CN109709543A - A method of search detecting unmanned plane - Google Patents

A method of search detecting unmanned plane Download PDF

Info

Publication number
CN109709543A
CN109709543A CN201910177529.3A CN201910177529A CN109709543A CN 109709543 A CN109709543 A CN 109709543A CN 201910177529 A CN201910177529 A CN 201910177529A CN 109709543 A CN109709543 A CN 109709543A
Authority
CN
China
Prior art keywords
unmanned plane
radar
module
radar module
search
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.)
Pending
Application number
CN201910177529.3A
Other languages
Chinese (zh)
Inventor
刘荣山
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.)
Fujian Xingtu Intelligent Control Technology Co Ltd
Original Assignee
Fujian Xingtu Intelligent Control 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 Fujian Xingtu Intelligent Control Technology Co Ltd filed Critical Fujian Xingtu Intelligent Control Technology Co Ltd
Priority to CN201910177529.3A priority Critical patent/CN109709543A/en
Publication of CN109709543A publication Critical patent/CN109709543A/en
Pending legal-status Critical Current

Links

Abstract

A kind of method that the present invention proposes search detecting unmanned plane, for scanning for detecting to the unmanned plane in designated flying zone, the method includes transmitting radar modules, the analysis module for receiving radar module and being connected with reception radar module;The analysis module storage has unmanned plane flow perturbation characteristic when unmanned plane during flying;The transmitting radar is the transmitting radar being set as to designated flying zone launching detection radar wave, the received radar module of analysis module obtains the radar reflection wave beam of designated flying zone, and the airflow state data of designated flying zone are analyzed from reflected beam, when airflow state data include the matched data of the man-machine flow perturbation characteristic of being and not being, that is, think that designated flying zone there may be the unmanned plane of state of flight;The present invention can make up the defect of traditional unmanned plane search, accurately scan for detecting to the unmanned plane during flying phenomenon of designated flying zone.

Description

A method of search detecting unmanned plane
Technical field
The present invention relates to the radar exploration technique field, especially a kind of method of search detecting unmanned plane.
Background technique
Since China opens gradually 1000 meters or less low altitude airspaces, unmanned plane, model plane, fire balloon, hot balloon etc. " low, Slowly, small " aircraft is more and more, while offering convenience to socio-economic development, chance also is brought to criminal, Various illegal flights cause serious security risk to key activities, key area." black to fly " especially frequently reported recently Cause numerous flight Emergency avoidances, the very disruptive normal flight of flight, landing.At the same time, it is also not excluded for individual illegal Molecule can carry video camera possibly also with the more dry illegal business of unmanned plane or terrorist activity, unmanned plane, can also transport explosive And other items, sound is small, is difficult to discover, and can pry through other people privacies and the attack of terrorism etc. using miniature drone to criminal and create Condition.
" black to fly " event is also possible to jeopardize life and property safety of people, disturb public order.Professional instruction is not received It is experienced, in order to meet personal interest, largely exist without the user that flight laws and regulations are realized without common sense;Civilian unmanned plane is light Two or three kilogram, tens kilograms of weight, tens meters, more than 100 meters in the air fall down, may cause casualties.If in public affairs Place " black to fly " more than garden et al., the danger that may cause is self-evident.
Search at present finds that the mode of aerial low slow Small object mainly has, passive radio-frequency spectrum detecting search discovery, Traditional passive or active search lighting discovery target surface, sound wave identification search discovery and visible light camera or infrared Thermal imaging system etc..
Monitoring radio-frequency spectrum is by passively detecting unmanned plane and ground remote control person " communication ", as remote control system, number pass The spectrum signal of system or image transmission system is to search for discovery unmanned plane.Monitoring radio-frequency spectrum wide, distance with reconnaissance range Far, swift feature is a practicable effective detecting means, if but unmanned plane target do not emit radio signal and In " silence " state, will be unable to detect unmanned plane using electromagnetic spectrum method.
Conventional radar search discovery unmanned plane is to utilize electromagnetic wave by existing 2D/3D mechanically or electrically scanning radar technology Detecting of the back wave phenomenon realization to unmanned plane target is generated when by different transmission mediums, but modern unmanned plane is generally all It is to be made of plastic foam, cork wood and composite, this material has special wave property, greatly reduces actual effect.In addition The radar scattering area of unmanned plane itself is very small, reduces effective scattering area, distance and the probability of detection detected by radar.
Sound wave identification search discovery unmanned plane is the noise by issuing when identification unmanned aerial vehicle onboard work to find and detect Survey unmanned plane.The audio detected is matched with the database for having recorded all unmanned plane machine audios, can be picked out Whether be unmanned plane the sound.But the current technology is effectively detected apart from short, and is easily disturbed.
Visible light/infrared detecting reflected using the thermal infrared of visible light or target, using over the horizon, high definition, is revealed It can be seen that video camera and infrared thermal imager sensor combinations carry out unmanned plane detecting.Visible light/infrared detecting can find various The unmanned plane of model can be realized all-weather, real time implementation, visual monitoring management.But unmanned plane is due to small in size, infrared Radiation is low with feature, so that being greatly shortened by the detective distance of infrared detecting, on anti-laser detecting, unmanned plane is easier to take Wave, transmission, leaded light material are such as inhaled, laser reflection and shape stealth design etc. are reduced, so that visible light/infrared detecting becomes more Add difficulty.
Summary of the invention
A kind of method that the present invention proposes search detecting unmanned plane can make up the defect of traditional unmanned plane search, accurately The unmanned plane during flying phenomenon of designated flying zone is scanned for detecting.
The present invention uses following technical scheme.
A method of search detecting unmanned plane, for scanning for detecting to the unmanned plane in designated flying zone, the side Method includes the analysis module for emitting radar module, receiving radar module and being connected with reception radar module;The analysis module storage There is unmanned plane flow perturbation characteristic when unmanned plane during flying;The transmitting radar is to be set as to designated flying zone emission detection The transmitting radar of radar wave, the received radar module of the analysis module obtain the radar reflection wave beam of designated flying zone, and from anti- The airflow state data that designated flying zone is analyzed in ejected wave beam, when airflow state data include the man-machine flow perturbation characteristic of being and not being When according to matched data, that is, think that designated flying zone there may be the unmanned plane of state of flight.
The transmitting radar module and the quantity for receiving radar module are carried out in one-to-one ratio or one-to-many ratio Configuration.
The transmitting radar module receives a part that radar module is weather radar, or is the one of Doppler radar Part.
The unmanned plane include fixed-wing unmanned plane, multi-rotor unmanned aerial vehicle or be provided simultaneously with fixed-wing and more rotors nobody Machine.
The unmanned plane flow perturbation characteristic includes the vortical disturbance spy generated when unmanned plane rotor works in the sky Data are levied, further include the body wake flow perturbation features data of unmanned plane.
The vortical disturbance characteristic, body wake flow perturbation features data are the sky that unmanned plane works or formed when moving Radar reflection wave beam feature caused by refractive index caused by gas turbulent flow and air density change changes.
When analysis module discovery airflow state data include the matched data of the man-machine flow perturbation characteristic of being and not being, Think that the unmanned plane flow perturbation point position of designated flying zone there may be the unmanned plane of state of flight.
The transmitting radar module and reception radar module are highly sensitive UHF Doppler radar module or V.H.F. radar Module.
The transmitting radar module includes transmitter;The reception radar module includes receiver, signal processor, data Processor and display;The transmitting radar module is connected through duplexer with radar antenna with radar module is received;The thunder It is connected up to antenna with beam scanning generator or servomechanism.
Technical solution of the present invention is the vortex generated when working in the sky for the rotor of multi-rotor unmanned aerial vehicle or solid The different degrees of variation for determining the atmospheric refraction index that the wake flow that wing unmanned plane body generates is occurred can scatter irregular thunder It is designed up to this phenomenon of wave beam, it is well known that the irregular variation of atmospheric refraction can generate irregular radar illumination and return Wave, and atmospheric refraction is irregularly irregular variation (vortex or wake flow internal gas flow by the temperature of air-flow, humidity and density Flow at high speed) caused by;When unmanned plane during flying, air-flow high-speed motion that vortex or wake flow generate when working in the sky with unmanned plane And flow, ground radar receiving module can detect the irregular echo that vortex or wake flow are scattered and search for discovery and arrive nobody Machine;And vortex or wake flow are that unmanned plane works the fundamemtal phenomena that can not be disappeared in the sky, obtain vortex or wake flow is irregular Radar return information just finds that unmanned plane provides a kind of most direct effective tool for search lighting.
The principle of the invention is unique, is skillfully constructed, feasibility height, and energy effective search finds aerial " low, small, slow " target, energy Effectively inhibit unmanned plane " black to fly " irregularity, the present invention program is not influenced by unmanned plane material, and due to mechanical The movement of aircraft and flying bird have larger difference, therefore can easily be distinguish to unmanned plane and flying bird.
Detailed description of the invention
The present invention is described in more detail with reference to the accompanying drawings and detailed description:
Attached drawing 1 is the schematic diagram that unmanned plane generates flow perturbation;
Attached drawing 2 is operation schematic diagram of the invention;
Attached drawing 3 is the composition schematic diagram of radar;
In figure: 1- unmanned plane;2- emits radar module;3- receives radar module.
Specific embodiment
As shown in Figure 1-3, a kind of method of search detecting unmanned plane, for being searched to the unmanned plane 1 in designated flying zone Rope detecting, the method includes transmitting radar modules 2, the analysis module for receiving radar module 3 and being connected with reception radar module; The analysis module storage has unmanned plane flow perturbation characteristic when unmanned plane during flying;The transmitting radar is to be set as to finger Determine the transmitting radar of airspace launching detection radar wave, the radar that the received radar module of analysis module obtains designated flying zone is anti- Ejected wave beam, and the airflow state data of designated flying zone are analyzed from reflected beam, when to include being and not being man-machine for airflow state data When the matched data of flow perturbation characteristic, that is, think that designated flying zone there may be the unmanned plane of state of flight.
The transmitting radar module and the quantity for receiving radar module are carried out in one-to-one ratio or one-to-many ratio Configuration.
The transmitting radar module receives a part that radar module is weather radar, or is the one of Doppler radar Part.
The unmanned plane include fixed-wing unmanned plane, multi-rotor unmanned aerial vehicle or be provided simultaneously with fixed-wing and more rotors nobody Machine.
The unmanned plane flow perturbation characteristic includes the vortical disturbance spy generated when unmanned plane rotor works in the sky Data are levied, further include the body wake flow perturbation features data of unmanned plane.
The vortical disturbance characteristic, body wake flow perturbation features data are the sky that unmanned plane works or formed when moving Radar reflection wave beam feature caused by refractive index caused by gas turbulent flow and air density change changes.
When analysis module discovery airflow state data include the matched data of the man-machine flow perturbation characteristic of being and not being, Think that the unmanned plane flow perturbation point position of designated flying zone there may be the unmanned plane of state of flight.
The transmitting radar module and reception radar module are highly sensitive UHF Doppler radar module or V.H.F. radar Module.
The transmitting radar module includes transmitter;The reception radar module includes receiver, signal processor, data Processor and display;The transmitting radar module is connected through duplexer with radar antenna with radar module is received;The thunder It is connected up to antenna with beam scanning generator or servomechanism.
Embodiment:
The lift of multi-rotor unmanned aerial vehicle be mainly derived from air is pushed by rotor blade high speed rotation and is utilized thus to obtain The active force of downwash flow and generate, therefore rotor upper and lower of the multi-rotor unmanned aerial vehicle in traveling or hovering because blade high speed revolve It changes the line of production raw vortex.
The wake flow that the vortex or fixed-wing unmanned plane body generated when the rotor of multi-rotor unmanned aerial vehicle works in the sky generates The different degrees of variation of the atmospheric refraction index occurred can scatter irregular radar beam.The irregular change of atmospheric refraction Change can generate irregular radar illumination echo, and atmospheric refraction be irregularly by air-flow temperature, humidity and density not Caused by rule variation (vortex or wake flow internal gas flow flow at high speed).
Air-flow high-speed motion that vortex or wake flow generate when working in the sky with unmanned plane and flow, ground launch radar The same wave beam that (transmitting radar module) is launched reaches in the swirling air stream of multi-rotor unmanned aerial vehicle, reflects from swirling air stream Be to the echo for receiving radar (receive radar module) it is different, handled in this way by rear end a series of signal and data processing Discovery is searched for unmanned plane etc. irregular echo that vortex or wake flow are scattered can be detected.
It is described through the invention since vortex or wake flow are that unmanned plane works the fundamemtal phenomena that can not be disappeared in the sky After scheme obtains vortex or the irregular radar return information of wake flow, just find that unmanned plane provides one kind most for search lighting Direct effective tool.

Claims (9)

1. a kind of method of search detecting unmanned plane, for scanning for detecting to the unmanned plane in designated flying zone, feature exists In: the method includes transmitting radar modules, the analysis module for receiving radar module and being connected with reception radar module;Described point Analysis module storage has unmanned plane flow perturbation characteristic when unmanned plane during flying;The transmitting radar is to be set as to designated flying zone The transmitting radar of launching detection radar wave, the received radar module of analysis module obtain the radar return of designated flying zone Beam, and from reflected beam analyze designated flying zone airflow state data, when airflow state data include the man-machine air-flow of being and not being When the data of perturbation features Data Matching, that is, think that designated flying zone there may be the unmanned plane of state of flight.
2. a kind of method of search detecting unmanned plane according to claim 1, it is characterised in that: the transmitting radar module It is configured with the quantity for receiving radar module in one-to-one ratio or one-to-many ratio.
3. a kind of method of search detecting unmanned plane according to claim 1, it is characterised in that: the transmitting radar module Or receive a part that radar module is weather radar, or a part for Doppler radar.
4. a kind of method of search detecting unmanned plane according to claim 1, it is characterised in that: the unmanned plane includes solid Determine wing unmanned plane, multi-rotor unmanned aerial vehicle or the unmanned plane for being provided simultaneously with fixed-wing and more rotors.
5. a kind of method of search detecting unmanned plane according to claim 4, it is characterised in that: the unmanned plane air-flow is disturbed Dynamic characteristic includes the vortical disturbance characteristic generated when unmanned plane rotor works in the sky, further includes the body of unmanned plane Wake flow perturbation features data.
6. a kind of method of search detecting unmanned plane according to claim 5, it is characterised in that: the vortical disturbance feature Data, body wake flow perturbation features data are that the air turbulence and air density change that unmanned plane works or formed when moving cause Refractive index change caused by radar reflection wave beam feature.
7. a kind of method of search detecting unmanned plane according to claim 1, it is characterised in that: when analysis module finds gas When stream status data includes the man-machine flow perturbation characteristic of being and not being matched data, that is, think the unmanned plane gas of designated flying zone Flow disturbance point position there may be the unmanned plane of state of flight.
8. a kind of method of search detecting unmanned plane according to claim 1, it is characterised in that: the transmitting radar module It is highly sensitive UHF Doppler radar module or V.H.F. radar module with radar module is received.
9. a kind of method of search detecting unmanned plane according to claim 8, it is characterised in that: the transmitting radar module Including transmitter;The reception radar module includes receiver, signal processor, data processor and display;The transmitting Radar module is connected through duplexer with radar antenna with radar module is received;The radar antenna and beam scanning generator or Servomechanism is connected.
CN201910177529.3A 2019-03-09 2019-03-09 A method of search detecting unmanned plane Pending CN109709543A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910177529.3A CN109709543A (en) 2019-03-09 2019-03-09 A method of search detecting unmanned plane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910177529.3A CN109709543A (en) 2019-03-09 2019-03-09 A method of search detecting unmanned plane

Publications (1)

Publication Number Publication Date
CN109709543A true CN109709543A (en) 2019-05-03

Family

ID=66266611

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201910177529.3A Pending CN109709543A (en) 2019-03-09 2019-03-09 A method of search detecting unmanned plane

Country Status (1)

Country Link
CN (1) CN109709543A (en)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070089502A1 (en) * 2003-08-11 2007-04-26 Martin Andrew L Detection of wake vortices and the like in the lower atmosphere
CN102721967A (en) * 2012-06-21 2012-10-10 中国人民解放军电子工程学院 Method for discovering target in air based on disturbance type of wind field
CN102759732A (en) * 2011-04-28 2012-10-31 谢媛媛 Novel method for detecting aerodynamic vehicle
CN107678023A (en) * 2017-10-10 2018-02-09 芜湖华创光电科技有限公司 A kind of passive location and identifying system to civilian unmanned plane
CN210072069U (en) * 2019-03-09 2020-02-14 福建星图智控科技有限公司 Unmanned aerial vehicle's device is listened in search

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070089502A1 (en) * 2003-08-11 2007-04-26 Martin Andrew L Detection of wake vortices and the like in the lower atmosphere
CN102759732A (en) * 2011-04-28 2012-10-31 谢媛媛 Novel method for detecting aerodynamic vehicle
CN102721967A (en) * 2012-06-21 2012-10-10 中国人民解放军电子工程学院 Method for discovering target in air based on disturbance type of wind field
CN107678023A (en) * 2017-10-10 2018-02-09 芜湖华创光电科技有限公司 A kind of passive location and identifying system to civilian unmanned plane
CN210072069U (en) * 2019-03-09 2020-02-14 福建星图智控科技有限公司 Unmanned aerial vehicle's device is listened in search

Similar Documents

Publication Publication Date Title
JP6480587B2 (en) Commercial and general aircraft avoidance using light, sound, and / or multispectral pattern detection
US10109204B1 (en) Systems and methods for unmanned aerial vehicle object avoidance
US9997079B2 (en) Commercial and general aircraft avoidance using multi-spectral wave detection
US9685089B2 (en) Commercial and general aircraft avoidance using acoustic pattern recognition
CN107883916A (en) Method and apparatus for sense aircraft areal deformation
Farlik et al. Radar cross section and detection of small unmanned aerial vehicles
Sabatini et al. A laser obstacle warning and avoidance system for manned and unmanned aircraft
CN107054679A (en) A kind of high motor-driven anti-UAS of active capture type and method
KR20180043912A (en) System for cooperative anti-drone and method for cooperation control of anti-drones
CN111412788A (en) Suspected target detection system of thunder field
JP2010044031A (en) Method for identifying aircraft, method for measuring aircraft noise and method for determining signals using the same
Salhi et al. Multi-array spherical LiDAR system for drone detection
CN206573714U (en) A kind of airport spy bird radar system
CN210072069U (en) Unmanned aerial vehicle's device is listened in search
CN109709543A (en) A method of search detecting unmanned plane
CN208805572U (en) A kind of radar target recognition equipment
CN206797767U (en) A kind of high motor-driven anti-UAS of active capture type
CN206038902U (en) Radar early warning system
Sud UAVs and Counter UAVs Technologies in the World and the Indigenous Capability
CN108981474A (en) A kind of capture system and method for antenna radar
IL308288A (en) Method and flexible apparatus permitting advanced radar signal processing, tracking, and classification/identification design and evaluation using single unmanned air surveillance (uas) device
Singh et al. Electronic Warfare System Using Anti-Radar UAV
Popescu The existing technologies on anti-drone systems
WO2019123526A1 (en) Device for collecting aircraft flight history information
Vozella et al. Solution Set Up for Airport Protection from Intruder Drones

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination