CN106341206A - Low-altitude unmanned aerial vehicle defense system - Google Patents
Low-altitude unmanned aerial vehicle defense system Download PDFInfo
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- CN106341206A CN106341206A CN201610729461.1A CN201610729461A CN106341206A CN 106341206 A CN106341206 A CN 106341206A CN 201610729461 A CN201610729461 A CN 201610729461A CN 106341206 A CN106341206 A CN 106341206A
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- warning system
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- 230000007123 defense Effects 0.000 title claims abstract description 18
- 238000001514 detection method Methods 0.000 claims abstract description 12
- 230000002457 bidirectional effect Effects 0.000 claims abstract description 3
- 230000003287 optical effect Effects 0.000 abstract 3
- 230000002093 peripheral effect Effects 0.000 abstract 2
- 230000001846 repelling effect Effects 0.000 abstract 1
- 238000004891 communication Methods 0.000 description 6
- 238000013461 design Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 230000006855 networking Effects 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
Classifications
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04K—SECRET COMMUNICATION; JAMMING OF COMMUNICATION
- H04K3/00—Jamming of communication; Counter-measures
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H11/00—Defence installations; Defence devices
- F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R23/00—Arrangements for measuring frequencies; Arrangements for analysing frequency spectra
- G01R23/16—Spectrum analysis; Fourier analysis
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO 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
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/02—Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
- G01S13/06—Systems determining position data of a target
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO 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
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/88—Radar or analogous systems specially adapted for specific applications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO 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
- G01S3/00—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received
- G01S3/02—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received using radio waves
- G01S3/04—Details
- G01S3/12—Means for determining sense of direction, e.g. by combining signals from directional antenna or goniometer search coil with those from non-directional antenna
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO 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
- G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
- G01S7/02—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
- G01S7/38—Jamming means, e.g. producing false echoes
-
- G—PHYSICS
- G08—SIGNALLING
- G08C—TRANSMISSION SYSTEMS FOR MEASURED VALUES, CONTROL OR SIMILAR SIGNALS
- G08C23/00—Non-electrical signal transmission systems, e.g. optical systems
- G08C23/04—Non-electrical signal transmission systems, e.g. optical systems using light waves, e.g. infrared
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N7/00—Television systems
- H04N7/18—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast
- H04N7/183—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast for receiving images from a single remote source
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- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Radar, Positioning & Navigation (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Computer Networks & Wireless Communication (AREA)
- Signal Processing (AREA)
- Mathematical Physics (AREA)
- Electromagnetism (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Multimedia (AREA)
- Traffic Control Systems (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
The invention discloses a low-altitude unmanned aerial vehicle defense system, which comprises a control center, an air defense early warning system and an electronic driving-away system. The control center is in bidirectional connection with the air defense early warning system and the electronic driving-away system. The air defense early warning system is formed by radar early warning systems and optical early warning systems. The electronic driving-away system is formed by roadbed electronic fences and a mobile individual-soldier driving-away device. The radar early warning systems adopt high/low-altitude combined detection radars, wherein the high/low-altitude combined detection radars are in peripheral multipoint arrangement. Each optical early warning system is formed by an infrared system and a visible light system. The optical early warning systems adopt peripheral multipoint arrangement. The mobile individual-soldier driving-away device is provided with an individual-soldier mobile electronic gun. The roadbed electronic fences are provided with frequency analysis units. The defense system realizes positioning, early warning and tracking of the low-altitude, slow and small-size unmanned aerial vehicles in the sky, and realizes repelling and forced landing of the unmanned aerial vehicles.
Description
Technical field
The invention belongs to unmanned air vehicle technique field, specifically, the present invention relates to a kind of low latitude unmanned plane system of defense.
Background technology
With the development of unmanned air vehicle technique in recent years, the application of unmanned plane is constantly widened, military affairs from the beginning, instead
Probably field gradually extends to the every aspect of our lives, now much local it can be seen that unmanned plane operates, Wo Menchang
Common taken photo by plane to a lot of shutterbugs using unmanned plane, but do not prevent some by the use of photography hobby as covering up, right
Some military installations of China are taken on the sly, steal the military information of China, to the interception major way of present unmanned plane are
Interception, the interception of net formula, the compacting of individual soldier's radio frequency and the area radio frequency of jettisoninging is suppressed, wherein jettisoning interception and the net formula operable distance of interception
Short, intercepting efficiency and success rate low;The compacting of individual soldier's radio frequency lacks effective unmanned plane early warning and unmanned plane positioning, follows the tracks of, effect
Scope is little;Area radio frequency compacting flexibility ratio low it is impossible to Intelligent Recognition, longevity of service, high energy consumption.
Content of the invention
The present invention provides a kind of low latitude unmanned plane system of defense it is therefore an objective to realize low, slow, SUAV in the air is carried out
Locking, early warning, tracking, are expelled to it and are force-landed.
To achieve these goals, the technical scheme that the present invention takes is: a kind of low latitude unmanned plane system of defense, including control
Center processed, antiaircraft early warning system and electronics expel system, and wherein control centre is expelled with antiaircraft early warning system and electronics respectively and is
System is bi-directionally connected, and described antiaircraft early warning system is made up of radar early warning system and optics early warning system, and electronics expels system by road
Base fence and mobile individual soldier expel device and constitute.
Preferably, described radar early warning system adopts high and low idle pattern formula detection radar, and described high and low idle pattern formula
Detection radar adopts periphery multiple spot to arrange, described optics early warning system is made up of infrared system and VISIBLE LIGHT SYSTEM, and optics is pre-
Alarm system adopts periphery multiple spot to arrange.
Preferably, described roadbed fence is laid using multiple spot, the interference of combined type multifrequency section, compacting, described mobile single
Soldier expels and is provided with individual soldier's mobile electronic rifle in device.
Preferably, it is provided with frequency analysis unit in described roadbed fence.
The present invention be realize low, slow, SUAV in the air carried out locking, early warning, tracking, it is expelled and is compeled
Fall, has done brand-new design to unmanned plane system of defense, the beneficial effect using above technical scheme is: described early radar warning system
System adopts high and low idle pattern formula detection radar, and high level matches with low level carries out scanning early warning to target spatial domain, adopts thunder on certain area
Reach the mode of networking detection, realize omnibearing non-blind area and detect;Infrared system in described optics early warning system, realize daytime,
Early warning is visualized under multiple environment such as night, rainy day, haze sky;Described roadbed fence is laid using multiple spot, and combined type is many
Band interference, compacting, the cut-out closely communication connection at unmanned plane and remote controlled floor station and unmanned plane positional information, make target no
Man-machine flight of cannot going up to the air, is in addition provided with frequency analysis unit in roadbed fence, can be with automatic identification UAV Communication
Chain, such as communication frequency, realize targetedly frequency range compacting;Described mobile individual soldier expels and is provided with individual soldier's mobile electronic rifle in device,
Using individual soldier's mobile electronic rifle, the unmanned plane in spatial domain is force-landed or so that it is maked a return voyage, realize remote interference, make up road
The short weakness of base fence operating distance.
Brief description
Fig. 1 is the structured flowchart of whole unmanned plane system of defense.
Fig. 2 is the antiaircraft schematic diagram of this system of defense;
Specific embodiment
Below against accompanying drawing, by the description to embodiment, the specific embodiment of the present invention is made further details of
Illustrate it is therefore an objective to help those skilled in the art to have more complete, accurate and deep reason to the design of the present invention, technical scheme
Solution, and contribute to its enforcement.
As shown in figure 1, the present invention is a kind of low latitude unmanned plane system of defense, it is to realize to low, slow, SUAV in the air
Carry out locking, early warning, tracking, it is expelled and is force-landed.
Specifically, as shown in figure 1, including control centre, antiaircraft early warning system and electronics to expel system, as shown in figure 1,
Wherein control centre expels system bidirectional with antiaircraft early warning system and electronics respectively and is connected, and described antiaircraft early warning system is pre- by radar
Alarm system and optics early warning system are constituted, and electronics expels system and expelled device and constituted by roadbed fence and mobile individual soldier;As Fig. 2
Shown, described radar early warning system adopts high and low idle pattern formula detection radar, and described high and low idle pattern formula detection radar is adopted
With periphery multiple spot arrangement, described optics early warning system is made up of infrared system and VISIBLE LIGHT SYSTEM, and optics early warning system adopts
Periphery multiple spot is arranged;Described roadbed fence is laid using multiple spot, the interference of combined type multifrequency section, compacting, described mobile individual soldier
Expel and in device, be provided with individual soldier's mobile electronic rifle;It is provided with frequency analysis unit in described roadbed fence.
With specific embodiment, specific works mode is illustrated below:
After having unmanned plane to fly into the early radar warning area in target spatial domain, by radar early warning system and optics early warning system
Carry out early warning, radar early warning system adopts high and low idle pattern formula detection radar, high level matches with low level carries out pre- to the scanning of target spatial domain
Alert, on certain area by the way of radar network composite detection, realize omnibearing non-blind area and detect, the unmanned plane that radar will detect
Distance, the information transfer such as flying speed and orientation to control centre, realize aerial target is carried out with early warning and follow the tracks of anticipation, one
Denier target flies into closely electrical isolation area, then expels system by control centre's comprehensive descision backward electronics of analysis and sends finger
Order, for the relatively low unmanned plane of flying height, by the way of roadbed fence, is laid using multiple spot, combined type multifrequency section
Interference, compacting, the cut-out closely communication connection at unmanned plane and remote controlled floor station and unmanned plane positional information, make UAV targets
Cannot go up to the air flight, in addition in roadbed fence, be provided with frequency analysis unit, can be with automatic identification UAV Communication chain, such as
Communication frequency, realizes targetedly frequency range compacting;For the higher unmanned plane of flying height, device is expelled using mobile individual soldier, institute
State mobile individual soldier and expel and in device, be provided with individual soldier's mobile electronic rifle, using individual soldier's mobile electronic rifle, the unmanned plane in spatial domain is entered
Row force-lands or so that it is maked a return voyage, and realizes remote interference, makes up the short weakness of roadbed fence operating distance.
Above in association with accompanying drawing, the present invention is exemplarily described it is clear that the present invention implements is not subject to above-mentioned side
The restriction of formula, as long as employ the improvement of the various unsubstantialities that method of the present invention design is carried out with technical scheme;Or not
Improved, the above-mentioned design of the present invention and technical scheme are directly applied to other occasions, all in protection scope of the present invention
Within.
Claims (4)
1. a kind of low latitude unmanned plane system of defense, expels system including control centre, antiaircraft early warning system and electronics, wherein controls
Center expels system bidirectional with antiaircraft early warning system and electronics respectively and is connected, described antiaircraft early warning system by radar early warning system and
Optics early warning system is constituted, and electronics expels system and expelled device and constituted by roadbed fence and mobile individual soldier.
2. a kind of low latitude unmanned plane system of defense according to claim 1 it is characterised in that: described radar early warning system is adopted
With high and low idle pattern formula detection radar, and described high and low idle pattern formula detection radar adopts periphery multiple spot to arrange, described optics
Early warning system is made up of infrared system and VISIBLE LIGHT SYSTEM, and optics early warning system adopts periphery multiple spot to arrange.
3. a kind of low latitude unmanned plane system of defense according to claim 1 it is characterised in that: described roadbed fence is adopted
Laid with multiple spot, the interference of combined type multifrequency section, compacting, described mobile individual soldier expels and is provided with individual soldier's mobile electronic rifle in device.
4. a kind of low latitude unmanned plane system of defense according to any one of claim 1,3 it is characterised in that: described roadbed
It is provided with frequency analysis unit in fence.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
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CN201610729461.1A CN106341206A (en) | 2016-08-26 | 2016-08-26 | Low-altitude unmanned aerial vehicle defense system |
PCT/CN2017/094082 WO2018036323A1 (en) | 2016-08-26 | 2017-07-24 | Defense system and method for defending against low-flying unmanned aerial vehicle |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201610729461.1A CN106341206A (en) | 2016-08-26 | 2016-08-26 | Low-altitude unmanned aerial vehicle defense system |
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CN201610729461.1A Pending CN106341206A (en) | 2016-08-26 | 2016-08-26 | Low-altitude unmanned aerial vehicle defense system |
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WO (1) | WO2018036323A1 (en) |
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
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CN106846922A (en) * | 2017-03-14 | 2017-06-13 | 武汉天宇智戎防务科技有限公司 | Low altitude short range cluster cooperates with defence system and defence method |
CN107067617A (en) * | 2017-05-16 | 2017-08-18 | 京东方科技集团股份有限公司 | A kind of method for safety monitoring and safety monitoring system based on unmanned plane |
CN107132583A (en) * | 2017-06-07 | 2017-09-05 | 嘉兴扬光电科技有限公司 | A kind of laser scanning barrier generation method detected for unmanned plane |
CN107219520A (en) * | 2017-05-31 | 2017-09-29 | 成都新越科技有限公司 | A kind of anti-unmanned plane distributed networking detection method and its device |
CN107424442A (en) * | 2017-06-30 | 2017-12-01 | 北京明朝万达科技股份有限公司 | Fence and the unmanned aerial vehicle (UAV) control method based on fence |
CN107728119A (en) * | 2017-10-18 | 2018-02-23 | 潘卫军 | The early warning of airport and terminal area unmanned plane and counter system and method |
WO2018036323A1 (en) * | 2016-08-26 | 2018-03-01 | 广东容祺智能科技有限公司 | Defense system and method for defending against low-flying unmanned aerial vehicle |
CN107830767A (en) * | 2017-10-24 | 2018-03-23 | 武汉康慧然信息技术咨询有限公司 | Unmanned plane counter method and medium based on remote control |
CN107846258A (en) * | 2017-09-07 | 2018-03-27 | 新疆美特智能安全工程股份有限公司 | A kind of unmanned plane system of defense |
CN108507415A (en) * | 2018-03-01 | 2018-09-07 | 上海市保安服务总公司 | Motor driven Modularized unmanned machine breaks through system |
CN108737013A (en) * | 2018-05-07 | 2018-11-02 | 东莞市灵睛智能科技有限公司 | A kind of multi-functional interference device and method for civilian multi-rotor unmanned aerial vehicle camera system |
CN109724473A (en) * | 2018-12-06 | 2019-05-07 | 天津中天高科防务技术有限公司 | A kind of defence method of the anti-unmanned plane system of defense of vehicle-mounted networking type in parallel |
CN109917327A (en) * | 2019-03-07 | 2019-06-21 | 青岛国数信息科技有限公司 | A kind of passive type unmanned plane detection system and algorithm based on radio link |
CN110244314A (en) * | 2019-06-24 | 2019-09-17 | 北京机械设备研究所 | One kind " low slow small " target acquisition identifying system and method |
CN110308741A (en) * | 2019-07-16 | 2019-10-08 | 杭州叙简科技股份有限公司 | A kind of multiple spot unmanned plane detecting system of defense and multiple spot unmanned plane detect striking method |
CN111121540A (en) * | 2019-12-27 | 2020-05-08 | 江苏中戎帝晓曼安防科技有限公司 | Radar-based cross-type anti-unmanned aerial vehicle monitoring system and method thereof |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101982720A (en) * | 2010-09-29 | 2011-03-02 | 北京机械设备研究所 | Interception method of low-altitude low-velocity small targets |
WO2016045772A1 (en) * | 2014-09-24 | 2016-03-31 | Diehl Bgt Defence Gmbh & Co. Kg | Anti-unmanned aerial vehicle defense apparatus, protective device for fighting an unmanned aircraft, and method for operating a protective device |
CN105575188A (en) * | 2016-03-07 | 2016-05-11 | 丁元沅 | Airborne autonomous monitoring and alarming system and method for safe operation of unmanned aerial vehicle |
CN105842718A (en) * | 2016-05-19 | 2016-08-10 | 湖南矩阵电子科技有限公司 | Portable anti-UAV (unmanned aerial vehicle) rifle |
CN105842683A (en) * | 2016-05-27 | 2016-08-10 | 南京博驰光电科技有限公司 | Unmanned aerial vehicle integrated defense system and method |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106341206A (en) * | 2016-08-26 | 2017-01-18 | 广东容祺智能科技有限公司 | Low-altitude unmanned aerial vehicle defense system |
-
2016
- 2016-08-26 CN CN201610729461.1A patent/CN106341206A/en active Pending
-
2017
- 2017-07-24 WO PCT/CN2017/094082 patent/WO2018036323A1/en active Application Filing
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101982720A (en) * | 2010-09-29 | 2011-03-02 | 北京机械设备研究所 | Interception method of low-altitude low-velocity small targets |
WO2016045772A1 (en) * | 2014-09-24 | 2016-03-31 | Diehl Bgt Defence Gmbh & Co. Kg | Anti-unmanned aerial vehicle defense apparatus, protective device for fighting an unmanned aircraft, and method for operating a protective device |
CN105575188A (en) * | 2016-03-07 | 2016-05-11 | 丁元沅 | Airborne autonomous monitoring and alarming system and method for safe operation of unmanned aerial vehicle |
CN105842718A (en) * | 2016-05-19 | 2016-08-10 | 湖南矩阵电子科技有限公司 | Portable anti-UAV (unmanned aerial vehicle) rifle |
CN105842683A (en) * | 2016-05-27 | 2016-08-10 | 南京博驰光电科技有限公司 | Unmanned aerial vehicle integrated defense system and method |
Cited By (21)
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WO2018036323A1 (en) * | 2016-08-26 | 2018-03-01 | 广东容祺智能科技有限公司 | Defense system and method for defending against low-flying unmanned aerial vehicle |
CN106846922A (en) * | 2017-03-14 | 2017-06-13 | 武汉天宇智戎防务科技有限公司 | Low altitude short range cluster cooperates with defence system and defence method |
CN107067617A (en) * | 2017-05-16 | 2017-08-18 | 京东方科技集团股份有限公司 | A kind of method for safety monitoring and safety monitoring system based on unmanned plane |
CN107219520A (en) * | 2017-05-31 | 2017-09-29 | 成都新越科技有限公司 | A kind of anti-unmanned plane distributed networking detection method and its device |
CN107132583A (en) * | 2017-06-07 | 2017-09-05 | 嘉兴扬光电科技有限公司 | A kind of laser scanning barrier generation method detected for unmanned plane |
CN107424442A (en) * | 2017-06-30 | 2017-12-01 | 北京明朝万达科技股份有限公司 | Fence and the unmanned aerial vehicle (UAV) control method based on fence |
CN107846258A (en) * | 2017-09-07 | 2018-03-27 | 新疆美特智能安全工程股份有限公司 | A kind of unmanned plane system of defense |
CN107728119A (en) * | 2017-10-18 | 2018-02-23 | 潘卫军 | The early warning of airport and terminal area unmanned plane and counter system and method |
CN107830767B (en) * | 2017-10-24 | 2019-09-10 | 泰州市天宇交通器材有限公司 | Based on the unmanned plane counter method remotely controlled and medium |
CN107830767A (en) * | 2017-10-24 | 2018-03-23 | 武汉康慧然信息技术咨询有限公司 | Unmanned plane counter method and medium based on remote control |
CN108507415A (en) * | 2018-03-01 | 2018-09-07 | 上海市保安服务总公司 | Motor driven Modularized unmanned machine breaks through system |
CN108737013A (en) * | 2018-05-07 | 2018-11-02 | 东莞市灵睛智能科技有限公司 | A kind of multi-functional interference device and method for civilian multi-rotor unmanned aerial vehicle camera system |
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CN109724473A (en) * | 2018-12-06 | 2019-05-07 | 天津中天高科防务技术有限公司 | A kind of defence method of the anti-unmanned plane system of defense of vehicle-mounted networking type in parallel |
CN109724473B (en) * | 2018-12-06 | 2021-10-29 | 天津中天高科防务技术有限公司 | Defense method of vehicle-mounted parallel networking type anti-unmanned aerial vehicle defense system |
CN109917327A (en) * | 2019-03-07 | 2019-06-21 | 青岛国数信息科技有限公司 | A kind of passive type unmanned plane detection system and algorithm based on radio link |
CN109917327B (en) * | 2019-03-07 | 2021-04-20 | 青岛国数信息科技有限公司 | Passive unmanned aerial vehicle detection system and algorithm based on radio link |
CN110244314A (en) * | 2019-06-24 | 2019-09-17 | 北京机械设备研究所 | One kind " low slow small " target acquisition identifying system and method |
CN110308741A (en) * | 2019-07-16 | 2019-10-08 | 杭州叙简科技股份有限公司 | A kind of multiple spot unmanned plane detecting system of defense and multiple spot unmanned plane detect striking method |
CN110308741B (en) * | 2019-07-16 | 2022-02-11 | 杭州叙简科技股份有限公司 | Multipoint unmanned aerial vehicle detection defense system and multipoint unmanned aerial vehicle detection striking method |
CN111121540A (en) * | 2019-12-27 | 2020-05-08 | 江苏中戎帝晓曼安防科技有限公司 | Radar-based cross-type anti-unmanned aerial vehicle monitoring system and method thereof |
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