RU2527315C1 - Device to control secondary emitter electromagnetic field - Google Patents

Abstract

FIELD: instrumentation.

SUBSTANCE: device comprises CD, radiation spectrum driver, transceiver antenna system, secondary radiator data driver, frequency spectrum converter, filter unit, radiation spectrum analyser and secondary radiation spectrum indicator unit. Note here that CD output is connected to radiation spectrum driver. 14 outputs of radiation spectrum driver are connected to 14 inputs of antenna commutator. 14 O/I of antenna commutator, 1^st to 14^th, are connected parallel with 14 I/O of four transceiver antenna systems. 14 outputs of antenna commutator, 15^th to 28^th, are connected with 14 inputs of secondary radiator data driver. CD output is connected via frequency spectrum converter and 10 outputs of filter unit with 10 inputs of secondary radiation spectrum analyser. 10 outputs of analyser are connected with tem inputs of secondary radiation spectrum indicator unit.

EFFECT: automated analysis.

11 cl, 16 dwg

Description

The invention relates to the field of radio communications and can be used to solve the problem of electromagnetic compatibility of electronic equipment, as well as the study of the parameters of the secondary radiation of various environments.

The well-known "Method for the detection of moving electrically conductive objects", patent RU 2303290, G08B 13/24 from 07.20.2007. The invention relates to the field of security and is intended for the detection of moving electrically conductive objects. It consists of a generator exciting electromagnetic radiation using an antenna system. For registration of excited currents in moving electrically conductive objects, receiving antenna systems connected to recording equipment are used. However, it cannot be used for immovable objects and non-conductive media, and also to determine the parameters of the secondary radiation, for example, the frequency of the secondary emitter, the polarization of the vector and the field level.

Known "Device for the simultaneous detection of several explosives and drugs in baggage", patent 2128832 RU, G01N 24/00, G01R 33/20 from 04/10/1999. The device comprises a reference frequency unit, a receiver and a storage device, a unit of frequency synthesizers for nuclear quadrupole resonance, and an adjustable key. However, it cannot be used to determine the parameters of the secondary radiation, for example, the frequency of the secondary emitter, the polarization of the vector, and the field level.

Known inventions are 2157002 RU, 98107128 RU, 2205386 RU G01N 24/08, G01R 33/20, published on 05.27.2003. The device contains blocks for determining the frequencies of nuclear quadrupole resonance. However, it cannot be used to determine the parameters of the secondary radiation, for example, the frequency of the secondary emitter, the polarization of the vector, and the field level.

The basic object can serve as a "Device for the detection and recognition of substances by nuclear quadrupole resonance (NQR)" G01N 24/00, according to the application 2010102971 from 01.29.2010. The device contains a high-frequency generator, a pulse modulator, a first inductor, a signal sensor, a low-noise amplifier, a logarithmic amplifier with an amplitude detector and an indicator, a signal divider, the first and second controlled attenuators, the first and second controlled phase shifters, the second inductor, and an oscilloscope. The base object has the following disadvantages:

- low efficiency of emitters of inductance coils (two orders of magnitude lower than an electric emitter);

- a strong dependence of the inductors on the frequency, the inductors relate to tuned emitters operating at the same frequency;

- the use of inductors does not allow to evaluate the polarization properties of secondary radiation in NQR;

- closely spaced frequencies of secondary NQR radiation do not allow their difference and identification of the type of substance;

- lack of automation of determining the parameters of secondary radiation in NQR.

The aim of the present invention is the automation of the analysis of the frequency properties of the secondary radiation field of the studied objects; the introduction of broadband antenna systems for irradiation and reception of secondary radiation, the studied objects; the introduction of a model for the frequency conversion of the spectrum of secondary radiation to improve recognition and increase the sensitivity of the device, improving the study of the polarization properties of the secondary radiation field.

To achieve this goal, the following devices are additionally introduced into the device, consisting of a clock pulse generator 1, radiation spectrum shaper 2: antenna switch 3, transceiver antenna system 4, radiation information shaper of secondary emitters 5, frequency spectrum converter 6, filter unit 7, block analysis of the emission spectrum 8, a block of indicators of the spectrum of the secondary radiation 9.

Figure 1 shows a device for monitoring the electromagnetic field of secondary emitters, where 1 is a clock pulse generator, 2 is a radiation spectrum shaper, 3 is an antenna switcher, 4 is a transceiver antenna system, 5 is a radiation information shaper of secondary emitters, 6 is a frequency converter spectrum, 7 - a block of ten filters, 8 - a block for analyzing the spectrum of secondary radiation, 9 - a block of indicators of the radiation spectrum.

Figure 2 presents the transceiver antenna system 4, where from 1 to 14 vibrators of different polarization (or vibrators located in a circle having different polarization of electromagnetic waves).

по $$C_{НАГ.}^{14}$$

, а с противоположного конца - через входную клемму с 1 по 14 к генератору через коммутатор 3.Figure 3 presents the transceiver antenna system 4, which shows the power supply circuit of the vibrators 1 to 14, each vibrator is an emitter with a load at the end (to increase the electric length of the emitter), with each vibrator from 1 to 14 from one end connected to an earth wire through a grounded container with $$C_{N\mathrm{BUT}G}^{\mathrm{one}}$$

by $$C_{N\mathrm{BUT}G.}^{\mathrm{one}\mathrm{four}}$$

, and from the opposite end - through the input terminal 1 to 14 to the generator through switch 3.

Figure 4 presents the shaper of the emission spectrum 2, where 10 is the element And 11 is the first trigger, fourteen discrete delay lines 32 for 20 ms, the first generator of the packet of two pulses 1 μs A1 contains: two valves B.1 and B.2 and a discrete delay line of 18 by 1 μs; the second packet generator of two pulses of 10 μs A2 contains: two valves B.3 and B.4, a discrete delay line 12 by 10 ms, a discrete delay line 14 by 10 μs, 13 - a second trigger; the third packet generator of two pulses of 100 μs A3 contains: two valves B.5 and B.6, a discrete delay line 15 by 10 ms, a discrete delay line 17 by 100 μs, 16 - the third trigger, Bk.16 - switch to start the device ; pulse switch A4 contains: the fifteenth switch (BK.15) for two switching positions and fourteen channels, and each channel has its own switch (BK.1 to BK.14) for four positions, for four operating modes, in thirteen channels, starting from the second to the fourteenth in each channel - a switch, a valve and two discrete delay lines; so in the second channel - the second switch BK.2, valve B.7, delay line 19 by 10 ms and delay line 32 by 20 ms; in the third channel, the third switch Vk.3, valve B.8, delay line 20 by 20 ms and delay line 32 by 20 ms; in the fourth channel, the fourth switch Vk.4, valve B.9, delay line 21 by 30 ms and delay line 32 by 20 ms; in the fifth channel, the fifth switch Vk.5, valve B.10, delay line 22 by 40 ms and delay line 32 by 20 ms; in the sixth channel, the sixth switch Vk.6, valve B.11, delay line 23 by 50 ms and delay line 32 by 20 ms; in the seventh channel, the seventh switch Vk.7, valve B.12, delay line 24 by 60 ms and delay line 32 by 20 ms; in the eighth channel - the eighth switch Vk.8, valve B.13, delay line 25 by 70 ms and delay line 32 by 20 ms; in the ninth channel - the ninth switch Vk.9, valve B.14, delay line 26 by 80 ms and delay line 32 by 20 ms; in the tenth channel, the tenth switch Vk.10, valve B.15, delay line 27 by 90 ms and delay line 32 by 20 ms; in the eleventh channel, the eleventh switch Bk.11, valve B.16, delay line 28 by 100 ms and delay line 32 by 20 ms; in the twelfth channel - the twelfth switch BK.12, valve B.17, delay line 29 by 110 ms and delay line 32 by 20 ms; in the thirteenth channel - the thirteenth switch Vk.13, valve B.18, delay line 30 to 120 ms and delay line 32 to 20 ms; in the fourteenth channel - the fourteenth switch Vk.14, valve B.19, delay line 31 to 130 ms and delay line 32 to 20 ms.

Figure 5 presents the antenna switch - 3, where 33-1 is the receiving diode-capacitive bridge, 33-2 is the transmitting diode-capacitive bridge, 34 is the control unit of the transceiver antenna system.

Figure 6 presents the control unit of the transceiver antenna system 34, where Tr.1 - transformer, 1 - fourteen primary windings of the transformer; section 2-1 and section 2-2 of the secondary winding of the transformer, B.1 and B.2 - valves, 35 and 37 - voltage amplifiers, 36 - element NOT.

In Fig.7 presents a diode-capacitive bridge - 33-1 and 33-2, where R ₁ and R ₂ - resistance, D ₁ and D ₂ - valves, C ₁ and C ₂ - capacity.

On Fig presents a shaper of radiation information of secondary emitters 5, where Tr.1 is a transformer with fourteen primary windings 1 and one secondary winding 2, a broadband amplifier 38.

Figure 9 shows the frequency spectrum converter - 6, where 39 is a 10 kHz generator, 40 is a converter.

Figure 10 shows the filter block for ten channels - 7, where 41-1 is a filter at frequencies of 1-10 kHz, 41-2 is a filter at frequencies of 10-50 kHz, 41-3 is a filter at frequencies of 50-100 kHz, 41-4 - filter at frequencies of 100-200 kHz, 41-5 - filter at frequencies of 200-400 kHz, 41-6 - filter at frequencies of 400-800 kHz, 41-7 - filter at frequencies of 800-1000 kHz, 41- 8 - a filter at a frequency of 1-10 MHz, 41-9 - a filter at a frequency of 10-20 MHz, 41-10 - a filter at a frequency of 20-40 MHz, 42-1 - a narrow-band amplifier for a frequency band of 1-10 kHz., 42 -2 - narrow-band amplifier in the frequency band 10-50 kHz, 42-3 - narrow-band amplifier in the frequency band 50-100 kHz, 42-4 - narrow-band amplifier n and a frequency band of 100-200 kHz, 42-5 is a narrow-band amplifier in the frequency range of 200-400 kHz, 42-6 is a narrow-band amplifier in the frequency range of 400-800 kHz, 42-7 is a narrow-band amplifier in the frequency range of 800-1000 kHz, 42-8 is a narrow-band amplifier in the frequency band 1-10 MHz, 42-9 is a narrow-band amplifier in the frequency band 10-20 MHz, 42-10 is a narrow-band amplifier in the frequency band 20-40 MHz.

11 is a block of analyzers of the spectrum of the secondary radiation into ten channels - 8, where 43-1 is the oscillatory system in the frequency band 1-10 kHz, 43-2 is the oscillatory system in the frequency band 10-50 kHz, 43-3 is the oscillatory system system for the frequency band 50-100 kHz, 43-4 - oscillatory system for the frequency band 100-200 kHz, 43-5 - oscillatory system for the frequency band 200-400 kHz, 43-6 - oscillatory system for the frequency band 400-800 kHz , 43-7 - oscillatory system in the frequency band 800-1000 kHz, 43-8 - oscillatory system in the frequency band 1-10 MHz, 43-9 - oscillatory system in the frequency band 10-20 M q, 43-10 - oscillating system to the band 20-40 MHz, 44 - Detector.

On Fig - block indicators of the spectrum of radiation 9, where ten voltage indicators 45 for ten channels, a spectrum analyzer 46 and a switch for ten switching positions 47.

, где два импульса длительностью 1 мкс и с разносом на 1 мкс или $${\tau }_{ИМП}^1={\tau }_{РАС}^1=1\text{ мкс}$$

; второй пакет импульсов с расстановкой - $${\tau }_{ИМП}^2*{\tau }_{РАС}^2*{\tau }_{ИМП}^2$$

, где $${\tau }_{ИМП}^2$$

- два импульса длительностью по 10 мкс каждый с разносом в 10 мкс или $${\tau }_{ИМП}^2={\tau }_{РАС}^2=10\text{ мкс}$$

; третий пакет импульсов с расстановкой - $${\tau }_{ИМП}^3*{\tau }_{РАС}^3*{\tau }_{ИМП}^3$$

, где $${\tau }_{ИМП}^3$$

- два импульса длительностью по 100 мкс каждый с разносом в 100 мкс или $${\tau }_{ИМП}^3={\tau }_{РАС}^3=100мкс$$

; разнос между тремя пакетами импульсов составляет 10 мс.In Fig.13 - a temporary arrangement of three packets of pulses, formed for the irradiation of the investigated media; the first packet of two pulses with the arrangement - $${\tau }_{\mathrm{AND}MP}^{\mathrm{one}}*{\tau }_{R\mathrm{BUT}\mathrm{FROM}}^{\mathrm{one}}*{\tau }_{\mathrm{AND}MP}^{\mathrm{one}}$$

where two pulses with a duration of 1 μs and a spacing of 1 μs or $${\tau }_{\mathrm{AND}MP}^{\mathrm{one}}={\tau }_{R\mathrm{BUT}\mathrm{FROM}}^{\mathrm{one}}=\mathrm{one}\text{μs}$$

; the second packet of pulses with the arrangement - $${\tau }_{\mathrm{AND}\mathrm{<figure-callout\; id="2"\; label="M\; P"\; filenames="00000028.png,00000029.png"\; state="\{\{state\}\}">M\; </figure-callout>}P}^2*{\tau }_{R\mathrm{BUT}\mathrm{FROM}}^2*{\tau }_{\mathrm{AND}\mathrm{<figure-callout\; id="2"\; label="M\; P"\; filenames="00000028.png,00000029.png"\; state="\{\{state\}\}">M\; </figure-callout>}P}^2$$

where $${\tau }_{\mathrm{AND}MP}^2$$

- two pulses with a duration of 10 μs each with a separation of 10 μs or $${\tau }_{\mathrm{AND}\mathrm{<figure-callout\; id="2"\; label="M\; P"\; filenames="00000028.png,00000029.png"\; state="\{\{state\}\}">M\; </figure-callout>}P}^2={\tau }_{R\mathrm{BUT}\mathrm{FROM}}^2=10\text{μs}$$

; the third packet of pulses with the arrangement - $${\tau }_{\mathrm{AND}\mathrm{<figure-callout\; id="3"\; label="M\; P"\; filenames="00000028.png,00000029.png"\; state="\{\{state\}\}">M\; </figure-callout>}P}^3*{\tau }_{R\mathrm{BUT}\mathrm{FROM}}^3*{\tau }_{\mathrm{AND}\mathrm{<figure-callout\; id="3"\; label="M\; P"\; filenames="00000028.png,00000029.png"\; state="\{\{state\}\}">M\; </figure-callout>}P}^3$$

where $${\tau }_{\mathrm{AND}MP}^3$$

- two pulses with a duration of 100 μs each with a separation of 100 μs or $${\tau }_{\mathrm{AND}\mathrm{<figure-callout\; id="3"\; label="M\; P"\; filenames="00000028.png,00000029.png"\; state="\{\{state\}\}">M\; </figure-callout>}P}^3={\tau }_{R\mathrm{BUT}\mathrm{FROM}}^3=\mathrm{one\; hundred}m\mathrm{to}\mathrm{from}$$

; the spacing between the three bursts of pulses is 10 ms.

On Fig - time distribution of three packets of pulses of radiation exposure of the media on fourteen channels, where the time offset in each subsequent channel is a shift of 10 ms compared with the previous channel.

On Fig - time distribution of three packets of pulses of exposure of the media on fourteen channels, where the time offset in each subsequent channel is a shift of 30 ms compared with the previous channel.

.In Fig.16 - oscillatory system 43 (there is a construction of oscillatory systems, the same for all 43-1, 43-2, 43-3, 43-4, ..., 43-10), where 1, 2, 3, 4 and 5 bridge circuits shown in the figure below, with parallel oscillatory circuits in the shoulders of the bridge, tuned to five frequencies in the band of each oscillatory system. A parallel oscillatory circuit formed by elements L and C at a frequency $$f=\mathrm{one}/\left(2\pi \sqrt{L\cdot C}\right)$$

.

The control device of the electromagnetic field of the secondary emitters (figure 1) contains a clock pulse generator 1, connected by the output to the input of the shaper of the radiation spectrum 2; fourteen outputs of the shaper 2 are connected to fourteen inputs of the antenna switch 3, fourteen outputs-inputs of the antenna switch 3, from first to fourteenth, are connected in parallel with fourteen inputs and outputs of four transceiver antenna systems 4; fourteen outputs of the antenna switch 3, from the fifteenth to the twenty-eighth, are connected to fourteen inputs of the radiation information generator of the secondary emitters 5; the output of the information shaper 5 is connected through the frequency spectrum converter 6, through ten outputs of the filter unit 7 with ten inputs of the secondary radiation spectrum analyzer 8; ten outputs of the analyzer 8 are connected to ten inputs of a block of ten indicators of the radiation spectrum 9.

, $$C_{НАГ}^2$$

, $$C_{НАГ}^3$$

, $$C_{НАГ}^4$$

, $$C_{НАГ}^5$$

, $$C_{НАГ}^6$$

, $$C_{НАГ}^7$$

, $$C_{НАГ}^8$$

, $$C_{НАГ}^9$$

, $$C_{НАГ}^{10}$$

, $$C_{НАГ}^{11}$$

, $$C_{НАГ}^{12}$$

, $$C_{НАГ}^{13}$$

, $$C_{НАГ}^{14}$$

.The transceiver antenna system 4 contains fourteen transceiver antennas (FIG. 2 and FIG. 3), on the one hand each of them is connected to one of the fourteen inputs of the transceiver antenna system 4, and on the other hand, each of the fourteen antennas is connected with a grounded load capacity (figure 3), where the load capacity is $$C_{N\mathrm{BUT}G}^{\mathrm{one}}$$

, $$C_{\mathrm{<figure-callout\; id="2"\; label="N\; BUT\; G"\; filenames="00000028.png,00000029.png"\; state="\{\{state\}\}">N\; </figure-callout>}\mathrm{BUT}G}^2$$

, $$C_{\mathrm{<figure-callout\; id="3"\; label="N\; BUT\; G"\; filenames="00000028.png,00000029.png"\; state="\{\{state\}\}">N\; </figure-callout>}\mathrm{BUT}G}^3$$

, $$C_{N\mathrm{BUT}G}^{\mathrm{four}}$$

, $$C_{\mathrm{<figure-callout\; id="5"\; label="N\; BUT\; G"\; filenames="00000028.png,00000029.png"\; state="\{\{state\}\}">N\; </figure-callout>}\mathrm{BUT}G}^5$$

, $$C_{\mathrm{<figure-callout\; id="6"\; label="N\; BUT\; G"\; filenames="00000028.png,00000029.png"\; state="\{\{state\}\}">N\; </figure-callout>}\mathrm{BUT}G}^6$$

, $$C_{\mathrm{<figure-callout\; id="7"\; label="N\; BUT\; G"\; filenames="00000028.png,00000029.png"\; state="\{\{state\}\}">N\; </figure-callout>}\mathrm{BUT}G}^7$$

, $$C_{\mathrm{<figure-callout\; id="8"\; label="N\; BUT\; G"\; filenames="00000028.png,00000029.png"\; state="\{\{state\}\}">N\; </figure-callout>}\mathrm{BUT}G}^8$$

, $$C_{\mathrm{<figure-callout\; id="9"\; label="N\; BUT\; G"\; filenames="00000028.png,00000029.png"\; state="\{\{state\}\}">N\; </figure-callout>}\mathrm{BUT}G}^9$$

, $$C_{N\mathrm{BUT}G}^{\mathrm{one}0}$$

, $$C_{N\mathrm{BUT}G}^{\mathrm{one}\mathrm{one}}$$

, $$C_{N\mathrm{BUT}G}^{\mathrm{one}2}$$

, $$C_{N\mathrm{BUT}G}^{\mathrm{one}3}$$

, $$C_{N\mathrm{BUT}G}^{\mathrm{one}\mathrm{four}}$$

.

The radiation spectrum shaper 2 (Fig. 4) contains the first trigger 11, element I 10, a discrete delay line 32 for 20 ms, Vk.16 - a switch for starting the device, a collective line with terminals 1,2 and 3, the first generator of a packet of two 1 μs of pulses A1, consisting of: the first B.1 and second B.2 gates, and the first discrete delay line 18 by 1 μs; a second generator of a packet of two pulses of 10 μs A2, consisting of: the third B.3 and fourth B.4 gates, the second discrete delay line 12 by 10 ms, the third discrete delay line 14 by 10 μs and the second trigger 13 by 10 μs; a third packet generator of two pulses of 100 μs A3, consisting of: the fifth B.5 and sixth B.6 gates, the fourth discrete delay line 15 by 10 ms, the fifth discrete delay line 17 by 100 μs and the third trigger 16 by 100 μs; pulse switch A4, consisting of: the fifteenth switch (Vk.15) for two switching positions and fourteen channels, and each channel has its own switch (from Vk.1 to Vk.14) for four positions, for four operating modes, in thirteen channels starting from the second to the fourteenth in each channel - a switch (from Vk.2 to Vk 14), a valve (from B.7 to B.19 and two discrete delay lines (from 19 to 32); the first input of the radiation spectrum shaper 2 is connected to the second input of the element And 10, and the first input of the element And 10 is connected to the first input of the of the radiation spectrum 2 through the short-circuit terminals “a” and “b” of the sixteenth switch Bk.16 (Start) and through the first trigger 11; the output of the And 10 element is connected in parallel with the inputs of the first A1 and second A2 pulse packet generators; the input of the first packet generator from of two pulses 1 μs A1 is connected to the output in parallel through the second valve B.2 and through the first valve B.1, through the first delay line 18 by 1 μs, the output of the first generator A1 is connected to the first terminal of the collective line; the input of the second packet generator of two pulses of 10 μs A2 is connected to the second trigger 13 through the second discrete delay line 12 for 10 ms, the output of the second trigger 13 is connected to the output of the second packet generator of two pulses of 10 μs A2 through the third gate B.3, through the third discrete delay line 14 by 10 μs and in parallel through the fourth gate B.4, the output of the second packet generator of two pulses of 10 μs A2 is connected to the second terminal of the collective line and in parallel with the input of the third packet generator of two pulses of 100 μs A3; the input of the third packet generator of two pulses of 100 μs A3 is connected to the third trigger 16 through the fourth discrete delay line 15 for 10 ms, the output of the third trigger 16 is connected to the output of the third packet generator of two pulses of 100 μs A3 through the fifth gate B.5, through the fifth discrete delay line 17 per 100 μs and in parallel through the sixth gate B.6, the output of the third packet generator of two pulses of 100 μs A3 is connected to the third terminal of the collective line; input pulse switch A4 is connected to a collective line; the input of the pulse switch A4 is connected in parallel with the fourteen outputs of the radiation spectrum shaper 2 through fourteen channels: in the first channel, the input of the pulse switch A4 is connected in parallel to the fourth, to the third terminals of the first switch Bk.1 directly, and to the second terminal of the first switch Bk.1 through the second terminal of the fifteenth switch Bk.15 into two positions (the second terminal is on or the second terminal is turned off from the input of the switch), the second terminal of the first switch Bk.1 is connected in parallel to the second terminals all x thirteen switches, the zero terminal of the first switch Vk.1 is connected to the first output of the radiation spectrum shaper 2; in the second channel, the input of the pulse switch A4 is connected in parallel to the fourth terminal of the second switch Bk.2 through the seventh valve B.7, through the sixth discrete delay line 19 by 10 ms and through the seventh discrete delay line 32 by 20 ms, and to the third terminal of the second switch Bk.2 through the seventh valve B.7 and through the sixth discrete delay line 19 by 10 ms, the zero terminal of the second switch Bk.2 is connected to the second output of the radiation spectrum shaper 2; in the third channel, the input of the pulse switch A4 is connected in parallel to the fourth terminal of the third switch Bk.3 through the eighth gate B.8, through the eighth discrete delay line 20 by 20 ms and through the ninth discrete delay line 32 by 20 ms, and to the third terminal of the third switch Vk.3 through the eighth gate B.8 and through the ninth discrete delay line 20 by 20 ms, the zero terminal of the third switch Vk.3 is connected to the third output of the radiation spectrum shaper 2; in the fourth channel, the input of the pulse switch A4 is connected in parallel to the fourth terminal of the fourth switch Bk.4 through the ninth valve B.9, through the tenth discrete delay line 21 by 30 ms and through the eleventh discrete delay line 32 by 20 ms, and to the third terminal of the fourth switch Vk.4 through the ninth valve B.9 and through the tenth discrete delay line 21 for 30 ms, the zero terminal of the fourth switch Vk.4 is connected to the fourth output of the radiation spectrum shaper 2; in the fifth channel, the input of the pulse switch A4 is connected in parallel to the fourth terminal of the fifth switch Bk.5 through the tenth valve B.10, through the twelfth discrete delay line 22 by 40 ms and through the thirteenth discrete delay line 32 by 20 ms, and to the third terminal of the fifth switch Vk.5 through the tenth valve B.10 and through the twelfth line of discrete delay 22 by 40 ms, the zero terminal of the fifth switch Vk.5 is connected to the fifth output of the radiation spectrum shaper 2; in the sixth channel, the input of the pulse switch A4 is connected in parallel to the fourth terminal of the sixth switch Bk.6 through the eleventh valve B.11, through the fourteenth discrete delay line 23 by 50 ms and through the fifteenth discrete delay line 32 by 20 ms, and to the third terminal of the sixth switch Bk.6 through the eleventh valve B.11 and through the fourteenth line of discrete delay 23 for 50 ms, the zero terminal of the sixth switch Bk.6 is connected to the sixth output of the shaper of the radiation spectrum 2; in the seventh channel, the input of the pulse switch A4 is connected in parallel to the fourth terminal of the seventh switch Bk.7 through the twelfth valve B.12, through the sixteenth discrete delay line 24 for 60 ms and through the seventeenth discrete delay line 32 for 20 ms, and to the third terminal of the seventh switch BK.7 through the twelfth gate B.12 and through the sixteenth discrete delay line 24 for 60 ms, the zero terminal of the seventh switch Bk.7 is connected to the seventh output of the radiation spectrum shaper 2; in the eighth channel, the input of the pulse switch A4 is connected in parallel to the fourth terminal of the eighth switch Bk.8 through the thirteenth valve B.13, through the eighteenth discrete delay line 25 by 70 ms and through the nineteenth discrete delay line 32 by 20 ms, and to the third terminal of the eighth switch BK.8 through the thirteenth valve B.13 and through the eighteenth discrete delay line 25 for 70 ms, the zero terminal of the eighth switch Bk.8 is connected to the eighth output of the radiation spectrum shaper 2; in the ninth channel, the input of the pulse switch A4 is connected in parallel to the fourth terminal of the ninth switch Bk.9 through the fourteenth valve B.14, through the twentieth discrete delay line 26 by 80 ms and through the twenty-first discrete delay line 32 by 20 ms, and to the third terminal the ninth switch BK.9 through the fourteenth gate B.14 and through the twentieth discrete delay line 26 by 80 ms, the zero terminal of the ninth switch Bk.7 is connected to the ninth output of the radiation spectrum shaper 2; in the tenth channel, the input of the pulse switch A4 is connected in parallel to the fourth terminal of the tenth switch Bk.10 through the fifteenth valve B.15, through the twenty-second discrete delay line 27 to 90 ms and through the twenty-third discrete delay line 32 to 20 ms, and to the third the terminal of the tenth switch BK.10 through the fifteenth gate of B.15 and through the twenty-second discrete delay line 27 by 90 ms, the zero terminal of the tenth switch of Bk.10 is connected to the tenth output of the radiation spectrum shaper 2; in the eleventh channel, the input of the pulse switch A4 is connected in parallel to the fourth terminal of the eleventh switch Bk.11 through the sixteenth valve B.16, through the twenty-fourth discrete delay line 28 for 100 ms and through the twenty-fifth discrete delay line 32 for 20 ms, and to the third the terminal of the eleventh switch Bk.11 through the sixteenth valve B.16 and through the twenty-fourth discrete delay line 28 by 100 ms, the zero terminal of the eleventh switch Bk.11 is connected to the eleventh output of the shaper of the radiation spectrum 2; in the twelfth channel, the input of the pulse switch A4 is connected in parallel to the fourth terminal of the twelfth switch Bk.12 through the seventeenth valve B.17, through the twenty-sixth discrete delay line 29 by 110 ms and through the twenty-seventh discrete delay line 32 by 20 ms, and to the third the terminal of the twelfth switch Bk.12 through the seventeenth valve B.17 and through the twenty-sixth discrete delay line 29 by 110 ms, the zero terminal of the twelfth switch Bk.12 is connected to the twelfth output of the radiation spectrum shaper 2; in the thirteenth channel, the input of the pulse switch A4 is connected in parallel to the fourth terminal of the thirteenth switch Bk.13 through the eighteenth valve B.18, through the twenty-eighth discrete delay line 30 for 120 ms and through the twenty-ninth discrete delay line 32 for 20 ms, and to the third the terminal of the thirteenth switch BK.13 through the eighteenth gate B.18 and through the twenty-eighth line of discrete delay 30 to 120 ms, the zero terminal of the thirteenth switch Bk.13 is connected to the thirteenth output of the shaper of the radiation spectrum 2; in the fourteenth channel - the input of the pulse switch A4 is connected in parallel to the fourth terminal of the fourteenth switch Bk.14 through the nineteenth valve B.19, through the thirty line of discrete delay 31 to 130 ms and through the thirty-first line of discrete delay 32 to 20 ms, and to the third terminal the fourteenth switch BK.14 through the nineteenth gate B.19 and through the thirty line of discrete delay 31 to 130 ms, the zero terminal of the fourteenth switch Bk.14 is connected to the fourteenth output of the shaper of the radiation spectrum 2, parallel to zero Vk.14 fourteenth switch terminal is connected through the thirty-second discrete line delay 32 to 20 ms with the input of the first flip-flop 11; the second terminals of all fourteen switches are connected to the zero terminal of the fifteenth switch Bk.15; the first terminals of all fourteen switches are free and designed to disable the selected channel.

Antenna switch 3 (Fig. 5) contains fourteen receiving diode-capacitive bridges 33-1 (on the receiving side of the antennas) and fourteen transmitting diode-capacitive bridges 33-2 (on the transmitting side of the antennas) and a control unit for the transceiving antenna system 34, while fourteen inputs from the first to fourteenth switch of antennas 3 are connected in parallel with the second inputs of fourteen transmitting diode-capacitive bridges 33-2, and from the first inputs of fourteen transmitting diode-capacitive bridges 33-2 are connected in parallel to the second output of the unit transceiver antenna system boards 34; the outputs of fourteen transmitting diode-capacitive bridges 33-2 are connected in parallel with the second inputs of the fourteen receiving diode-capacitive bridges 33-1 and with fourteen inputs-outputs from the first to fourteenth antenna switch 3; the first inputs of fourteen receiving diode-capacitive bridges 33-1 are connected in parallel with the first output of the control unit of the transceiver antenna system 34; the outputs of fourteen receiving diode-capacitive bridges 33-1 are connected in parallel with fourteen outputs starting from the fifteenth to twenty-eighth antenna switch 3; for example, the first channel is formed by a connection - the first input of the antenna switch 3 is connected in parallel with the first input of the control unit of the transceiver antenna system 34 and with the second input of the transmitting diode-capacitive bridges 33-2, and the first input of this transmitting bridge 33-2 is connected to the second the output of the control unit of the transceiver antenna system 34, the output of this bridge 33-2 is connected in parallel with the first input-output of the antenna switch 3, and through the second input of the receiving diode-capacitive bridge 33-1 with the fifteenth output of the antenna switch 3, the first input of this receiving bridge 33-1 is connected to the first output of the control unit of the transceiver antenna system 34; the second channel - the second input of the antenna switch 3 is connected in parallel with the second input of the control unit of the transceiver antenna system 34 and with the second input of the transmitting diode-capacitive bridges 33-2, and the first input of the transmitting bridge 33-2 is connected to the second output of the control unit transmitting antenna system 34, the output of this bridge 33-2 is connected in parallel with the second input-output of the antenna switch 3, and through the second input of the receiving diode-capacitive bridge 33-1 with the sixteenth output of the antenna switch 3, the first input of this bridge 33-1 is connected a first output transmission-reception antenna system control unit 34; the third channel - the third input of the antenna switch 3 is connected in parallel with the third input of the control unit of the transceiver antenna system 34 and with the second input of the transmitting diode-capacitive bridges 33-2, and the first input of this bridge 33-2 is connected to the second output of the control unit transmitting antenna system 34, the output of this bridge 33-2 is connected in parallel with the third input-output of the antenna switch 3, and through the second input of the receiving diode-capacitive bridge 33-1 with the seventeenth output of the antenna switch 3, the first input of this bridge 33-1 is connected to first m output transmission-reception antenna system control unit 34; the fourth channel - the fourth input of the antenna switch 3 is connected in parallel with the fourth input of the control unit of the transceiver antenna system 34 and with the second input of the transmitting diode-capacitive bridges 33-2, and the first input of this bridge 33-2 is connected to the second output of the control unit transmitting antenna system 34, the output of this bridge 33-2 is connected in parallel with the fourth input-output of the antenna switch 3, and through the second input of the receiving diode-capacitive bridge 33-1 with the eighteenth output of the antenna switch 3, the first input of this bridge 33-1 with union of a first output control unit transceiver antenna system 34; fifth channel - the fifth input of the antenna switch 3 is connected in parallel with the fifth input of the control unit of the transceiver antenna system 34 and with the second input of the transmitting diode-capacitive bridges 33-2, and the first input of this bridge 33-2 is connected to the second output of the control unit transmitting antenna system 34, the output of this bridge 33-2 is connected in parallel with the fifth input-output of the antenna switch 3, and through the second input of the receiving diode-capacitive bridge 33-1 with the nineteenth output of the antenna switch 3, the first input of this bridge 33-1 is connected to first you the progress of the control unit of the transceiver antenna system 34; sixth channel - the sixth input of the antenna switch 3 is connected in parallel with the sixth input of the control unit of the transceiver antenna system 34 and with the second input of the transmitting diode-capacitive bridges 33-2, and the first input of this bridge 33-2 is connected to the second output of the control unit transmitting antenna system 34, the output of this bridge 33-2 is connected in parallel with the sixth input-output of the antenna switch 3, and through the second input of the diode-capacitive bridge 33-1 with the twentieth output of the antenna switch 3, the first input of the bridge 33-1 is connected to the first output block control phenomena of a transceiver antenna system 34; seventh channel - the seventh input of the antenna switch 3 is connected in parallel with the seventh input of the control unit of the transceiver antenna system 34 and with the second input of the diode-capacitive bridges 33-2, and the first input of the bridge 33-2 is connected to the second output of the control unit of the transceiver antenna system 34, the output of the bridge 33-2 is connected in parallel with the seventh input-output of the antenna switch 3, and through the second input of the diode-capacitive bridge 33-1 with the twenty-first output of the antenna switch 3, the first input of the bridge 33-1 is connected to the first output of the control unit reception transmitting antenna system 34; the eighth channel - the eighth input of the antenna switch 3 is connected in parallel with the eighth input of the control unit of the transceiver antenna system 34 and with the second input of the diode-capacitive bridges 33-2, and the first input of the bridge 33-2 is connected to the second output of the control unit of the transceiver antenna system 34, the output of the bridge 33-2 is connected in parallel with the eighth input-output of the antenna switch 3, and through the second input of the diode-capacitive bridge 33-1 with the twenty second output of the antenna switch 3, the first input of the bridge 33-1 is connected to the first output of the control unit reception transmitting antenna system 34; the ninth channel - the ninth input of the antenna switch 3 is connected in parallel with the ninth input of the control unit of the transceiver antenna system 34 and with the second input of the diode-capacitive bridges 33-2, and the first input of the bridge 33-2 is connected to the second output of the control unit of the transceiver antenna system 34, the output of the bridge 33-2 is connected in parallel with the ninth input-output of the antenna switch 3, and through the second input of the diode-capacitive bridge 33-1 with the twenty-third output of the antenna switch 3, the first input of the bridge 33-1 is connected to the first output of the control unit the reception -peredayuschey antenna system 34; tenth channel - the tenth input of the antenna switch 3 is connected in parallel with the tenth input of the control unit of the transceiver antenna system 34 and with the second input of the diode-capacitive bridges 33-2, and the first input of the bridge 33-2 is connected to the second output of the control unit of the transceiver antenna system 34, the output of the bridge 33-2 is connected in parallel with the tenth input-output of the antenna switch 3, and through the second input of the diode-capacitive bridge 33-1 with the twenty-fourth output of the antenna switch 3, the first input of the bridge 33-1 is connected to the first output of the control unit at mo-transmitting antenna system 34; eleventh channel - the eleventh input of the antenna switch 3 is connected in parallel with the eleventh input of the control unit of the transceiver antenna system 34 and with the second input of the diode-capacitive bridges 33-2, and the first input of the bridge 33-2 is connected to the second output of the control unit of the transceiver antenna system 34, the output of the bridge 33-2 is connected in parallel with the eleventh input-output of the antenna switch 3, and through the second input of the diode-capacitive bridge 33-1 with the twenty-fifth output of the antenna switch 3, the first input of the bridge 33-1 is connected to the first output of and control transceiver antenna system 34; twelfth channel - the twelfth input of the antenna switch 3 is connected in parallel with the twelfth input of the control unit of the transceiver antenna system 34 and with the second input of the transmitting diode-capacitive bridges 33-2, and the first input of this transmitting bridge 33-2 is connected to the second output of the control unit transmitting antenna system 34, the output of this transmitting bridge 33-2 is connected in parallel with the twelfth input-output of the antenna switch 3, and through the second input of the receiving diode-capacitive bridge 33-1 with the twenty-sixth output of the switch an enn 3, the first input of the receiver bridge 33-1 is connected to the first output of the transmission-reception antenna system control unit 34; thirteenth channel - the thirteenth input of the antenna switch 3 is connected in parallel with the thirteenth input of the control unit of the transceiver antenna system 34 and with the second input of the transmitting diode-capacitive bridges 33-2, and the first input of this transmitting bridge 33-2 is connected to the second output of the control unit the transmitting antenna system 34, the output of this transmitting bridge 33-2 is connected in parallel with the thirteenth input-output of the antenna switch 3, and through the second input of the receiving diode-capacitive bridge 33-1 with the twenty-seventh output of the switch a Tenn 3, the first input receiving the bridge 33-1 is connected to the first output of the transmission-reception antenna system control unit 34; fourteenth channel - the fourteenth input of the antenna switch 3 is connected in parallel with the fourteenth input of the control unit of the transceiver antenna system 34 and with the second input of the transmitting diode-capacitive bridges 33-2, and the first input of the transmitting bridge 33-2 is connected to the second output of the control unit transmitting antenna system 34, the output of the transmitting bridge 33-2 is connected in parallel with the fourteenth input-output of the antenna switch 3, and through the second input of the receiving diode-capacitive bridge 33-1 with the twenty-eighth output of the ant n 3, the first input receiving the bridge 33-1 is connected to the first output of the transmission-reception antenna system control unit 34.

The control unit of the transceiver antenna system 34 (Fig.6), where the transformer Tr-1 with fourteen primary 1 and a secondary winding consisting of two sections 2-1 and 2-2, two voltage amplifiers 35 and 37, the element is NOT 36, two valves B.1 and B.2; while the fourteen inputs of the control unit of the transceiver antenna system 34 are connected in parallel with the terminal “a” of the fourteen primary windings 1 of the transformer Tr.1, and the terminal “b” of the fourteen primary windings 1 of the transformer Tr.1 is grounded; two sections 2-1 and 2-2 of the secondary winding are connected at the grounded point "0", and the terminals "c" and "e" form the two outputs of the control unit of the transceiver antenna system 34, terminal "c" of the first section of the secondary winding 2- 1 through the valve B.1 and the voltage amplifier 35 is connected to the first output of the control unit of the transceiver antenna system 34, and the terminal "d" of the second section of the secondary winding 2-2 through the valve B.2, the element 36 and the voltage amplifier 37 is connected to the second output of the control unit of the transceiver antenna system 34.

The diode-capacitive bridge is made the same for the receiving 33-1, and for the transmitting 33-2 (Fig.7), where R ₁ and R ₂ are the resistance, equal in magnitude and high resistance of at least 100 megohms, B.1 and B.2 - valves, C ₁ and C ₂ - capacitance, while the first input of the diode-capacitive bridge is connected in parallel to the diagonal of the bridge, to points "a" and "b", so the first input of the bridge is connected through the first active resistance R ₁ to point "a", and through the second active resistance R ₂ to point "b"; the second input of the diode-capacitive bridge is connected to point “d”, point “d” is connected to point “c” in parallel in two circuits: the first through the second capacitance C ₂ and the first valve B.1, and the second through the second valve B .2 and a first container C ₁ ; point "c" is connected to the output of the diode-capacitive bridge.

The shaper of radiation information of the secondary emitters - 5 (Fig. 8), containing Tr. 1 - a transformer with fourteen primary windings - 1 and one secondary winding - 2, a broadband amplifier - 38, while the fourteen inputs of the shaper of radiation information of the secondary emitters 5 form fourteen parallel independent channels, in each of the fourteen channels, the input of the radiation information generator of the secondary emitters 5 is connected via a broadband amplifier 38 to the terminal “a” of the primary winding of the transformer Tr. 1, and MMA "b" in each of the fourteen primary transformer windings Tr.1 grounded; the output of the radiation information generator of the secondary emitters 5 is connected to the terminal “c” of the secondary winding of the transformer Tr. 1, and the terminal “d” of the secondary winding of the transformer Tr. 1 is grounded.

The frequency spectrum converter 6 (Fig. 9), comprising a 10 kHz generator 39 and a mixer 40, wherein the input of the frequency spectrum converter 6 is connected to the output of the frequency spectrum converter 6 through the first input of the mixer 40, and the second input of the converter 40 is connected to the output of the generator 39 .

A filter block for ten channels 7 (FIG. 10), comprising ten filters 41-1 to 41-10 and ten narrow-band amplifiers 42, while the input of the filter block for ten channels 7 is connected in parallel with ten inputs of ten filters; the output of the first filter 41-1 with a bandwidth of 1 kHz to 10 kHz is connected to the first output of the filter unit 7 through a narrow-band amplifier 42; the output of the second filter 41-2 with a bandwidth of 10 kHz to 50 kHz is connected to the second output of the filter unit 7 through a narrow-band amplifier 42; the output of the third filter 41-3 with a passband from 50 kHz to 100 kHz is connected to the third output of the filter unit 7 through a narrow-band amplifier 42; the output of the fourth filter 41-4 with a bandwidth of 100 kHz to 200 kHz is connected to the fourth output of the filter unit 7 through a narrow-band amplifier 42; the output of the fifth filter 41-5 with a passband from 200 kHz to 400 kHz is connected to the fifth output of the filter unit 7 through a narrow-band amplifier 42; the output of the sixth filter 41-6 with a bandwidth of 400 kHz to 800 kHz is connected to the sixth output of the filter unit 7 through a narrow-band amplifier 42; the output of the seventh filter 41-7 with a bandwidth of 800 kHz to 1000 kHz is connected to the seventh output of the filter unit 7 through a narrow-band amplifier 42; the output of the eighth filter 41-8 with a bandwidth of 1.0 to 10 MHz is connected to the eighth output of the filter unit 7 through a narrow-band amplifier 42; the output of the ninth filter 41-9 with a bandwidth of 10 to 20 MHz is connected to the ninth output of the filter unit 7 through a narrow-band amplifier 42; the output of the tenth filter 41-10 with a bandwidth of 20 to 40 MHz is connected to the tenth output of the filter unit 7 through a narrow-band amplifier 42.

The spectrum analyzer of the secondary radiation into ten channels 8 (Fig. 11), where from 43-1 to 43-10 are oscillatory systems (a parallel oscillatory circuit tuned to the indicated frequency bands), 42 is a detector; the first input of the analyzer 8 is connected to the input of the first oscillating system 43-1 at a frequency of 1-10 kHz, the output of the first system 43-1 is connected in parallel with the eleventh output of the analyzer 8, and with the first output of the analyzer 8 through the first detector; the second input of the analyzer 8 is connected to the input of the second oscillating system 43-2 at a frequency of 10-50 kHz, the output of the second system 43-2 is connected in parallel with the twelfth output of the analyzer 8, and with the second output of the analyzer 8 through a second detector; the third input of the analyzer 8 is connected to the input of the third oscillatory system 43-3 at a frequency of 50-100 kHz, the output of the third system 43-3 is connected in parallel with the thirteenth output of the analyzer 8, and with the third output of the analyzer 8 through a third detector; the fourth input of the analyzer 8 is connected to the input of the fourth oscillating system 43-4 at a frequency of 100-200 kHz, the output of the fourth system 43-4 is connected in parallel with the fourteenth output of the analyzer 8, and with the fourth output of the analyzer 8 through the fourth detector; the fifth input of the analyzer 8 is connected to the input of the fifth oscillating system 43-5 at a frequency of 200-400 kHz, the output of the fifth system 43-5 is connected in parallel with the fifteenth output of the analyzer 8, and with the fifth output of the analyzer 8 through the fifth detector; the sixth input of the analyzer 8 is connected to the input of the sixth oscillating system 43-6 at a frequency of 400-800 kHz, the output of the sixth system 43-6 is connected in parallel with the sixteenth output of the analyzer 8, and with the sixth output of the analyzer 8 through the sixth detector; the seventh input of the analyzer 8 is connected to the input of the seventh oscillatory system 43-7 at frequencies of 800-1000 kHz, the output of the seventh system 43-7 is connected in parallel with the seventeenth output of the analyzer 8, and with the seventh output of the analyzer 8 through the seventh detector; the eighth input of analyzer 8 is connected to the input of the eighth oscillating system 43-8 at a frequency of 1-10 MHz, the output of the eighth system 43-8 is connected in parallel with the eighteenth output of the analyzer 8, and with the eighth output of the analyzer 8 through the eighth detector; the ninth input of the analyzer 8 is connected to the input of the ninth oscillatory system 43-9 at a frequency of 10-20 MHz, the output of the ninth system 43-9 is connected in parallel with the nineteenth output of the analyzer 8, and with the ninth output of the analyzer 8 through the ninth detector; the tenth input of analyzer 8 is connected to the input of the tenth oscillatory system 43-10 at frequencies of 20-40 MHz, the output of the tenth system 43-10 is connected in parallel with the twentieth output of analyzer 8, and with the tenth output of analyzer 8 through the tenth detector.

Each of the oscillatory systems 43 (Fig.16), presented in the form of 43-1, 43-2, 43-3, 43-4, 43-5, 43-6, 43-7, 43-8, 43-9 and 43-10 in figure 11, contains five bridges in each of the oscillatory systems: in the first oscillatory system 43-1 - five bridges, in the second oscillatory system 43-2 - five bridges, in the third oscillatory system 43-3 - five bridges, in the fourth vibrational system 43-4 - five bridges, in the fifth vibrational system 43-5 - five bridges, in the sixth vibrational system 43-6 - five bridges, in the seventh vibrational system 43-7 - five bridges, in the eighth vibrational system 43- 8 - five mo stov, in the ninth vibrational system 43–9 - five bridges, in the tenth vibrational system 43–10 - five bridges. Each bridge to the oscillatory system is made in the same way in the form of the electrical circuit shown in Fig. 16 by the first figure 1, the difference in the settings of the parallel oscillatory circuits included in the shoulders of the bridge. The input of each oscillatory system (43-1, 43-2, ..., 43-10) is connected to the output of the system, while five oscillatory bridges are connected in parallel to the input-output, each bridge contains four parallel oscillatory circuits L, C, included in four side of the bridge, the first diagonal of the bridge is connected on one side to the entrance of the bridge, and on the other it is grounded, the high-resistance resistance R is included in the second diagonal.

The block of indicators of the spectrum of radiation 9 (Fig), containing ten voltage indicators 45 for ten channels, a spectrum analyzer 46 and a switch for ten positions of inclusion 47, while ten inputs of the block of indicators of the spectrum of radiation 9 are connected to the inputs of ten voltage indicators (as an indicator you can use: a voltmeter, LED, incandescent lamp and any signaling device for the presence of voltage in a given frequency band), and ten inputs from the fifteenth to the twentieth block of indicators of the spectrum of radiation 9 are connected in parallel to the terminals "a" of the switch to turn on ten positions 47 and the terminal "b" of the switch 47 are connected to the input of the spectrum analyzer 47.

The principle of operation of the device.

Based on the structural diagram of figure 1, the device for monitoring the electromagnetic field of the secondary emitters works as follows: a clock pulse generator (GTI) at the output excites a sequence of pulses of 1 μs duration, these pulses are fed to the input of the radiation spectrum shaper 2, and only one pulse is supplied to the shaper 2 , which synchronizes the three generators in the shaper 2 (figure 4). The generators at the output create two pulses of different durations (Fig.13), thus forming a packet of pulses. This packet by the pulse switch in the shaper 2 distributes over fourteen channels at the output of the shaper. Packets using the antenna switch 3 are received on fourteen lines and feed four transceiver antenna systems 4. An excited electromagnetic field by the antenna systems makes the media under investigation excited: electrical boards, electrical circuits, block structures, dielectric and weakly conductive materials, etc. These studied media can emit a secondary field, and its level depends on the block or design features, on the material and advantages and disadvantages. The radiated secondary electromagnetic field is fixed by the antenna system 4 and in the form of induced emf enters through fourteen lines to fourteen outputs of the antenna switch 3 from the fifteenth to the twenty-eighth. This EMF, arriving at fourteen inputs of the radiation information generator of the secondary emitters 5, is summed up and fed to the frequency spectrum converter 6, where the frequencies of the secondary radiation are separated. At the output of the converter 6, a filter unit 7 is installed, which ensures the separation of the secondary radiation frequencies and their arrival through ten channels to the frequency spectrum analyzer 8 with their subsequent indication in the indication unit 9. Let us consider in detail the operation of all blocks.

The clock generator 1 (GTI) excites at the output a continuous sequence of pulses with a duration τ _GTI = 1 μs, which are fed to the first input of the radiation spectrum shaper 2 (Fig. 1) and through it to the second input of the And element 10 (Fig. 2). Of this sequence of pulses of the GTI 1, only one pulse passes through the And 10 element, which coincides in time with the pulse of the first trigger 11, triggered through the input of the trigger 11 from the trigger element (Start), by the GTI pulses along the first input of the spectrum former 2 by closing the terminals “a” and “b” of the sixteenth switch Vk.16, the “Start” button. Moreover, the trigger 11 is triggered once by the GTI pulse through the “Start” element with the start of the “Control Devices ...” launch. Subsequent launches of trigger 11 are carried out by pulses arriving through the zero terminal of the fourteenth switch BK.14, through the thirty-second delay line 32 with a delay of 1 ms at the input of trigger 11, i.e. trigger trigger pulse 11 arrives only after the distribution of pulses by the A4 pulse switch across all fourteen outputs of driver 2. Thus, the trigger 11 triggered by the GTI pulse is synchronized with the GTI pulse 1 arriving at the second input of the And 10 element, which ensures the passage of the GTI pulse through the element And 10, which goes in parallel to two generators A1 and A2. Generator A1 generates two pulses at the output, the first pulse is generated by passing a GTI pulse to output A1 through valve B.2, and the second due to passing through the second circuit formed by valve B.1 and discrete delay line 18 with a delay of 1 μs ( τ _RAS = 1 μs). As a result, the generator A1 generates two pulses with an arrangement at the output: 1 μs * 1 μs * 1 μs or τ _GTI * τ _RAS * τ _GTI (Fig.13). Thus, the first packet of pulses of two pulses of 1 μs with a spacing of 1 μs is formed. The spectrum of frequencies excited by pulses lies in the range from 1 MHz to 40 MHz. At the same time, the GTI pulse 1 is fed to the input of the second generator A2. In the A2 generator, this pulse is delayed by a discrete delay line 12 by 1 ms and is fed to the input of the second trigger 13, the latter at its output creates one pulse with a duration of 10 μs. The ten microsecond pulse of trigger 13 is supplied to output A2 via two circuits: one circuit through the gate B.4, and the other forms a pulse delay by the delay line 14 by 10 μs and the circuit consists of the gate B.3 and the discrete delay line 14. As a result, the output generator A2 generates two pulses with an alignment: 10 μs * 10 μs * 10 μs or τ _UTI * τ _RAS * τ _UTI (Fig.13). Thus, the second packet consists of two pulses of 10 μs with a spacing of 10 μs. The spectrum of frequencies excited by pulses lies in the range from 100 kHz to 10 MHz. The pulses from the input of the second generator A2 go to the input of the third generator A3. In the generator A3, this pulse train is delayed by a discrete delay line 15 by 1 ms and is fed to the input of the third trigger 16, the last one generates one pulse with a duration of 100 μs at its output. One hundred microsecond pulse of trigger 16 is output via two circuits: one circuit through the B.6 gate, and the other forms a pulse delay by the 100 μs delay line and the circuit consists of the B.5 gate and the discrete delay line 17. As a result, the generator A3 creates a packet of two pulses with an arrangement: 100 μs * 100 μs * 100 μs or τ _UTI * τ _RAS * τ _UTI (Fig.13). Thus, the second packet consists of two pulses of 100 μs with a spacing of 100 μs. The spectrum of frequencies excited by pulses lies in the range from 1 kHz to 200 kHz. The outputs of the three generators A1, A2 and A3 are connected to the collective line at terminals 1, 2 and 3, respectively, and the collective line is connected to the input of the pulse commutator A4. The input of the pulse switch is connected in parallel with fourteen outputs through the delay elements in each channel formed by the delay elements, in addition, a switch from Vk.1 to Vk.14 is included in each channel, which provide different modes of operation of the switch. So the zero terminal of each switch is connected to one of the outputs of the radiation spectrum shaper 2 and depends on the switch in which channel it is turned on. Each switch has four positions. Turning on the zero terminal in the first position, this is when connecting the zero terminal of the switch to the terminal first, which allows you to disconnect the channel from work. The second position is when connecting the zero terminal of the switch to the second terminal, which allows you to create a simultaneous mode of operation of all fourteen channels, this is the connection of all channels in parallel to the first output and, therefore, all packets will act in time simultaneously in all channels. The third position of each switch is the connection of the zero terminal of the switch with the third terminal, which will create an operating mode in which the appearance of three pulse packets in each subsequent channel with a time shift of 10 ms, which reflects the distribution of packets in the channels in Fig. 14. This time shift is provided by discrete delay lines of 10 ms from 19 to 31 lines. The first channel is formed by directly connecting the first output of the radiation spectrum shaper 2 through the zero terminal and through the third terminal of the first switch Bk.1 to the input of the A4 switch, so three pulse packets (Fig. 12) will arrive at the first output without delay from the input of the A4 switch. The second channel is formed by connecting the second output of the radiation spectrum shaper 2 through the zero terminal and through the third terminal of the second switch Bk.2, through the sixth discrete delay line 19 by 10 ms, through the seventh gate B.7 to the input of switch A4, therefore, at the second output of the shaper 2 three bursts of pulses will appear with a time delay of 10 ms in comparison with bursts of pulses on the first output. The third channel is formed by connecting the third output of the radiation spectrum shaper 2 through the zero terminal and through the third terminal of the third Bk.3 switch, through the eighth discrete delay line 20 by 20 ms, through the eighth gate B.8 to the input of switch A4, therefore, at the third output of shaper 2 three bursts of pulses will appear with a time delay of 20 ms in comparison with bursts of pulses on the first output. The fourth channel is formed by connecting the fourth output of the radiation spectrum shaper 2 through the zero terminal and through the third terminal of the fourth switch Bk.4, through the tenth discrete delay line 21 for 30 ms, through the ninth gate B.9 to the input of switch A4, therefore, at the fourth output of the shaper 2 three bursts of pulses will appear with a time delay of 30 ms in comparison with bursts of pulses on the first output. The fifth channel is formed by connecting the fifth output of the radiation spectrum shaper 2 through the zero terminal and through the third terminal of the fifth switch Bk.5, through the twelfth discrete delay line 22 by 40 ms, through the tenth gate B.10 to the input of switch A4, therefore, at the fifth output of the shaper 2 three bursts of pulses will appear with a time delay of 40 ms in comparison with bursts of pulses on the first output. The sixth channel is formed by connecting the sixth output of the radiation spectrum shaper 2 through the zero terminal and through the third terminal of the sixth switch Bk.6, through the fourteenth discrete delay line 23 by 50 ms, through the eleventh gate B.11 to the input of switch A4, therefore, at the sixth output of the shaper 2 three bursts of pulses will appear with a time delay of 50 ms in comparison with bursts of pulses on the first output. The seventh channel is formed by connecting the seventh output of the radiation spectrum shaper 2 through the zero terminal and through the third terminal of the seventh switch Bk.7, through the sixteenth discrete delay line 24 for 60 ms, through the twelfth gate B.12 to the input of switch A4, therefore, at the seventh output of the shaper 2 three bursts of pulses will appear with a time delay of 60 ms in comparison with bursts of pulses on the first output. The eighth channel is formed by connecting the eighth output of the radiation spectrum shaper 2 through the zero terminal and through the third terminal of the eighth switch Bk.8, through the eighteenth discrete delay line 25 by 70 ms, through the thirteenth gate B.13 to the input of switch A4, therefore, on the eighth output of the shaper 2 three bursts of pulses will appear with a time delay of 70 ms in comparison with bursts of pulses on the first output. The ninth channel is formed by connecting the ninth output of the radiation spectrum shaper 2 through the zero terminal and through the third terminal of the ninth switch Bk.9, through the twentieth discrete delay line 26 by 80 ms, through the fourteenth gate B.14 to the input of switch A4, therefore, at the ninth output of the shaper 2 three bursts of pulses will appear with a time delay of 80 ms in comparison with bursts of pulses on the first output. The tenth channel is formed by connecting the tenth output of the radiation spectrum shaper 2 through the zero terminal and through the third terminal of the tenth switch Bk.10, through the twenty-second discrete delay line 27 by 90 ms, through the fifteenth gate B.15 to the input of switch A4, therefore, at the tenth output of the shaper 2 three bursts of pulses will appear with a time delay of 90 ms in comparison with bursts of pulses on the first output. The eleventh channel is formed by connecting the eleventh output of the radiation spectrum shaper 2 through the zero terminal and through the third terminal of the eleventh switch Bk.11, through the twenty-fourth discrete delay line 28 for 100 ms, through the sixteenth gate B.16 to the input of switch A4, therefore at the eleventh output of the shaper 2 three bursts of pulses will appear with a time delay of 100 ms in comparison with bursts of pulses on the first output. The twelfth channel is formed by connecting the twelfth output of the radiation spectrum shaper 2 through the zero terminal and through the third terminal of the twelfth switch Bk.12, through the twenty-sixth discrete delay line 29 by 110 ms, through the seventeenth gate B.17 to the input of switch A4, therefore, at the twelfth output of the shaper 2 three bursts of pulses will appear with a time delay of 110 ms in comparison with bursts of pulses on the first output. The thirteenth channel is formed by connecting the thirteenth output of the radiation spectrum shaper 2 through the zero terminal and through the third terminal of the thirteenth switch Bk.13, through the twenty-eighth discrete delay line 30 by 120 ms, through the eighteenth gate B.18 to the input of switch A4, therefore at the thirteenth output of the shaper 2 three bursts of pulses will appear with a time delay of 120 ms in comparison with bursts of pulses on the first output. The fourteenth channel is formed by connecting the fourteenth output of the radiation spectrum shaper 2 through the zero terminal and through the third terminal of the fourteenth switch Bk.14, through the thirtieth discrete delay line 31 by 130 ms, through the nineteenth gate B.19 to the input of switch A4, therefore, on the fourteenth output of shaper 2 three bursts of pulses will appear with a time delay of 130 ms in comparison with bursts of pulses on the first output. The fourth position of each switch is the connection of the zero terminal of the switch with the fourth terminal, which will create an operating mode in which the appearance of three pulse packets in each subsequent channel with a time shift of 30 ms, which reflects the distribution of packets in the channels in Fig. 15. This time shift allows you to transmit three packets of pulses sequentially in each channel only after their action in time in the previous channel ends. This time shift is provided by discrete delay lines of 10 ms from the 19th to 31st lines and lines of 32 by 20ms (Fig. 15). The first channel is formed by directly connecting the first output of the radiation spectrum shaper 2 through the zero terminal and through the fourth terminal of the first switch Bk.1 to the input of the A4 switch, so three pulse packets (Fig. 13) will arrive at the first output without delay from the input of the A4 switch. The second channel is formed by connecting the second output of the radiation spectrum shaper 2 through the zero terminal and through the fourth terminal of the second switch Bk.2, through the seventh discrete delay line 32 by 20 ms, through the sixth discrete delay line 19 by 10 ms, through the seventh valve B.7 to the input of switch A4, therefore, at the second output of the former 2, three pulse packets will appear with a time delay of 30 ms in comparison with the pulse packets at the first output, i.e. after passing packets on the first channel. The third channel is formed by connecting the third output of the radiation spectrum shaper 2 through the zero terminal and through the fourth terminal of the third switch Bk.3, through the ninth discrete delay line 32 by 20 ms, through the eighth discrete delay line 20 by 20 ms, through the eighth B.8 k the input of the A4 switch, therefore, at the third output of the driver 2, three pulse packets will appear with a time delay of 40 ms in comparison with the pulse packets on the first output. The fourth channel is formed by connecting the fourth output of the radiation spectrum shaper 2 through the zero terminal and through the fourth terminal of the fourth switch Bk.4, through the eleventh discrete delay line 32 by 20 ms, through the tenth discrete delay line 21 by 30 ms, through the ninth valve B.9 to the input of the A4 switch, therefore, at the fourth output of the driver 2, three pulse packets will appear with a time delay of 50 ms in comparison with the pulse packets on the first output. The fifth channel is formed by connecting the fifth output of the radiation spectrum shaper 2 through the zero terminal and through the fourth terminal of the fifth switch Bk.5, through the thirteenth discrete delay line 32 by 20 ms through the twelfth discrete delay line 22 by 40 ms, through the tenth valve B.10 to the input A4 switch, therefore, on the fifth output of the former 2, three pulse packets will appear with a time delay of 60 ms in comparison with the pulse packets on the first output. The sixth channel is formed by connecting the sixth output of the radiation spectrum shaper 2 through the zero terminal and through the fourth terminal of the sixth switch Bk.6, through the fifteenth discrete delay line 32 by 20 ms, through the fourteenth discrete delay line 23 by 50 ms, through the eleventh valve B.11 to the input of the A4 switch, therefore, at the sixth output of the shaper 2, three pulse packets will appear with a time delay of 70 ms in comparison with the pulse packets on the first output. The seventh channel is formed by connecting the seventh output of the radiation spectrum shaper 2 through the zero terminal and through the fourth terminal of the seventh switch Bk.7, through the seventeenth discrete delay line 32 by 20 ms, through the sixteenth discrete delay line 24 by 60 ms, through the twelfth gate B.12 to the input of the A4 switch, therefore, at the seventh output of the former 2, three pulse packets will appear with a time delay of 80 ms in comparison with the pulse packets on the first output. The eighth channel is formed by connecting the eighth output of the radiation spectrum shaper 2 through the zero terminal and through the fourth terminal of the eighth switch Bk.8, through the nineteenth discrete delay line 32 by 20 ms, through the eighteenth discrete delay line 25 by 70 ms, through the thirteenth gate B.13 to the input of the A4 switch, therefore, at the eighth output of the former 2, three pulse packets will appear with a time delay of 90 ms in comparison with the pulse packets on the first output. The ninth channel is formed by connecting the ninth output of the radiation spectrum shaper 2 through the zero terminal and through the fourth terminal of the ninth switch Bk.9, through the twenty-first discrete delay line 32 by 20 ms, through the twentieth discrete delay line 26 by 80 ms, through the fourteenth gate B.14 to the input of the A4 switch, therefore, at the ninth output of the former 2, three pulse packets will appear with a time delay of 100 ms in comparison with the pulse packets on the first output. The tenth channel is formed by connecting the tenth output of the radiation spectrum shaper 2 through the zero terminal and through the fourth terminal of the tenth switch Bk.10, through the twenty-third discrete delay line 32 by 20 ms, through the twenty-second discrete delay line 27 by 90 ms, through the fifteenth valve B. 15 to the input of the A4 switch, therefore, at the tenth output of the former 2, three pulse packets will appear with a time delay of 110 ms in comparison with the pulse packets on the first output. The eleventh channel is formed by connecting the eleventh output of the radiation spectrum shaper 2 through the zero terminal and through the fourth terminal of the eleventh switch Bk.11, through the twenty-fifth discrete delay line 32 by 20 ms, through the twenty-fourth discrete delay line 28 by 100 ms, through the sixteenth valve B. 16 to the input of the A4 switch, therefore, at the eleventh output of the former 2, three pulse packets will appear with a time delay of 120 ms in comparison with the pulse packets on the first output. The twelfth channel is formed by connecting the twelfth output of the radiation spectrum shaper 2 through the zero terminal and through the fourth terminal of the twelfth switch Bk.12, through the twenty-seventh discrete delay line 32 by 20 ms, through the twenty-sixth discrete delay line 29 by 110 ms, through the seventeenth valve B. 17 to the input of the A4 switch, therefore, at the twelfth output of the former 2, three pulse packets will appear with a time delay of 130 ms in comparison with the pulse packets on the first output. The thirteenth channel is formed by connecting the thirteenth output of the radiation spectrum shaper 2 through the zero terminal and through the fourth terminal of the thirteenth switch Bk.13, through the twenty-ninth discrete delay line 32 by 20 ms, through the twenty-eighth discrete delay line 30 by 120 ms, through the eighteenth gate B. 18 to the input of the A4 switch, therefore, at the thirteenth output of the former 2, three pulse packets will appear with a time delay of 140 ms in comparison with the pulse packets on the first output. The fourteenth channel is formed by connecting the fourteenth output of the radiation spectrum shaper 2 through the zero terminal and through the fourth terminal of the fourteenth switch Bk.14, through the thirty-first 32-bit discrete delay line for 20 ms, through the thirty-third discrete delay line 31 for 130 ms, through the nineteenth valve B.19 to the input of the A4 switch, therefore, at the fourteenth output of the former 2, three pulse packets will appear with a time delay of 150 ms in comparison with the pulse packets on the first output. The zero terminal of the fourteenth switch Vk.14 is connected in parallel via a 32-bit delay line 32 ms to the input of trigger 11, this connection allows packets to pass from the zero terminal of the fourteenth switch Vk.14 to trigger trigger 11. The trigger triggers the passage of a calibrated GTI pulse 1 for the generators work to create three pulse packets with their subsequent sequential distribution over the fourteen outputs of the shaper 2 using the A4 switch for the selected program. Upon reaching the fourteenth output of the shaper, the process of generating pulses and their distribution will resume. The switch 15 to two switching positions, it allows you to apply to the second inputs of all fourteen switches through their connection to the second terminals of the zero terminals at the same time three packets, thus ensuring the simultaneous output of three pulse packets on all fourteen channels.

до четырнадцатой - $$C_{НАГ}^{14}$$

. Четырнадцать входов с 1 по 14 блока управления приемо-передающей антенной системой 34 (фиг.6) коммутатора антенн 3 соединены с четырнадцатью первичными обмотками 1 трансформатора Тр.1. Трансформатор Тр.1 суммирует все пакеты импульсов, поступающие по четырнадцати каналам, и на вторичной обмотке возбуждается ЭДС, соответствующая действию каждого импульса действующего в первичных обмотках. Когда в любой первичной обмотке появляется импульс, то на выходе вторичной обмотки возбуждается ЭДС, причем эта ЭДС передается на первый усилитель напряжения 35. На выходе усилителя высокое напряжение, поступающее на первый выход блока управления 34, данное напряжение поступает на первый вход четырнадцати приемных диодно-емкостных мостов 33-1, чем обеспечивается запирание всех приемных мостов 33-1 для проникновения через них высокого напряжения генераторов в приемный тракт. Когда импульсы в первичных обмотках отсутствуют, на втором выходе блока 34 второго усилителя 37 создается высокое напряжение для запирания передающих диодно-емкостных мостов 33-2, чтобы случайно высокое напряжение генераторов не попало в приемный канал на выходы с 15 по 28 коммутатора 3. Работа основана на том, что в цепи секции вторичной обмотки 2-2 наведенные импульсы через вентиль В.2 поступают на элемент НЕ 36, на выходе напряжение ноль и на выходе второго усилителя напряжения 37 и, следовательно, на втором выходе блока управления 34 напряжения нет. Поэтому передающие диодно-емкостные мосты 33-2 открыты для прохождения через них пакетов импульсов по всем четырнадцати каналам на антенные системы 4. В случае отсутствия импульсов в первичных обмотках трансформатора Тр.1 во вторичной обмотке импульса нет, то на входе элемента НЕ 36 напряжения нет, следовательно, на выходе элемента НЕ появится напряжение, которое после усиления вторым усилителем 37 поступает на второй выход блока управления 34, обеспечивая запирание передающих диодно-емкостных мостов 33-2, что обеспечивает прием излучения вторичных излучателей от антенной системы 4.Fourteen outputs of the radiation spectrum shaper 2 are connected to fourteen inputs of the antenna switch 3; however, for each of the fourteen inputs of the antenna switch 3 receives three packets of pulses. The pulses in each channel out of fourteen arrive at the second input of fourteen transmitting diode-capacitive bridges 33-2. The transmitting diode-capacitive bridge 33-2 in each channel ensures the passage of these pulse packets to the fourteen outputs of the receive-transmit switch of the antenna 3. Moreover, the high voltage of the pulse packets simultaneously arrives at the second inputs of the fourteen receiving diode-capacitive bridges 33-1, which are currently the moment is closed for passing packets to the receiving part, that is, to the output from the fifteenth to twenty-eighth antenna switch 3. The operation of locking and unlocking the bridges 33-1 and 33-2 is carried out by the receiver-control unit gives the antenna system 34. The control voltage for bridges 33-1 and 33-2 synchronized pulse packets arriving at the input 34 of the control unit of the first through fourteenth switch with three inputs respectively from the first to the fourteenth. The locking control voltage is supplied out of phase at the two outputs of the control unit. Moreover, when a high voltage pulse is received at the input of the switch 3, a high voltage appears at the first output of the control unit 34, which is supplied to the first input of the fourteen receiving diode-capacitive bridges 33-1, locking these bridges 33-1 so that the pulse packets of the generators did not enter the reception exits from the fifteenth to the twenty-eighth. In the absence of a high voltage of the pulse packets at the second output of the control unit 34, a locking voltage appears for the transmitting diode-capacitive bridges 33-2. During this period, the reaction of irradiation of the experimented elements to secondary radiation (re-radiation) by the antenna system 4 is recorded and the reaction in the form of induced voltages (EMF) is supplied to the first input of fourteen receiving diode-capacitive bridges 33-1, which are open at this time, and then goes to the outputs of switch 3 from the fifteenth to the twenty-eighth. Moreover, the secondary radiation is recorded through fourteen channels, which ensures the study of the polarization properties and their levels of secondary emitters. Three packets of pulses distributed in time over different of the fourteen channels in the form of high voltage levels are supplied to fourteen conductors (figure 2), representing the transceiver antenna system 4. The structure of the design of the transceiver antenna system 4 is presented in figure 3 where fourteen inputs are connected to fourteen antennas. Each antenna, from the first to the fourteenth, is a conductor loaded on a grounded capacitance. Fourteen conductors work in the mode of strong elongation, therefore, to increase their effective length, fourteen conductors are loaded on the capacitance from the first - $$C_{N\mathrm{BUT}G}^{\mathrm{one}}$$

until the fourteenth - $$C_{N\mathrm{BUT}G}^{\mathrm{fourteen}}$$

. Fourteen inputs from 1 to 14 of the control unit of the transceiver antenna system 34 (Fig.6) of the antenna switch 3 are connected to fourteen primary windings 1 of the transformer Tr. 1. The transformer Tr. 1 summarizes all the pulse packets arriving through fourteen channels, and an EMF is excited on the secondary winding, corresponding to the action of each pulse acting in the primary windings. When a pulse appears in any primary winding, an EMF is excited at the output of the secondary winding, and this EMF is transmitted to the first voltage amplifier 35. At the output of the amplifier, a high voltage is supplied to the first output of the control unit 34, this voltage is supplied to the first input of fourteen receiving diode capacitive bridges 33-1, which ensures locking of all receiving bridges 33-1 for penetration through them of high voltage generators into the receiving path. When there are no pulses in the primary windings, a high voltage is generated at the second output of unit 34 of the second amplifier 37 to block the transmitting diode-capacitive bridges 33-2, so that accidentally the high voltage of the generators does not fall into the receiving channel at outputs 15 to 28 of switch 3. Operation on the fact that in the circuit of the section of the secondary winding 2-2, the induced pulses through the valve B.2 are fed to the element HE 36, the output voltage is zero and the output of the second voltage amplifier 37 and, therefore, there is no voltage at the second output of the control unit 34 t Therefore, the transmitting diode-capacitive bridges 33-2 are open for pulse packets to pass through them through all fourteen channels to the antenna systems 4. If there are no pulses in the primary windings of the transformer Tr.1, there is no pulse in the secondary winding, then there is no voltage at the input of the element HE 36 therefore, the voltage does not appear at the output of the element, which, after amplification by the second amplifier 37, is supplied to the second output of the control unit 34, providing locking of the transmitting diode-capacitive bridges 33-2, which ensures reception of radiation egg emitters from the antenna system 4.

The diode-capacitive bridges receiving 33-1 and transmitting 33-2 are structurally identical, as they perform the same functions. The receiving bridges 33-1 provide protection of the receiving path when the antenna system 4 is high voltage, and the transmitting bridges 33-2 provide protection of the receiving path from accidental, unauthorized influences of high voltage from generators A.1, A.2 and A.3 through the distribution A4 chain. The diode-capacitive bridge 33-1 (or 33-2) contains two parallel circuits between the terminals “c” and “e”: the first circuit is a series connection of the first valve B.1 and the second capacity C ₂ ; the second circuit is a series connection of the second valve B.2 and the first tank C ₁ . The gates in the chains are turned on. Terminal “d” is connected to the second input of the bridge 33-1 (33-2), and terminal “c” is connected to the output of the bridge 33-1 (33-2). The connection points of the valve with the capacity in each circuit form the terminals “b” and “a”. High resistance impedances of the same magnitude are connected to terminals “b” and “a”, i.e. R ₁ = R ₂ . Resistance R ₁ and R _{2 are} connected in parallel to the first input of the bridge 33-1 (33-2). At the first input of the bridge, a control high voltage is supplied through the resistances R ₁ and R ₂ to the cathodes of valves B.1 and B.2, ensuring that they are locked to allow currents flowing through them to the bridge at the second input to the bridge output. The control voltage for bridges 33-1 is supplied by the first output of the control unit 34, and for bridges 33-2 by the second output of the control unit.

After irradiation of the studied objects in the antenna system, the latter excite the secondary electromagnetic field, which induces the EMF in the antenna system 4. This EMF enters through the receiving bridges 33-1 of the antenna switch 3 to fourteen outputs of the switch 3 from the fifteenth to the twenty-eighth (Fig. 1). These fourteen outputs are connected to fourteen inputs of the radiation information generator of the secondary emitters 5 (Fig. 8). Fourteen inputs of the secondary radiation emitter information generator 5 are connected in each of the fourteen channels to terminal “a” of the primary winding of transformer Tr.1 through broadband amplifier 38. Terminal “b” of fourteen primary shells of transformer Tr.1 is grounded. Secondary winding 2 of transformer Tr.1 with terminal “c” is connected to the output of the radiation driver of radiation of secondary emitters 5, and terminal “d” of secondary winding 2 of transformer Tr.1 is grounded. The incoming induced EMF over fourteen channels by transformer Tr. 1 in the radiation information generator of secondary emitters 5 are summed. The need for summation allows you to create an overall picture of the radiation spectrum of secondary emitters with their subsequent separation during subsequent processing. Indeed, the studied object can emit polarized waves that are different from the excitation fields, so the summation will add the fields to the overall picture of different polarization, but the same frequency spectrum. This is the purpose of the shaper information radiation secondary emitters 5.

The output of the radiation information generator of the secondary emitters 5 is connected to the input of the frequency spectrum converter 6, in which the input of the frequency spectrum converter 6 is connected to its output through the first input of the converter 40 (Fig. 9), the second input of the converter 40 is connected to the output of the sinusoidal voltage generator 39. Purpose frequency converter 6 to spread the closely spaced frequencies of the secondary emitters for their recognition. Indeed, the frequency of the generator 39 is 10 kHz, therefore, adjacent frequencies after their conversion will have frequencies 10 kHz higher, therefore, the frequency can be detected in the secondary radiation mixture. In the case of a direct study of the radiation frequencies by secondary emitters, the spectrum analyzer in the indicator block 9 (Fig. 12) has the opportunity to turn off the frequency conversion through a detour using the switch to two switching positions: spectrum analysis using the frequency converter and without using it. To turn off the converter, the Bk.1 switch is put into the second position, while the input of the frequency spectrum converter 6 through the second terminals of the Bk.1 switch will be connected to the output of the frequency spectrum converter 6 and the frequency of the secondary radiation at the output will not undergo frequency conversion.

The output of the frequency spectrum converter 6 is connected to the input of the filter unit 7 (Fig. 10), the input of which is connected in parallel to ten frequency filters 41-1 to 41-10, the outputs of ten frequency filters through a narrow-band amplifier 4, in each of ten channels, are connected with ten outputs of the filter unit 7. Thus, the voltage of the mixture of frequencies of the radiation of the secondary emitters from the output of the Converter 6 is supplied to a system of ten filters that divide the frequency spectrum into ten channels. The first filter 41-1 allows the passage of frequencies from 1 to 10 kHz; the second filter 41-2 allows the passage of frequencies from 10 to 50 kHz; the third filter 41-3 skips frequencies from 50 to 100 kHz; the fourth filter 41-1 allows the passage of frequencies from 100 to 200 kHz; the fifth filter 41-5 passes frequencies from 200 to 400 kHz; the sixth filter 41-6 allows the passage of frequencies from 400 to 800 kHz; the seventh filter 41-7 allows the passage of frequencies from 800 to 1000 kHz; the eighth filter 41-8 passes frequencies from 1 to 10 MHz; the ninth filter 41-9 allows the passage of frequencies from 10 to 20 MHz; the tenth filter 41-10 skips frequencies from 20 to 40 MHz. Amplified by narrow-band amplifiers 42 in each frequency channel at the output of the filters are fed to the output of the filter unit 7.

на одну из пяти для полосы. Таким образом, в каждой колебательной системе полоса настройки образуется настройкой пяти мостовых схем на пять частот. Например, для первой полосы частот колебательной системы 43-1 с полосой 1-10 кГц (фиг.16), первый мост 1 настраивается для параллельных колебательных контуров на частоту 1,3 кГц, второй мост 2 настраивается для параллельных колебательных контуров на частоту 2,3 кГц, третий мост 3 настраивается для параллельных колебательных контуров на частоту 4,3 кГц, четвертый мост 4 настраивается для параллельных колебательных контуров на частоту 6,3 кГц, пятый мост 5 настраивается для параллельных колебательных контуров на частоту 8,3 кГц. Для второй полосы частот колебательной системы 43-2 с полосой 10-50 кГц (фиг.16), первый мост 1 настраивается для параллельных колебательных контуров на частоту 10,3 кГц, второй мост 2 настраивается для параллельных колебательных контуров на частоту 20,3 кГц, третий мост 3 настраивается для параллельных колебательных контуров на частоту 30,3 кГц, четвертый мост 4 настраивается для параллельных колебательных контуров на частоту 40,3 кГц, пятый мост 5 настраивается для параллельных колебательных контуров на частоту 50,3 кГц. Для третьей полосы частот колебательной системы 43-3 с полосой 50-100 кГц (фиг.16), первый мост 1 настраивается для параллельных колебательных контуров на частоту 55,3 кГц, второй мост 2 настраивается для параллельных колебательных контуров на частоту 65,3 кГц, третий мост 3 настраивается для параллельных колебательных контуров на частоту 75,3 кГц, четвертый мост 4 настраивается для параллельных колебательных контуров на частоту 85,3 кГц, пятый мост 5 настраивается для параллельных колебательных контуров на частоту 95,3 кГц. Для четвертой полосы частот колебательной системы 43-4 с полосой - 100-200 кГц (фиг.16), первый мост 1 настраивается для параллельных колебательных контуров на частоту 110,3 кГц, второй мост 2 настраивается для параллельных колебательных контуров на частоту 125,3 кГц, третий мост 3 настраивается для параллельных колебательных контуров на частоту 150,3 кГц, четвертый мост 4 настраивается для параллельных колебательных контуров на частоту 175,3 кГц, пятый мост 5 настраивается для параллельных колебательных контуров на частоту 195,3 кГц. Для пятой полосы частот колебательной системы 43-5 с полосой - 200-400 кГц (фиг.16), первый мост 1 настраивается для параллельных колебательных контуров на частоту 210,3 кГц, второй мост 2 настраивается для параллельных колебательных контуров на частоту 250,3 кГц, третий мост 3 настраивается для параллельных колебательных контуров на частоту 300,3 кГц, четвертый мост 4 настраивается для параллельных колебательных контуров на частоту 350,3 кГц, пятый мост 5 настраивается для параллельных колебательных контуров на частоту 395,3 кГц. Для шестой полосы частот колебательной системы 43-6 с полосой - 400-800 кГц (фиг.16), первый мост 1 настраивается для параллельных колебательных контуров на частоту 450,3 кГц, второй мост 2 настраивается для параллельных колебательных контуров на частоту 500,3 кГц, третий мост 3 настраивается для параллельных колебательных контуров на частоту 600,3 кГц, четвертый мост 4 настраивается для параллельных колебательных контуров на частоту 700,3 кГц, пятый мост 5 настраивается для параллельных колебательных контуров на частоту 795,3 кГц. Для седьмой полосы частот колебательной системы 43-7 с полосой - 800-1000 кГц (фиг.16), первый мост 1 настраивается для параллельных колебательных контуров на частоту 850,3 кГц, второй мост 2 настраивается для параллельных колебательных контуров на частоту 890,3 кГц, третий мост 3 настраивается для параллельных колебательных контуров на частоту 920,3 кГц, четвертый мост 4 настраивается для параллельных колебательных контуров на частоту 950,3 кГц, пятый мост 5 настраивается для параллельных колебательных контуров на частоту 995,3 кГц. Для восьмой полосы частот колебательной системы 43-8 с полосой - 1-10 МГц (фиг.16), первый мост 1 настраивается для параллельных колебательных контуров на частоту 2,3 МГц, второй мост 2 настраивается для параллельных колебательных контуров на частоту 4,3 МГц, третий мост 3 настраивается для параллельных колебательных контуров на частоту 6,3 МГц, четвертый мост 4 настраивается для параллельных колебательных контуров на частоту 8,3 МГц, пятый мост 5 настраивается для параллельных колебательных контуров на частоту 9,3 МГц. Для девятой полосы частот колебательной системы 43-9 с полосой - 10-20 МГц (фиг.16), первый мост 1 настраивается для параллельных колебательных контуров на частоту 12,3 МГц, второй мост 2 настраивается для параллельных колебательных контуров на частоту 14,3 МГц, третий мост 3 настраивается для параллельных колебательных контуров на частоту 16,3 МГц, четвертый мост 4 настраивается для параллельных колебательных контуров на частоту 18,3 МГц, пятый мост 5 настраивается для параллельных колебательных контуров на частоту 19,3 МГц. Для десятой полосы частот колебательной системы 43-10 с полосой - 20-40 МГц (фиг.16), первый мост 1 настраивается для параллельных колебательных контуров на частоту 22,3 МГц, второй мост 2 настраивается для параллельных колебательных контуров на частоту 27,3 МГц, третий мост 3 настраивается для параллельных колебательных контуров на частоту 33,3 МГц, четвертый мост 4 настраивается для параллельных колебательных контуров на частоту 35,3 МГц, пятый мост 5 настраивается для параллельных колебательных контуров на частоту 39,3 МГц. Таким образом, колебательная система позволяет обнаружить частоту вторичного излучения и усилить уровень напряжения в цепи за счет величины добротности колебательного контура моста для данной частоты вторичного излучения.Ten outputs of the filter unit 7 (Fig. 10) are connected to ten inputs of the analysis unit of the spectrum of secondary radiation 8. Ten inputs of the analysis unit of the spectrum of secondary radiation 8 are connected to the inputs of ten oscillatory systems (or circuits) from 43-1 to 43-10. The outputs of ten oscillatory systems are connected in parallel through a detector 44, in each of ten channels, with ten outputs from the first to tenth block of analysis of the spectrum of secondary radiation 8, as well as with ten outputs from the eleventh to twentieth block of analysis of the spectrum of secondary radiation 8. Thus, ten the outputs of ten parallel oscillatory circuits form in parallel ten outputs of the analysis unit 8 through ten detectors 44 and ten outputs of the analysis unit 8 directly connected to ten outputs of the oscillatory circuit but. The first oscillation system 43-1 is tuned to a frequency band from 1 to 10 kHz; the second system 43-2 is tuned to a frequency band from 10 to 50 kHz; the third system 43-3 is tuned to a frequency band from 50 to 100 kHz; the fourth system 43-4 is tuned to the frequency band from 100 to 200 kHz; the fifth system 43-5 is tuned to a frequency band from 200 to 400 kHz; the sixth system 43-6 is tuned to a frequency band from 400 to 800 kHz; the seventh system 43-7 is tuned to the frequency band from 800 to 1000 kHz; the eighth system 43-8 is tuned to the frequency band from 1 to 10 MHz; the ninth system 43-9 is tuned to the frequency band from 10 to 20 MHz; the tenth system 43-10 is tuned to the frequency band from 20 to 40 MHz. Moreover, the adjustment of the oscillatory system in each of the ten channels allows you to select the frequency of the secondary radiation. Oscillation system 43 (Fig.16) (there is a construction of oscillatory systems the same for all 43-1, 43-2, 43-3, 43-4, ..., 43-10), where 1, 2, 3, 4 and 5 are bridge the circuits shown in the figure below, with parallel oscillatory circuits in the shoulders of the bridge, tuned to five frequencies in the band of each oscillatory system from 43-1 to 43-10. Parallel oscillatory circuit formed by elements L and C with frequency tuning $$f=\mathrm{one}/\left(2\pi \sqrt{L\cdot C}\right)$$

one out of five for the strip. Thus, in each oscillatory system, a tuning band is formed by tuning five bridge circuits to five frequencies. For example, for the first frequency band of the oscillation system 43-1 with a band of 1-10 kHz (Fig. 16), the first bridge 1 is tuned for parallel oscillatory circuits to a frequency of 1.3 kHz, the second bridge 2 is tuned for parallel oscillatory circuits to a frequency of 2, 3 kHz, the third bridge 3 is tuned for parallel oscillatory circuits at a frequency of 4.3 kHz, the fourth bridge 4 is tuned for parallel oscillatory circuits at a frequency of 6.3 kHz, the fifth bridge 5 is tuned for parallel oscillatory loops at a frequency of 8.3 kHz. For the second frequency band of the oscillation system 43-2 with a band of 10-50 kHz (Fig. 16), the first bridge 1 is tuned for parallel oscillatory circuits to a frequency of 10.3 kHz, the second bridge 2 is tuned for parallel oscillatory circuits to a frequency of 20.3 kHz , the third bridge 3 is tuned for parallel oscillatory circuits at a frequency of 30.3 kHz, the fourth bridge 4 is tuned for parallel oscillatory circuits at a frequency of 40.3 kHz, the fifth bridge 5 is tuned for parallel oscillatory circuits at a frequency of 50.3 kHz. For the third frequency band of the oscillation system 43-3 with a band of 50-100 kHz (Fig. 16), the first bridge 1 is tuned for parallel oscillatory circuits to a frequency of 55.3 kHz, the second bridge 2 is tuned for parallel oscillatory circuits to a frequency of 65.3 kHz , the third bridge 3 is tuned for parallel oscillatory circuits at a frequency of 75.3 kHz, the fourth bridge 4 is tuned for parallel oscillatory circuits at a frequency of 85.3 kHz, the fifth bridge 5 is tuned for parallel oscillatory circuits at a frequency of 95.3 kHz. For the fourth frequency band of the oscillation system 43-4 with a band of 100-200 kHz (Fig. 16), the first bridge 1 is tuned for parallel oscillatory circuits to a frequency of 110.3 kHz, the second bridge 2 is tuned for parallel oscillatory circuits to a frequency of 125.3 kHz, the third bridge 3 is tuned for parallel oscillatory circuits to a frequency of 150.3 kHz, the fourth bridge 4 is tuned for parallel oscillatory circuits to a frequency of 175.3 kHz, the fifth bridge 5 is tuned for parallel oscillatory circuits to a frequency of 195.3 kHz. For the fifth frequency band of the oscillation system 43-5 with a band of 200-400 kHz (Fig. 16), the first bridge 1 is tuned for parallel oscillatory circuits to a frequency of 210.3 kHz, the second bridge 2 is tuned for parallel oscillatory circuits to a frequency of 250.3 kHz, the third bridge 3 is tuned for parallel oscillatory circuits to a frequency of 300.3 kHz, the fourth bridge 4 is tuned for parallel oscillatory circuits to a frequency of 350.3 kHz, the fifth bridge 5 is tuned for parallel oscillatory loops to a frequency of 395.3 kHz. For the sixth frequency band of the oscillation system 43-6 with a band of 400-800 kHz (Fig. 16), the first bridge 1 is tuned for parallel oscillatory circuits to a frequency of 450.3 kHz, the second bridge 2 is tuned for parallel oscillatory circuits to a frequency of 500.3 kHz, the third bridge 3 is tuned for parallel oscillatory circuits to a frequency of 600.3 kHz, the fourth bridge 4 is tuned for parallel oscillatory circuits to a frequency of 700.3 kHz, the fifth bridge 5 is tuned for parallel oscillatory loops to a frequency of 795.3 kHz. For the seventh frequency band of the oscillation system 43-7 with a band of 800-1000 kHz (Fig. 16), the first bridge 1 is tuned for parallel oscillatory circuits to a frequency of 850.3 kHz, the second bridge 2 is tuned for parallel oscillatory circuits to a frequency of 890.3 kHz, the third bridge 3 is tuned for parallel oscillatory circuits to a frequency of 920.3 kHz, the fourth bridge 4 is tuned for parallel oscillatory circuits to a frequency of 950.3 kHz, the fifth bridge 5 is tuned for parallel oscillatory circuits to a frequency of 995.3 kHz. For the eighth frequency band of the oscillation system 43-8 with a band of 1-10 MHz (Fig. 16), the first bridge 1 is tuned for parallel oscillatory loops to a frequency of 2.3 MHz, the second bridge 2 is tuned for parallel oscillatory loops to a frequency of 4.3 MHz, the third bridge 3 is tuned for parallel oscillatory circuits at a frequency of 6.3 MHz, the fourth bridge 4 is tuned for parallel oscillatory circuits at a frequency of 8.3 MHz, the fifth bridge 5 is tuned for parallel oscillatory loops at a frequency of 9.3 MHz. For the ninth frequency band of the oscillation system 43-9 with a band of 10-20 MHz (Fig. 16), the first bridge 1 is tuned for parallel oscillatory circuits to a frequency of 12.3 MHz, the second bridge 2 is tuned for parallel oscillatory circuits to a frequency of 14.3 MHz, the third bridge 3 is tuned for parallel oscillatory circuits at a frequency of 16.3 MHz, the fourth bridge 4 is tuned for parallel oscillatory circuits at a frequency of 18.3 MHz, the fifth bridge 5 is tuned for parallel oscillatory loops at a frequency of 19.3 MHz. For the tenth frequency band of the oscillation system 43-10 with a band of 20-40 MHz (Fig. 16), the first bridge 1 is tuned for parallel oscillatory circuits to a frequency of 22.3 MHz, the second bridge 2 is tuned for parallel oscillatory circuits to a frequency of 27.3 MHz, the third bridge 3 is tuned for parallel oscillatory circuits at a frequency of 33.3 MHz, the fourth bridge 4 is tuned for parallel oscillatory circuits at a frequency of 35.3 MHz, the fifth bridge 5 is tuned for parallel oscillatory loops at a frequency of 39.3 MHz. Thus, the oscillatory system allows you to detect the frequency of the secondary radiation and increase the voltage level in the circuit due to the value of the Q factor of the oscillatory circuit of the bridge for a given frequency of secondary radiation.

The outputs from the first to the tenth analysis block 8 (Fig. 11) with ten outputs of the oscillatory circuits are made through a detector in each channel, which allows to obtain a signaling voltage indicating the presence of a secondary emitter frequency in a given frequency band and to perform a spectral analysis of this channel according to the channel number using a spectrum analyzer through the outputs from the eleventh to twentieth analysis unit 8 (Fig.11). An indicator 45 of the presence of a voltage level at the output of the detector 44, in each of ten channels, is located in the block of indicators of the radiation spectrum 9. By signaling, for example, a lit LED, the channel number is set in which the secondary radiation frequency is present. Using the switch 47 to ten positions connect one of the inputs, from the eleventh to the twentieth, the installed channel to the spectrum analyzer 46 and study the frequency spectrum in a given frequency band. If several emission bands are detected, then all the bands detected by the LEDs are subject to investigation by the spectrum analyzer.

The authors are not aware of technical solutions from the field of radio communications containing features equivalent to the distinguishing features of the claimed device. The authors are not aware of technical solutions from other technical fields having the properties of the claimed technical object of the invention. Thus, the claimed technical solution, according to the authors, has the criterion of essential features.

Claims (11)

1. The control device of the electromagnetic field of the secondary emitters, containing a clock pulse generator and a radiation spectrum shaper, characterized in that an antenna switch, a transceiver antenna system, a secondary radiation emitter information generator, a frequency spectrum converter, a filter unit, a radiation spectrum analysis unit are additionally introduced , a block of indicators of the spectrum of the secondary radiation, while the output of the clock generator is connected to the input of the shaper of the radiation spectrum; fourteen outputs of the radiation spectrum shaper are connected to fourteen inputs of the antenna switch; fourteen outputs-inputs of the antenna switch, from the first to the fourteenth, connected in parallel with fourteen inputs-outputs of the four transceiver antenna systems; fourteen outputs of the antenna switch, from the fifteenth to the twenty-eighth, are connected to fourteen inputs of the radiation information generator of the secondary emitters; the output of the information generator is connected through the frequency spectrum converter, through ten outputs of the filter block with ten inputs of the secondary radiation spectrum analysis block; ten outputs of the analysis unit are connected to ten inputs of the radiation spectrum indicator block. 2. The electromagnetic field control device of the secondary emitters according to claim 1, characterized in that the radiation spectrum shaper comprises a first trigger, element I, fourteen discrete delay lines for 20 ms, a collective line with terminals 1, 2 and 3, a first generator for generating a packet of two pulses of 1 μs A1, consisting of: the first and second valves, the first discrete delay line for 1 μs; a second generator for generating a packet of two pulses of 10 μs A2 each, consisting of: the third and fourth gates, the second discrete delay line for 10 ms, the third discrete delay line for 10 μs and the second trigger 13 for 10 μs; a third generator for generating a packet of two pulses of 100 μs A3 each, consisting of: the fifth and sixth gates, the fourth discrete delay line for 10 ms, the fifth discrete delay line for 100 μs and the third trigger for 100 μs; pulse switch A4, consisting of: the fifteenth switch (Vk.15) for two switching positions and fourteen channels, and each channel has its own switch (from Vk.1 to Vk.14) for four positions, for four operating modes, in thirteen channels Starting from the second to the fourteenth, each channel has its own channels — a switch, a valve, and two discrete delay lines; the first input of the radiation spectrum shaper is connected to the second input of the And element, and the first input of the And element is connected to the first input of the radiation spectrum shaper through the short-circuit terminals “a” and “b” of the sixteenth switch (Start) and through the first trigger 11; the output of the element And is connected in parallel with the inputs of the first A1 and second A2 pulse packet generators; the input of the first packet generator of two pulses of 1 μs A1 is connected to the output in parallel through the second valve, as well as through the first valve and through the first delay line by 1 μs, the output of the first generator A1 is connected to the first terminal of the collective line; the input of the second packet generator of two pulses of 10 μs A2 is connected to the second trigger through the second discrete delay line for 10 ms, the output of the second trigger is connected to the output of the second packet generator through the third gate, through the third discrete delay line by 10 μs and in parallel through the fourth valve , the output of the second packet generator of two pulses of 10 μs A2 is connected to the second terminal of the collective line and in parallel with the input of the third packet generator of two pulses of 100 μs A3; the input of the third packet generator of two pulses of 100 μs A3 is connected to the third trigger through the fourth discrete delay line for 10 ms, the output of the third trigger is connected to the output of the third generator through the fifth valve, through the fifth discrete delay line by 100 μs and in parallel through the sixth valve, output a third packet generator of two pulses of 100 μs is connected to the third terminal of the collecting line; input pulse switch A4 is connected to a collective line; the input of the pulse switch A4 is connected in parallel with the fourteen outputs of the radiation spectrum shaper through fourteen channels: in the first channel, the input of the pulse switch is connected in parallel to the fourth, to the third terminals of the first switch directly, and to the second terminal of the first switch through the second terminal of the fifteenth switch in two positions ( two positions at which the second terminal is turned on or the second terminal is turned off from the input of the switch), the second terminal of the first switch is connected in parallel to the second glue mam all thirteen switches, the zero terminal of a first switch coupled to the first output of the radiation spectrum; in the second channel, the input of the A4 pulse switch is connected in parallel to the fourth terminal of the second switch through the seventh valve, through the sixth discrete delay line for 10 ms and through the seventh discrete delay line for 20 ms, and to the third terminal of the second switch through the seventh valve and through the sixth line discrete delay for 10 ms, the zero terminal of the second switch is connected to the second output of the radiation spectrum shaper; in the third channel, the input of the A4 pulse switch is connected in parallel to the fourth terminal of the third switch through the eighth valve, through the eighth discrete delay line for 20 ms and through the ninth discrete delay line for 20 ms, and to the third terminal of the third switch through the eighth valve and through the ninth line discrete delay for 20 ms, the zero terminal of the third switch is connected to the third output of the radiation spectrum shaper; in the fourth channel, the input of the A4 pulse switch is connected in parallel to the fourth terminal of the fourth switch through the ninth valve, through the tenth discrete delay line for 30 ms and through the eleventh discrete delay line for 20 ms, and to the third terminal of the fourth switch through the ninth valve and through the tenth line discrete delay for 30 ms, the zero terminal of the fourth switch is connected to the fourth output of the radiation spectrum shaper; in the fifth channel, the input of the pulse switch A4 is connected in parallel to the fourth terminal of the fifth switch through the tenth valve, through the twelfth discrete delay line for 40 ms and through the thirteenth discrete delay line for 20 ms, and to the third terminal of the fifth switch through the tenth valve and through the twelfth line discrete delay for 40 ms, the zero terminal of the fifth switch is connected to the fifth output of the radiation spectrum shaper; in the sixth channel, the input of the A4 pulse switch is connected in parallel to the fourth terminal of the sixth switch through the eleventh valve, through the fourteenth discrete delay line for 50 ms and through the fifteenth discrete delay line for 20 ms, and to the third terminal of the sixth switch through the eleventh valve and through the fourteenth line discrete delay of 50 ms, the zero terminal of the sixth switch is connected to the sixth output of the radiation spectrum shaper; in the seventh channel, the input of the pulse switch A4 is connected in parallel to the fourth terminal of the seventh switch via the twelfth gate, through the sixteenth discrete delay line for 60 ms and through the seventeenth discrete delay line for 20 ms, and to the third terminal of the seventh switch through the twelfth gate and through the sixteenth line discrete delay for 60 ms, the zero terminal of the seventh switch is connected to the seventh output of the radiation spectrum shaper; in the eighth channel, the input of the pulse switch A4 is connected in parallel to the fourth terminal of the eighth switch through the thirteenth gate, through the eighteenth discrete delay line for 70 ms and through the nineteenth discrete delay line for 20 ms, and to the third terminal of the eighth switch through the thirteenth gate and through the eighteenth line discrete delay for 70 ms, the zero terminal of the eighth switch is connected to the eighth output of the radiation spectrum shaper; in the ninth channel, the input of the A4 pulse switch is connected in parallel to the fourth terminal of the ninth switch through the fourteenth gate, through the twentieth discrete delay line for 80 ms and through the twenty-first discrete delay line for 20 ms, and to the third terminal of the ninth switch through the fourteenth gate and through the twentieth discrete delay line for 80 ms, the zero terminal of the ninth switch is connected to the ninth output of the radiation spectrum shaper; in the tenth channel, the input of the pulse switch A4 is connected in parallel to the fourth terminal of the tenth switch through the fifteenth valve, through the twenty-second discrete delay line for 90 ms and through the twenty-third discrete delay line for 20 ms, and to the third terminal of the tenth switch through the fifteenth valve and through twenty-second line of discrete delay for 90 ms, the zero terminal of the tenth switch is connected to the tenth output of the shaper of the radiation spectrum; in the eleventh channel, the input of the pulse switch A4 is connected in parallel to the fourth terminal of the eleventh switch through the sixteenth valve, through the twenty-fourth discrete delay line for 100 ms and through the twenty-fifth discrete delay line for 20 ms, and to the third terminal of the eleventh switch through the sixteenth valve and through the twenty-fourth line of discrete delay for 100 ms, the zero terminal of the eleventh switch is connected to the eleventh output of the shaper of the radiation spectrum; in the twelfth channel, the input of the pulse switch A4 is connected in parallel to the fourth terminal of the twelfth switch through the seventeenth valve, through the twenty-sixth discrete delay line for 110 ms and through the twenty-seventh discrete delay line for 20 ms, and to the third terminal of the twelfth switch through the seventeenth valve and through the twenty-sixth line of a discrete delay of 110 ms, the zero terminal of the twelfth switch is connected to the twelfth output of the radiation spectrum shaper; in the thirteenth channel, the input of the pulse switch A4 is connected in parallel to the fourth terminal of the thirteenth switch through the eighteenth gate, through the twenty-eighth discrete delay line for 120 ms and through the twenty-ninth discrete delay line for 20 ms, and to the third terminal of the thirteenth switch through the eighteenth gate and through twenty-eighth line of discrete delay for 120 ms, the zero terminal of the thirteenth switch is connected to the thirteenth output of the radiation spectrum shaper; in the fourteenth channel, the input of the A4 pulse switch is connected in parallel to the fourth terminal of the fourteenth switch through the nineteenth valve, through the thirty discrete delay line for 130 ms and through the thirty-first discrete delay line for 20 ms, and to the third terminal of the fourteenth switch through the nineteenth valve and through the thirty discrete delay line for 130 ms, the zero terminal of the fourteenth switch is connected to the fourteenth output of the radiation spectrum shaper, in parallel the zero terminal of the fourteenth lyuchatelya connected through the thirty-second line of discrete delay of 20 ms to the input of the first flip-flop; the second terminals of all fourteen switches are connected to the zero terminal of the fifteenth switch; the first terminals of all fourteen switches are free and designed to disconnect the selected channel from the collective line and from the generators. 3. The control device of the electromagnetic field of the secondary emitters according to claim 2, characterized in that the antenna switch contains: fourteen receiving diode-capacitive bridges, fourteen transmitting diode-capacitive bridges and a control unit for the receiving-transmitting antenna system, with fourteen inputs from the first to the fourteenth antenna switch is connected in parallel with the second inputs of the fourteen transmitting diode-capacitive bridges, and the first inputs of the fourteen transmitting diode-capacitive bridges are connected in parallel with the second the output of the control unit of the transceiver antenna system; the outputs of fourteen transmitting diode-capacitive bridges are connected in parallel with the second inputs of fourteen receiving diode-capacitive bridges and with fourteen inputs-outputs from the first to fourteenth antenna switch; the first inputs of fourteen receiving diode-capacitive bridges are connected in parallel with the first output of the control unit of the transceiver antenna system; the outputs of fourteen receiving diode-capacitive bridges are connected in parallel with fourteen outputs starting from the fifteenth to twenty-eighth antenna switch; the first channel is formed by a connection - the first input of the antenna switch is connected in parallel with the first input of the control unit of the transceiver antenna system and with the second input of the transmitting diode-capacitive bridge, and the first input of the bridge is connected with the second output of the control unit of the transceiver antenna system, the output of the transmitting diode the capacitive bridge of the first channel is connected in parallel with the first input-output of the antenna switch, and through the second input of the receiving diode-capacitive bridge with the fifteenth output of the antenna switch, th input of the receiver diode-bridge capacitor connected to the first output of the control unit transceiver antenna system; the second channel - the second input of the antenna switch is connected in parallel with the second input of the control unit of the transceiver antenna system and with the second input of the transmitting diode-capacitive bridge, and the first input of the transmitting bridge is connected with the second output of the control unit of the transceiver antenna system, the output of this transmitting bridge connected in parallel with the second input-output of the antenna switch, and through the second input of the receiving diode-capacitive bridge with the sixteenth output of the antenna switch, the first input of this receiving bridge is connected nen with the first output of the control unit of the transceiver antenna system; the third channel - the third input of the antenna switch is connected in parallel with the third input of the control unit of the transceiver antenna system and with the second input of the transmitting diode-capacitive bridge, and the first input of this transmitting bridge is connected to the second output of the control unit of the transceiver antenna system, the output of the transmitting bridge connected in parallel with the third input-output of the antenna switch, and through the second input of the receiving diode-capacitive bridge with the seventeenth output of the antenna switch, the first input of the receiving bridge is connected to rvym output control unit transceiver antenna system; fourth channel - the fourth input of the antenna switch is connected in parallel with the fourth input of the control unit of the transceiver antenna system and with the second input of the transmitting diode-capacitive bridge, and the first input of this transmitting bridge is connected to the second output of the control unit of the transceiver antenna system, the output of the transmitting bridge connected in parallel with the fourth input-output of the antenna switch, and through the second input of the receiving diode-capacitive bridge with the eighteenth output of the antenna switch, the first input of this receiving the bridge is connected to the first output of the control unit of the transceiver antenna system; fifth channel - the fifth input of the antenna switch is connected in parallel with the fifth input of the control unit of the transceiver antenna system and with the second input of the transmitting diode-capacitive bridge, and the first input of this transmitting bridge is connected to the second output of the control unit of the transceiver antenna system, the output of the transmitting bridge connected in parallel with the fifth input-output of the antenna switch, and through the second input of the receiving diode-capacitive bridge with the nineteenth output of the antenna switch, the first input of this receiving bridge is connected to the first output of the control unit of the transceiver antenna system; sixth channel - the sixth input of the antenna switch is connected in parallel with the sixth input of the control unit of the transceiver antenna system and with the second input of the transmitting diode-capacitive bridge, and the first input of this transmitting bridge is connected to the second output of the control unit of the transceiver antenna system, the output of this transmitting the bridge is connected in parallel with the sixth input-output of the antenna switch, and through the second input of the receiving diode-capacitive bridge with the twentieth output of the antenna switch, the first input of this receiving bridge is connected nen to the first output of the control unit transceiver antenna system; seventh channel - the seventh input of the antenna switch is connected in parallel with the seventh input of the control unit of the transceiver antenna system and with the second input of the transmitting diode-capacitive bridge, and the first input of this transmitting bridge is connected to the second output of the control unit of the transceiver antenna system, the output of this transmitting the bridge is connected in parallel with the seventh input-output of the antenna switch, and through the second input of the receiving diode-capacitive bridge with the twenty-first output of the antenna switch, the first input of this receiving osta connected to the first output of the control unit transceiver antenna system; eighth channel - the eighth input of the antenna switch is connected in parallel with the eighth input of the control unit of the transceiver antenna system and with the second input of the transmitting diode-capacitive bridge, and the first input of this transmitting bridge is connected to the second output of the control unit of the transceiver antenna system, the output of this transmitting the bridge is connected in parallel with the eighth input-output of the antenna switch, and through the second input of the receiving diode-capacitive bridge with twenty-second output of the antenna switch, the first input of this receiving osta connected to the first output of the control unit transceiver antenna system; the ninth channel - the ninth input of the antenna switch is connected in parallel with the ninth input of the control unit of the transceiver antenna system and with the second input of the transmitting diode-capacitive bridge, and the first input of this transmitting bridge is connected to the second output of the control unit of the transceiver antenna system, the output of this transmitting the bridge is connected in parallel with the ninth input-output of the antenna switch, and through the second input of the receiving diode-capacitive bridge with the twenty-third output of the antenna switch, the first input of this receiving the bridge is connected to the first output of the control unit of the transceiver antenna system; tenth channel - the tenth input of the antenna switch is connected in parallel with the tenth input of the control unit of the transceiver antenna system and with the second input of the transmitting diode-capacitive bridge, and the first input of this transmitting bridge is connected to the second output of the control unit of the transceiver antenna system, the output of this transmitting the bridge is connected in parallel with the tenth input-output of the antenna switch, and through the second input of the receiving diode-capacitive bridge with the twenty-fourth output of the antenna switch, the first input of this th bridge is connected to the first output of the control unit of the transceiver antenna system; eleventh channel - the eleventh input of the antenna switch is connected in parallel with the eleventh input of the control unit of the transceiver antenna system and with the second input of the transmitting diode-capacitive bridge, and the first input of this transmitting bridge is connected to the second output of the control unit of the transceiver antenna system, the output of this transmitting the bridge is connected in parallel with the eleventh input-output of the antenna switch, and through the second input of the receiving diode-capacitive bridge with the twenty-fifth output of the antenna switch, the first the course of this receiving bridge is connected to the first output of the control unit of the transceiver antenna system; the twelfth channel - the twelfth input of the antenna switch is connected in parallel with the twelfth input of the control unit of the transceiver antenna system and with the second input of the transmitting diode-capacitive bridge, and the first input of this transmitting bridge is connected to the second output of the control unit of the transceiver antenna system, the output of this transmitting the bridge is connected in parallel with the twelfth input-output of the antenna switch, and through the second input of the receiving diode-capacitive bridge with the twenty-sixth output of the antenna switch, the first input this receiving bridge is connected to the first output of the control unit of the transceiver antenna system; thirteenth channel - the thirteenth input of the antenna switch is connected in parallel with the thirteenth input of the control unit of the transceiver antenna system and the second input of the transmitting diode-capacitive bridge, and the first input of this transmitting bridge is connected to the second output of the control unit of the transceiver antenna system, the output of this transmitting the bridge is connected in parallel with the thirteenth input-output of the antenna switch, and through the second input of the receiving diode-capacitive bridge with the twenty-seventh output of the antenna switch, the first input d of this receiving bridge is connected to the first output of the control unit of the transceiver antenna system; fourteenth channel - the fourteenth input of the antenna switch is connected in parallel with the fourteenth input of the control unit of the transceiver antenna system and the second input of the transmitting diode-capacitive bridge, and the first input of this transmitting bridge is connected to the second output of the control unit of the transceiver antenna system, the output of this transmitting the bridge is connected in parallel with the fourteenth input-output of the antenna switch, and through the second input of the receiving diode-capacitive bridge with the twenty-eighth output of the antenna switch, rvy receiver input of this bridge is coupled to the first output of the control unit transceiver antenna system. 4. The control device of the electromagnetic field of the secondary emitters according to claim 3, characterized in that the control unit of the transceiver antenna system contains a transformer Tr-1 with fourteen primary and two sections of the secondary windings, two voltage amplifiers, an element NOT, two valves; while fourteen inputs of the control unit of the transceiver antenna system are connected in parallel with terminal “a” of the fourteen primary windings of the transformer, and terminal “b” of the fourteen primary windings of the transformer is grounded; two sections of the secondary winding are grounded at point “0”, and the terminals of sections “c” and “d” form two outputs of the control unit of the transceiver antenna system, terminal “c” of the first section of the secondary winding is connected to the first output of the unit through a valve and voltage amplifier control the transceiver antenna system, and terminal “d” of the second section of the secondary winding of the transformer through the valve, the element NOT and the voltage amplifier is connected to the second output of the control unit of the transceiver antenna system. 5. The control device of the electromagnetic field of the secondary emitters according to claim 4, characterized in that the receiving diode-capacitive bridge and the transmitting diode-capacitive bridge contain the same elements: two resistors (R ₁ and R ₂ are high-resistance active, with a resistance of at least 100 MΩ ), two valves, two tanks (C ₁ and C ₂ ), while the first input of the diode-capacitive bridge is connected in parallel to the diagonal of the bridge, to points “a” and “b”, so the first bridge input is connected through the first active resistance R ₁ to the point "a", and through the second active resistance R ₂ to the point "b"; the second input of the diode-capacitive bridge is connected to point “d”, point “d” is connected to point “c” in parallel in two circuits: the first through the second tank and the first valve, and the second through the second valve and the first tank; point "c" is connected to the output of the diode-capacitive bridge. 6. The control device of the electromagnetic field of the secondary emitters according to claim 4, characterized in that the transceiver antenna system contains fourteen transceiver antennas arranged in a circle and fourteen capacities, while on the one hand each of the fourteen transceiver antennas is connected with one of the fourteen inputs of the transceiver antenna system, and on the other hand, each of the fourteen antennas is connected to a grounded load capacity - $$C_{N\mathrm{BUT}G}^{\mathrm{one}}$$

, $$C_{N\mathrm{BUT}G}^2$$

, $$C_{N\mathrm{BUT}G}^3$$

, $$C_{N\mathrm{BUT}G}^{\mathrm{four}}$$

, $$C_{N\mathrm{BUT}G}^5$$

, $$C_{N\mathrm{BUT}G}^6$$

, $$C_{N\mathrm{BUT}G}^7$$

, $$C_{N\mathrm{BUT}G}^8$$

, $$C_{N\mathrm{BUT}G}^9$$

, $$C_{N\mathrm{BUT}G}^{\mathrm{one}0}$$

, $$C_{N\mathrm{BUT}G}^{\mathrm{one}\mathrm{one}}$$

, $$C_{N\mathrm{BUT}G}^{\mathrm{one}2}$$

, $$C_{N\mathrm{BUT}G}^{\mathrm{one}3}$$

, $$C_{N\mathrm{BUT}G}^{\mathrm{one}\mathrm{four}}$$

. 7. The control device of the electromagnetic field of the secondary emitters according to claim 5, characterized in that the shaper of radiation information of the secondary emitters comprises a transformer with fourteen primary windings and one secondary winding, a broadband amplifier, while fourteen inputs of the shaper of radiation information of the secondary emitters form fourteen parallel independent channels , in each of the fourteen channels, the input of the radiation information generator of the secondary emitters is connected through its own in each channel, a broadband amplifier with terminal “a” of the transformer primary winding, and terminal “b” in each of the fourteen primary transformer windings is grounded; the output of the radiation emitter of the secondary emitters is connected to the terminal “c” of the secondary winding of the transformer, and the terminal “d” of the secondary winding of the transformer is grounded. 8. The control device of the electromagnetic field of the secondary emitters according to claim 6, characterized in that the frequency spectrum converter comprises a 10 kHz generator, a mixer, a two-position switch, wherein the input of the frequency spectrum converter is connected to the output of the frequency spectrum converter in parallel through the first switch terminal and the first input of the mixer, and also through the second terminal of the switch directly, the second input of the mixer is connected to the output of the generator. 9. The control device of the electromagnetic field of the secondary emitters according to claim 7, characterized in that the filter unit contains ten channels, in each channel: a narrow-band filter and narrow-band amplifiers, while the input of the filter unit to ten channels is connected in parallel with ten inputs of ten filters; the output of the first filter with a bandwidth of 1 kHz to 10 kHz is connected to the first output of the filter unit through a narrow-band amplifier; the output of the second filter with a bandwidth of 10 kHz to 50 kHz is connected to the second output of the filter unit through a narrow-band amplifier; the output of the third filter with a passband from 50 kHz to 100 kHz is connected to the third output of the filter unit through a narrow-band amplifier; the output of the fourth filter with a passband from 100 kHz to 200 kHz is connected to the fourth output of the filter unit through a narrow-band amplifier; the output of the fifth filter with a bandwidth of 200 kHz to 400 kHz is connected to the fifth output of the filter unit through a narrow-band amplifier; the output of the sixth filter with a passband from 400 kHz to 800 kHz is connected to the sixth output of the filter unit through a narrow-band amplifier; the output of the seventh filter with a bandwidth of 800 kHz to 1000 kHz is connected to the seventh output of the filter unit through a narrow-band amplifier; the output of the eighth filter with a bandwidth of 1.0 MHz to 10 MHz is connected to the eighth output of the filter unit through a narrow-band amplifier; the output of the ninth filter with a bandwidth of 10 MHz to 20 MHz is connected to the ninth output of the filter unit through a narrow-band amplifier; the output of the tenth filter with a bandwidth of 20 MHz to 40 MHz is connected to the tenth output of the filter block through a narrow-band amplifier. 10. The control device of the electromagnetic field of the secondary emitters of claim 8, characterized in that the analyzer of the spectrum of the secondary radiation into ten channels contains ten channels, in each channel an oscillatory system with a given frequency band and detector, while the first input of the analyzer is connected to the input of the first oscillatory systems with a frequency band from 1 kHz to 10 kHz, the output of the first oscillatory system is connected to the eleventh output of the analyzer, and in parallel with the first output of the analyzer through the first detector; the second input of the analyzer is connected to the input of the second oscillatory system with a frequency band from 10 kHz to 50 kHz, the output of the second oscillatory system is connected to the twelfth output of the analyzer, and in parallel with the second output of the analyzer through a second detector; the third input of the analyzer is connected to the input of the third oscillatory system with a frequency band from 50 kHz to 100 kHz, the output of the third oscillatory system is connected to the thirteenth output of the analyzer, and in parallel with the third output of the analyzer through a third detector; the fourth input of the analyzer is connected to the input of the fourth oscillatory system with a frequency band from 100 kHz to 200 kHz, the output of the fourth oscillatory system is connected to the fourteenth output of the analyzer, and in parallel with the fourth output of the analyzer through the fourth detector; the fifth input of the analyzer is connected to the input of the fifth oscillatory system with a frequency band from 200 kHz to 400 kHz, the output of the fifth oscillatory system is connected to the fifteenth output of the analyzer, and in parallel with the fifth output of the analyzer through the fifth detector; the sixth input of the analyzer is connected to the input of the sixth oscillatory system with a frequency band from 400 kHz to 800 kHz, the output of the sixth oscillatory system is connected to the sixteenth output of the analyzer, and in parallel with the sixth output of the analyzer through the sixth detector; the seventh input of the analyzer is connected to the input of the seventh oscillatory system with a frequency band from 800 kHz to 1000 kHz, the output of the seventh oscillatory system is connected to the seventeenth output of the analyzer, and in parallel with the seventh output of the analyzer through the seventh detector; the eighth input of the analyzer is connected to the input of the eighth oscillatory system with a frequency band from 1 MHz to 10 MHz, the output of the eighth oscillatory system is connected to the eighteenth output of the analyzer, and in parallel with the eighth output of the analyzer through the eighth detector; the ninth input of the analyzer is connected to the input of the ninth oscillatory system with a frequency band from 10 MHz to 20 MHz, the output of the ninth oscillatory system is connected to the nineteenth output of the analyzer, and in parallel with the ninth output of the analyzer through the ninth detector; the tenth input of the analyzer is connected to the input of the tenth oscillatory system with a frequency band from 20 MHz to 40 MHz, the output of the tenth oscillatory system is connected to the twentieth output of the analyzer, and in parallel with the tenth output of the analyzer through the tenth detector; each of ten oscillatory systems contains five bridges connected in parallel to the input-output of the oscillating system, each bridge contains a parallel oscillatory circuit in four arms, the first diagonal of the bridge is connected to the input of the output of the system on one side, and is grounded on the other, and a high-resistance resistance is included in the second diagonal . 11. The monitoring device of the electromagnetic field of the secondary emitters according to claim 9, characterized in that the block of indicators of the spectrum of radiation contains ten voltage indicators for ten channels, a spectrum analyzer and a switch for ten positions of inclusion, while ten inputs of the block of indicators of the spectrum of radiation from the first to tenth connected to the inputs of ten voltage indicators (as an indicator you can use: a voltmeter, LED, incandescent lamp and any signaling device for the presence of voltage), and ten inputs from fifteen of the twentieth block of indicators of the spectrum of radiation are connected in parallel to the terminals “a” of the switch for ten switching positions, and the terminals “b” of the switch are connected to the input of the spectrum analyzer.

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