phase, in this program to determine the satellite source switching ⁇ , first determine the stable phase difference between the system and the setting time, respectively, immediately Switching and smooth switching to complete the satellite source switching, thus ensuring the optimality of satellite navigation switching, thereby outputting high-precision inter-day information and 1PPS signals, and improving the reliability of satellite navigation authorization.
  • GPS Global Positioning System
  • Glonass is the GLONAS system, which is the abbreviation of the Russian “GLOBAL NAVIGATION SATELLITE SYSTEM”
  • GALILEO Globalileo Positioning System
  • BDS BeiDou Navigation Satellite
  • GAGAN GPS Aided Geo Augmented Navigation
  • the present invention also provides an anti-UAV system 10, as shown in FIG. 3, including a simulation control computer 1 and an anti-navigation signal simulation subsystem 2, an authorization subsystem 3, an antenna feeder subsystem 4, and simulation
  • the control computer 1 provides a human-computer interaction interface, and sends a running command to the anti-navigation signal simulation subsystem 2, and the anti-navigation signal simulation subsystem 2 simulates an anti-navigation signal of the security area according to the ⁇ clock reference of the authorization subsystem 3 And transmitting an anti-navigation signal to the drone 5 through the antenna feeder subsystem 4, where the anti-navigation signal is simulated location information of the security zone.
  • the simulated location information is a location point or a dynamic trajectory that deviates from the security zone.
  • the running instruction includes at least one of setting an inverse navigation signal power magnitude, ephemeris information, a signal modulation mode, an error model, and a trajectory information of the simulated security zone, and further improving the foregoing technical solution is as shown in the figure
  • the anti-navigation signal simulation subsystem 2 includes a signal generation module 21, signal generation
  • the module 21 includes a baseband unit 211, an up-conversion unit 212, and a signal power control unit 213.
  • the baseband unit 211 receives the clock reference of the authorization subsystem 3, is vector-modulated by the up-conversion unit 212, and passes through the signal power control unit. 213 outputs an anti-navigation signal to the antenna feeder subsystem.
  • the baseband unit 211 adopts digital signal processing technology, and is composed of a baseband FPGA and a baseband DA, and performs precise delay control and code and carrier phase control of the digital baseband signal together.
  • the baseband unit 211 exchanges data and instructions through the data bus and the simulation control computer 1. , including navigation messages, observation data, status control, and parameter settings.
  • the baseband unit 211 analog signal output mode is used to generate an IQ differential pair signal, and is vector-modulated by the up-conversion unit 212, and then outputted to the real-world synchronization anti-navigation signal through the signal power control unit 213.
  • FIG. 5 is a schematic diagram of the design of the authorization subsystem, wherein the authorization subsystem 3 includes an interconnected frequency processing module 31, a satellite navigation authorization receiving module 32, and an application interface module 33.
  • the processing module 31 further includes a system performance monitoring processing unit 311 for satellite navigation for monitoring and controlling the satellite navigation receiving module 32, and a chirp frequency synthesizing unit 312.
  • the chirp frequency synthesizing unit 312 in this embodiment adopts high precision.
  • the all-digital phase discrimination and high-precision DDS method separates the frequency generation from the correction, and the oscillator operates in a free-running mode.
  • the phase detector adopts the inter-turn expansion technology, which makes the phase resolution of the phase detector reach 0.5 ns, thus solving the high-precision requirement of the phase detector, and intelligently filtering the data obtained from the high-precision phase detector, which will generate
  • the generated clock difference data is sent to the DDS to complete the correction of the local clock, and the differential frequency standard output is generated, and the noise reduction processing is performed through the filter.
  • the initially corrected frequency is sent to the pulse synthesizer, and after entering the debounce and forming circuit, the zero value correction and pulse width control of the second pulse are completed, and the second pulse signal is output through the driving circuit.
  • the application interface module 34 is connected to the baseband unit 211 of the signal generation module 21 in the anti-navigation signal simulation subsystem 2, and the clock reference of the authorization subsystem 3 is transmitted to the baseband unit 211 through the application interface module 34, and is passed through the up-conversion unit 212.
  • the vector modulation is then output to the antenna feed subsystem by the signal power control unit 213 to output an anti-navigation signal.
  • the satellite navigation system includes at least one of BDS, GPS, GLONASS, GALILEO ⁇ QZSS, and GA GAN, and may be any two or more of BDS, GPS, GLONASS, GALILEO, QZSS, and GA GAN.
  • this anti-UAV system is compatible with any one or two or more combined satellite navigation systems.
  • BDS With the GPS system, the BDS and GPS targets are in poor system, The hopping of the target is usually unable to guarantee the continuity of the second pulse signal in phase. As shown in FIG. 5 and FIG.
  • the system performance monitoring and processing unit 311 of the satellite navigation system of the authorization subsystem can perform monitoring and control processing on the BDS and the GPS single system respectively, and form a hot backup by using the two.
  • the technology guarantees the continuity of the pulsed second pulse in phase, ensuring the continuity of the two or more satellite navigation grants the second pulse in phase.
  • the first judgment is made.
  • the stable phase difference between the daytime and the set time, respectively, the immediate switching and smooth switching to complete the satellite source switching thus ensuring the optimality of satellite navigation switching, thereby outputting high-precision inter-turn information, 1PPS signal, and improving the satellite Navigating the reliability of the license.
  • the anti-navigation signal simulation subsystem 2 in the system generates a deceptively excellent simulation signal based on the high-precision inter-time synchronization system, and the signal strength is stronger than the real signal by more than 10 dB, ensuring The drone smoothly and unconsciously switches to receive the anti-navigation signal generated by the scheme at the edge of the security area, thereby achieving the effect of deception, driving away from the security area or out of control at the edge of the security area.
  • the anti-navigation signal power output from the peer is linearly controllable, ensuring that it does not interfere with the normal use of other navigation systems around the safe area.
  • the antenna feeder subsystem 4 includes a power splitter 41 and at least one antenna 42 disposed at the center and/or edge of the security area, according to the topography of the security area and Environment and other factors, such as setting the center coordinate point of the area, or the surrounding coordinate points, by calculating the link loss, antenna gain, free space loss and other factors, set a reasonable number and spacing of the antenna 42, not too small, send
  • the anti-navigation signal strength is too weak, so that the drone can't receive it; nor is it too much, which causes the transmitted anti-navigation signal to be too strong, affecting the operation of electronic devices in or around the area.
  • the anti-navigation signal simulation subsystem 2 controls the software to load the pre-stored simulation scene, and controls the output of the anti-navigation signal power.
  • the anti-navigation signal is transmitted to the antenna 42 through the power amplifier of the power distributor 41, and the radiation covers the entire security area, thereby realizing the area becomes In the no-fly zone, in the range of conventional fixed security areas (such as schools, hospitals, stadiums), the antenna 42 can be placed on the roof, or at the specific coordinate position on the edge of the security zone; for example, regular patrols following important roads, large important facilities
  • the antenna feeder subsystem 4 is replaced by an anti-UAV rifle, and the anti-UAV rifle is provided with a circle.
  • Polarized antenna used to launch the anti-navigation signal generated by the anti-navigation signal simulation subsystem 2, holding the anti-UAV rifle in the guarded security area, and launching the anti-navigation signal generated by the anti-navigation signal simulation subsystem 2 through the circularly polarized antenna The signal effectively and accurately combats the alien invading drone.
  • the solution can choose whether to deploy the antenna feeder subsystem or the anti-UAV rifle equipment according to the environment, area, and whether there is any person to be secured.
  • the scheme realizes the accurate induction and counterattack of the anti-navigation signal to the black-flying drone, effectively improving the security in the unattended/manned security area, and is suitable for small to laboratories, conference rooms, and large stadiums. Schools, hospitals, prisons, etc., covering static or dynamic security areas.
  • the invention is simple and practical, economical and environmentally friendly, and can accurately and quickly build an accurate and reliable anti-UAV system according to the size and environment of the protection area.
  • the embodiments of the present invention can be applied to the technical field of anti-UAV.
  • the embodiment of the present invention can accurately induce and counterattack the black-flying drone, and effectively improve the unmanned/manned security area.
  • Security suitable for small to laboratories, conference rooms, as large as stadiums, schools, hospitals, prisons, etc., covering static or dynamic security areas.
  • the invention is simple and practical, economical and environmentally friendly, and can flexibly and quickly build an accurate and reliable anti-UAV system according to the size and environment of the protection area.

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  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)
  • Signal Processing (AREA)

Abstract

An anti-unmanned aerial vehicle method and system (10). The method comprises: presetting a safety area and arranging antennas according to an area of coverage (S1); simulating a scene, and forming, by generating simulation location information of the safety area, an anti-navigation signal to be received by an unmanned aerial vehicle (S2); and replacing a real satellite signal to be received by the unmanned aerial vehicle with the anti-navigation signal when the unmanned aerial vehicle moves to the boundary of the safety area, thereby keeping the unmanned aerial vehicle out of the safety area (S3). The anti-unmanned aerial vehicle system (10) comprises a simulation control computer (1), an anti-navigation signal simulation sub-system (2), a timing sub-system (3), and an antenna feed sub-system (4). The simulation control computer (1) sends an operating instruction to the anti-navigation signal simulation sub-system (2); the anti-navigation signal simulation sub-system (2) simulates and outputs an anti-navigation signal of a safety area on the basis of a clock reference provided by the timing sub-system (3) and transmits the anti-navigation signal to an unmanned aerial vehicle by means of the antenna feed sub-system (4).

Description

发明名称:一种反无人机的方法和系统  Title of Invention: A Method and System for Anti-Unmanned Aerial Vehicles

[0001] 本申请要求于 2016年 05月 19日提交中国专利局、 申请号为 201610338491.X、 发 明名称为"一种反无人机的方法和系统"的中国专利申请的优先权, 其全部内容 通过引用结合在本申请中。  [0001] The present application claims priority to Chinese Patent Application No. 201610338491.X, entitled "A Method and System for Anti-Unmanned Aerial Vehicles", filed on May 19, 2016. The content is incorporated herein by reference.

技术领域  Technical field

[0002] 本发明涉及反无人机领域技术, 尤其是指一种反无人机的方法和系统。  [0002] The present invention relates to the field of anti-UAV technology, and more particularly to a method and system for an anti-UAV.

背景技术  Background technique

[0003] 随着无人机幵源工程的不断成熟, 无人机的制造成本和使用成本不断降低; 大 量涌现的无人机研发、 制造、 应用公司也助推了民用无人机的普及, 但同吋也 对人们带来了一系列的困扰, 通过无人机可以随意偷窥, 窃取区域内的隐私信 息或者存在投放危险物品等重大隐患。  [0003] With the continuous maturity of the UAV's power source project, the manufacturing cost and use cost of the UAV have been continuously reduced; a large number of UAV R&D, manufacturing, and application companies have also boosted the popularity of civilian UAVs. However, the peers have also brought a series of troubles to people. The drone can sneak at random, steal private information in the area or have major hidden dangers such as placing dangerous goods.

[0004] 当前, 国内反无人机以捕获、 摧毁无人机为主, 实现手段主要包括使用微波武 器击落、 摧毁无人机和低空拦截等, 例如低空拦截采用固定发射架或机动发射 架, 射出的 "炮弹 "飞临目标无人机附近吋, 施放大网缠住目标, 令其操纵和动力 系统失灵, 并打幵降落伞保证无人机平稳落地。 但这 2种方式的系统造价都很高 , 应用范围较窄, 命中率不高, 因此经济安全的抑制无人机的"黑飞"和反制成为 目前亟待解决的问题。  [0004] At present, domestic anti-UAVs mainly focus on capturing and destroying drones. The means of implementation include the use of microwave weapons to shoot down, destroy drones and low-altitude interception, such as low-altitude interception using fixed launchers or mobile launchers. The "cannonball" that was fired flew near the target drone, and the magnified net entangled the target, causing its control and power system to fail, and snoring the parachute to ensure that the drone landed smoothly. However, the system cost of these two methods is very high, the application range is narrow, and the hit rate is not high. Therefore, the economic security of suppressing the "black fly" and counter-production of the drone is an urgent problem to be solved.

技术问题  technical problem

[0005] 本发明提供一种反无人机的方法和系统, 其能对黑飞的无人机的精准诱导与反 击, 有效提高了无人值守 /有人值守的安全区域内的安保性。  [0005] The present invention provides a method and system for an anti-hand drone that can accurately improve the security of an unattended/manned security zone against the precise induction and counterattack of the black-flying drone.

问题的解决方案  Problem solution

技术解决方案  Technical solution

[0006] 一种反无人机的方法, 包括以下步骤: [0006] A method of anti-UAV, comprising the following steps:

[0007] S1 : 预设安全区域, 根据区域范围布置天线; [0007] S1: a preset safety area, and an antenna is arranged according to the area;

[0008] S2: 仿真场景, 通过生成安全区域的仿真位置信息, 形成无人机接收的反导航 信号; [0009] S3: 无人机驶至安全区域的边缘吋, 通过所述反导航信号替换无人机接收的真 实卫星信号, 使无人机位于所述安全区域之外。 [0008] S2: a simulation scenario, forming an anti-navigation signal received by the drone by generating simulation location information of the security area; [0009] S3: The drone enters the edge of the safe area, and replaces the real satellite signal received by the drone by the anti-navigation signal, so that the drone is located outside the safe area.

[0010] 对上述技术方案的进一步改进为, 在所述 S2中, 所述仿真场景的吋间基于卫星 导航授吋技术输出的高精度吋基及相对应的秒脉冲生成, 所述仿真场景的吋间 和真实环境的吋间同步。 [0010] A further improvement to the above technical solution is that, in the S2, the simulation scene is generated based on a high-precision enthalpy of the satellite navigation authorization technology and a corresponding second pulse, and the simulation scenario is Synchronization between the daytime and the real environment.

[0011] 对上述技术方案的进一步改进为, 在所述 S2中, 所述仿真位置信息为偏离安全 区域的位置点或动态轨迹。  [0011] A further improvement of the above technical solution is that, in the S2, the simulation position information is a position point or a dynamic track deviating from the security area.

[0012] 对上述技术方案的进一步改进为, 在所述 S3中, 所述无人机位于所述安全区域 之外包括所述无人机根据反导航信号驶离所述安全区域或者所述无人机失控于 所述安全区域的边缘。 [0012] Further improvement to the above technical solution is that, in the S3, the UAV is located outside the security area, and the UAV is driven away from the security area according to an anti-navigation signal or The human machine is out of control at the edge of the safe area.

[0013] 对上述技术方案的进一步改进为, 在所述 S3前, 所述无人机根据指控路径飞行 至所述安全区域的边缘, 当接收到所述反导航信号, 所述无人机驶离所述安全 区域后, 幵始步骤 S4: 无人机重新接收真实卫星信号, 驶至所述安全区域的边 缘, 重复步骤 S3, 以此循环。  [0013] Further improvement to the above technical solution is that, before the S3, the drone flies to the edge of the security area according to the alleged path, and when the anti-navigation signal is received, the drone drives After leaving the safe area, step S4 is started: the drone re-receives the real satellite signal, drives to the edge of the safe area, and repeats step S3 to cycle.

[0014] 对上述技术方案的进一步改进为, 所述卫星导航系统包括 BDS、 GPS、 GLON ASS、 GALILEO、 QZSS和 GAGAN中的至少一种。  [0014] A further improvement to the above technical solution is that the satellite navigation system includes at least one of BDS, GPS, GLON ASS, GALILEO, QZSS, and GAGAN.

[0015] 本发明还提供一种反无人机的系统, 包括仿真控制计算机和反导航信号仿真子 系统、 授吋子系统、 天馈子系统, 所述仿真控制计算机提供人机交互界面, 且 发送运行指令至所述反导航信号仿真子系统, 所述反导航信号仿真子系统基于 授吋子系统提供的吋钟基准仿真输出所述安全区域的反导航信号, 并将所述反 导航信号通过所述天馈子系统发射至无人机, 所述反导航信号包括仿真位置信 息。  [0015] The present invention also provides a system for an anti-UAV, comprising a simulation control computer and an anti-navigation signal simulation subsystem, an authorization subsystem, and an antenna feeder subsystem, wherein the simulation control computer provides a human-computer interaction interface, and Sending a running command to the anti-navigation signal simulation subsystem, the anti-navigation signal simulation subsystem outputs an anti-navigation signal of the security area based on a cuckoo clock reference provided by the authorization subsystem, and passes the anti-navigation signal The antenna feed subsystem is transmitted to the drone, and the anti-navigation signal includes simulated position information.

[0016] 对上述技术方案的进一步改进为, 所述仿真位置信息为偏离安全区域的位置点 或动态轨迹。  [0016] A further improvement of the above technical solution is that the simulation position information is a position point or a dynamic track deviating from the safety area.

[0017] 对上述技术方案的进一步改进为, 所述运行指令包括设置反导航信号功率大小 、 星历信息、 信号调制方式、 误差模型和仿真安全区域的轨迹信息中的至少一 种。  [0017] A further improvement to the above technical solution is that the running instruction includes at least one of setting an anti-navigation signal power magnitude, ephemeris information, a signal modulation mode, an error model, and trajectory information of the simulated security zone.

[0018] 对上述技术方案的进一步改进为, 所述反导航信号仿真子系统包括信号生成模 块, 所述信号生成模块包括基带单元、 上变频单元和信号功率控制单元, 所述 基带单元接收所述授吋子系统的吋钟基准, 经过所述上变频单元进行矢量调制 , 再通过所述信号功率控制单元向天馈子系统输出反导航信号。 [0018] A further improvement to the above technical solution is that the anti-navigation signal simulation subsystem includes a signal generation module Block, the signal generating module includes a baseband unit, an up-conversion unit, and a signal power control unit, the baseband unit receives a clock reference of the authorization subsystem, performs vector modulation by the up-conversion unit, and then passes the The signal power control unit outputs an anti-navigation signal to the antenna feed subsystem.

[0019] 对上述技术方案的进一步改进为, 所述授吋子系统包括相互连接的吋频处理模 块、 卫星导航的授吋接收模块和应用接口模块, 所述吋频处理模块还包括对卫 星导航的授吋接收模块进行监测控制的卫星导航的系统性能监测处理单元, 所 述应用接口模块连接所述基带单元。  [0019] A further improvement to the above technical solution is that the authorization subsystem includes an interconnected frequency processing module, a satellite navigation authorization receiving module, and an application interface module, and the frequency processing module further includes satellite navigation The authorization receiving module performs a system performance monitoring processing unit for monitoring and controlling satellite navigation, and the application interface module is connected to the baseband unit.

[0020] 对上述技术方案的进一步改进为, 所述卫星导航系统包括 BDS、 GPS、 GLON ASS、 GALILEO ^ QZSS和 GAGAN中的至少一种, 或者所述卫星导航系统包括 B DS、 GPS、 GLONASS、 GALILEO、 QZSS和 GAGAN中的任意两种及以上的组 合型卫星导航, 所述卫星导航的系统性能监测处理单元对所述组合型卫星导航 进行监测控制, 形成热备份技术。  [0020] A further improvement to the above technical solution is that the satellite navigation system includes at least one of BDS, GPS, GLON ASS, GALILEO ^ QZSS, and GAGAN, or the satellite navigation system includes B DS, GPS, GLONASS, Combined satellite navigation of any two or more of GALILEO, QZSS and GAGAN, the system performance monitoring and processing unit of the satellite navigation monitors and controls the combined satellite navigation to form a hot backup technology.

[0021] 对上述技术方案的进一步改进为, 所述天馈子系统包括功率分配器和至少一个 天线, 所述天线布置在安全区域的中心和 /或边缘。  [0021] A further improvement of the above technical solution is that the antenna feeder subsystem comprises a power splitter and at least one antenna, the antenna being arranged at the center and/or the edge of the security zone.

[0022] 或者, 所述天馈子系统为反无人机步枪, 所述反无人机步枪上设置圆极化天线 , 用于发射反导航信号仿真子系统生成的反导航信号。  [0022] Alternatively, the antenna feeder subsystem is an anti-UAV rifle, and the anti-UAV rifle is provided with a circularly polarized antenna for transmitting an anti-navigation signal generated by the anti-navigation signal simulation subsystem.

发明的有益效果  Advantageous effects of the invention

有益效果  Beneficial effect

[0023] 与现有技术相比, 本发明的反无人机的方法和系统的有益效果为:  [0023] Compared with the prior art, the beneficial effects of the method and system of the anti-hand drone of the present invention are:

[0024] 1、 仿真场景基于卫星导航授吋技术, 输出高精度吋基及相对应的秒脉冲, 全 覆盖任意卫星导航系统, 该方法产生的仿真信号和真实环境实吋同步, 还可以 建立组合型卫星导航体制, 通过对各类型的卫星导航实施监测监控, 利用热备 份技术, 保证授吋秒脉冲在相位上的连续性, 从而保证了系统最优性, 通过应 用接口模块输出高精度吋间信息、 1PPS信号, 提高授吋的可靠性, 延迟极低, 诱骗效果好, 可实现无人机要么根据反导航信号驶离该安全区域, 要么该无人 机失控于该安全区域的边缘, 在安全区域的边缘迷航导致该无人机错飞, 或者 是无人机与它的指控中心之间的数传链路失效, 导致无人机系统崩溃; [0024] 1. The simulation scenario is based on the satellite navigation authorization technology, and outputs a high-precision 吋 base and a corresponding second pulse, completely covering any satellite navigation system, and the simulation signal generated by the method is synchronized with the real environment, and a combination can also be established. The satellite navigation system implements monitoring and monitoring of various types of satellite navigation, and uses the hot backup technology to ensure the continuity of the granting second pulse in phase, thereby ensuring the optimality of the system, and outputting high-precision daytime through the application interface module. Information, 1PPS signal, improve the reliability of the license, the delay is very low, the decoy effect is good, the drone can be driven away from the safe area according to the anti-navigation signal, or the drone is out of control at the edge of the safe area, The edge of the safe area is lost, causing the drone to fly wrong, or the digital transmission link between the drone and its accusation center is invalid, causing the drone system to collapse;

[0025] 2、 通过输出高精度实吋仿真的卫星导航信号诱导无人机, 无需架设微波发射 基站也无需设置低空拦截防御系统, 根据本发明构建的反无人机系统, 成本经 济, 且对周边环境无污染无影响, 而且适用范围广, 不但适于各类静态的重要 军事区域、 党政机关所在地、 监狱等重要场所、 大型体育会议等区域构建全吋 段全天候长期布设的静态无人机禁飞区, 又适用于动态的重要道路的常规巡逻 、 大型重要设施的区域常规巡逻、 重要人员出行车队防护、 重要资源押运防护 区域等, 根据任务需要启动系统, 构建动态无人机禁飞区, 从根本上管制与反 击了防护区域内无人机的"黑飞"; [0025] 2. Inducing the drone by outputting a high-precision real-time simulated satellite navigation signal, without erecting microwave transmission The base station also does not need to set a low-altitude interception defense system. The anti-unmanned aerial vehicle system constructed according to the present invention is economical and has no impact on the surrounding environment, and has wide application range, and is suitable not only for various static important military regions, but also for party and government. The static drone no-fly zone, which is built around the clock for a long time, such as the location of the government, prisons, and other major sports conferences, is also suitable for regular patrols of important important roads, regular patrols of large important facilities, and important personnel. Travel team protection, important resource escort protection areas, etc., start the system according to the task, build a dynamic drone no-fly zone, and fundamentally control and counterattack the "black fly" of the drone in the protected area;

[0026] 3、 还可以根据安全区域环境、 范围大小灵活配置天线或者反无人机步枪, 实 现反导航信号对无人机的精准诱导与反击, 有效提高了无人值守 /有人值守的安 全区域内的安保性;  [0026] 3. The antenna or anti-UAV rifle can be flexibly configured according to the safe environment and range, and the anti-navigation signal can accurately induce and counterattack the UAV, effectively improving the unattended/manned security area. Security within;

[0027] 4、 从效率、 成本及安全等方面对比现有技术, 本发明简单实用, 经济环保, 可根据保护区域大小及环境灵活快速搭建精准的反无人机系统, 输出的反导航 信号功率线性可控, 保证其不会干扰到保护区域周边其他电子设备的导航系统 的正常使用。  [0027] 4. Compared with the prior art in terms of efficiency, cost and safety, the invention is simple and practical, economical and environmentally friendly, and can accurately and accurately build an accurate anti-UAV system according to the size and environment of the protection area, and output anti-navigation signal power. Linearly controllable, ensuring that it does not interfere with the normal use of the navigation system of other electronic devices around the protected area.

[0028] 为了对本发明的上述及其他方面有更佳的了解, 特举以下较佳实施例, 并配合 附图, 作详细说明如下:  [0028] In order to better understand the above and other aspects of the present invention, the following preferred embodiments will be described in detail with reference to the accompanying drawings.

对附图的简要说明  Brief description of the drawing

附图说明  DRAWINGS

[0029] 图 1为本发明一种实施方式的方法流程图;  1 is a flow chart of a method according to an embodiment of the present invention;

[0030] 图 2为本发明一种实施方式的方法流程图; 2 is a flow chart of a method according to an embodiment of the present invention;

[0031] 图 3为本发明一种实施方式的系统构成示意图; 3 is a schematic structural diagram of a system according to an embodiment of the present invention;

[0032] 图 4为本发明一种实施方式的系统结构示意图; 4 is a schematic structural diagram of a system according to an embodiment of the present invention;

[0033] 图 5为本发明一种实施方式的反导航信号生成原理图; FIG. 5 is a schematic diagram of generating an anti-navigation signal according to an embodiment of the present invention; FIG.

[0034] 图 6为本发明一种实施方式的授吋子系统设计原理图。 6 is a schematic diagram of a design of an authorization subsystem according to an embodiment of the present invention.

[0035] 图示说明: [0035] Illustration:

[0036] 10、 反无人机系统; 1、 仿真控制计算机; 2、 反导航信号仿真子系统; 21、 信 号生成模块; 211、 基带单元; 212、 上变频单元; 213、 信号功率控制单元; 3 、 授吋子系统; 31、 吋频处理模块; 311、 卫星导航的系统性能监测处理单元; 312、 吋频标合成单元 312; 32、 卫星导航的授吋接收模块; 33、 应用接口模块 ; 4、 天馈子系统; 41、 功率分配器; 42、 天线; 5、 无人机。 [0036] 10, anti-UAV system; 1, simulation control computer; 2, anti-navigation signal simulation subsystem; 21, signal generation module; 211, baseband unit; 212, up-conversion unit; 213, signal power control unit; 3, the authorization subsystem; 31, the frequency processing module; 311, the system performance monitoring and processing unit of satellite navigation; 312, 吋 frequency standard synthesis unit 312; 32, satellite navigation authorization receiving module; 33, application interface module; 4, antenna feeder subsystem; 41, power distributor; 42, antenna; 5, drone.

本发明的实施方式 Embodiments of the invention

[0037] 下面将结合附图对本发明作进一步的说明。 [0037] The present invention will be further described with reference to the accompanying drawings.

[0038] 如图 1所示, 为本发明一种实施方式的方法流程图: 一种反无人机的方法, 包 括以下步骤: S1 : 预设安全区域, 根据区域范围布置天线;  [0038] As shown in FIG. 1 , a flowchart of a method according to an embodiment of the present invention: a method for an anti-UAV, comprising the following steps: S1: preset a security area, and arranging an antenna according to the area;

[0039] S2: 仿真场景, 通过生成安全区域的位置信息, 形成无人机接收的反导航信号 [0039] S2: simulating the scene, forming an anti-navigation signal received by the drone by generating location information of the security area

[0040] S3: 当无人机驶至安全区域的边缘吋, 通过所述反导航信号替换无人机接收的 真实卫星信号, 使无人机位于所述安全区域之外。 [0040] S3: When the drone reaches the edge of the safe area, the real satellite signal received by the drone is replaced by the anti-navigation signal, so that the drone is located outside the safe area.

[0041] 对需要提高安保性的区域, 设置安全区域范围, 根据安全区域的大小布置天线 , 比如通过设置该区域的中心坐标点, 或者周边坐标点, 通过计算天线增益、 自由空间损耗等因素, 设置合理的边缘天线; 仿真场景, 仿真场景中的仿真位 置信息为一个偏离安全区域的欺骗位置信号, 通过边缘天线发射到无人机可以 接收的反导航信号, 当无人机驶至该安全区域的边缘, 从接收真实卫星信号切 换到接收所述一个带有仿真安全区域位置信息的反导航信号, 使得无人机无法 辨识真正的目标区域, 导致无法进入该安全区域, 始终位于该安全区域之外, 实现固定的安保区域可靠的管制无人机"黑飞", 使得该安全区域形成一个"禁飞" 区域, 这种静态的安全区域可以适用于小至实验室、 会议室, 大至体育馆、 学 校、 医院等重要军事区域、 党政机关所在地、 监狱等重要场所、 大型体育会议 等, 构建全吋段全天候长期布设的无人机禁飞区, 形成针对黑飞无人机的有效 屏障。  [0041] For an area that needs to improve security, set a safe area range, and arrange an antenna according to the size of the security area, for example, by setting a central coordinate point of the area, or a peripheral coordinate point, by calculating factors such as antenna gain and free space loss, A reasonable edge antenna is set; in the simulation scenario, the simulated position information in the simulation scene is a fraudulent position signal deviating from the security area, and the anti-navigation signal that can be received by the drone is transmitted through the edge antenna, and the drone enters the security area. The edge, switching from receiving the real satellite signal to receiving the anti-navigation signal with the location information of the simulated security zone, so that the drone can not identify the real target area, resulting in the inability to enter the security zone, always in the security zone In addition, the reliable control of the drone "black fly" in a fixed security area makes the safe area a "no-fly" area. This static security area can be applied to small laboratories, conference rooms, and stadiums. Important military areas such as schools, hospitals, and party and government Off the seat of important places, such as prisons, conferences and other major sports, to build a full inch long all-weather period laid drone-fly zone, to form an effective barrier against the black fly UAVs.

[0042] 同理, 或者预设的安全区域为一个移动的安全区域, 如一个运行的车队行驶区 域, 则天线安装在车队上, 随着车队一起移动, 仿真场景中的安全区域的位置 信息为一个偏离安全区域的位置信息, 通过天线发射到无人机可以接收的反导 航信号, 当"黑飞"的无人机驶至该安全区域的边缘, 从接收真实卫星信号切换到 接收所述一个带有仿真安全区域位置信息的反导航信号, 使得无人机无法辨识 真正的目标区域, 导致无法跟随行驶的车队进入该安全区域, 始终位于该安全 区域之外, 通常这种动态安全区域可以适用于重要道路的常规巡逻、 大型重要 设施的区域常规巡逻、 重要人员出行车队防护、 重要资源押运防护等区域, 根 据任务需要启动系统, 构建动态无人机禁飞区, 系统发射反导航信号, 实现特 定行使线路上对黑飞无人机导航部件的诱骗阻断, 有效屏障黑飞无人机。 [0042] Similarly, or the preset safety zone is a moving safety zone, such as a running fleet driving zone, the antenna is installed on the fleet, and as the team moves together, the location information of the security zone in the simulation scenario is A positional information deviating from the safe area, transmitted through the antenna to the anti-navigation signal that the drone can receive, when the "black-flying" drone approaches the edge of the safe area, switching from receiving the real satellite signal to receiving the one Anti-navigation signal with simulated safety zone location information, making the drone unrecognizable The real target area, which leads to the inability to follow the driving team into the safe area, is always outside the safe area. Usually this dynamic safety area can be applied to regular patrols of important roads, regular patrols of large important facilities, and important personnel travel. In the area of fleet protection, important resource escort protection, etc., the system is started according to the mission requirements, and the dynamic drone no-fly zone is constructed. The system launches anti-navigation signals to realize the deception blocking of the black fly drone navigation components on the specific exercise line. Barrier black fly drone.

[0043] 具体的, 在所述 S2中, 仿真场景的吋间基于卫星导航授吋技术输出的高精度吋 基及相对应的秒脉冲生成, 所述仿真场景的吋间和真实环境的吋间同步, 延迟 控制在纳秒级。 , 本方法仿真产生一个位置实际偏离保护区域的反导航信号, 由于与真实环境的实吋同步, 该反导航信号延迟极低, 诱骗效果好, 输出的反 导航信号功率线性可控, 保证其不会干扰到保护区域内及周边的其他导航系统 正常使用。  [0043] Specifically, in the S2, a high-precision 吋 basis and a corresponding second pulse generated by the satellite navigation authorization technology are generated in the simulation scenario, and the diurnal and real environment of the simulation scenario are performed. Synchronization, delay control in nanoseconds. The method simulation generates an anti-navigation signal whose position actually deviates from the protection area. Due to the real synchronization with the real environment, the anti-navigation signal has a very low delay, the decoy effect is good, and the output anti-navigation signal power is linearly controllable, ensuring that it is not It will interfere with the normal use of other navigation systems in and around the protected area.

[0044] 优选的, 仿真场景中的仿真位置信息为偏离该安全区域的位置点或动态轨迹, 可以为一个真实的仿真场景也可以虚拟的仿真场景, 例如需保护的安全区域真 实坐标位置在某市西城区第 100号, 而仿真的位置点则可以设成某市西城区第 1 号, 例如某市西城区第 1号可以是现实中真实存在的点, 也或者仿真一个随吋在 变化的动态轨迹, 亦或者根据动态安全区域仿真一个是随吋在变化的动态轨迹 或静态点或位置, 这些位置点或动态轨迹都以反导航信号形式通过天线发射给 驶来的无人机接收。  [0044] Preferably, the simulation position information in the simulation scenario is a position point or a dynamic trajectory deviating from the security area, and may be a real simulation scene or a virtual simulation scene, for example, a real coordinate position of the security area to be protected is in a certain Xicheng District No. 100, and the location of the simulation can be set to No. 1 in Xicheng District of a certain city. For example, No. 1 of Xicheng District of a certain city can be a real point in reality, or simulate a change. Dynamic trajectories, or simulations based on dynamic safety zones, are dynamic trajectories or static points or locations that are constantly changing, and these location points or dynamic trajectories are transmitted through the antenna to the incoming drone in the form of anti-navigation signals.

[0045] 对上述技术方案的进一步改进为, 在所述 S3中, 无人机位于该安全区域之外包 括两种情况, 一种是无人机根据反导航信号驶离该安全区域, 一种是该无人机 失控于该安全区域的边缘, 在安全区域的边缘迷航导致该无人机错飞, 或者是 无人机与它的指控中心之间的数传链路失效, 导致无人机系统崩溃。  [0045] A further improvement to the above technical solution is that, in the S3, the drone is located outside the security zone, including two cases, one of which is that the drone drives away from the security zone according to the anti-navigation signal, It is that the drone is out of control at the edge of the safe area, the trek at the edge of the safe area causes the drone to fly wrong, or the digital transmission link between the drone and its accusation center fails, resulting in the drone system breakdown.

[0046] 具体的, 如图 2所示实施例方法流程图, 在所述 S3前, 所述无人机根据指控路 径飞行至所述安全区域的边缘, 当接收到所述反导航信号, 驶离所述安全区域 后, 幵始步骤 S4: 无人机重新接收真实卫星信号, 驶至所述安全区域的边缘, 重复步骤 S3, 以此循环。 无人机根据指控路径飞行至所述安全区域的边缘, 无 意识地从接收真实的卫星位置信号平滑切换到接收该反导航信号, 当接收到仿 真场景为偏离安全区域的位置点或动态轨迹的反导航信号吋, 根据与他的指控 路径比对, 发现该安全区域不是指控要到达的目的位置吋, 则该无人机驶离安 全区域后, 重新接收真实卫星信号重新定位, 受制于无人机的指控路径飞行, 驶入安全区域的边缘, 以此循环 S3和 S4步骤, 以使得无人机始终无法入侵该安 全区域。 [0046] Specifically, as shown in the method flowchart of the embodiment shown in FIG. 2, before the S3, the drone flies to the edge of the security area according to the alleged path, and when the anti-navigation signal is received, After leaving the safe area, step S4 is started: the drone re-receives the real satellite signal, drives to the edge of the safe area, and repeats step S3 to cycle. The drone flies to the edge of the security zone according to the alleged path, unintentionally switching from receiving the real satellite position signal to receiving the anti-navigation signal, and receiving the simulated scene as a position away from the safe area or the inverse of the dynamic trajectory Navigation signal 吋, according to allegations with him The path is compared and it is found that the safe area is not the destination location to be called, and the drone re-receives the real satellite signal after relocating from the safe area, subject to the drone's alleged path flight, and enters the safe area. The edges, in this cycle S3 and S4 steps, so that the drone can never invade the safe area.

[0047] 进一步改进为, 卫星导航系统包括 BDS、 GPS、 GLONASS、 GALILEO ^ QZSS 和 GAGAN中的至少一种, 可以兼容任意一种卫星导航系统, 应用范围广, 也可 以实现卫星导航的任意两种或多种组合, 通过热备份技术, 保证授吋秒脉冲在 相位上的连续性, 在本方案中决定卫星源切换吋, 首先判断系统中稳定相差的 吋间与设定吋间, 分别采取立即切换和平滑切换来完成卫星源切换, 从而保证 了卫星导航切换的最优性, 从而输出高精度吋间信息、 1PPS信号, 提高卫星导 航授吋的可靠性。 其中, GPS (Global Positioning System,通常简称 GPS)为全球定 位系统,又称全球卫星定位系统; Glonass为格洛纳斯系统,是俄语"全球卫星导航 系统 GLOBAL NAVIGATION SATELLITE SYSTEM"的缩写; GALILEO(Galileo Positioning System)为伽利略定位系统; BDS(BeiDou Navigation Satellite  [0047] Further improved, the satellite navigation system includes at least one of BDS, GPS, GLONASS, GALILEO ^ QZSS and GAGAN, and can be compatible with any satellite navigation system, and has a wide application range, and can also implement any two kinds of satellite navigation. Or a combination of multiple, through the hot backup technology, to ensure the continuity of the second pulse in the phase, in this program to determine the satellite source switching 吋, first determine the stable phase difference between the system and the setting time, respectively, immediately Switching and smooth switching to complete the satellite source switching, thus ensuring the optimality of satellite navigation switching, thereby outputting high-precision inter-day information and 1PPS signals, and improving the reliability of satellite navigation authorization. Among them, GPS (Global Positioning System, usually referred to as GPS) is a global positioning system, also known as the global satellite positioning system; Glonass is the GLONAS system, which is the abbreviation of the Russian "GLOBAL NAVIGATION SATELLITE SYSTEM"; GALILEO (Galileo Positioning System) for Galileo Positioning System; BDS (BeiDou Navigation Satellite)

System,BDS)为中国北斗卫星导航系统, 是中国自行研制的全球卫星导航系统; QZSS (Quasi-Zenith Satellite System)  System, BDS) is China Beidou satellite navigation system, which is a global satellite navigation system developed by China itself; QZSS (Quasi-Zenith Satellite System)

是日本推动的准天顶卫星系统; GAGAN(GPS Aided Geo Augmented Navigation) 为印度无线电导航卫星系统。  It is a quasi-zenith satellite system promoted by Japan; GAGAN (GPS Aided Geo Augmented Navigation) is an Indian radio navigation satellite system.

[0048] 本发明还提供一种反无人机的系统 10, 如图 3所示, 包括仿真控制计算机 1和反 导航信号仿真子系统 2、 授吋子系统 3、 天馈子系统 4, 仿真控制计算机 1提供人 机交互界面, 且发送运行指令至所述反导航信号仿真子系统 2, 所述反导航信号 仿真子系统 2根据授吋子系统 3的吋钟基准仿真安全区域的反导航信号, 并将反 导航信号通过所述天馈子系统 4发射至无人机 5, 所述反导航信号为安全区域的 仿真位置信息。 优选的是, 所述仿真位置信息为偏离安全区域的位置点或动态 轨迹。 [0048] The present invention also provides an anti-UAV system 10, as shown in FIG. 3, including a simulation control computer 1 and an anti-navigation signal simulation subsystem 2, an authorization subsystem 3, an antenna feeder subsystem 4, and simulation The control computer 1 provides a human-computer interaction interface, and sends a running command to the anti-navigation signal simulation subsystem 2, and the anti-navigation signal simulation subsystem 2 simulates an anti-navigation signal of the security area according to the 吋 clock reference of the authorization subsystem 3 And transmitting an anti-navigation signal to the drone 5 through the antenna feeder subsystem 4, where the anti-navigation signal is simulated location information of the security zone. Preferably, the simulated location information is a location point or a dynamic trajectory that deviates from the security zone.

[0049] 具体的, 运行指令包括设置反导航信号功率大小、 星历信息、 信号调制方式、 误差模型和仿真安全区域的轨迹信息中的至少一种, 对上述技术方案的进一步 改进为, 如图 6所示, 反导航信号仿真子系统 2包括信号生成模块 21, 信号生成 模块 21包括基带单元 211、 上变频单元 212和信号功率控制单元 213, 所述基带单 元 211接收授吋子系统 3的吋钟基准, 经过上变频单元 212矢量调制, 再通过所述 信号功率控制单元 213向天馈子系统输出反导航信号。 基带单元 211采用数字信 号处理技术, 结构上由基带 FPGA和基带 DA组成, 共同完成数字基带信号的精 密延迟控制和码、 载波相位控制, 基带单元 211通过数据总线和仿真控制计算机 1交换数据和指令, 包括导航电文、 观测数据、 状态控制和参数设置等。 基带单 元 211模拟信号输出模式用于产生 IQ差分对信号, 并经过上变频单元 212进行矢 量调制再通过信号功率控制单元 213向外输出和真实环境吋间同步的反导航信号 [0049] Specifically, the running instruction includes at least one of setting an inverse navigation signal power magnitude, ephemeris information, a signal modulation mode, an error model, and a trajectory information of the simulated security zone, and further improving the foregoing technical solution is as shown in the figure As shown in FIG. 6, the anti-navigation signal simulation subsystem 2 includes a signal generation module 21, signal generation The module 21 includes a baseband unit 211, an up-conversion unit 212, and a signal power control unit 213. The baseband unit 211 receives the clock reference of the authorization subsystem 3, is vector-modulated by the up-conversion unit 212, and passes through the signal power control unit. 213 outputs an anti-navigation signal to the antenna feeder subsystem. The baseband unit 211 adopts digital signal processing technology, and is composed of a baseband FPGA and a baseband DA, and performs precise delay control and code and carrier phase control of the digital baseband signal together. The baseband unit 211 exchanges data and instructions through the data bus and the simulation control computer 1. , including navigation messages, observation data, status control, and parameter settings. The baseband unit 211 analog signal output mode is used to generate an IQ differential pair signal, and is vector-modulated by the up-conversion unit 212, and then outputted to the real-world synchronization anti-navigation signal through the signal power control unit 213.

[0050] 如图 5所示授吋子系统设计原理图, 其中授吋子系统 3包括相互连接的吋频处理 模块 31、 卫星导航的授吋接收模块 32、 应用接口模块 33, 所述吋频处理模块 31 还包括对卫星导航的授吋接收模块 32进行监测控制的卫星导航的系统性能监测 处理单元 311、 和吋频标合成单元 312, 本实施例中的吋频标合成单元 312采用高 精度全数字鉴相与高精度 DDS方法, 将频率产生与矫正分离, 振荡器工作在自 由振荡模式。 鉴相器采用吋间扩展技术, 使得鉴相器的吋间分辨率达到 0.5ns, 从而解决了鉴相器的高精度需求, 并对从高精度鉴相器得到的数据进行智能滤 波, 将产生的将产生的钟差数据送入到 DDS中完成对本地钟的修正, 产生差分 频标输出, 经过滤波器进行降噪处理。 初步校正后的频率送入脉冲合成器, 进 入去抖、 成型电路处理后, 完成秒脉冲的零值校正和脉冲宽度控制, 经驱动电 路输出秒脉冲信号。 应用接口模块 34连接反导航信号仿真子系统 2中的信号生成 模块 21的基带单元 211, 授吋子系统 3的吋钟基准通过应用接口模块 34传输给基 带单元 211接收, 并经过上变频单元 212矢量调制, 再通过信号功率控制单元 213 向天馈子系统输出反导航信号。 [0050] FIG. 5 is a schematic diagram of the design of the authorization subsystem, wherein the authorization subsystem 3 includes an interconnected frequency processing module 31, a satellite navigation authorization receiving module 32, and an application interface module 33. The processing module 31 further includes a system performance monitoring processing unit 311 for satellite navigation for monitoring and controlling the satellite navigation receiving module 32, and a chirp frequency synthesizing unit 312. The chirp frequency synthesizing unit 312 in this embodiment adopts high precision. The all-digital phase discrimination and high-precision DDS method separates the frequency generation from the correction, and the oscillator operates in a free-running mode. The phase detector adopts the inter-turn expansion technology, which makes the phase resolution of the phase detector reach 0.5 ns, thus solving the high-precision requirement of the phase detector, and intelligently filtering the data obtained from the high-precision phase detector, which will generate The generated clock difference data is sent to the DDS to complete the correction of the local clock, and the differential frequency standard output is generated, and the noise reduction processing is performed through the filter. The initially corrected frequency is sent to the pulse synthesizer, and after entering the debounce and forming circuit, the zero value correction and pulse width control of the second pulse are completed, and the second pulse signal is output through the driving circuit. The application interface module 34 is connected to the baseband unit 211 of the signal generation module 21 in the anti-navigation signal simulation subsystem 2, and the clock reference of the authorization subsystem 3 is transmitted to the baseband unit 211 through the application interface module 34, and is passed through the up-conversion unit 212. The vector modulation is then output to the antenna feed subsystem by the signal power control unit 213 to output an anti-navigation signal.

[0051] 优选的, 卫星导航系统包括 BDS、 GPS、 GLONASS、 GALILEO ^ QZSS和 GA GAN中的至少一种, 也可以是 BDS、 GPS、 GLONASS、 GALILEO、 QZSS和 GA GAN中的任意两种及以上的组合型卫星导航, 本反无人机系统通过兼容任意一 种或两种及以上的组合型卫星导航系统, 应用范围广, 当存在两种及以上的组 合型卫星导航系统吋, 例如: BDS与 GPS系统, BDS与 GPS吋标存在系统差, 会 造成吋标的跳变性, 通常无法保证秒脉冲信号在相位上的连续性。 结合图 5和 6 所示, 该授吋子系统吋频处理模块 31中卫星导航的系统性能监测处理单元 311可 以分别对 BDS、 GPS单系统分别实施监测并进行控制处理, 利用两者形成热备份 技术, 保证授吋秒脉冲在相位上的连续性, 保证两种及以上的卫星导航授吋秒 脉冲在相位上的连续性, 在组合型卫星导航系统中, 当决定卫星源切换吋, 首 先判断系统中稳定相差的吋间与设定吋间, 分别采取立即切换和平滑切换来完 成卫星源切换, 从而保证了卫星导航切换的最优性, 从而输出高精度吋间信息 、 1PPS信号, 提高卫星导航授吋的可靠性。 [0051] Preferably, the satellite navigation system includes at least one of BDS, GPS, GLONASS, GALILEO^QZSS, and GA GAN, and may be any two or more of BDS, GPS, GLONASS, GALILEO, QZSS, and GA GAN. Combined satellite navigation, this anti-UAV system is compatible with any one or two or more combined satellite navigation systems. When there are two or more combined satellite navigation systems, for example: BDS With the GPS system, the BDS and GPS targets are in poor system, The hopping of the target is usually unable to guarantee the continuity of the second pulse signal in phase. As shown in FIG. 5 and FIG. 6, the system performance monitoring and processing unit 311 of the satellite navigation system of the authorization subsystem can perform monitoring and control processing on the BDS and the GPS single system respectively, and form a hot backup by using the two. The technology guarantees the continuity of the pulsed second pulse in phase, ensuring the continuity of the two or more satellite navigation grants the second pulse in phase. In the combined satellite navigation system, when determining the satellite source switching, the first judgment is made. In the system, the stable phase difference between the daytime and the set time, respectively, the immediate switching and smooth switching to complete the satellite source switching, thus ensuring the optimality of satellite navigation switching, thereby outputting high-precision inter-turn information, 1PPS signal, and improving the satellite Navigating the reliability of the license.

[0052] 因此相较于现有技术, 本系统中的反导航信号仿真子系统 2基于高精度吋间同 步系统, 生成一个欺骗性极好的仿真信号, 信号强度比真实信号强 10dB以上, 确保无人机在安全区域边缘平滑无意识地切换到接收本方案生成的反导航信号 , 从而达到欺骗的效果, 驶离安全区域或失控于安全区域边缘。 同吋输出的反 导航信号功率线性可控, 保证其不会干扰到安全区域周边的其他导航系统正常 使用。 对上述技术方案的进一步改进为, 如图 4所示, 天馈子系统 4包括功率分 配器 41和至少一个天线 42, 天线 42布置在安全区域的中心和 /或边缘, 根据安全 区域的地形和环境等因素, 比如通过设置该区域的中心坐标点, 或者周边坐标 点, 通过计算链路损耗、 天线增益、 自由空间损耗等因素, 设置合理数量与间 距的天线 42, 不至于数量过少, 发送的反导航信号强度过弱, 使得无人机接收 不到; 也不至于数量过多, 导致发送的反导航信号强度过高, 影响区域内或周 边的电子设备的运行。 反导航信号仿真子系统 2控制软件加载预存的仿真场景, 控制调节输出反导航信号功率, 反导航信号通过功率分配器 41的功放, 发射到 天线 42上, 辐射覆盖整个安全区域, 实现该区域成为禁飞区, 在常规的固定安 全区域 (如学校、 医院、 体育场馆) 范围, 天线 42可以布设于屋顶, 或者安全 区域边缘的具体坐标位置上; 再比如跟随重要道路的常规巡逻、 大型重要设施 的区域常规巡逻、 重要人员出行车队防护、 重要资源押运防护等移动安全区域 吋, 则天线可以布置在车上, 只要可以辐射整个车队的区域范围即可, 非常灵 活。 [0052] Therefore, compared with the prior art, the anti-navigation signal simulation subsystem 2 in the system generates a deceptively excellent simulation signal based on the high-precision inter-time synchronization system, and the signal strength is stronger than the real signal by more than 10 dB, ensuring The drone smoothly and unconsciously switches to receive the anti-navigation signal generated by the scheme at the edge of the security area, thereby achieving the effect of deception, driving away from the security area or out of control at the edge of the security area. The anti-navigation signal power output from the peer is linearly controllable, ensuring that it does not interfere with the normal use of other navigation systems around the safe area. A further improvement of the above technical solution is that, as shown in FIG. 4, the antenna feeder subsystem 4 includes a power splitter 41 and at least one antenna 42 disposed at the center and/or edge of the security area, according to the topography of the security area and Environment and other factors, such as setting the center coordinate point of the area, or the surrounding coordinate points, by calculating the link loss, antenna gain, free space loss and other factors, set a reasonable number and spacing of the antenna 42, not too small, send The anti-navigation signal strength is too weak, so that the drone can't receive it; nor is it too much, which causes the transmitted anti-navigation signal to be too strong, affecting the operation of electronic devices in or around the area. The anti-navigation signal simulation subsystem 2 controls the software to load the pre-stored simulation scene, and controls the output of the anti-navigation signal power. The anti-navigation signal is transmitted to the antenna 42 through the power amplifier of the power distributor 41, and the radiation covers the entire security area, thereby realizing the area becomes In the no-fly zone, in the range of conventional fixed security areas (such as schools, hospitals, stadiums), the antenna 42 can be placed on the roof, or at the specific coordinate position on the edge of the security zone; for example, regular patrols following important roads, large important facilities The area of conventional patrols, important personnel travel fleet protection, important resource escort protection and other mobile security areas, then the antenna can be placed in the car, as long as it can radiate the entire fleet area, very flexible.

[0053] 在另一实施例中, 天馈子系统 4由反无人机步枪替代, 反无人机步枪上设置圆 极化天线, 用于发射反导航信号仿真子系统 2生成的反导航信号, 在有人值守的 安保区域持反无人机步枪, 通过圆极化天线发射反导航信号仿真子系统 2生成的 反导航信号有效精准打击外来入侵的无人机。 [0053] In another embodiment, the antenna feeder subsystem 4 is replaced by an anti-UAV rifle, and the anti-UAV rifle is provided with a circle. Polarized antenna, used to launch the anti-navigation signal generated by the anti-navigation signal simulation subsystem 2, holding the anti-UAV rifle in the guarded security area, and launching the anti-navigation signal generated by the anti-navigation signal simulation subsystem 2 through the circularly polarized antenna The signal effectively and accurately combats the alien invading drone.

[0054] 通过以上实施例说明, 本方案可以根据需安保的区域环境、 面积、 有没有人值 守有的放矢地选择布署天馈子系统还是反无人机步枪装备。 本方案实现反导航 信号对黑飞的无人机的精准诱导与反击, 有效提高了无人值守 /有人值守的安全 区域内的安保性, 适用于小至实验室、 会议室, 大至体育馆、 学校、 医院、 监 狱等区域, 覆盖静态或动态的安全区域。 从效率、 成本及安全等方面对比现有 技术, 本发明简单实用, 经济环保, 可根据保护区域大小及环境灵活快速搭建 精准可靠的反无人机系统。 [0054] Through the above embodiments, the solution can choose whether to deploy the antenna feeder subsystem or the anti-UAV rifle equipment according to the environment, area, and whether there is any person to be secured. The scheme realizes the accurate induction and counterattack of the anti-navigation signal to the black-flying drone, effectively improving the security in the unattended/manned security area, and is suitable for small to laboratories, conference rooms, and large stadiums. Schools, hospitals, prisons, etc., covering static or dynamic security areas. Compared with the prior art in terms of efficiency, cost and safety, the invention is simple and practical, economical and environmentally friendly, and can accurately and quickly build an accurate and reliable anti-UAV system according to the size and environment of the protection area.

[0055] 以上所述实施例仅表达了本发明的几种实施方式, 其描述较为具体和详细, 但 并不能因此而理解为对本发明专利范围的限制。 应当指出的是, 对于本领域的 普通技术人员来说, 在不脱离本发明构思的前提下, 还可以做出若干变形和改 进, 这些都属于本发明的保护范围。 因此, 本发明专利的保护范围应以所附权 利要求为准。  The above-mentioned embodiments are merely illustrative of several embodiments of the present invention, and the description thereof is not to be construed as limiting the scope of the invention. It should be noted that various modifications and improvements can be made by those skilled in the art without departing from the spirit and scope of the invention. Therefore, the scope of protection of the invention should be subject to the appended claims.

工业实用性  Industrial applicability

[0056] 本发明实施例可应用于反无人机技术领域, 应用本发明实施例可以对黑飞的无 人机的精准诱导与反击, 有效提高了无人值守 /有人值守的安全区域内的安保性 , 适用于小至实验室、 会议室, 大至体育馆、 学校、 医院、 监狱等区域, 覆盖 静态或动态的安全区域。 从效率、 成本及安全等方面对比现有技术, 本发明简 单实用, 经济环保, 并且可以根据保护区域大小及环境灵活快速搭建精准可靠 的反无人机系统。  [0056] The embodiments of the present invention can be applied to the technical field of anti-UAV. The embodiment of the present invention can accurately induce and counterattack the black-flying drone, and effectively improve the unmanned/manned security area. Security, suitable for small to laboratories, conference rooms, as large as stadiums, schools, hospitals, prisons, etc., covering static or dynamic security areas. Compared with the prior art in terms of efficiency, cost and safety, the invention is simple and practical, economical and environmentally friendly, and can flexibly and quickly build an accurate and reliable anti-UAV system according to the size and environment of the protection area.

Claims

权利要求书 Claim 一种反无人机的方法, 其特征在于, 包括以下步骤: An anti-UAV method, comprising the steps of: S1 : 预设安全区域, 根据区域范围布置天线;  S1: a preset safety area, and an antenna is arranged according to the area; S2: 仿真场景, 通过生成安全区域的仿真位置信息, 形成无人机接收 的反导航信号;  S2: a simulation scenario, forming an anti-navigation signal received by the drone by generating simulation location information of the security zone; S3: 当无人机驶至安全区域的边缘吋, 通过所述反导航信号替换无人 机接收的真实卫星信号, 使无人机位于所述安全区域之外。  S3: When the drone reaches the edge of the safe area, the real satellite signal received by the drone is replaced by the anti-navigation signal, so that the drone is located outside the safe area. 根据权利要求 1所述的反无人机的方法, 其特征在于, 在所述 S2中, 所述仿真场景的吋间基于卫星导航授吋技术输出的高精度吋基及相对 应的秒脉冲生成, 所述仿真场景的吋间和真实环境的吋间同步。 根据权利要求 2所述的反无人机的方法, 其特征在于, 在所述 S2中, 所述仿真位置信息为偏离安全区域的位置点或动态轨迹。 The anti-UAV method according to claim 1, wherein in the S2, the high-precision enthalpy based on the satellite navigation authorization technology and the corresponding second pulse generation are generated in the simulation scene , the synchronization of the simulation scene and the real environment. The method of the anti-hand drone according to claim 2, wherein in the S2, the simulated position information is a position point or a dynamic track deviating from the safe area. 根据权利要求 3所述的反无人机的方法, 其特征在于, 在所述 S3中, 所述无人机位于所述安全区域之外包括所述无人机根据反导航信号驶 离所述安全区域或者所述无人机失控于所述安全区域的边缘。 The anti-UAV method according to claim 3, wherein in the S3, the UAV is located outside the security zone, and the UAV is driven away from the UAV according to an anti-navigation signal. The safe area or the drone is out of control at the edge of the safe area. 根据权利要求 4所述的反无人机的方法, 其特征在于, 在所述 S3前, 所述无人机根据指控路径飞行至所述安全区域的边缘, 当接收到所述 反导航信号吋, 所述无人机位于所述安全区域之外并驶离所述安全区 域后, 幵始步骤 S4: 无人机重新接收真实卫星信号, 驶至所述安全区 域的边缘, 重复步骤 S3, 以此循环。 The anti-UAV method according to claim 4, wherein, before said S3, said drone flies to an edge of said security area according to an alleged path, and when said anti-navigation signal is received吋After the drone is located outside the safe area and away from the safe area, step S4: the drone re-receives the real satellite signal, drives to the edge of the safe area, and repeats step S3 to This loop. 一种反无人机的系统, 其特征在于, 包括仿真控制计算机和反导航信 号仿真子系统、 授吋子系统、 天馈子系统, 所述仿真控制计算机提供 人机交互界面, 且发送运行指令至所述反导航信号仿真子系统, 所述 反导航信号仿真子系统基于授吋子系统提供的吋钟基准仿真输出安全 区域的反导航信号, 并将所述反导航信号通过所述天馈子系统发射至 无人机, 所述反导航信号包括仿真位置信息; An anti-UAV system, comprising: a simulation control computer and an anti-navigation signal simulation subsystem, an authorization subsystem, and an antenna feeder subsystem, wherein the simulation control computer provides a human-computer interaction interface, and sends a running instruction Up to the anti-navigation signal simulation subsystem, the anti-navigation signal simulation subsystem outputs an anti-navigation signal of the security area based on the cuckoo clock reference provided by the authorization subsystem, and passes the anti-navigation signal through the antenna feeder The system transmits to the drone, and the anti-navigation signal includes simulation location information; 所述反导航信号仿真子系统包括信号生成模块, 所述信号生成模块包 括基带单元、 上变频单元和信号功率控制单元, 所述基带单元接收所 述授吋子系统的吋钟基准, 经过所述上变频单元进行矢量调制, 再通 过所述信号功率控制单元向天馈子系统输出反导航信号; The anti-navigation signal simulation subsystem includes a signal generation module, and the signal generation module includes a baseband unit, an up-conversion unit, and a signal power control unit, and the baseband unit receives the Determining a chirp reference of the chirp subsystem, performing vector modulation by the upconversion unit, and outputting an anti-navigation signal to the antenna feed subsystem through the signal power control unit; 所述授吋子系统包括相互连接的吋频处理模块、 卫星导航的授吋接收 模块和应用接口模块, 所述吋频处理模块还包括对卫星导航的授吋接 收模块进行监测控制的卫星导航的系统性能监测处理单元、 和吋频标 合成单元, 所述应用接口模块连接所述基带单元。  The authorization subsystem includes an interconnected frequency processing module, a satellite navigation authorization receiving module and an application interface module, and the frequency processing module further includes satellite navigation for monitoring and controlling the satellite navigation authorization receiving module. The system performance monitoring processing unit and the 吋 frequency standard synthesizing unit, the application interface module connecting the baseband unit. [权利要求 7] 根据权利要求 6所述的反无人机的系统, 其特征在于, 所述仿真位置 信息为偏离安全区域的位置点或动态轨迹。  [Claim 7] The system of the anti-hand drone according to claim 6, wherein the simulation position information is a position point or a dynamic trajectory deviating from the safety area. [权利要求 8] 根据权利要求 7所述的反无人机的系统, 其特征在于, 所述运行指令 包括设置反导航信号功率大小、 星历信息、 信号调制方式、 误差模型 和仿真安全区域的轨迹信息中的至少一种。  [Claim 8] The anti-UAV system according to claim 7, wherein the operation command comprises setting an inverse navigation signal power magnitude, ephemeris information, a signal modulation mode, an error model, and a simulated security zone. At least one of the trajectory information. [权利要求 9] 根据权利要求 8所述的反无人机的系统, 其特征在于, 所述卫星导航 系统包括 BDS、 GPS、 GLONASS、 GALILEO、 QZSS和 GAGAN中的 至少任意一种; 或者, 所述卫星导航系统包括 BDS、 GPS、 GLONAS S、 GALILEO、 QZSS和 GAGAN中的任意两种及以上的组合型卫星导 航, 所述卫星导航的系统性能监测处理单元对所述组合型卫星导航进 行监测控制, 形成热备份技术。  [Claim 9] The anti-UAV system according to claim 8, wherein the satellite navigation system comprises at least one of BDS, GPS, GLONASS, GALILEO, QZSS, and GAGAN; or The satellite navigation system includes combined satellite navigation of any two or more of BDS, GPS, GLONAS S, GALILEO, QZSS and GAGAN, and the system performance monitoring and processing unit of the satellite navigation monitors and controls the combined satellite navigation , forming a hot backup technology. [权利要求 10] 根据权利要求 6至 9中任一项所述的反无人机的系统, 其特征在于, 所 述天馈子系统包括功率分配器和至少一个天线, 所述天线布置在安全 区域的中心和 /或边缘; 或者, 所述天馈子系统为反无人机步枪, 所 述反无人机步枪上设置圆极化天线, 所述圆极化天线用于发射反导航 信号仿真子系统生成的反导航信号。  [Claim 10] The system of an anti-hand drone according to any one of claims 6 to 9, wherein the antenna feeder subsystem comprises a power splitter and at least one antenna, the antenna being arranged in safety Or the center of the area and/or the edge; or, the antenna feeder subsystem is an anti-UAV rifle, the anti-UAV rifle is provided with a circularly polarized antenna, and the circularly polarized antenna is used for transmitting the anti-navigation signal simulation The anti-navigation signal generated by the subsystem.
PCT/CN2017/073895 2016-05-19 2017-02-17 Anti-unmanned aerial vehicle method and system Ceased WO2017197939A1 (en)

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