CN110530209A - The highly integrated anti-UAV system of one kind and method - Google Patents
The highly integrated anti-UAV system of one kind and method Download PDFInfo
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- CN110530209A CN110530209A CN201910791683.XA CN201910791683A CN110530209A CN 110530209 A CN110530209 A CN 110530209A CN 201910791683 A CN201910791683 A CN 201910791683A CN 110530209 A CN110530209 A CN 110530209A
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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
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Abstract
The highly integrated anti-UAV system of one kind and method, belong to anti-air vehicle technique field.The present invention overcomes the problems, such as the coordinate system disunity between each equipment and the occlusion issue between equipment, devise a kind of vehicle-mounted/fixed anti-UAV system set up of the high integration for integrating command and control, radar, photoelectricity, radio detection, compacting interference and navigation spoofer, including servo turntable, radar equipment, command and control system equipment, radio detection equipment, optoelectronic device, navigation spoofer, compacting jamming equipment.The present invention has many advantages such as that function is complete, small in size, easy to operate, high reliablity.
Description
Technical field
The present invention relates to a kind of highly integrated anti-UAV system and methods, belong to anti-air vehicle technique field.
Background technique
With the fast development of unmanned air vehicle technique, unmanned plane is not only played an important role in military field, in civilian neck
Domain is also widely applied.However, with the continuous reduction for using difficulty, unmanned plane brought to people's production and living it is huge
While convenient, " black to fly " also causes safety hazard to country, society and the people with abuse.
Currently, anti-UAV system equipment mostly tracks and identifies equipment by detection, intercepts in disposal facility and command and control
Heart composition.It mainly includes radar equipment, optoelectronic device and radio detection equipment that detection, which tracks and identifies equipment,；Intercept disposal facility
Main includes compacting interference and navigation spoofer；Command and control system mainly includes industrial personal computer, interchanger, display, keyboard
And command and control software, to realize Fusion, Situation Assessment, command and control and synthesis display.Anti- unmanned plane system
System is mostly vehicle-mounted or fixed erection.When vehicle-mounted erection, since vehicular platform volume is limited, it is difficult to while on same chassis
Radar, photoelectricity, radio detection equipment, compacting interference and navigation spoofer are set up, and unobstructed between each other；Work as fixed frame
If when, although space is enough big, each equipment can also realize that separation is set up, coordinate system disunity between each equipment, for reality
Now accurate detection and disposition, it is necessary to the coordinate system of each equipment is subjected to unification, this work is complicated and as long as equipment displacement
It is unified to need to re-start coordinate system.
The anti-unmanned more discretes of machine equipment most of at present are set up, although this structure is able to achieve the effect of anti-unmanned plane,
But due to depositing blocking between devices, certainly exist unmanned plane can not be carried out in some or multiple angular ranges it is effective
Detection track and identify or dispose.
Summary of the invention
Technical problem solved by the present invention is having overcome the deficiencies of the prior art and provide a kind of highly integrated anti-unmanned plane
System and method devises one kind for the coordinate system disunity problem between each equipment and the occlusion issue between equipment
Gu integrate command and control, radar, photoelectricity, radio detection, compacting interference and navigation spoofer high integration it is vehicle-mounted/
Surely the anti-UAV system set up is very necessary, which has many such as function is complete, small in size, easy to operate, reliability is high
Advantage.
The technical solution of the invention is as follows: a kind of highly integrated anti-UAV system, including servo turntable, radar are set
Standby, command and control system equipment, radio detection equipment, optoelectronic device, navigation spoofer, compacting jamming equipment；
The target prior information detected is sent to command and control system for detecting target by the radio detection equipment
System equipment；
The radar equipment, optoelectronic device, navigation spoofer and compacting jamming equipment are installed on servo turntable；Institute
Radar equipment is stated according to target prior information real-time tracking and measures distance, orientation, movement velocity and the pitch angle of target, and will
The target information detected is exported in real time to command and control system equipment；
The command and control system equipment receives and processes target prior information, is set according to target prior information control radar
It is standby to carry out quadratic probing, servo turntable rotary motion is controlled according to the target information that radar equipment detects, makes optoelectronic device, lead
Spoofer and compacting jamming equipment navigate towards target, while controlling optoelectronic device and target is identified and positioned, according to knowledge
Not and the target control of positioning navigates spoofer to target transmission navigation spoofed signal, according to the target control identified and positioned
It suppresses jamming equipment and sends corresponding interference signal, complete anti-goal task.
Further, the radar equipment is mounted on the top of servo turntable, the optoelectronic device, navigation spoofer and
Compacting jamming equipment is mounted on the two sides of servo turntable according to respective weight, so that the weight difference of two sides is minimum.
Further, the optoelectronic device and navigation spoofer are mounted on the side of servo turntable, suppress jamming equipment
It is mounted on the other side of servo turntable.
Further, the servo turntable includes ontology orientation rotation platform, top orientation rotation platform and side pitching turntable；
The ontology orientation rotation platform is for radar equipment, optoelectronic device, navigation spoofer and suppresses jamming equipment in the horizontal direction
Upper rotation；The radar equipment is mounted on the orientation rotation platform of top, the direction of rotation of the top orientation rotation platform and ontology
The direction of rotation of orientation rotation platform is remained unchanged for realizing the direction of radar equipment on the contrary, speed is identical；The side pitching rotation
Turntable is used to adjust optoelectronic device, navigation spoofer and the direction for suppressing jamming equipment.
It further, further include lodging mechanism；The servo turntable is mounted on lodging mechanism, and the lodging mechanism is realized
It is fixed at any angle between 0~90 ° of servo turntable and ground.
It further, further include electric lifting rod；The radio detection equipment is mounted on electric lifting rod, electronic
When elevating lever rises, the investigative range of radio detection equipment is expanded；In electric lifting rod landing, reduce storage volume.
It further, further include motor vehicles；The servo turntable and command and control system equipment are located on motor vehicles.
It further, further include to servo turntable, radar equipment, command and control system equipment, radio detection equipment, light
Electric equipment, navigation spoofer and the power-supply device that jamming equipment offer power supply is provided；The power-supply device is positioned at motor vehicle
Power takeoff generation unit source in enging cabin, the power takeoff generation unit source is when motor vehicles are mobile by the kinetic energy of motor vehicle engine
It is converted into power storage.
Further, the servo turntable, radar equipment, command and control system equipment, radio detection equipment, photoelectricity are set
It is communicated between standby, navigation spoofer and compacting jamming equipment by RJ45 network interface or optical fiber or mobile communication.
The anti-unmanned plane method that a kind of highly integrated anti-UAV system of one kind according to is realized, including walk as follows
It is rapid:
To target acquisition；
Servo turntable rotary motion is controlled according to the target information detected, makes optoelectronic device, navigation spoofer and pressure
Jamming equipment processed controls optoelectronic device and identifies and positions to target towards target, according to the target identified and positioned
Control navigation spoofer sends navigation spoofed signal to target, according to the target control compacting jamming equipment hair identified and positioned
Corresponding interference signal is sent, its cisco unity malfunction is made, completes anti-goal task.
The advantages of the present invention over the prior art are that:
(1) present invention uses integrated structure design, comprehensive integration anti-unmanned plane common detection means (radar, light
Electricity, radio detection) and disposition means (compacting interference, navigation are inveigled), integration degree is high, and function is complete；Meanwhile knot of the present invention
Structure is compact, and simple, structural elements technically reliable is connected between each equipment, and global reliability is higher.
(2) structure of the invention can realize that the orientation machine of all wt from small to large sweeps pitching phase-scan radar, integrated photoelectricity
The installation of equipment, integration navigation spoofer and integration compacting jamming equipment, by the radio detection for being erected at side
Equipment together constitutes complete anti-UAV system, compared with each equipment discrete installation in the prior art, can save at double
Space and set-up time, while Integration Design can mitigate system gross weight at double.
(3) if structure of the invention as vehicle-mounted in use, lodging mechanism can be increased below turntable, realize turntable and turntable
The key lodging of all devices (radar, photoelectricity, compacting interference, navigation are inveigled) of upper dress, can greatly reduce system and set up the time,
It is easy to operate, it is convenient for rapid deployment.
Detailed description of the invention
Fig. 1 is the structural diagram of the invention (main view under vehicle-mounted working condition)；
Fig. 2 is the structural diagram of the invention (left view under vehicle-mounted working condition)；
Fig. 3 is the structural diagram of the invention (main view under vehicle-mounted rounding state)；
Fig. 4 is the structural diagram of the invention (left view under vehicle-mounted rounding state)；
Fig. 5 is the structural diagram of the invention (fixed to set up under working condition)；
Fig. 6 is servo turntable structure diagram of the present invention；
In figure, 1- vehicle chassis；2- lodging mechanism；Orientation, 32- servo turntable are bowed under 3- servo turntable, 31- servo turntable
It faces upward, 33- servo turntable upper position (reversing device)；4- radar equipment；5- command and control system equipment；6- radio detection is set
It is standby；7- electric lifting rod；8- optoelectronic device；9- navigation spoofer；10- suppresses jamming equipment.
Specific embodiment
Invention is further explained with reference to the accompanying drawings and examples.
Embodiment one
As shown in Figure 1,2,3, 4, a kind of highly integrated anti-UAV system of the present invention, including vehicle chassis 1, servo turn
Platform lodging mechanism 2, servo turntable 3, radar equipment 4, command and control system equipment 5, radio detection 6, electric lifting rod 7, light
Electric equipment 8, navigation spoofer 9, compacting jamming equipment 10, azimuthal section 31 under servo turntable, servo turntable pitching part 32,
Servo turntable upper position (reversing device) part 33.
The target prior information detected is sent to command and control system for detecting target by radio detection equipment 6
Equipment 5；The radar equipment 4, optoelectronic device 8, navigation spoofer 9 and compacting jamming equipment 10 are installed in servo turntable 3
On；The radar equipment 4 is according to target prior information real-time tracking and measures distance, orientation, movement velocity and the pitching of target
Angle, and the target information detected is exported in real time to command and control system equipment 5；Command and control system equipment 5 receives and locates
Target prior information is managed, quadratic probing is carried out according to target prior information control radar equipment 4, is detected according to radar equipment 4
Target information control 3 rotary motion of servo turntable, make optoelectronic device 8, navigation spoofer 9 and compacting 10 direction of jamming equipment
Target, while controlling optoelectronic device 8 and target is identified and positioned, it is inveigled and is set according to the target control navigation identified and positioned
Standby 9 send navigation spoofed signal to target, are sent according to the target control compacting jamming equipment 10 identified and positioned corresponding dry
Signal is disturbed, anti-goal task is completed.The anti-goal task is the breaking through UAV targets of the task.
Radar equipment 4 is mounted on the top of servo turntable 3, the optoelectronic device 8, navigation spoofer 9 and compacting interference
Equipment 10 is mounted on the two sides of servo turntable 3 according to respective weight, so that the weight difference of two sides is minimum.Optoelectronic device 8 and navigation
Spoofer 9 is mounted on the side of servo turntable 3, and compacting jamming equipment 10 is mounted on the other side of servo turntable 3.
Vehicle chassis 1 includes original-pack 4 seats, the standard cabinet in boot and the electricity in vehicle body back side left and right sidewall
Source wall box and signal wall box place the 19-inch standard cabinet of one group of 33U behind driver's cabin, place meter inside cabinet in boot
It calculates machine host, interchanger, turning table control cabinet, turntable power supply box, vehicle distribution box, power takeoff generation unit and controls cabinet, electric up-down
Bar cabinet etc., servo turntable lodging mechanism 2 and electric lifting rod 7 and vehicle chassis 1 are connected, and servo turntable 3 passes through bolt and watches
It takes turntable lodging mechanism 2 to be connected, command and control system equipment 5 is including main frame, interchanger and is mounted on driver's cabin first
Arrange keyboard and mouse and the display etc. of heater.
Servo turntable 3 includes ontology orientation rotation platform 31, top orientation rotation platform 33 and side pitching turntable 32；Described
Body orientation rotation platform 31 is for radar equipment 4, optoelectronic device 8, navigation spoofer 9 and suppresses jamming equipment 10 in the horizontal direction
Upper rotation；The radar equipment 4 is mounted on top orientation rotation platform 33, the direction of rotation of the top orientation rotation platform 33 with
The direction of rotation of ontology orientation rotation platform 31 is remained unchanged for realizing the direction of radar equipment 4 on the contrary, speed is identical；It is described
Side pitching turntable 32 is used to adjust optoelectronic device 8, navigation spoofer 9 and the direction for suppressing jamming equipment 10.Specifically, it watches
Taking turntable 3 includes orientation 31, servo turntable pitching 32 and servo turntable upper position (reversing device) 33 under servo turntable, and radar is set
Standby 4 are connect by bolt with servo turntable upper position (reversing device) 33, and optoelectronic device 8 passes through bolt and navigation spoofer 9
It is connected by bolt with servo turntable pitching 32 after being fixed with one, compacting jamming equipment 10 passes through bolt and servo turntable top
Position (reversing device) 33 is connected, and is connected below electric lifting rod 7 by welding and vehicle chassis 1, radio detection 6 passes through bolt
It is connected with the ring flange of 7 top of electric lifting rod.
The invention also includes lodging mechanisms 2；The servo turntable 3 is mounted on lodging mechanism 2, and the lodging mechanism 2 is real
It is fixed at any angle between 0~90 ° of existing servo turntable 3 and ground.
The invention also includes motor vehicles 1；The servo turntable 3 and command and control system equipment 5 are located at motor vehicles 1
On.
Power-supply device is the power takeoff generation unit source in 1 enging cabin of motor vehicles, and the power takeoff generation unit source is in motor vehicle
1 by the kinetic energy of 1 engine of motor vehicles converts power storage when mobile.
Fig. 3,4 show driving states, and when vehicle reaches position, first vehicle comes to a complete stop, takes out one company of ground cable
Connect power supply wall box earthing rod, one by ground connection pestle with greatly be connected, chassis power takeoff generation unit and mains-supplied can be used in system
Two ways power supply, two kinds of power supply mode operating procedures are roughly the same, below with chassis power takeoff generation unit power supply mode introduction；It opens
Chassis power takeoff generator control cabinet, system power case power switch turn to chassis power taking power supply, and vehicle can be powered, then successively
Opening general supply and required task device are spaced apart can be to each device power；Using electric leveling supporting leg or chassis oil gas hanging
It hangs to work normally vehicle attitude control to radar equipment and require, operator is climbed to roof by the ladder at compartment rear portion, will first be consolidated
The locking device for determining lodging mechanism is opened, and is powered on to lodging mechanism 2, and a key of operation lodging mechanism handle plays perpendicular switch, lodging
Mechanism can be by all devices filled on servo turntable 3 and turntable (radar 4, optoelectronic device 8, navigation spoofer 9, compressed dry
Disturb equipment 10) it holds up to vertical state, lodging mechanism can realize any 0~90 ° of rotation, and can stop in any angular position
Only；It is powered on to electric lifting rod 7, operates the operation handle of electric lifting rod 7, pressed next key and rise key, electric lifting rod 7 will
Radio detection 6 rises, and completes the expansion (state as shown in Figure 1, 2) of system equipment at this time；Each upper installing is standby to be passed through
RJ45 network interface access switch, the main frame of command and control system equipment 5 are connected with interchanger, can directly pass through
Network interface reads each task device, and (servo turntable 3, radar equipment 4, radio detection equipment 6, optoelectronic device 8, navigation are inveigled
Equipment 9, compacting jamming equipment 10) it state and controls each equipment and works normally；The zero-bit of all task devices is headstock direction,
After vehicle comes to a complete stop simultaneously normal power supply, north finder or Differential positioning instrument (headstock direction is zero-bit) are opened, headstock side is measured
It is issued to radar equipment 4, servo turntable 3 and radio detection 6 to the angle with direct north, and by the angle, is so far completed
The static calibration of each equipment, can be realized and the detection of unmanned plane target is tracked and identified and disposed；When system after hours,
It successively operates electric lifting rod 7, lodging mechanism 2 and electric leveling supporting leg and controls handle, system is restored to driving rounding state
(state as shown in Figure 3,4)；So far i.e. completing system is completely unfolded, works normally and removes receipts.
Embodiment two
As shown in figure 5, a kind of highly integrated anti-UAV system of the present invention, may be equally applied to fixed erection, i.e., will
Servo turntable 3 is that electric lifting rod 7 is directly connected with ground, and alternating current or hydro power generation power supply, each task can be used in power supply mode
Equipment (servo turntable 3, radar equipment 4, radio detection equipment 6, optoelectronic device 8, navigation spoofer 9, compacting jamming equipment
10) it is connected by modes such as RJ45 network interface or optical fiber or mobile communication with the computer in the computer room of command and control center, is counted
Calculation machine can be realized the state of each task device is read, instruction issues and receiving device reports information etc., it is fixed when setting up by
It is fixed in position, servo turntable 3 and electric lifting rod 7 can be passed through into coordinate system after setting up well for the first time and convert progress coordinate system
Unification, so far total system can work normally.
As shown in fig. 6, servo turntable and upper installing standby (radar equipment, optoelectronic device, compacting jamming equipment, navigation trick
Equipment), orientation can realize 360 ° of continuous rotations of circumference under servo turntable, servo turntable pitching can realize -14 ° of pitch axis~
128 ° of rotations, pitch axis upper position can realize 360 ° of continuous rotations of circumference, and can be made according to lower orientation motion conditions and lower section
The contrary, speed in position and acceleration magnitude are equal, rotate angle counter motion of the same size, to keep the side of radar equipment
Position axis zero degree is constant.
A kind of highly integrated anti-unmanned plane method, includes the following steps:
To target acquisition；
3 rotary motion of servo turntable is controlled according to the target information detected, makes optoelectronic device 8, navigation 9 and of spoofer
Jamming equipment 10 is suppressed towards target, while controlling optoelectronic device 8 and target is identified and positioned, according to what is identified and positioned
Target control navigates spoofer 9 to target transmission navigation spoofed signal, according to the target control compacting interference identified and positioned
Equipment 10 sends corresponding interference signal, makes its cisco unity malfunction, completes anti-goal task.
The content that description in the present invention is not described in detail belongs to the well-known technique of those skilled in the art.
Claims (10)
1. a kind of highly integrated anti-UAV system, it is characterised in that: including servo turntable (3), radar equipment (4), commander's control
System equipment (5) processed, radio detection equipment (6), optoelectronic device (8), navigation spoofer (9), compacting jamming equipment (10)；
The target prior information detected is sent to command and control system for detecting target by the radio detection equipment (6)
It unites equipment (5)；
The radar equipment (4), optoelectronic device (8), navigation spoofer (9) and compacting jamming equipment (10) are installed in servo
On turntable (3)；The radar equipment (4) is according to target prior information real-time tracking and measures the distance of target, orientation, moves speed
Degree and pitch angle, and the target information detected is exported in real time to command and control system equipment (5)；
The command and control system equipment (5) receives and processes target prior information, is set according to target prior information control radar
Standby (4) carry out quadratic probing, control servo turntable (3) rotary motion according to the target information that radar equipment (4) detects, make light
Electric equipment (8), navigation spoofer (9) and compacting jamming equipment (10) control optoelectronic device (8) to target towards target
It is identified and positioned, navigation spoofed signal is sent to target according to target control navigation spoofer (9) identified and positioned,
Corresponding interference signal is sent according to target control compacting jamming equipment (10) identified and positioned, completes anti-goal task.
2. the highly integrated anti-UAV system of one kind according to claim 1, it is characterised in that: the radar equipment (4)
It is mounted on the top of servo turntable (3), the optoelectronic device (8), navigation spoofer (9) and compacting jamming equipment (10) basis
Respective weight is mounted on the two sides of servo turntable (3), so that the weight difference of two sides is minimum.
3. the highly integrated anti-UAV system of one kind according to claim 2, it is characterised in that: the optoelectronic device (8)
The side of servo turntable (3) is mounted on navigation spoofer (9), compacting jamming equipment (10) is mounted on servo turntable (3)
The other side.
4. the highly integrated anti-UAV system of one kind according to claim 2, it is characterised in that: the servo turntable (3)
Including ontology orientation rotation platform (31), top orientation rotation platform (33) and side pitching turntable (32)；The ontology orientation rotation
Platform (31) is for radar equipment (4), optoelectronic device (8), navigation spoofer (9) and suppresses jamming equipment (10) in the horizontal direction
Upper rotation；The radar equipment (4) is mounted on top orientation rotation platform (33), the rotation of the top orientation rotation platform (33)
Direction is with the direction of rotation of ontology orientation rotation platform (31) on the contrary, speed is identical, for realizing the direction holding of radar equipment (4)
It is constant；The side pitching turntable (32) is for adjusting optoelectronic device (8), navigation spoofer (9) and compacting jamming equipment
(10) direction.
5. the highly integrated anti-UAV system of one kind according to claim 1, it is characterised in that: further include lodging mechanism
(2)；The servo turntable (3) is mounted on lodging mechanism (2), and the lodging mechanism (2) realizes servo turntable (3) and ground 0
It is fixed at any angle between~90 °.
6. the highly integrated anti-UAV system of one kind according to claim 1, it is characterised in that: further include electric lifting rod
(7)；The radio detection equipment (6) is mounted on electric lifting rod (7), when electric lifting rod (7) rise, expands nothing
The investigative range of line electricity detection equipment (6)；When electric lifting rod (7) land, reduce storage volume.
7. the highly integrated anti-UAV system of one kind according to claim 1, it is characterised in that: further include motor vehicles
(1)；The servo turntable (3) and command and control system equipment (5) are located on motor vehicles (1).
8. the highly integrated anti-UAV system of one kind according to claim 7, it is characterised in that: further include to servo turntable
(3), radar equipment (4), command and control system equipment (5), radio detection equipment (6), optoelectronic device (8), navigation are inveigled and are set
Standby (9) and compacting jamming equipment (10) provide the power-supply device of power supply；The power-supply device is positioned at motor vehicles (1) engine
Power takeoff generation unit source in cabin, the power takeoff generation unit source turn the kinetic energy of motor vehicles (1) engine when motor vehicles (1) is mobile
Turn to power storage.
9. the highly integrated anti-UAV system of one kind according to claim 1, it is characterised in that: the servo turntable (3),
Radar equipment (4), command and control system equipment (5), radio detection equipment (6), optoelectronic device (8), navigation spoofer (9)
It is communicated between compacting jamming equipment (10) by RJ45 network interface or optical fiber or mobile communication.
10. a kind of anti-unmanned plane method that the highly integrated anti-UAV system of one kind according to claim 1 is realized, special
Sign is, includes the following steps:
To target acquisition；
Servo turntable (3) rotary motion is controlled according to the target information detected, makes optoelectronic device (8), navigation spoofer (9)
With compacting jamming equipment (10) towards target, while controlling optoelectronic device (8) and target identified and positioned, according to identification and
Target control navigation spoofer (9) of positioning sends navigation spoofed signal to target, according to the target control identified and positioned
It suppresses jamming equipment (10) and sends corresponding interference signal, make its cisco unity malfunction, complete anti-goal task.
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Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111610538A (en) * | 2020-05-26 | 2020-09-01 | 郝建新 | Unmanned aerial vehicle navigation decoy system |
| CN112325704A (en) * | 2020-10-20 | 2021-02-05 | 中国人民解放军海军工程大学 | Unmanned aerial vehicle-mounted optical fiber laser false target and use method thereof |
| CN112346043A (en) * | 2020-11-06 | 2021-02-09 | 江苏方天电力技术有限公司 | Unmanned aerial vehicle detection method and device based on frequency spectrum identification |
| CN112415505A (en) * | 2020-10-16 | 2021-02-26 | 上海无线电设备研究所 | Radar, photoelectric and interference integrated detection-suppression device and method |
| CN112835021A (en) * | 2020-12-31 | 2021-05-25 | 杭州海康机器人技术有限公司 | Positioning method, device, system and computer readable storage medium |
| CN113357966A (en) * | 2021-06-18 | 2021-09-07 | 浙江瑞通电子科技有限公司 | Vehicle-mounted equipment for detecting deception suppression anti-unmanned aerial vehicle and method thereof |
| CN114132247A (en) * | 2021-12-31 | 2022-03-04 | 盛航(台州)科技有限公司 | Vehicle-mounted unmanned aerial vehicle counter-braking system |
| CN114489148A (en) * | 2021-12-30 | 2022-05-13 | 中国航天***科学与工程研究院 | Anti-unmanned aerial vehicle system based on intelligent detection and electronic countermeasure |
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| CN112415505A (en) * | 2020-10-16 | 2021-02-26 | 上海无线电设备研究所 | Radar, photoelectric and interference integrated detection-suppression device and method |
| CN112325704B (en) * | 2020-10-20 | 2022-07-29 | 中国人民解放军海军工程大学 | Unmanned aerial vehicle-mounted optical fiber laser false target and use method thereof |
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| CN112346043B (en) * | 2020-11-06 | 2023-10-10 | 江苏方天电力技术有限公司 | Unmanned aerial vehicle detection method and device based on frequency spectrum identification |
| CN112835021A (en) * | 2020-12-31 | 2021-05-25 | 杭州海康机器人技术有限公司 | Positioning method, device, system and computer readable storage medium |
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| CN114489148A (en) * | 2021-12-30 | 2022-05-13 | 中国航天***科学与工程研究院 | Anti-unmanned aerial vehicle system based on intelligent detection and electronic countermeasure |
| CN114489148B (en) * | 2021-12-30 | 2023-08-29 | 中国航天***科学与工程研究院 | Anti-unmanned aerial vehicle system based on intelligent detection and electronic countermeasure |
| CN114132247A (en) * | 2021-12-31 | 2022-03-04 | 盛航(台州)科技有限公司 | Vehicle-mounted unmanned aerial vehicle counter-braking system |
| CN114132247B (en) * | 2021-12-31 | 2024-07-16 | 盛航(台州)科技有限公司 | Vehicle-mounted unmanned aerial vehicle reaction system |
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