RU2738508C1 - System for observation and counteraction to unmanned aerial vehicles - Google Patents

Abstract

FIELD: aviation.

SUBSTANCE: system for observation and counteraction to drone (UAV) comprises ground control center (GCC) of air space, means of detection (DM) UAV, means of neutralization (NM) UAV. GCC comprises a control computer, an automated workstation (AWS), digital communication equipment, remote control station. UAV DM comprises a radar station, an optical-electronic system for detecting and tracking UAV, a radio reconnaissance system. UAV NM comprises UAV-interceptor, silencer of communication channels, launcher of missiles, antiaircraft gun, laser installation, radio-beam device.

EFFECT: higher reliability of mass reflection of hyper-speed, planning, and low-speed mini- and microUAV.

13 cl, 10 dwg

Description

Technology area

The invention relates to systems for monitoring and countering unmanned aerial vehicles and can be used for detection, tracking, recognition and neutralization of unmanned aerial vehicles (UAVs), including mini and micro UAVs.

State of the art

Known systems for monitoring and countering unmanned aerial vehicles / RU 2578524, RU 2695015, RU 2701421 /.

The closest in purpose and technical essence to the claimed invention is the system / RU 2701421, 09/26/2019 / monitoring and countering the UAV, containing a ground control center (NCC) of the airspace, connected at the entrance to the UAV detection means (SO), and at the exit - with means of neutralization (SN) of the UAV. UAS include at least one radar station (radar), and SN - at least one unmanned aerial vehicle interceptor (UAV) equipped with a communication radio modem and means of capture and delivery to the ground of the detected UAV.

In this case, in addition to radars, onboard COs can include video cameras, thermal imagers, and ground COs can additionally include sonars.

The disadvantage of the known system / RU 2701421 / is the limited ability to detect and counter UAVs.

This is due to the fact that, due to the small size and radio transparency of modern UAVs, their detection by existing radars (blind in relation to mini- and micro-UAVs in a plastic case) in / RU 2701421 / is recognized as practically impossible. For this, in / RU 2701421 / it is proposed to additionally use sonars (sound detectors), video cameras and thermal imagers.

However, these additional means in their pure form do not allow to ensure the measurement of coordinates and tracking of detected UAVs and, as a consequence, do not allow to issue precise target designation to countermeasures (SP) of UAVs.

In turn, the resource of the SP UAV of the known system / RU 2701421 / is limited by the use of an UAV-interceptor (UAV) with a reset network to capture the UAV.

In the event of a massive raid by mini and micro UAVs, countering them requires the use of an appropriate number of bulky UAVs equipped with “blind” airborne radars, a video camera, a thermal imager and a UAV capture network.

In general, these disadvantages of the known system / RU 2701421 / limit its ability to detect and counter UAVs.

The objective of the invention is to expand the functionality of the system to detect and counter UAVs.

The technical result arising from the solution of this problem is to increase the reliability of the reflection of the massive raid of mini and micro UAVs.

The essence of the invention

The solution to the problem and the achievement of the claimed technical result is ensured by the fact that the monitoring and countermeasures system (SNP) for unmanned aerial vehicles (UAVs) contains a ground control center (NCC) of the airspace, connected at the entrance to the UAV detection means (SO), and at the exit - with means of neutralization (SN) of the UAV. Moreover, the UAS include at least one radar station (radar), and the SN - at least one unmanned aerial vehicle (UAV) equipped with a communication radio modem and means of capturing and delivering the detected UAV to the ground.

New in the SNP is:

- Implementation of NCC with the ability to control heterogeneous means of SO and SN for the detection and neutralization of hyperspeed, gliding and low-speed mini and micro UAVs.

- Implementation of a radar with the ability to detect mini and micro UAVs in a plastic case.

- Additional supply of CO with at least one optical-electronic detection system (OES) with the possibility of auto-tracking and identification of the UAV type.

- Additional supply of CO with at least one electronic intelligence system (RTR) of UAV control and data transmission channels.

- Additional supply of SN with at least one muffler for UAV communication and navigation channels.

- Additional supply of SM with at least one missile launcher to intercept heat-emitting UAVs.

- Additional supply of CH with at least one anti-aircraft gun to combat hyperspeed gliding UAVs.

- Additional supply of SN with at least one laser installation for melting plastic UAV bodies.

- Additional supply of SN with at least one radio-beam device 3.6 for remote electrical breakdown of electronic equipment of the UAV.

- Installation of MV components on separate power servo drives and their connection via signal and control inputs / outputs from the NCC control computer via modem communication channels.

Proof of achievement of the stated technical result and solution of the task

The implementation of the NTS with the ability to control the NCC by heterogeneous means of SO and SN for the detection and neutralization of heterogeneous UAVs, as well as additional equipment and a rational choice of means of the detection and countermeasures system (SNP) allow to expand the functionality of the SNP and achieve the declared technical result - increasing the reliability of reflection of mass raid of hyperspeed , gliding and low-speed mini and micro UAVs.

The essence of the invention is illustrated by the drawings shown in FIG. 1-10.

FIG. 1 shows a functional diagram of the UAV detection and countermeasures system (SNP), FIG. 2 is a functional diagram of the airspace ground control center (NCC), FIG. 3 is a functional diagram of a UAV detection radar with the ability to detect mini and micro UAVs with a radio-transparent dielectric housing, FIG. 4 is a functional diagram of an optoelectronic detection system (OES) with the possibility of auto-tracking and identification of the UAV type, FIG. 5 is a functional diagram of an electronic reconnaissance system (RTR) of UAV control and data transmission channels, FIG. 6 - muffler of communication and navigation channels of the UAV, FIG. 7 is a functional diagram of a missile launcher for intercepting heat-emitting UAVs; FIG. 8 is a functional diagram of an anti-aircraft gun for combating hyperspeed and gliding UAVs, FIG. 9 is a functional diagram of a laser installation for melting plastic UAV bodies, FIG. 10 is a functional diagram of a radio-beam device for remote electrical breakdown of UAV electronic equipment.

FIG. 1-10 positions indicate:

1 - ground control center (NCC) airspace;

1.1 - control electronic computer (computer);

1.2 - automated workstation (AWP) of the operator NCC 1;

1.3 - remote control panel;

1.4 digital communication equipment;

2 - means of detection (SO) of unmanned aerial vehicles (UAV);

2.1 - radar station (radar) with the ability to detect UAVs with a radio-transparent body, including mini and micro UAVs;

2.1.1 - reflector transceiver antenna of circular view with cosec ² beam in the elevation plane and a narrow beam in the azimuth plane;

2.1.2 - antenna switch;

2.1.3 - four-channel receiver for horizontal and vertical polarization signals;

2.1.4 - digital signal processing device;

2.1.5 - transmitter;

2.1.6 - generator of a sequence of probing signals (ST) of nanosecond and microsecond duration;

2.1.7 - digital correlator;

2.1.8 - automated workstation (AWP) of the radar operator 2.1;

2.1.9 - radio modem for communication with NCC 1;

2.2 - optoelectronic systems (OES) for UAV detection and tracking;

2.2.1 - power servo drive (SSP) OES 2.2;

2.2.2 - block of optical lenses;

2.2.3 - block of matrix photodetectors;

2.2.4 - analog-to-digital converter (ADC);

2.2.5 - modem of radio communication of OES 2.2 with NCC 1;

2.3 - electronic intelligence system (RTR) of UAV control and data transmission channels;

2.3.1 - power servo drive (SSP) of the 2.3 RTR system;

2.3.2 - broadband antenna;

2.3.3 - broadband radio receiver with digital output;

2.3.4 - digital spectrum analyzer;

2.3.5 - meter of parameters of communication and navigation equipment of UAV onboard equipment;

2.3.6 - radio modem for communication of the 2.3 RTR system with NCC 1;

3 - UAV neutralization means (SN);

3.1 - unmanned aerial vehicle UAV-interceptor (UAV);

3.2 - muffler of UAV communication and navigation channels;

3.2.1 - power tracking drive (SSP) of the muffler 3.2;

3.2.2 - block of antenna emitters for jamming altimeter, navigator and UAV control channels;

3.2.3 - block of jamming amplifiers;

3.2.4 - block of jammers;

3.2.5 - modem of radio communication of the muffler 3.2 with NCC 1;

3.3 - launcher (PU) missiles with an infrared (IR) homing head to intercept heat-emitting UAVs;

3.3.1 - power tracking drive (SSP) of the launcher 3.3;

3.3.2 - starting block;

3.3.3 - missile with a thermal homing head (GOS);

3.3.4 - radio modem for communication PU 3.3 with NCC 1;

3.4 - anti-aircraft gun (ZO) to combat hyperspeed and gliding UAVs;

3.4.1 - supporting-rotary device (OCP) ZO;

3.4.2 - mobile platform;

3.4.3 - feeding device for shots with bundles of needles or shrapnel;

3.4.4 - radio modem for communication between ZO and NCC 1;

3.4.5 - communication antenna of the radio modem 3.4.4;

3.5 - laser installation (LU) for melting the plastic bodies of the UAV;

3.5.1 - radio modem for communication LU 3.5 with NCC 1;

3.5.2 - slewing support (OCP) LU 3.5;

3.5.3 - multi-beam fiber laser;

3.5.4 - optical system for converging laser beams 3.5.3;

3.6 - radio-beam device (RU) for remote electrical breakdown of electronic equipment of the UAV;

3.6.1 - generator of powerful electromagnetic pulses (EMP) of centimeter range of electromagnetic waves (EMP) for remote electrical breakdown of electronic equipment of UAVs;

3.6.2 - EMP antenna emitter (Casegrain lens);

3.6.3.1 - reflector;

3.6.2.2 - counter-reflector;

3.6.3 - electrically insulated mobile cabin;

3.6.4 - support-rotary device (OPU) of the radiator 3.6.2;

4 - command post (CP) of aerospace defense (VKO).

Disclosure of the essence of the invention

The monitoring and countermeasures system (SNP) for unmanned aerial vehicles (UAVs) contains a ground control center (NCC) 1 of the airspace, connected at the entrance to the UAV detection equipment (CO) 2, and at the exit to the UAV neutralization means (SN) 3.

Ground control center (NCC) 1 is made with the possibility of operational control of heterogeneous means of CO and CH. To do this, it contains a control electronic computer (computer) 1.1, an automated workstation (AWP) 1.2, a remote control panel 1.3 for the system control and digital communication equipment 1.4 with a remote control panel 1.3, with CO 2, with CH 3 and with connected by interface lines of modem communication. command post (CP) 4 aerospace defense (VKO).

UAV detection means 2 (SO) include at least one radar station (radar) 2.1, at least one optoelectronic system (OES) 2.2 UAV detection and tracking, at least one electronic reconnaissance system 2.3 (RTR), UAV control and data transmission channels ...

The UAV detection radar 2.1 is designed to detect mini and micro UAVs with a plastic housing. It contains a 2.1.1 circular reflector transceiver antenna with a cosec2 beam in the elevation plane and a narrow beam in the azimuth plane. The antenna 2.1.1 is connected according to the sounding signals through the antenna switch 2.1.2 and the transmitter 2.1.5 with the generator 2.1.6 of the sequence of sounding signals (S) of nanosecond and microsecond duration. According to the response signals, it is connected through an antenna switch 2.1.2, a four-channel receiver 2.1.3 for signals of horizontal and vertical polarization, a digital signal processing device 2.1.4, a digital correlator 2.1.7, an automated workstation (AWS) 2.1.8 Radar 2.1 and a radio modem 2.1.9 communication with digital communication equipment 1.4 NCC 1. Moreover, the SWs of nanosecond and microsecond duration of the shaper 2.1.6 are made respectively unmodulated and with intra-pulse modulation with a pause between them of a fraction of microseconds and their frequency spacing by 1-50 MHz.

The optoelectronic system (OES) 2.2 for UAV detection is capable of auto-tracking and identification of the UAV type. To do this, it contains a block of lenses 2.2.2, block 2.2.3 of matrix photodetectors of the visible and infrared range of electromagnetic waves (EMW), an analog-to-digital converter (ADC) installed on the power tracking drive (SSP) 2.2.1 and serially connected by photo-television signals 2.2.4, and modem 2.2.5 of radio communication with digital communication equipment 1.4 NCC 1. At the same time, the lens unit 2.2.2 contains telescopic lenses with a focal length of 130 to 1450 mm to provide auto tracking and identification of the UAV type in the near, middle and far zones their detection accordingly.

The system 2.3 radio technical intelligence (RTR) of the control and data transmission channels of the UAV contains a modem 2.3.6 of radio communication with equipment 1.4 of digital communication NCC 1, as well as installed on a power tracking drive (SSP) 2.3.1 and serially connected broadband antenna 2.3.2, broadband a radio receiver 2.3.3. with a digital output, a digital spectrum analyzer 2.3.4, a meter 2.3.5 of the parameters of communication and navigation equipment of the UAV onboard equipment, connected to the signal input of the communication radio modem 2.3.6, the control output of which is connected to the input of the SSP 2.3.1.

Detection means (CO) 2.1-2.3 by signal outputs and control commands for the detection and tracking of the UAV are connected through the corresponding communication modems and digital communication equipment 1.4 to the control computer 1.1 NCC 1.

The outputs of the computer 1.1 NTSK 1 are connected to the control inputs of the neutralization means (SN) 3 of the UAV according to the UAV counteraction control commands.

Neutralization means (SN) 3 contain at least one unmanned aerial vehicle (UAV) interceptor (UAV) 3.1, at least one muffler for 3.2 communication and navigation channels of the UAV, at least one launcher 3.3 missiles for intercepting heat-emitting UAVs, at least one anti-aircraft gun 3.4 to combat hyperspeed gliding UAVs, at least one 3.5 laser system for melting plastic UAV bodies, at least one radio-beam device 3.6 for remote electrical breakdown of UAV electronic equipment.

UAV 3.1, contains a radio modem for communication with the NCC 1, a detector of the source of UAV control signals, at least one mini-rocket with a homing head to destroy the control source and / or at least one jammer of UAV communication channels, and also contains a drop-out network for UAV capture and delivery to the ground (not shown in the figures).

The jammer of 3.2 communication and navigation channels of the UAV contains the 3.2.1 radio communication modem connected in series with the digital communication equipment 1.4 NCC 1, the block 3.2.4 jammers, the block 3.2.3 jamming amplifiers and the block 3.2.2 antenna emitters for jamming the altimeter, navigator and UAV control channels.

The launcher (PU) of 3.3 missiles for intercepting heat-emitting UAVs contains a power tracking drive (SSP) 3.3.1, on which the launching unit (SB) 3.3.2 of 3.3.3 missiles with thermal homing heads (GOS) is installed. Moreover, SSP 3.3.1 and SB 3.3.2 are connected through a radio communication modem 3.3.4 with NCC 1.

An anti-aircraft gun 3.4 for combating hyperspeed and gliding UAVs contains a small-caliber anti-aircraft gun 3.4.3 of obstruction fire installed on the OPU 3.4.1 of a mobile platform 3.4.2, a power supply device for 3.4.3 shots with beams of needles or shrapnel, a radio modem 3.4.4 and an antenna 3.4. 5 communication with equipment 1.4 of digital communication NTSK 1. At the same time, the anti-aircraft gun 3.4.3 of the obstruction fire is made of a turret type, with a caliber not exceeding 35 mm and with a rate of fire not less than 1000 rounds per minute.

The 3.5 laser installation for melting the plastic UAV housings contains a radio communication modem 3.5.1 with digital communication equipment 1.4 NCC 1, as well as a 3.5.3 multibeam fiber laser installed on the OPU 3.5.2 with an optical system 3.5.4 converging beams.

The radio-beam device 3.6 for remote electrical breakdown of electronic equipment of the UAV contains a generator 3.6.1 of powerful electromagnetic pulses (EMP) of the centimeter range of electromagnetic waves, connected through a waveguide system filled with a neutral gas, with the input of the emitter 3.6.2 EMP. The generator 3.6.1 EMP is installed in the electrically insulated mobile cabin 3.6.3, and the emitter 3.6.2 EMP is on the OPU 3.6.4, installed on the roof of the cabin 3.6.3. In this case, the generator 3.6.1 EMP and OPU 3.6.4 are connected through the control inputs through a radio modem 3.6.5 communication, equipment 1.4 for digital communication with the control computer 1.1 NCC 1. The generator 3.6.1 EMP is made in the form of a magnetron or klystron, and the emitter 3.6. 2 EMP - in the form of a Casegrain lens, including a reflector 3.6.3.1 and a counter-reflector 3.6.3.2, or in the form of a reflector 3.6.3.1, on the outer concave surface of which solid-state EMP amplifiers are evenly distributed (not shown in the figures).

The specified neutralization means 3.1-3.6 СН 3, according to the control signals and the processing of UAV neutralization commands, are connected through the appropriate communication modems and digital communication equipment 1.4 to the control computer 1.1 NCC 1.

The surveillance and countermeasures system (SNP) can contain from 1 to 10 of each type of UAV surveillance and countermeasures.

Work of the SNP

The surveillance and countermeasures system (SNP) of the UAV works as follows.

When describing the operation of the SNP, it is assumed that the launch of a UAV on a defense object such as the S-400 anti-aircraft missile system (SAM) is carried out from aircraft that are not included in the affected area of the air defense system, or in the affected area - using mobile ground launchers and foot saboteurs put forward in the direction of the air defense missile system and invisible (due to the restrictions on the height of the detection zone) information means of the air defense missile system "S-400".

As a result, a simultaneous launch of a "swarm" of UAVs is possible, leading to an overload of information resources, a rapid depletion of the ammunition load of the air defense missile system and unhindered entry into the zone of responsibility of the air defense missile system “S-400” of the main forces and means of aerospace attack.

Under these conditions, the radar 2.1, OES 2.2 and the RTR 2.3 SNP system in the circular view mode under the control of the 1.1 NTSK 1 computer conduct simultaneous observation of the airspace in the middle and near zone from the S-400 air defense system.

At the same time, the use of a sequence of probing signals (ES) of nanosecond and microsecond duration in the radar station 2.1 and polarization processing of the received signals make it possible to detect UAVs both in metal and dielectric (radio-transparent) cases, including mini and micro UAVs.

In turn, the use of three different-focus lenses in OES 2.2 and the use of a block of matrix photodetectors of the visible and infrared (IR) range of EME allow changing the field of view of OES 2.2, identifying the type of UAV by its image and radiated heat, and also passively (without radiation into the air) to determine the distance to it according to the relative number of illuminated pixels on the photodetector matrix.

The use in the RTR 2.3 system of broadband means of angular direction finding and UAV recognition by the radiation of its communication and navigation equipment makes it possible to measure the frequency and amplitude-time characteristics of the UAV control signals, as well as the bearing (angular direction) to the emitting UAV and to the source of its flight control signals.

The results of measurements of the radar 2.1, OES 2.2 and RTR 2.3 in real time through the corresponding radio modems 2.1.9, 2.2.5, 2.3.6 and digital communication equipment 1.4 are fed to the control computer 1.1 NTSK 1.

Computer 1.1, based on fuzzy logic algorithms, analyzes all signs of signals from radar 2.1, OES 2.2 and RTR 2.3 (trajectory, spectral, polarization), identifies them and forms a single field of the air situation, taking into account the threats and importance of the UAV.

Based on the formed air situation, computer 1.1 organizes the target distribution of UAVs between means 3.1-3.6 neutralization (SN) 3, taking into account the combat capabilities of these means and the vulnerability of UAVs, including hyperspeed, gliding, mini and micro UAVs in a dielectric and metal case.

The results of target allocation from the computer 1.1 through the communication system 1.4 of the NCC 1 are fed to the air interceptor 3.1 UAV (UAV) and to the corresponding OPU and SSP means 3.2-3.6 UAV neutralization.

At the same time, the 3.1 interceptor flies into the target designation area and conducts a free search for the UAV, measuring the radiation parameters of its communication and UAV navigation equipment and jamming the indicated control channels. If a ground source of radio control of the UAV is detected, the 3.1 interceptor fires a mini-rocket with a homing head in its direction. The result of hitting the UAV radio control source and jamming the control channels is assessed by the disappearance of control commands and the change in the UAV's trajectory, respectively. In the presence of a "swarm" of mini and micro UAVs, the interceptor 3.1 throws out a drop-out parachute net on their way of movement, followed by its landing with captured UAVs. The results of the combat work of the interceptor 3.1 in real time are transmitted automatically to the 1.1 NTSK 1 computer through the appropriate radio communication channels.

At the same time, the ground-based OPU and SSP means 3.2-3.6 UAV neutralization work out the target designation commands.

At the same time, the UAV corresponding to the target distribution falls into the zone of influence of specific means 3.2-3.6 of neutralization of the highest efficiency.

So the ground-based muffler of 3.2 control channels of the UAV, having received through the NCC 1 from the meter 2.3.5 of the RTR 2.3 system, reconnoitered information about the amplitude-time (AVX) and amplitude-frequency characteristics (AFC) of the communication and navigation equipment of the on-board equipment of the UAV sets up its block 3.2.4 generators of interference on the frequency and parameters of radio signals for communication and control of the dedicated UAV. The efficiency of the 3.2 muffler in intercepting UAVs is assessed by the 1.1 NTSK 1 computer by the disappearance of the UAV mark on the radar 2.1 screen and / or the disappearance of signals from the UAV onboard equipment in the 2.3 RTR system, working in tandem with the 3.2 muffler.

Launchers (PU) 3.3 3.3.3 missiles with an infrared (IR) homing head are distributed by the 1.1 NTSK 1 computer over the heat-emitting UAVs detected by the OES 2.2. When practicing target designation and turning the launch unit (SB) 3.3.2 in the direction of the heat-emitting UAV, 3.3.3 missiles installed in it, using IR heads, detect the UAV allocated for destruction and take it for auto-tracking. Data on the UAV capture by the homing heads via the 3.3.4 communication modem PU 3.3 are transmitted to the computer 1.4 of the NCC 1. The computer 1.4 gives permission to launch one of the 3.3.3 missiles to the dedicated UAV and after the 3.3.3 rocket leaves the launch block 3.3.2 it deploys PU 3.3 for the next heat-emitting UAV. The assessment of the defeat of a heat-emitting UAV is assessed by computer 1.4 by the disappearance of the corresponding radar mark from the radar 2.1 screen and / or distortion of the UAV image received by the computer 1.4 from the OES 2.2 accompanying the dedicated PU 3.3 of the UAV.

Anti-aircraft guns (ZO) 3.4 in the system 3 neutralization of the computer 1.4 target is distributed mainly over hyperspeed and gliding UAVs. The interception of these UAVs is carried out by placing a defensive fire on the way of their movement with beams of needles and / or shrapnel with a firing rate of at least 1000 rounds / min.

Laser installations (LU) 3.5 COMPUTER 1.4 are targeted mainly for UAVs with a plastic case, recognized by the radar 2.1 based on the analysis of their polarization characteristics. In this case, the defeat of such UAVs is carried out by melting the plastic parts of the UAV by focusing and / or converging laser beams on the UAV selected for destruction.

Radio Beam Devices (RU) 3.6 Computers 1.4 are mainly distributed over low-speed UAVs with a metal body. In this case, the defeat of such UAVs is carried out by focusing on it electromagnetic radiation with an energy density sufficient for an electric discharge of an electromagnetic wave through the metal skin of the UAV and the emergence of an induced electric field inside the UAV body with an intensity sufficient for electrical breakdown of the electronic equipment of the UAV.

The operator through AWS 1.2 or remote control panel 1.3 NCC 1 has the ability to independently analyze images, radar and radio direction-finding signals to assign a priority UAV feature to a target and make a decision on its neutralization.

Such a constructive implementation of the UAV's surveillance and countermeasures system (SRS) makes it possible to neutralize UAVs performing unauthorized flights with the least damage and the greatest efficiency, both in peacetime and in wartime.

Industrial applicability

The invention was developed at the level of the technical design and working documentation for individual elements of the surveillance and countermeasures system (SNP) of the UAV. Algorithms for target allocation for the control computer 1.1 SNP were developed and mathematical modeling of the system was carried out. The simulation results showed the solution to the task and the achievement of the stated technical result - an increase in the reliability of reflection of a massive raid of supersonic, gliding, mini- and micro-UAVs.

Claims (13)

1. A system for monitoring and countering unmanned aerial vehicles (UAVs), containing a ground control center (NCC) of the airspace, connected at the entrance to the UAV detection means (SO), and at the exit to the UAV neutralization means (SN), and The UAV SO includes at least one radar station (radar), and the SN - at least one unmanned aerial vehicle interceptor (UAV) equipped with a communication radio modem and means of capture and delivery to the ground of the detected UAV, characterized in that the NCC is made with the possibility of operational control of heterogeneous by means of SO and SN, the radar is made with the additional possibility of detecting mini- and micro-UAVs in a plastic case, SO additionally contain at least one optoelectronic system (OES) for detecting and tracking UAVs, at least one electronic intelligence system (RTR) of control and transmission channels data UAV, SN additionally contains installed on separate power servo drives n e less than one muffler for communication and navigation channels of UAVs, at least one missile launcher for intercepting heat-emitting UAVs, at least one anti-aircraft gun to combat hyperspeed gliding UAVs, at least one laser installation for melting plastic UAV hulls, at least one radio-beam device for remote electrical breakdown of the electronic equipment of the UAV, and the power servo drives of the said elements of the SN are connected via the control inputs to the control computer through the corresponding communication channels of the NCC. 2. The system according to claim 1, characterized in that the NCC, made with the ability to control heterogeneous means of CO and CH, contains a control electronic computer (PC), an automated workstation (AWP), a remote control panel for the system, connected by interface lines of modem communication digital communication equipment with a remote control, with CO, with CH and with the command post (CP) of the aerospace defense (VKO) control. 3. The system according to claim 1, characterized in that the UAV detection radar, configured to detect mini and micro UAVs in a plastic case, contains a mirror transceiver antenna with a circular view with a cosec ² beam in the elevation plane and a narrow beam in the azimuth plane, connected along sounding signals through an antenna switch and a transmitter with a generator of a sequence of probing signals (SE) of nanosecond and microsecond duration, and according to the response signals - through an antenna switch, a four-channel receiver of horizontal and vertical polarization signals, a digital signal processing device, a digital correlator, an automated workstation (AWP ) Radar and radio modem for communication with digital communication equipment of the NCC, and the ES of nanosecond and microsecond duration are made, respectively, unmodulated and with intra-pulse modulation with a pause between them of a fraction of μs and their frequency separation by 1-50 MHz. 4. The system according to claim 1, characterized in that the OES of UAV detection with the possibility of auto-tracking and identification of the UAV type contains a unit of lenses, a unit of matrix photodetectors, an analog-to-digital converter (ADC) installed on a power tracking drive (SSP) and connected in series by photo-television signals. ) and a radio communication modem with digital communication equipment NCC, and the lens unit contains telescopic lenses with a focal length of 130 to 1450 mm to provide auto-tracking and identification of the UAV type in the near, middle and far zones of their detection, respectively. 5. The system according to claim 1, characterized in that the RTR system contains a radio communication modem with digital communication equipment NCC, as well as a broadband antenna, a broadband radio receiver with a digital output, a digital spectrum analyzer, a parameter meter installed on a power tracking drive (SSP) and serially connected means of communication and navigation of the onboard equipment of the UAV, connected to the signal input of the modem, the control output of which is connected to the input of the SSP. 6. The system according to claim 1, characterized in that the jammer of communication and navigation channels of the UAV contains installed on the power tracking drive (SSP) and serially connected radio communication modem with digital communication equipment NCC, a block of jammers, a block of jamming amplifiers and a block of antenna emitters for jamming the altimeter, navigator and UAV control channels. 7. The system according to claim 1, characterized in that the launcher (PU) of missiles for intercepting heat-emitting UAVs contains a power tracking drive (SSP), on which the launch block (SB) of missiles with thermal homing heads (GOS) is installed, and the SSP and SB are connected via radio modem with NCC. 8. The system according to claim 1, characterized in that the anti-aircraft gun for combating hyperspeed gliding UAVs contains a small-caliber anti-aircraft barrage gun installed on the control room of the mobile platform, a feeding device for shots with beams of needles or shrapnel, a radio modem and an antenna for communication with digital communication equipment NCC. 9. The system according to claim 8, characterized in that the defensive fire anti-aircraft gun is made of a turret type, with a caliber of not more than 35 mm and with a rate of fire of at least 1000 rounds per minute. 10. The system according to claim. 1, characterized in that the laser installation for melting plastic UAV bodies contains a radio modem for communication with digital communication equipment NCC, as well as installed on the OPU multi-beam fiber laser with an optical beam convergence system. 11. The system according to claim 1, characterized in that the radio-beam device for remote electrical breakdown of the electronic equipment of the UAV contains a generator of powerful electromagnetic pulses (EMP) of the centimeter range of electromagnetic waves connected through a waveguide system filled with neutral gas to the input of the EMP emitter, the EMP generator is installed in an electrically insulated mobile cabin, and the EMP emitter is on the OPU installed on the roof of the cabin, while the EMR generator and OPU 3 are connected via control inputs to the digital communication equipment NCC through a communication radio modem. 12. The system according to claim 9, characterized in that the EMP generator is made in the form of a magnetron or klystron, and the EMP emitter is in the form of a Casegrain lens, including a reflector and a counterreflector, or in the form of a reflector, on the outer concave surface of which solid-state EMP amplifiers are evenly distributed ... 13. The system according to claim 1, characterized in that the unmanned aerial vehicle interceptor (UAV) additionally contains a detector of the source of UAV control signals, at least one mini-rocket with a homing head to destroy the control source and / or at least one jammer of UAV communication channels.

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