RU183683U1 - TECHNICAL EXPLORATION BATTLE MACHINE - Google Patents

Abstract

The utility model relates to the field of military equipment, namely, to a technical reconnaissance fighting vehicle based on a protected vehicle, which can be widely used for the technical reconnaissance of damaged weapons and military equipment necessary for organizing technical support. The technical result of this utility model is optical, engineering and radiation reconnaissance of the combat area. The specified technical result is achieved due to the fact that the combat vehicle is technical reconnaissance, which is a car with the ability to protect the crew in the inhabited compartment of the main systems and assemblies from the effects of damaging facts of weapons on it, it contains an electric power supply system, a life support system, an on-board information and control system, an optical-electronic system, a radiation reconnaissance complex, a radio-controlled explosive device interlock, a television viewing device, projector lighting system.

Description

The utility model relates to the field of military equipment, namely to a technical reconnaissance fighting vehicle based on a protected vehicle, which can be widely used for technical reconnaissance of damaged weapons and military equipment necessary for organizing technical support.

An analysis of the nature and content of recent armed conflicts, the forms and methods of warfare at various theaters of military operations of the Ground Forces of the Ministry of Defense of the Russian Federation showed that modern combat operations require high mobility, tactical and operational independence of units and units.

The implementation of the brigade principle of manning the Ground Forces, based on the use of advanced weapons and military equipment (IWT), increasing the maneuverability and speed of combat operations determine the need to reduce the duration of military repairs of the IWT. Reducing the duration of the repair of military equipment can be achieved in the repair and reconstructive bodies (RVO) of the Ground Forces by the timely collection, analysis, generalization and transmission of data necessary for the organization of tank and auto-technical support of subunits and units, which is possible only using modern specialized means of technical intelligence.

At present, the technical intelligence in the units and formations of the Ground Forces has been entrusted with the guiding documents to the following military units: technical intelligence groups (GTR); evacuation groups (EG); repair and evacuation groups (REG) and repair groups (RemG).

To date, there are no specialized technical reconnaissance vehicles developed and adopted in accordance with the established procedure for the supply of the Ministry of Defense of the Russian Federation on protected vehicles.

The development of a technical reconnaissance combat vehicle will increase the efficiency of tank and auto-technical support of units and units in combat operations, reduce the time for returning weapons and military equipment to service, increase the staffing ratio of operational combat vehicles of combat units and, as a result, increase their level of combat readiness.

Known military service reconnaissance vehicle (SBRM) described in the magazine of the military-industrial complex "Military Parade", No. 2 (PO) March - April 2012, LLC "Military Parade", p. 16-20. The composition of the SBRM product: on-board information management system; optoelectronic system; remote-controlled weapons platform; ground reconnaissance radar; direction finder; acoustic shot detection system (shooter position determination); reconnaissance complex based on a remotely piloted aircraft; complex reconnaissance and signaling equipment; lifting mast; radio communication system; navigation system; power supply system; radio blasting device blocker; base chassis.

The disadvantages of the well-known RBM are the lack of means for detecting mine explosive obstacles, the low noise immunity of navigation equipment and, as a result, the inability to work in conditions of the use of electronic suppression by the enemy, the lack of identification of all crew members at the beginning of a work session with automated workstations.

A well-known reconnaissance vehicle (Engineering troops: Photo album - M .: Edition UNIV MO RF, 1998, 72 pp.) Performed on a tracked chassis, armored, floating. It can obtain data on the nature of the terrain, water barriers and troop movement paths, as well as on the presence of mine-explosive barriers on them.

The well-known engineering reconnaissance vehicle has low survivability, since with combat damage there is a high probability of death of the crew and the machine itself, as well as performance, since it can perform only one of the presented tasks.

Known articulated engineering reconnaissance vehicle described in the patent of the Russian Federation No. 2205351 from 11/14/2001. An articulated engineering reconnaissance vehicle contains three armored self-propelled sections. One section is the central one, placed between two motor-transmission sections in a suspended state by means of an automatic coupling device. All of these sections are made floating, with each engine-transmission section equipped with a remote device with a wide-range mine detector and a rutting mine trawl. The front engine-transmission section has a wide-angle mine detector main control panel, and the rear one has a duplicate control panel. The central section contains the compartments of the control and operator of an engineering reconnaissance echo sounder with reconnaissance, surveillance and orientation instruments.

The disadvantage of a joint engineering reconnaissance vehicle is: low noise immunity of navigation equipment, which does not allow working under conditions of the enemy using electronic jamming; low maneuverability in combat conditions and, as a result, low survivability due to the absence of a jammer of radio-controlled explosive devices designed to block the radio frequencies of explosive devices.

Known armored reconnaissance and patrol vehicle BRDM-2 (Combat reconnaissance and patrol vehicle BRDM-2. Technical description and operating instructions. Part 1. Moscow. Military publishing house, 1987. Open edition).

BRDM-2 contains a protected housing, instrumentation, a radio station, surveillance devices.

Shortcomings of the BRDM-2: low security, armor protects against bullets of small arms and fragments; the impossibility of determining the geographical coordinates of the location of the BRDM-2; lack of funds display with electronic navigation map; the lack of computing tools for the installation of a combat geographic information system (GIS) and, as a result, low situational awareness of crew members when performing combat missions; there is no life support system providing air conditioning of the inhabited compartment; low maneuverability in combat damage to armored glass due to the lack of a television viewing device; there is no complex detection of mine-explosive barriers.

The Typhoon protected vehicle is described in the Military Parade magazine of military-industrial complex, No. 2 (110) March-April 2012, Military Parade LLC, p. 21. The composition of the product "Typhoon": on-board information management system; life support system designed for heating and conditioning the habitable compartment, purification of atmospheric air from toxic substances, radioactive dust, bacteriological aerosols and hazardous substances; power supply system designed to power all elements of the machine.

Currently, the anti-mine component of the comprehensive protection of armored vehicles is especially relevant. Providing mine protection has become one of the main problems facing developers of modern military combat vehicles. Today, the defining factor in the design of an armored car is the protection of the crew, ensuring the operability of the car after undermining is fading into the background.

The closest analogue (prototype) of this utility model is the Typhoon protected machine.

Protected vehicle "Typhoon" is part of a promising type of military automotive equipment in accordance with the requirements of orders of the Ministry of Defense of the Russian Federation of 1997 No. 483 and of 2011 No. 2482.

Protected vehicle "Typhoon" provides protection for the crew in the inhabited compartments, as well as the main systems and assemblies, when exposed to damaging factors of weapons of at least class 1 according to OTT 9.1.12.1-2010.

The disadvantages of the well-known Typhoon machine: the impossibility of conducting optical reconnaissance due to the lack of an optoelectronic system; low maneuverability in combat conditions and, as a result, low survivability due to the absence of a blocker of radio-controlled explosive devices designed to block the radio frequencies of explosive devices; low maneuverability in combat damage to armored glass due to the lack of a television viewing device; low noise immunity of navigation equipment when the enemy uses electronic means of suppression; there is no complex detection of mine-explosive barriers.

The technical result of this utility model is the conduct of optical, engineering and radiation reconnaissance of the war zone.

The technical result is achieved due to the fact that the technical reconnaissance vehicle, which is a car with the ability to protect the crew in the habitable compartment of the main systems and assemblies from exposure to the damaging facts of weapons, an electrical supply system designed to power all elements of the machine, a life support system, designed to heating and conditioning the inhabited compartment, purification of atmospheric air from toxic substances, radioactive dust, bacteriological aerosols and airborne hazardous substances, an onboard information and control system designed to collect, store, process and display information about the terrain, control the means and systems of the machine, transmit intelligence, navigation and diagnostic data, additionally contains an optical-electronic system designed to conduct optical reconnaissance day and night, difficult meteorological conditions, a radiation reconnaissance complex designed to conduct radiation reconnaissance of the area, a radio control blocker explosive devices, designed to block the radio frequencies of explosive devices when the vehicle is moving, a television viewing device designed to provide control of the machine during combat damage to armored glass, a floodlight system designed to search for failed models of military equipment and conduct work in the dark, a complex for detecting mine-explosive barriers designed to search for anti-tank, anti-vehicle and anti-landing mines with metal hulls and parts installed in the soil and on its surface, while the first input-output of the said on-board information and control system is connected to the first input and output of the optoelectronic system, the second input and output of the on-board information and control system is connected to the first input the output of the jammer of radio-controlled explosive devices, the third input-output of the on-board information-control system is connected to the first input-output of the radiation reconnaissance complex, the fourth input-output of the said on-board inform the control system is connected to the first input-output of the power supply system, the fifth input-output of the on-board information and control system is connected to the first input-output of the life support system, while the first output of the television viewing device is connected to the sixth input of the on-board information and control system, the first the input-output of the projection lighting system is connected to the eighth input-output of the on-board information-control system, the first input-output of the mine-explosive detection complex deniy is connected to the ninth input-output of the on-board information and control system, the second output of the power supply system is connected to the seventh input of the on-board information and control system, the second input of the optoelectronic system, the second input of the jammer of radio-controlled explosive devices, the second input of the radiation reconnaissance complex, the second input of the television viewing device, the second input of the life support system, the second input of the projector lighting system, the second input of the mine-explosive detection complex x barriers.

In another particular embodiment, the on-board information and control system contains an automated commander’s workstation designed to control reconnaissance equipment and a vehicle’s crew, an operator’s automated workstation designed to conduct optical-electronic and radiation reconnaissance, and to monitor weapons and military equipment on the battlefield in the daytime and at night, in the presence of precipitation, smoke curtains and dusting of the atmosphere, communication equipment designed to provide communication with a higher level unit crew members, intercom equipment intended to provide commutation of communication facilities and crew intercom, inertial navigation equipment designed to determine heading, location of the vehicle in conditions of adversary’s use of electronic suppression of satellite navigation systems, satellite navigation equipment designed to determine the coordinates of the location of the machine, ground speed and track angle, while the first input-output is automatically the operator’s workstation is connected to the first input-output of the commander’s automated workstation, the second input-output of which is connected to the first input-output of the internal communication and switching equipment, the third input-output of the said internal communication and switching equipment is connected to the first input-output of the communication equipment , the second input-output of the operator’s workstation is connected to the second input-output of the intercom and switching equipment, while the third input of the operator’s workstation ra is connected to the first output inertial - navigation apparatus, a second input connected to the first output of the satellite navigation.

In another particular embodiment, the communication equipment includes a radio station designed to provide communication to the crew with a higher control link and an antenna-feeder device, which consists of an antenna designed to receive and transmit messages on the VHF channel, an antenna lifting mechanism designed to raise the antenna and connecting a high-frequency cable to a radio station, a control panel designed to control the position of the antenna and light indication of emergency mode, while the first input-output of the antenna is connected nen with second input-output antenna lifting mechanism, the third input-output of which is connected to the first input-output of said control unit, the first input-output of the antenna lifting mechanism coupled to a second input-output station.

In another particular embodiment, the internal communication and switching apparatus comprises an internal communication and switching unit for switching voice or telecode channels, transmitting control and monitoring commands from the commander’s workstation to the radio of the communication equipment, and issuing voice alerts to all crew members from an automated workstation places of the commander, the commander’s subscriber console, designed to ensure the connection of the chest switch to the intercom unit transmitting, receiving from the intercom unit and switching unit information about the status of switching and indicating received information on the front panel of the unit, transmitting to the intercom unit and switching unit information about the status of the buttons and volume control located on the front panel of the unit, the operator’s subscriber station and the driver’s subscriber station designed to connect the chest switch to the unit of internal communication and switching, the formation of a volume control signal, chest switches commander, operator and driver I, designed to connect tank headsets to the commander’s subscriber’s console, operator’s and driver’s subscriber’s panels, generate commands for a tone signal and control the operating mode of the radio equipment, while the first input-output of the internal communication and switching unit is connected to the first input the output of the commander’s subscriber console, the second input-output of the said intercom and switching unit is connected to the first input-output of the operator’s subscriber console and the first input-output of the subscriber driver’s remote control, the second input-output of the commander’s subscriber’s console is connected to the first input-output of the commander’s chest switch, the second operator’s user’s input-output is connected to the first input-output of the operator’s chest switch, the second driver’s user’s input-output is connected to the first input - the output of the chest switch of the driver, while the third input-output of the said unit of internal communication and switching is connected to the first input-output of the communication unit of the base, the second input-output of which is Inonii the first input-output of the antenna.

In another particular embodiment, the inertial navigation equipment contains an inertial navigation unit and an onboard computing unit, which consists of an interface unit for receiving and transmitting information between machine elements, a panel computer for solving combat missions and displaying an electronic navigation map , navigation and reconnaissance data on the display, applying the location of damaged weapons and military equipment to electronic navigation a map, determination of the access and evacuation routes for the deployment of repair and restoration bodies on an electronic navigation map, a network data storage device designed to store a combat geographic information system, a solid state data storage device designed to store an electronic navigation map, navigation and reconnaissance data, hardware and software module trust load and a path measurement sensor designed to measure the distance traveled, with the first output inertia IAL navigation unit is connected to the first input of the interface unit, the second input-output of which is connected to the first input-output of the panel computer, the second input-output of which is connected to the first input-output of the network data storage device, the second input-output of which is connected to the first input - the output of the solid-state data storage device, while the first input-output of the aforementioned hardware-software trust download module is connected to the third input-output of the panel computer, the first output of the said path measurement sensor oedinen a second input inertial navigation unit.

The claimed utility model is illustrated by the following drawings: FIG. 1, which shows a structural diagram of a combat vehicle of technical intelligence; FIG. 2, which shows a block diagram of an onboard information management system; FIG. 3, which shows a block diagram of communication equipment; FIG. 4, which shows a block diagram of intercom and switching equipment; FIG. 5, which shows a structural diagram of an inertial navigation apparatus; FIG. 6, which shows satellite navigation equipment; FIG. 7, which shows a block diagram of an optoelectronic system; FIG. 8, which shows a general view and overall dimensions of an optoelectronic system; FIG. 9, which shows a general view and overall dimensions of an adaptive television laser range finder; FIG. 10, which shows a block diagram of a power supply; FIG. 11, which shows a general view of a technical reconnaissance combat vehicle.

Consider the structure and operation of a combat reconnaissance and strike machine.

As can be seen from the drawing of FIG. 1 and FIG. 11, a technical reconnaissance vehicle (BMTR), contains a protected vehicle designed to protect the crew in the inhabited compartment, as well as the main systems and assemblies when they are affected by weapons, the power supply system 7, designed to power all elements of the machine, life support system 6 designed for heating and conditioning the habitable compartment, purification of atmospheric air from toxic substances, radioactive dust, bacteriological aerosols and hazardous substances, b gate information management system (BIUS) 2, designed to collect, store, process and display information about the terrain, control the means and systems of the machine, transmit intelligence, navigation and diagnostic data, optical-electronic system (ECO) 3, designed to conduct optical day and night reconnaissance, difficult meteorological conditions, a radiation reconnaissance complex (RRC) 5, designed to conduct radiation reconnaissance of the area, a blocker of radio-controlled explosive devices ) 4, designed to block the radio frequencies of explosive devices while the vehicle is moving, a television viewing device (TSU) 8, designed to provide control of the machine in combat damage to armored glasses, a searchlight system (STR) 9, designed to search for failed models of military equipment and work in the dark, the detection complex of mine explosive barriers 10, designed to search for anti-tank, anti-vehicle and anti-landing mines with metal Orpuses and parts installed in the ground and on its surface.

The first input-output of the aforementioned BIUS 2 is connected to the first input-output of the OES 3, the second input-output of the BIUS 2 is connected to the first input-output of the BRVU 4, the third input-output of the BIUS 2 is connected to the first input-output of the RRC 5, the fourth input-output the said BIUS 2 is connected to the first input-output of the power supply system 7, the fifth input-output of the BIUS 2 is connected to the first input-output of the life support system 6, while the first output of the TSU 8 is connected to the sixth input of the said BIUS 2, the first input-output of the SPO 9 is connected with the eighth input-output BIUS 2, the first input-output complex detection of mine-explosive barriers 10 is connected to the ninth input-output of the BIUS 2, the second output of the power supply system 7 is connected to the seventh input of the BIUS 2, the second input of the ECO 3, the second input of the BRVU 4, the second input of the RRC 5, the second input of the TSU 8, the second input of the system life support 6, the second entrance of the ACT 9, the second entrance of the detection complex mine-explosive barriers 10.

As can be seen from the drawing of FIG. 2, BIUS 2 contains the automated workplace of the commander (ARMK) 11, designed to control reconnaissance equipment and the crew of the machine, the automated workplace of the operator (ARMO) 12, designed to conduct optoelectronic and radiation reconnaissance, monitoring weapons and military equipment on the battlefield in the daytime and at night, in the presence of precipitation, smoke curtains and dusting of the atmosphere, communication equipment 13, designed to provide communication with a higher command link and crew members, internal equipment communications and switching (AVSK) 14, designed to provide commutation of communications and internal communications crew, inertial navigation equipment (INA) 15, designed to determine the course, location of the machine in the conditions of the enemy using means of electronic suppression of satellite navigation systems, satellite navigation equipment (ASN) 16, designed to determine the coordinates of the location of the machine, ground speed and track angle.

In this case, the first input-output ARMO 12 is connected to the first input-output ARMK, the second input-output of which is connected to the first input-output ABCK 14, the third input-output of the said ABC 14 is connected to the first input-output of communication equipment 13, the second input is the output of the ARMO 12 is connected to the second input-output ABCK 14, while the third input of the ARMO 12 is connected to the first output of the INA 15, the second input of which is connected to the first output of the ASN 16.

As can be seen from the drawing of FIG. 3, communication equipment 13 contains a radio station 18, designed to provide communication to the crew with a higher control link and an antenna-feeder device (AFU) 17, which consists of an antenna 20, designed to receive and transmit messages over the VHF channel, antenna lifting mechanism 21, designed for lifting the antenna and connecting the high-frequency cable to the radio station 18, the control panel 19, designed to control the position of the antenna and light indication of emergency mode.

In this case, the first input-output of the antenna 20 is connected to the second input-output of the lifting mechanism of the antenna 21, the third input-output of which is connected to the first input-output of the said control panel 19, the first input-output of the lifting mechanism of the antenna 21 is connected to the second input-output of the radio station eighteen.

As can be seen from the drawing of FIG. 4, AVSK 14 contains an internal communication and switching unit (BVSK) 22, designed for switching voice or telecode channels, broadcasting control and control commands from AWPK 11 to radio station 18 of communication equipment 13, issuing voice alerts to all crew members with AWP 11, subscriber the commander’s console (AIC) 23, designed to connect the chest switch (NP) 27 to the BVSK 22, receive from the BVSK 22 information about the switching status and display received information on the front panel of the unit, transmit information to the BVSK 22 when the buttons and volume control are located on the front panel of the unit, the operator’s subscriber console (ALO) 25 and driver’s subscriber console (AR) 26, designed to connect the chest switch to BVSK 22, generate a volume control signal, commander’s chest switches (NPC) 27, operator (NPO) 28 and driver (HUB) 29, designed to connect tank headsets to the AIC 23, ALO 25 and APV 26, the formation of commands for the tone signal and the control signal of the operating mode of the radio station 18 communication equipment 13.

In this case, the first input-output of BVSK 22 is connected to the first input-output of the AIC 23, the second input-output of the mentioned BVSK 22 is connected to the first input-output of the ALO 25 and the first input-output of the APV 26, the second input-output of the AIC 23 is connected to the first input the output of the NPK 27, the second input-output of the APO 25 is connected to the first input-output of the NGO 28, the second input-output of the reclosure device 26 is connected to the first input - the output of the NIV 29, while the third input-output of the mentioned BVSK 22 is connected to the first input-output BSB 24, the second input-output of which is connected to the first input-output of the antenna 30.

As can be seen from the drawing of FIG. 5, INA 15 contains an inertial navigation unit (INB) 31 and an on-board computing unit (BVB) 32, which consists of an interface unit 33 for receiving and transmitting information between machine elements, a panel computer (PC) 34, designed to solve combat missions and displaying an electronic navigation map, navigation and reconnaissance data on a display, plotting the location of damaged weapons and military equipment on an electronic navigation map (ENC), determining access routes and evacuation of deployment sites of repair and restoration bodies on an electronic navigation chart, network data storage device (SND) 35, designed to store a combat geographic information system (GIS), solid-state data storage device (TND) 38, designed to store ENC, navigation and reconnaissance data, hardware - software module trust download (APMDZ) 37 and the sensor measuring path (DIP) 36, designed to measure the distance traveled.

The first output of the INB 31 is connected to the first input of the interface unit 33, the second input-output of which is connected to the first input-output of the PC 34, the second input-output of which is connected to the first input-output of the SND 35, the second input-output of which is connected to the first the input-output of the high pressure pump 38, while the first input-output of the aforementioned APMDZ 37 with the third input-output of the PC 34, the first output of the aforementioned DIP 36 is connected to the second input of the battery 31.

As can be seen from the drawing of FIG. 6, ANS 16 includes a satellite navigation antenna 39 high-frequency cable of satellite navigation antenna 40 and a central control and navigation unit (CCU) 41 with an integrated display device 45. Satellite navigation antenna 39, made in the form of an adaptive antenna array, contains a power connector 42 and a high-frequency connector 43 for connecting the high-frequency cable 40 of the satellite navigation antenna to the high-frequency connector 44 of the CBU 41. In this case, the CBU 41 comprises an integrated display device 45, a switch 46 an electrical connector Power 47 and interface 48.

As can be seen from the drawing of FIG. 7, OES 3 contains: an infrared lens 49, an infrared detector 50, an electronic thermal imaging unit 51, a television lens 53, a video processor and video document unit 54, a video data storage device 55, an infrared monitoring monitor 56, a television monitoring monitor 57, a control unit 58, a slewing rotary the device (OPU) 59, the manipulator of the control of the OPU 60, the manipulator of the television device 61, the manipulator of the thermal imaging device 62 and the temperature control unit 63.

In this case, the infrared lens 49 is connected to the infrared detector 50, which is connected to the electronic thermal imaging unit 51. The electronic thermal imaging unit 51 is connected to the television lens 53. The electronic thermal imaging unit 51 and the electronic television unit 53 are connected to the video processor and video document unit 54. The video storage device 55, infrared monitoring monitor 56, television monitoring monitor 57, control unit 58 are connected to the video processor and video documenting unit 54. OPU 59 the manipulator is controlled I OPU 60, the television apparatus control arm 61, thermal imaging device joystick control 63, temperature control unit 63 are connected to the control unit 58.

As can be seen from the drawing of FIG. 8, OES 3 contains a television channel with a television lens 52 and a thermal imaging channel with an infrared lens 49, located on the RAM 59.

As can be seen from the drawing of FIG. 9, OES 3 may include an adaptive television laser rangefinder, which consists of a video camera 66 and a laser rangefinder 65.

As can be seen from the drawing of FIG. 10, the power supply system 7 comprises: an electric generator 72; introductory shield 67; generator 76; relay regulator 75; filter 74; rectifier 73; power filter 71; rechargeable batteries 69; network shutdown machine 70.

The power unit 72, the circuit breaker 70 and the distribution board 68 are connected to the input shield 67. The batteries 69, the power filter 71, the relay regulator 75, the filter 74 and the rectifier 73 are connected to the distribution board 68. The generator 76 is connected to the relay of the regulator 75.

As can be seen from the drawing of FIG. 11, BMTR 1 is made on the basis of a protected vehicle from a promising type of military automotive equipment in accordance with the requirements of the order of the Ministry of Defense of the Russian Federation of 1997 No. 483 and of 2011 No. 2482. In the drawing of FIG. 11 shows an arrangement of elements on the BMTR 1 chassis.

BMTR 1 works as follows.

BMTR 1 is intended for manning the units of technical intelligence of promising formations (military units) and operations as part of the following military units: technical intelligence groups; evacuation groups; repair and evacuation groups and repair groups. OES 3 BMTR provides the following types of work during technical reconnaissance in combat conditions:

- observation of the battlefield in order to search for failed weapons and military equipment samples in the daytime and at night, in the presence of precipitation, smoke screens, dusting of the atmosphere, in the infrared range;

- finding in the designated strip (district, line) of failed weapons and military equipment, determining their location and accessories, mapping the location;

INA 15 and ASN 16 provide:

- mapping the location of BMTR 1 on ARMK 11 and ARMO 12 with ENC, including when the enemy uses electronic means of suppression;

- automatic range detection to destination;

- automatic display of destinations on the ENC after their introduction into the display device ARMK 11 and ARMO 12;

- work with ENK ARMK 11 and ARMO 12 while driving;

- storage of ENC in SND 35 and theater 38;

- automatic recording and storage of the route in ARMK 11 and ARMO 12, theater of operations 38 movement BMTR;

- automatic search for failed weapons and military equipment samples by address and coordinates;

- automatic determination of the maximum and average speed of the BMTR 1;

- automatic determination of travel time to failed weapons and military equipment;

- measuring, collecting, processing, presenting and transmitting information to higher-level control units via VHF communication channels.

KRC 5 provides:

- determination of the degree of contamination of the places of failure of weapons and military equipment samples, access and evacuation routes (radiation reconnaissance);

The detection complex of mine explosive barriers 10 provides:

- conducting engineering reconnaissance of the entrance paths and evacuation of failed weapons and military equipment;

- identification of mine-explosive barriers on the access and evacuation routes and explosive devices on failed weapons and military equipment;

- finding ways convenient for the approach of evacuation and repair forces and means to failed weapons and military equipment, finding and clarifying areas (places) of concentration of the largest number of failed weapons and military equipment and determining their affiliation;

- clarification of the evacuation routes of weapons and military equipment, areas (locations) of deployment (deployment) and ways of moving repair and evacuation units;

- finding shelters to accommodate failed weapons and military equipment and places convenient for the deployment (deployment) of repair forces and equipment;

- determination of the location and the possibility of using captured weapons and military equipment.

BRVU 4 provides: protection of the crew from the damaging factors of enemy weapons.

Consider the work of BMTR 1 in conducting technical reconnaissance in combat conditions: monitoring the battlefield in order to search for failed weapons and military equipment in the daytime and at night, in the presence of precipitation, smoke curtains, dusting the atmosphere, in the television and infrared range.

Communication equipment 13 provides internal communication between all crew members and with the higher management using radio station 18.

The crew commander of BMTR 1, using a headset (not shown) connected to the NPK 27, through the AIC 23 and the BVSK 22 sends a command to the operator, which is part of the crew, through ALO 25 and NPO 28, to conduct optical reconnaissance of the terrain. The operator, using the ARMO 12, which is part of the BIUS 2, sends a command to the drive of the control panel 59 to review the terrain of the ECO 3. The ECO 3 contains a lens 49 and 52, which allow the BMTR 1 operator to conduct optical reconnaissance in the television range using the lens 52, the electronic television unit 53 and the unit 54. Using the lens 49, the detector 50, the units 51 and 52 — optical reconnaissance in the infrared range. The operator observes the results of optical reconnaissance in the television and infrared ranges on the television surveillance monitor 57 and the infrared observation monitor 56. All optical reconnaissance data is recorded in the video storage device 55, which can be used in the future for analysis and decision making. The depth of the detailed optical reconnaissance zone is up to 5,000 meters in the television range and up to 3,000 meters in the infrared range. BIUS 2 contains ARMK 11 and ARMO 12. An operator with ARMO 12 transmits real-time IWT data to the ARMK 11. The BMTR 1 crew commander, using radio station 18, transmits intelligence data to a higher command link. Product АВСК 14 solves the following tasks:

- providing internal telephone communications crew BMTR 1;

- ensuring the release of BMTR 1 subscribers to external telephone radio communications through any of two radio communication channels;

- ensuring the release of BMTR 1 subscribers to external telephone communication via any of two wire communication channels;

- switching two channels of data transmission equipment on the data transmission lines of a radio station or external wired communication lines;

- ensuring the release of the BMTR 1 commander with AWPK 11 to external telephone radio communications when the power supply of the AVSK 14 product is disconnected;

- providing manual adjustment of the volume of the audible signals for each crew member;

- ensuring the formation and issuance of voice messages to all crew members (regardless of the operating mode of the AVSK 14 product) according to commands received from ARMK 11;

- providing listening to external radio signals when conducting internal communications and listening to internal communications signals when conducting external radio communications;

- ensuring the transfer, at the initiative of the commander or operator of BMTR 1, of a call signal to external subscribers via wire lines and the formation of a control signal for transmission of a tonal call by radio station 18;

- ensuring access to all members of the crew of BMTR 1 for external radio communications;

- providing wireless digital duplex telephone communication between crew members upon leaving BMTR 1 to ensure a hands-free mode, which increases the efficiency and quality of work.

Negotiating in all communication modes is carried out through a tank headset ТШ-4М (not shown in the drawing), connected to NPK 27, NPO 28 and NPV 29. When connecting chest switches wireless (NBP) - crew members equipped with airbag units (not shown shown) are connected through the antenna 30 to the BSB 24, and conduct radio communication via an outbred radio channel.

With the help of NPK 27, NGO 28 and HUB 29, the following tasks are solved:

- amplification and compression of the dynamic range of the speech signal coming from the laryngophone TSh-4M (not shown in the drawing);

- amplification of the signal coming from the BVSK 22 unit to the phones TSh-4M (not shown in the drawing);

- generation of “TRANSMISSION” signals for controlling the operation mode (“Reception / Transmission”) of the radio station 18 during negotiations on radio communications and “CALL” for negotiating in the “emergency telephone” mode, sending a tone signal via wire and tone channels radio call 18.

The workplaces of all BMTR 1 crew members are equipped with APK 23, APO 25 and APV 26 panels, respectively.

Product АВСК 14 provides three types of internal telephone communication: circular telephone communication; selective telephone communications; emergency telephone connection.

Circular telephony - default view. The commander, driver and operator, after supplying power to the ABCK 14 product, find themselves in this type of communication. In this mode, communication is carried out without any additional actions. The phrase spoken to the TSh-4M laryngophones (not shown in the drawing) will be heard by all other BMTR 1 crew members, including subscribers connected through the BSB 24 product.

Selective telephone communication is intended for negotiating between any two BMTR subscribers 1. Negotiations conducted between these subscribers will not be heard by other subscribers of the object who are not participating in selective communication. The establishment and breaking of this type of communication is carried out using the buttons located in the “SUBSCRIBERS INSIDE” field. COMMUNICATIONS "on the front panel of the consoles APK 23 and ALO 25 (not shown in the drawing).

Emergency telephone communication is intended for emergency notification of all crew members, regardless of the type of communication they are in. Emergency communication is held when the “CALL” button is pressed (not shown in the drawing) on NPK 27, NPO 28 and NPV 29. This type of communication is entered 3 seconds after the start of holding the “CALL” button.

The call signal received from external communication subscribers is displayed on the front panel of the APK 23 remote control unit by flashing yellow and green indicators corresponding to the caller, and is also accompanied by sound signals in the phones of the tank headset of the commander and operator. Light indication of the ringing signal is carried out only if the connection with the calling subscriber of the external connection is not established (not shown in the drawing).

The product АВСК 14 allows you to switch two channels of data transmission equipment (not shown in the drawing) on the data line of the radio station 18 or wired communication lines. Switching control of these channels is carried out by commands from AWK 11.

When switching channels of data transmission equipment (not shown in the drawing) to wired communication lines, it should be borne in mind that the commander or operator can occupy the corresponding lines for voice communication using their control panels. In this case, commands from ARMK 11 about switching to the same communication lines are not an error, but voice communication is given priority. For example, if a commander’s connection is established via a telephone line, and at this moment, using the AWP 11, the data transmission equipment (not shown) is switched to the same telephone line, then the data transmission equipment will be connected there only after the commander is disconnected. Moreover, the commander can at any time again establish a connection on this telephone line. In this case, the data transmission equipment (not shown in the drawing) will be disconnected from the line, and the commander will be connected to this line. After the commander is disconnected, the previously specified connection of the data transmission equipment (not shown in the drawing) will be restored automatically without additional control from AWP 11.

The AVSK 14 product provides the ability to conduct external radio communications to the BMTR 1 commander, even if no power has been supplied to the product. In the absence of power on the product ABCK 14, the telephone circuits of the APK 23 remote control are automatically switched to the first channel of the radio station 18.

The AVSK 14 product provides voice notification to the BMTR crew 1. Voice notification is carried out according to commands from ARMK 23 from the BIUS 2 always with maximum volume and regardless of the operation mode of subscribers of the AVSK 14 product. Voice messages generated by the AVSK 14 product: "Fire in the aft compartment" ; "Fire in the fighting compartment"; "Fire in the control department"; "Fire in the engine compartment"; "Fire in the compartment of the power unit"; "Attention! Atom"; "Warning! Gases"; "Warning! Radiation"; "Warning! Laser irradiation"; "Dangerous roll angle to starboard side"; "Dangerous roll angle to port side"; "Dangerous pitch angle on the nose"; "Dangerous pitch angle aft"; "Warning, dangerous degree of gas contamination."

Turn on / off the wireless mode by pressing and holding the button “FREE. COMMUNICATION "(not shown in the drawing) on the BSB 24. If the indicator" FREE. COMMUNICATION ”lights up in green, then the wireless mode is on. Any crew member who left BMTR 1, subject to preliminary registration, located at his airbag unit, after turning on the airbag unit, which is made by the power button, is in this form of communication via antenna 30. In this mode, communication is carried out without any additional actions. The phrase spoken in the headset’s laryngophone / microphone will be heard by all other BMTR crew 1. The volume knob of the airbag unit (not shown in the drawing) can be used to adjust the sound volume in the headset at any time. Increase - clockwise, decrease - against.

On the front panels of the APC 23, ALO 25 and APV 26 panels are controls (buttons), with which you can control both your own switching and switching of other subscribers (not shown in the drawing).

The toggle switch “MANAGEMENT)) (not shown in the drawing) on the APK 23 remote control affects the priority of establishing communication with other crew members. For example, if the commander established a connection with an external subscriber via radio station 18 and the toggle switch “CONTROL)) is set to“ COMAN)), then the operator using the ALO 25 remote control will not be able to negotiate through this radio station 18 until the commander releases it.

If the toggle switch) is set to the “NAV” position (not shown in the drawing), then the operator will be able to disconnect the commander’s connection and establish his own when connecting to external subscribers through radio station 18.

Using the APC 23, APO 25 and APV 26 remotes, the following communication modes can be established: internal individual selective telephone communication with BMTR crew members; listening to external telephone radio communications while conducting internal communications; external individual selective telephone radio communication; external individual selective telephone communication via wire lines.

The listening mode of external telephone radio communications can only be set for the commander or operator. This mode is set using the buttons “PC1” (radio station 18) and “PC2” (reserve). In order to listen to the selected radio station, you must click on the appropriate button once (not shown in the drawing).

If you successfully set the listening mode, the corresponding indicator will blink green. On the remote control from which this mode was not set, the presence of this connection will be indicated by flashing amber indicators next to the subscriber and radio buttons between which this operating mode is set. For example, the commander chose the listening mode of radio station 18, then on the APK 23 remote control the PC1 indicator will blink green, on the APO 25 remote control the KOM and PC1 indicators will blink yellow (not shown in the drawing).

Consider the operation of ASN 16. Navigation signals from satellite navigation systems (SNA) GLONASS and GPS (not shown) are continuously fed to a satellite navigation antenna 39, which performs spatial processing of signals from the SNA. The satellite navigation antenna 39 is made in the form of an adapted antenna array, which contains the first, second, third, fourth and fifth antenna module. The interference signal (not shown in the drawing), enters the satellite navigation antenna 39, excites the first, second, third and fourth antenna module with its phase, which allows you to extract information about the spatial position of the sources and use it to suppress interference effects.

The suppression of interference (not shown in the drawing) occurs due to the formation of a "dip" in the radiation pattern of the satellite navigation antenna 39 in the direction of the interference source.

The central control and navigation unit (TsBUN) 41 contains a multi-band navigation module (not shown), which receives signals from antenna 39 with frequency letters L1 + L2 + L5 GLONASS, L1 + L2 + L5 GPS and B1 + B2 BeiDou (in the drawing not shown). Analysis of the presence of interference from electronic warfare equipment (not shown in the drawing) occurs at the software and hardware level, which allows you to create "zeros" of the radiation pattern in the direction of the interference sources.

By combining the TsBUN 41 with a satellite navigation antenna 39, which is made in the form of an adapted antenna array, one of the problems of the utility model is solved: increasing the noise immunity of navigation equipment.

The navigation data from TsBUN 41, through the interface connector 48, enters the INA 15. The INA 15 measures accelerations and angular velocities, rotation and tilt angles of the BMTR 1, directional angle (course). INA 15 together with DIP 36 and ASN 16 solves the navigation problem in the absence of signals from the SNA.

The INB 31 includes (not shown in the drawing) a computing unit, three fiber-optic gyroscopes (FOG) and three accelerometers. Among the advantages of FOG, in comparison with dynamically tuned gyroscopes (DNG), which are widely used in combat vehicles of the ground forces are: the absence of rotating units in the structure, which increases reliability; reduced power consumption and weight and size characteristics; short readiness time; invariance to external accelerations; performance in conditions of high mechanical overload. The advantage of using FOG in stabilization systems is the high stability of the scale factor and the absence of the influence of the non-orthogonality of the measuring axes due to the small range of angular velocities. A method for determining the direction of the directional angle using VOG is known and described in the literature, for example, on pages 43-45 of the monograph by S.A. Mosienko (Ground robotic shock and reconnaissance systems for units of the Ground Forces. / Mosienko S.A. - M .: Sampoligraphist, 2014, -250 s).

When external noise (not shown) of electronic warfare equipment on the ASN 16 is applied, the computing unit (not shown in the drawing) INB 31 will receive data from DIP 36, then it will transmit odometric data to PC 34 to display BMTR 1 location on PC 34 ENC, ARMK 11 and ARMO 12.

PC 34 has (not shown in the drawing) a calculator and a display designed to display the ENC (not shown) combat GIS, which are necessary for situational awareness of crew members. PK 34 is a part of ARMK 11 (not shown in the drawing). The display of the PC 34 displays the following information (not shown in the drawing):

- current BMTR 1 coordinates in a rectangular coordinate system (SK-42) or in a geographical coordinate system (WGS-84, SK-42, SK-95, P3-90.02, P3-90.11);

- the true BMTR 1 course (in degrees, degrees-minutes, degrees-minutes-seconds, radians, divisions of the goniometer);

- elevation angle (in degrees, degrees-minutes, degrees-minutes-seconds, radians, divisions of the goniometer);

- target designation angles (in degrees, degrees-minutes, degrees-minutes-seconds, radians, goniometer divisions);

- the difference between the values of the current angles and the values of the target designation angles (in degrees, degrees-minutes, degrees-minutes-seconds, radians, divisions of the goniometer);

- BMTR 1 location on the battlefield GIS ENC.

A PC 34 with a combat GIS (not shown in the drawing) displays the current location, direction of movement and orientation of the BMTR 1 on the ENC, the location of the military and military equipment and targets, the distance to military equipment, and the direction to military equipment from the current position.

DIP 36 is designed to reckon the BMTR 1 traveled path in off-road conditions (dirt, sand) and snow drifts (ice, snow). DIP 36 contains (not shown) a combined microwave transceiver and an integrated microwave transceiver in a metal casing. To mount DIP 36 on the BMTR 1, a bracket is used (not shown in the drawing). The output from DIP 36 is transmitted via RS-232 to INB 31, where the measured data are calculated and output to PC 34. DIP 36, in another embodiment (not shown in the drawing), can be a typical odometer widely used in all types of armored vehicles .

INB 31, on-board computing unit 32 provide operation in three modes: integrated mode - the main mode of operation of the product, ensuring the determination of BMTR 1 location coordinates according to information from INB 31 and DIP 36 with coordinate correction according to information from ASN 16; autonomous mode - provides for determining the location coordinates of the BMTR 1 machine according to information from INB 31 and DIP 36, in the absence of signals from the ASN 16 (with electronic interference); satellite navigation mode - provides the determination of the coordinates of the location of the vehicle BMTR 1 according to the signals of the SNA ASN 16.

The radio station 18 has communication equipment 13 and has the following features: providing searchless, non-tuning, two-way, half-duplex radio communications in telephone mode with various types of modulation at various capacities; receiving and transmitting confidential information closed with technical masking with transmission rates of 2.4 and 16 kbit / s; reception and transmission of digital information from terminal equipment with transmission rates of 1.2; 2.4; 4.8; 9.6 and 16 kbps. To raise the antenna 20, the lifting mechanism of the antenna 21 is used, the operator, using the control panel 19, has the ability to fix up to three positions: horizontal, vertical and inclined.

BRVU 4 protects the BMTR 1 from explosion by blocking the control signals of radio fuses over the radio channel by creating an interfering signal that blocks all available frequencies used for transmission. To enable BRVU 4 in the cabin BMTR 1 there are control panels (not shown).

КРР 5 is intended for measuring the power of the ambient dose equivalent of photon radiation (DER), storing the measured data in the device’s memory with the possibility of outputting information to the ARMK 11 and ARMO 12, and mapping the radiation situation in the area.

The BIUS 2 software was developed in accordance with the requirements of the Unified Data Protection System, the Guidelines for the Development of Military Software Products, the Concepts for the Creation and Equipping of Basic Information Protected Computer Technologies of the Armed Forces of the Russian Federation, Directive No. 331/3/0437 of August 19, 2002 GOST R 8.654-2009. In order to protect information from unauthorized access (SZI NSD), BMTR 1 uses on-board computers and PC 34 built-in in ARMK 11, ARMO 12, certified for compliance with the class of protection against unauthorized access to the information set for them in accordance with the requirements of the Russian Federation State Technical Commission 1992 " Computer facilities. Protection from unauthorized access to information. Indicators of protection from unauthorized access to information ", not less than 4 classes. APMDZ 37 is included in the composition of SC 34 SZI NSD, APMDZ is included in ARMK 11 and ARMO 12 (not shown in the drawing). APMDZ 37 provides: identification of all members of the BMTR 1 crew at the beginning of a session with ARMK 11, ARMO 12 and PK 34; protection against unauthorized initial loading of software (software), not a regular copy of the operating system, including from removable storage media.

ECO 3 detected ground targets and military hardware, the coordinates are automatically sent to ARMO 12, which includes a monitor 56 and 57, military hardware displays monitors 56 and 57 with the military intelligence GIS.

The integration of ECO 3 with ASN 16 and INA 15 increased the situational awareness of the BMTR 1 crew members by increasing the information content of the obtained intelligence data. Manipulators 60, 61, 62, which are part of ARMO 12, provide an overview of the area with damaged weapons and military equipment.

Increasing the maneuverability of the BMTR 1 control in case of combat damage to the armored glass is solved using the TSU 8, which consists of an all-weather camera 91, an interface unit and a display unit (not shown in the drawing).

To carry out engineering reconnaissance of the places of failure of damaged (faulty) weapons and military equipment, access and evacuation routes, deployment areas of airborne missiles, the STR 9 is used. Composition of the STR 9: front headlight 90 and rear headlight (not shown), mounted on rotary support devices that allow the driver or commander to control the lighting from the control unit at night.

The life support system 6 includes (not shown) a filtering and ventilation unit, a heater, and air conditioning.

The power supply system 7 includes: an electric generator 72. The electric generator 72 may be a diesel type AD-4-P / 28.5-1 VM1 (not shown in the drawing). The power unit 72 is designed to power the BMTR 1 equipment in the parking lot with a constant voltage of 26 V with the generator 76 turned off. The power unit 72 consists of a four-kilowatt DC generator, an engine and a control unit (not shown in the drawing). To regulate the voltage generated by the DC generator of the electric unit 72, a voltage regulator is installed. The voltage regulator (not shown in the drawing) consists of an electronic voltage regulator of the generator, assembled on a printed circuit board, a system for remote starting the engine of the electrical unit and protecting the generator armature circuit from reverse current. Voltage regulation is reduced to a change in the excitation current of the generator when the current in the load changes. The voltage generator 76 is designed to power all elements and systems BMTR 1 in a buffer mode with rechargeable batteries 69 when working in motion and at short stops. It is a three-phase alternating current generator with electromagnetic excitation with silicon diodes built into the generator. The generator 76 is shielded, and the minus one, its terminal is connected to the chassis of the vehicle 85. The voltage at the generator output when the generator rotor speed and load current 0-110 A change is maintained using a relay controller within 27-29 V.

BRUM 1 has a 10 mine detection complex designed for engineering reconnaissance and search for anti-tank, anti-vehicle and anti-landing mines with metal bodies and parts installed in the ground and on its surface.

Currently, the situation with the search for mines is as follows: the search for mines is associated with costs that are orders of magnitude higher than the costs of installing them; the search for mines is dangerous, and the low probability of detecting mines leads to casualties; the high probability of "false alarm" leads to a decrease in the speed of clearance, which is unacceptable in combat conditions; There are no universal mine search methods applicable in all conditions.

The IMP-2 mine detector is widely known, which consists of a search element, a three-knee rod assembly, an amplifier unit and headphones. The mine detector IMP-2 allows you to detect mines with metal bodies and parts located on the surface and in the thickness of the soil (snow, under water) when carrying out work to overcome mine-explosive barriers and mine clearance. The disadvantages of IMP-2 are the inability to detect mines that do not have metal parts, and the proximity of the search area to the device operator, which increases the risk of destruction in case of the possible operation of an explosive device.

In the patent of the Russian Federation No. 2485556 C1 dated 12/15/2011 a system for searching and detecting mines is described. The system consists of a multisensor module, a telescopic probe, an aerodynamic lifting device, a video camera, a radar unit, a control unit and a shoulder pack with a power supply and a computer. The satchel is connected by a multicore cable with a protective helmet, a control unit, a radar unit and with a display installed in goggles. A multisensor module may contain meters operating on different physical principles. The lifting device is a helicopter-type unmanned aerial vehicle. The lifting device is controlled by the system operator using the control panel on the control unit. Information from the video camera and multisensor unit is sent to the system operator on the display with safety glasses and headphones in the protective helmet after processing in the computer located in the backpack.

The disadvantages of the known system for the search and detection of mines: low detection quality associated with the problems of separation of the intrinsic emissions of body materials and explosive mines from noise components; the proximity of the search zone to the operator of the device, which increases the risk of damage in case of the possible operation of an explosive device; the heavy weight of the multisensor module with a telescopic probe, which causes fatigue of the device operator and reduces the time of continuous search. The principle of operation of the mine-explosive obstacle detection complex 10 is similar to that described in the Russian Federation No. 2485556 C1 of 12/15/2011.

Thus, the problem of the utility model is solved: carrying out optical, engineering and radiation reconnaissance of the war zone.

The manufacture of BMTR 1 is carried out from typical products of Russian manufacturers. Chassis from a promising type of military automotive equipment in accordance with the requirement of the order of the Ministry of Defense of the Russian Federation of 1997 No. 483 and of 2011 No. 2482. The car has the following indicators of basic technical characteristics: 4 × 4 wheel arrangement, load capacity of at least 1000 kg, cruising range of at least 1000 km, maximum speed of at least 100 km / h. The car protects the BMTR 1 crew in the inhabited compartments, as well as the main systems and assemblies, when exposed to the damaging factors of weapons of at least class 1 according to OTT 9.1.12.1-2010 and can be of the "Patrol" type manufactured by ASTEYS. BIUS 2, INA 15 and ASN 16, manufactured by NPO PROGRESS LLC. OES 3 manufactured by ASTRON OKB JSC, communication equipment 13 and AVSK 14 manufactured by TsNII VOLNA CJSC. Antenna lifting mechanism 21 and control panel 19, manufactured by Elektroavtomatika OJSC. BRVU 4 type "PELENA-6BM" manufactured by KOBRA JSC, UAV VT 79 type "Grand VA" produced by YuVS-YURION LLC, PK 34 type ORION PK-E-842-01 manufactured by LLC NPK ATRI. Power supply system 7 and life support system 8, typical and widely used in military and military equipment: filter and ventilation unit type FVUA-100A, heater OV-65 and air conditioning KTN-2.

The main elements of BMTR 1 were manufactured. Preliminary tests of the prototype confirmed the feasibility of the proposed technical solution to obtain the above technical result.

Claims (5)

1. A technical reconnaissance vehicle, which is a car with the ability to protect the crew in the inhabited compartment of the main systems and assemblies from exposure to damaging facts of weapons, an electric power supply system designed to power all elements of the machine, a life support system designed to heat and condition the inhabited compartment, air purification from toxic substances, radioactive dust, bacteriological aerosols and hazardous substances, on-board information-pack a focal system designed to collect, store, process and reflect information about the terrain, control the means and systems of the machine, transmit intelligence, navigation and diagnostic data, characterized in that it further comprises an optical-electronic system designed to conduct optical reconnaissance of the terrain day and night , in difficult meteorological conditions, a radiation reconnaissance complex designed to conduct radiation reconnaissance of the area, a blocker of radio-controlled explosive devices, designed to block the radio frequencies of explosive devices while the vehicle is moving, a television viewing device designed to provide control of the machine during combat damage to armored glass, a floodlight system designed to search for failed models of military equipment and to carry out work in the dark, a mine detection complex explosive barriers designed to search for anti-tank, anti-vehicle and anti-landing mines with metal shells and a part installed in the ground and on its surface, while the first input-output of the said on-board information-control system is connected to the first input-output of the optoelectronic system, the second input-output of the on-board information-control system is connected to the first input-output of the radio-controlled interlock explosive devices, the third input-output of the on-board information and control system is connected to the first input and output of the radiation reconnaissance complex, the fourth input and output of the on-board information and control system connected to the first input-output of the power supply system, the fifth input-output of the on-board information and control system is connected to the first input and output of the life support system, while the first output of the television viewing device is connected to the sixth input of the on-board information and control system, the first input-output of the system projection lighting is connected to the eighth input-output of the onboard information-control system, the first input-output of the mine detection complex is connected to the ninth in one output of the on-board information and control system, the second output of the power supply system is connected to the seventh input of the on-board information and control system, the second input of the optoelectronic system, the second input of the jammer of radio-controlled explosive devices, the second input of the radiation reconnaissance complex, the second input of the television viewing device, the second the entrance of the life support system, the second input of the projector lighting system, the second input of the mine-explosive obstacle detection complex. 2. The technical reconnaissance fighting vehicle according to claim 1, characterized in that the on-board information and control system contains an automated workplace for the commander, designed to control reconnaissance equipment and the crew of the machine, an automated workplace for the operator, designed for optical-electronic and radiation reconnaissance, observation of samples of weapons and military equipment on the battlefield in the daytime and at night, in the presence of precipitation, smoke curtains and dusting of the atmosphere, communication equipment designed to sintering communications with a higher command link and crew members, internal communication and switching equipment, designed to provide commutation of communication means and internal crew communication, inertial-navigation equipment, designed to determine the course and location of the machine in conditions of the enemy using electronic means of suppressing satellite navigation systems, satellite navigation equipment designed to determine the coordinates of the vehicle’s location, ground speed and track angle, p and the first input-output of the operator’s automated workstation is connected to the first input-output of the commander’s automated workstation, the second input-output of which is connected to the first input-output of the internal communication and switching equipment, the third input-output of the said internal communication and switching equipment is connected to the first input-output of communication equipment, the second input-output of the operator’s workstation is connected to the second input-output of the equipment of internal communication and switching, while the third input is automatic of the operator’s workstation is connected to the first output of the inertial navigation equipment, the second input of which is connected to the first output of the satellite navigation equipment. 3. A technical reconnaissance fighting vehicle according to claim 2, characterized in that the communication equipment comprises a radio station designed to provide communication to the crew with a higher command link and an antenna-feeder device, which consists of an antenna designed to receive and transmit messages via VHF channel, the antenna lifting mechanism, designed to lift the antenna and connect the high-frequency cable to the radio station, the control panel, designed to control the position of the antenna and light indication of emergency mode, p In this case, the first input-output of the antenna is connected to the second input-output of the antenna lift mechanism, the third input-output of which is connected to the first input-output of the above control panel, the first input-output of the antenna lift mechanism is connected to the second input-output of the radio station. 4. The technical reconnaissance fighting vehicle according to claim 2, characterized in that the internal communication and switching equipment comprises an internal communication and switching unit for switching voice or telecode channels, broadcasting control and monitoring commands from the commander’s workstation to the radio station of the communication equipment, issuing warning voice signals to all crew members from the commander’s workstation, commander’s subscriber console, designed to provide a chest switch the receiver to the intercom and switching unit, receiving information on the switching status from the intercom and switching unit and indicating received information on the front panel of the unit, transmitting information about the state of the buttons and volume control located on the front panel of the unit to the intercom and switching unit operator’s and driver’s subscriber’s panels, designed to connect the chest switch to the internal communication and switching unit, generate a volume control signal, chest straps recipients of the commander, operator and driver, designed to connect tank headsets to the subscriber console of the commander, subscriber panels of the operator and driver, generate commands for the tone signal and the control signal of the operating mode of the radio communications equipment, with the first input-output unit of internal communication and switching connected to the first input-output of the commander’s subscriber console, the second input-output of said intercom and switching unit is connected to the first input-output of the subscriber’s console the operator and the first input-output of the subscriber console of the driver, the second input-output of the subscriber console of the commander is connected to the first input-output of the chest switch of the commander, the second input-output of the subscriber console of the operator is connected to the first input-output of the chest switch of the operator, the second input-output of the subscriber console the driver is connected to the first input-output of the chest switch of the driver, while the third input-output of the said unit of internal communication and switching is connected to the first input-output of the communication unit ba ovogo, the second input-output of which is connected to the first input-output of the antenna. 5. The technical reconnaissance fighting vehicle according to claim 2, characterized in that the inertial-navigation equipment contains an inertial-navigation unit and an on-board computing unit, which consists of an interface unit for receiving and transmitting information data between machine elements, a panel computer designed for solving combat missions and displaying an electronic navigation map, navigation and reconnaissance data on a display, plotting the location of damaged weapons and military equipment technicians on an electronic navigation map, determining the access and evacuation routes for the deployment of repair and restoration bodies on an electronic navigation map, a network data storage device designed to store a combat geographic information system, a solid state data storage device designed to store an electronic navigation map, navigation and reconnaissance data, hardware-software module of trust loading and a path measuring sensor designed to measure the distance covered of the way, the first output of the inertial navigation unit is connected to the first input of the interface unit, the second input-output of which is connected to the first input-output of the panel computer, the second input-output of which is connected to the first input-output of the network data storage device, the second input is the output of which is connected to the first input-output of the solid-state data storage device, while the first input-output of the aforementioned hardware-software trust download module is connected to the third input-output of the panel computer, the first output said path measurement sensor connected to a second input of the inertial navigation unit.

Images