RU2717282C2 - Air weapon control system - Google Patents

Abstract

FIELD: aviation.

SUBSTANCE: invention relates to on-board equipment of aircraft and is intended for control of preparation and use of aircraft engagement means. System comprises an integrated controller of autonomous operation, a multiplex channel of information exchange, single-channel actuating units, lines of transmission of analogue signals and single commands, the first unit of distribution and conversion of information, multiplex channel for transmitting data to aircraft hitting means, additionally including multichannel execution units, second information distribution and conversion unit, mounting unit, autonomous operation panel, ground preparation console. Expanded functional capabilities.

EFFECT: higher controllability and information value, degree of energy and information integration with aircraft engagement facilities and on-board equipment of aircrafts.

5 cl, 5 dwg

Description

Aircraft Weapons Management System

The invention relates to on-board equipment of aircraft and is intended to control the preparation and use of aircraft weapons.

A known control system for aviation weapons, containing a controller of energy and information channels and interface units, the controller is connected via an intersystem multiplex data transmission channel with a set of on-board equipment, through a local multiplex data transmission channel - with interface units connected by an energy channel to aircraft weapons , by separate communication lines, the controller and interface units are connected to the aircraft’s power system and to the organ control units located in the cockpit of the aircraft (IPC B 64 D 7/00, RF patent No. 2350512, publ. 20.10.2008).

The disadvantages of this system are:

- limited functionality that does not allow connecting more than one aviation weapon to the interface units;

- limited functionality that does not allow the discharge of suspended fuel tanks when they are placed at the suspension points of aircraft weapons;

- limited functionality that does not allow the opening of the hatch leaves before using aircraft weapons when placing suspension points and aircraft weapons inside the fuselage of the aircraft;

- limited functionality that does not allow the control of aircraft weapons, having means of protection against unauthorized use;

- insufficient reliability of operation and fault tolerance in case of failure of the controller, intersystem or local multiplex data transmission channels;

- a low degree of ensuring controllability and information content in the conditions of preflight training on the ground and in flight;

- low noise immunity during "hot" disconnection of aircraft weapons from the object - the side of the aircraft;

- a low degree of mechanical interfacing with structural elements of aircraft, which complicates the installation of components on board the aircraft.

Also known is a control system for aviation weapons, containing a controller of energy and information channels and interface units, while the controller is connected via an intersystem multiplex data transmission channel with a set of on-board equipment, and through a local multiplex data transmission channel, with interface units connected by an energy channel and a multiplex channel data transmission to aircraft weapons with aircraft weapons, separate control lines The unit and interface units are connected to the aircraft’s power system and to the controls located in the aircraft’s cockpit, each of the interface units is connected to an intersystem multiplex data transmission channel and the corresponding multiplex data transmission channel to aircraft weapons by an additional multiplex channel (IPC B 64 D 7 / 00, F 41 F 3/06, G 06 F 17/00 RF patent No. 2392192, publ. 06/20/2010).

The system has disadvantages:

- limited functionality that does not allow connecting more than one aviation weapon to the interface units;

- limited functionality that does not allow the discharge of suspended fuel tanks when they are placed at the suspension points of aircraft weapons;

- limited functionality that does not allow the opening of the hatch leaves before using aircraft weapons when placing suspension points and aircraft weapons inside the fuselage of the aircraft;

- limited functionality that does not allow to control aircraft weapons, having special means of protection against unauthorized use;

- insufficient reliability of operation and fault tolerance in case of failure of the intersystem multiplex data transmission channel;

- a low degree of ensuring controllability and information content in the conditions of preflight training on the ground and in flight;

- a low degree of mechanical interfacing with structural elements of aircraft, which complicates the installation of components on board the aircraft.

The closest prototype to the claimed technical solution is a weapon control system containing an on-board digital computer, a unit for specifying the modes of preparation and use of weapons, units for selecting the type and logic of the weapon according to the number of suspension points, an information conversion unit, a switching unit, a weapon interface unit and a unit interfacing with airborne equipment (IPC G 06 F 19/00, G 06 F 171/00, F 41 F 3/06 RF patent No. 2179335, publ. 02/10/2002).

This system solves the problem of increasing the controllability and information content in flight, integration with the aircraft information system, but its disadvantages are:

- limited functionality that does not allow connecting more than one aviation weapon to the weapon type and logic selection blocks;

- limited functionality that does not allow the discharge of suspended fuel tanks when they are placed at the suspension points of aircraft weapons;

- limited functionality that does not allow the opening of the hatch leaves before using aircraft weapons when placing suspension points and aircraft weapons inside the fuselage of the aircraft;

- limited functionality that does not allow to control aircraft weapons, having special means of protection against unauthorized use;

- insufficient operational reliability and fault tolerance in case of disruption of the information exchange channels between the weapon type and logic selection units and aviation weapons, between the onboard digital computer and the weapon interface units;

- a low degree of ensuring controllability and information content in the conditions of preflight training on the ground and in flight;

- a low degree of mechanical interfacing with structural elements of aircraft, which complicates the installation of components on board the aircraft.

The technical task of the claimed invention is the creation of a system that allows you to expand the functionality, increase the reliability of operation and fault tolerance, controllability and information content, the degree of mechanical interfacing with the structural elements of the aircraft control systems of aviation weapons.

The problem is solved as follows.

Option 1. The control system for aviation weapons containing an integrated controller of autonomous operation, a multiplex information exchange channel, single-channel executive blocks, transmission lines for analog signals and one-time commands, the first block for the distribution and conversion of information, a multiplex channel for transmitting data to aircraft weapons are additionally introduced multichannel executive blocks, the second block of information distribution and conversion, mounting block, stand-alone remote control you, a ground-based training console, whereby the first input-output of the integrated autonomous operation controller is connected via a multiplexed data exchange channel with the aircraft onboard equipment mated, the first inputs and outputs of the first and second information distribution and conversion blocks, the first inputs and outputs of single-channel executive and multi-channel blocks executive units, the second and fifth groups of entrances, the third and fourth groups of exits - with mating avionics apparatus, sixth inputs and outputs - with inputs and outputs of the stand-alone remote control and ground preparation console, the eighth and seventeenth inputs and outputs - with third inputs and outputs of multi-channel executive units, which, in turn, are transmitted via analog signal and single command transmission lines and, accordingly, the fifth , the sixth, seventh and eighth points of the suspension are connected to aircraft weapons, the ninth, tenth, eleventh, twelfth, thirteenth, fourteenth, fifteenth and sixteenth inputs-outputs - with third inputs-outputs dams of single-channel executive units, which in turn are through analogue signal and single-command transmission lines, multiplexed data transmission channels to aviation weapons and, accordingly, the first, second, third, fourth, ninth, tenth, eleventh and twelfth suspension points are connected to aviation weapons , the second and third inputs of the first and second blocks of information distribution and conversion are connected to the mated aircraft equipment, and the fourth inputs and outputs - through respectively the first, second, third, fourth, fifth, sixth, seventh, eighth, ninth, tenth, eleventh and twelfth suspension points with aviation weapons, an integrated battery controller, the first and second information distribution and conversion units are placed on / in assembly unit, information, mechanical and electrical interfaces of the elements of the aircraft weapon control system located on / in the assembly unit, with mated aircraft avionics Arata, actuating single-channel units, executive units multichannel, remote battery life, the remote ground training and aviation destruction means via the mounting unit.

Option 2. It is characterized in that the information distribution and conversion unit, the sash control unit, the first and second outboard fuel tank discharge control units, the sash control panel, the first and second assembly units are additionally introduced, the first input-output of the integrated autonomous operation controller being connected via multiplex channel of information exchange with interfaced onboard equipment of the aircraft, the first inputs and outputs of the information distribution and conversion unit and the control unit sashes, the first inputs and outputs of single-channel blocks of executive and multi-channel blocks of executive, the eighteenth input-output - with the first input-output of the first control unit dumping outboard fuel tanks, the second inputs and outputs of which are connected through the ninth point of the suspension with aviation weapons, the nineteenth input -exit - with the first input-output of the second control unit dumping outboard fuel tanks, the second inputs-outputs of which are connected through the tenth point of the suspension with aircraft defeat, the fourth inputs and outputs of the distribution and information conversion unit are connected through the seventh, eighth, ninth, tenth, eleventh and twelfth suspension points, respectively, with aviation means of destruction, the outputs of the remote control are connected to the inputs of the first and second control units for dumping outboard fuel tanks, the second inputs and outputs of the sash control unit are connected to the inputs and outputs of the sash control panel, the third inputs and outputs are connected to the mating equipment on board the aircraft ATA, fourth inputs and outputs - with shutters of the first, second, third, fourth, fifth and sixth suspension points, multi-channel executive units via analog signal and single command transmission lines, multiplex data transmission channels to aircraft weapons and, accordingly, the fifth, sixth, seventh and the eighth suspension point are connected to aviation weapons, the integrated autonomous operation controller and the sash control unit are located on / in the first mounting unit, the distribution and conversion unit Formations are located on / in the second assembly block.

Option 3. It is distinguished by the fact that an information distribution and conversion unit, sash control unit, first and second outboard fuel tank discharge control units, sash control panel, first and second mounting units, aircraft weapon control panel, and aircraft weapon control unit are additionally introduced and a multiplex information exchange channel, the first input-output of the integrated battery controller being connected via a multiplex information exchange channel and with the mating equipment on board the aircraft, the first inputs and outputs of the information distribution and conversion unit and the sash control unit, the first inputs and outputs of the single-channel executive and multi-channel executive blocks, the fifth input-output of the aircraft weapon control unit, the eighteenth input-output - with the first input-output of the first control unit dumping outboard fuel tanks, the second inputs and outputs of which are connected through the ninth point of the suspension with aviation means of destruction, the nineteenth input-output - with the first input-output of the second control unit for dumping outboard fuel tanks, the second inputs and outputs of which are connected through the tenth point of the suspension with aviation means of destruction, the twentieth input-output - with the sixth input-output of the control unit, fourth the inputs and outputs of the information distribution and conversion unit are connected through the seventh, eighth, ninth, tenth, eleventh and twelfth points of the suspension with aviation weapons, respectively, the first outputs The autonomous operation is connected to the first inputs of the aircraft weapon control unit, the second outputs to the inputs of the first and second control units for dumping outboard fuel tanks, the second inputs and outputs of the sash control unit are connected to the inputs and outputs of the sash control panel, and the third inputs and outputs are connected to mated onboard equipment of the aircraft, the fourth inputs and outputs - with leaflets of the first, second, third, fourth, fifth and sixth points of the suspension, multi-channel actuating units via and transmission of analog signals and one-time commands, multiplex data transmission channels to aviation weapons and, accordingly, the fifth, sixth, seventh and eighth suspension points are connected to aviation weapons, the inputs of the aircraft weapon control panel are connected through the seventh, eighth, ninth and tenth suspension points with aviation weapons, outputs - with the seventh inputs of the control unit, the second inputs of the aircraft weapons control unit are connected to the mating side m aircraft equipment, the third input-output - through the seventh, eighth, ninth and tenth points of the suspension with aviation weapons, the fourth input-output - through the multiplex information channel, the seventh, eighth, ninth and tenth suspension points with aviation weapons, an integrated autonomous operation controller and a leaf control unit are located on / in the first mounting unit, an information distribution and conversion unit is located on / in the second mounting unit.

Option 4. It is distinguished by the fact that an information transmission line is additionally introduced, and the seventh input-output of the integrated autonomous operation controller is connected via an information transmission line to the second inputs and outputs of the single-channel executive units and multi-channel executive units, the second inputs and outputs of the ground preparation console are connected to mated aircraft equipment.

Option 5. It is distinguished by the additional introduction of a control panel for aviation weapons, a control unit for aviation weapons, a multiplex information exchange channel, an information transfer line and a third assembly block, moreover, the first input-output of the integrated offline controller is connected via a multiplex information exchange channel with interfaced aircraft equipment, the first inputs and outputs of the first and second distribution and information conversion units and, the first inputs and outputs of single-channel blocks of executive and multi-channel blocks of executive, the fifth input-output of the control unit, the seventh input-output - through the data line with the mated aircraft equipment, the second inputs and outputs of single-channel blocks of executive and multi-channel blocks of executive, the twentieth input-output - with the sixth input-output of the control unit for aviation weapons, the first outputs of the remote control are connected to the first inputs of the control unit phenomena by aviation means of destruction, the second outputs - with the mating equipment on board the aircraft, multi-channel executive units via transmission lines of analog signals and one-time commands, multiplex data transmission channels to aviation means of destruction and, respectively, the fifth, sixth, seventh and eighth suspension points are connected to aviation means defeat, the input-output of the control panel of aviation weapons is connected to the seventh input-output of the control unit of aircraft and defeats, the third inputs and outputs of the control unit for aviation weapons are connected through the first, second, eleventh and twelfth points of suspension with aviation weapons, the fourth input-output is through a multiplexed information exchange channel, the first, second, eleventh and twelfth points of suspension with aviation means of destruction, the second inputs and outputs of the ground preparation console are connected to the mating equipment of the aircraft, the control unit of aviation means of destruction once placed on / in the third assembly block.

The set of distinctive features of the claimed invention provides the fulfillment of the technical task.

The claimed invention is illustrated by drawings, where:

- FIG. 1 is a functional diagram of embodiment 1 of the claimed invention;

- FIG. 2 is a functional diagram of option 2 of the claimed invention;

- FIG. 3 is a functional diagram of a variant 3 of the claimed invention;

- FIG. 4 is a functional diagram of embodiment 4 of the claimed invention;

- FIG. 5 is a functional diagram of embodiment 5 of the claimed invention.

Option 1. The aircraft weapon control system contains an integrated autonomous operation controller 1, a multiplex information exchange channel 2, single-channel executive units 3, transmission lines for analog signals and one-time commands 4, the first 5 and second 8 information distribution and conversion blocks, multi-channel executive units 6 , a multiplex channel for transmitting data to aviation weapons 7, mounting block 9, remote control 10 and the ground preparation console 11.

In this case, the first input-output of the integrated autonomous operation controller 1 is connected via a multiplex information exchange channel 2 to the aircraft onboard equipment mating, the first inputs and outputs of the first 5 and second 8 information distribution and conversion blocks, the first inputs and outputs of single-channel executive 3 and multi-channel executive units 6, the second and fifth groups of entrances, the third and fourth groups of exits - with interfaced aircraft equipment, the sixth entrances are outputs - with inputs and outputs of the stand-alone operation panel 10 and the ground-based training console 11, the eighth and seventeenth inputs and outputs - with the third inputs and outputs of the multi-channel actuating units 6, which in turn are transmitted through analog signal transmission lines and one-off commands 4 and, accordingly, the fifth 5th , the sixth 6TP, the seventh 7TP and the eighth 8TP suspension points are connected to aviation weapons, the ninth, tenth, eleventh, twelfth, thirteenth, fourteenth, fifteenth and sixteenth inputs and outputs - with third inputs and outputs single-channel executive blocks 3, which in turn are through analog signal and single command transmission lines 4, multiplex data transmission channels to aviation weapons 7 and, accordingly, the first 1tp, second 2tp, third 3tp, fourth 4tp, ninth 9tp, tenth 10tp, eleventh 11tp and the twelfth 12tp suspension points are connected to aircraft weapons, the second and third inputs of the first 5 and second 8 information distribution and conversion units are connected to the mating equipment on board the aircraft ATA, and the fourth inputs and outputs - through the first 1tp, second 2tp, third 3tp, fourth 4tp, fifth 5tp, sixth 6tp, seventh 7tp, eighth 8tp, ninth 9tp, tenth 10tp, eleventh 11tp and twelfth 12tp air suspension points defeat, integrated autonomous operation controller 1, the first 5 and second 8 information distribution and conversion units are located on / in the mounting unit 9, information, mechanical and electrical interfaces of the elements of the aircraft weapon control system located on / Block assembly 9, with the mating equipment onboard the aircraft, actuators 3 single-channel units, executive units 6 multichannel, remote battery life 10, remote control 11 and the ground training aviation destruction means through the mounting block 9.

Option 2. It differs from option 1 in that the system contains one information distribution and conversion unit 5, sash control unit 12, first 13 and second 14 outboard fuel tank discharge control units, sash control panel 15, first 9 and second 16 mounting units.

In this case, in contrast to option 1, the first input-output of the integrated autonomous operation controller 1 is connected via a multiplex information exchange channel 2 with the aircraft onboard equipment mating, the first inputs and outputs of the information distribution and conversion unit 5 and the sash control unit 12, the first inputs - the outputs of single-channel executive units 3 and multi-channel executive units 6, the eighteenth input-output - with the first input-output of the first control unit dumping outboard fuel tanks 13, the second inputs and outputs of which are connected through the ninth suspension point 9tp with aircraft weapons / outboard fuel tanks, the nineteenth input-output - with the first input-output of the second control unit for dumping the outboard fuel tanks 14, the second inputs and outputs of which are connected through the tenth a suspension point 10tp with aircraft weapons / outboard fuel tanks, the fourth inputs and outputs of the information distribution and conversion unit 5 are connected through a seventh 7tp, an eighth 8tp, a ninth 9tp, respectively tenth 10tp, eleventh 11tp and twelfth 12tp of the suspension point with aviation weapons, the outputs of the autonomous operation 10 are connected to the inputs of the first 13 and second 14 control units for dumping outboard fuel tanks, the second inputs and outputs of the control unit for the sash 12 are connected to the inputs and outputs of the control panel 15, the third inputs and outputs - with the mating equipment of the aircraft, the fourth inputs and outputs - with the leaves of the first 1TP, second 2TP, third 3TP, fourth 4TP, fifth 5TP and sixth 6TP suspension points ki, multi-channel actuating units 6 via analog signal and single command transmission lines 4, multiplex data transmission channels to aviation weapons 7 and, respectively, fifth 5th, 6th 6th, 7th 7th and 8th 8th suspension points are connected to aviation means of destruction, integrated autonomous operation controller 1 and the sash control unit 12 is located on / in the first mounting unit 9, the information distribution and conversion unit 5 is placed on / in the second mounting unit 16.

Option 3. It differs from option 1 in that the system comprises at least one information distribution and conversion unit 5, sash control unit 12, first 13 and second 14 outboard fuel tank discharge control units, sash control panel 15, first 9 and second 16 mounting blocks, control panel for aviation weapons of destruction 17, control module for aviation weapons of destruction 18 and multiplex information exchange channel 19.

In this case, in contrast to option 1, the first input-output of the integrated autonomous operation controller 1 is connected via a multiplex information exchange channel 2 with the aircraft onboard equipment mating, the first inputs and outputs of the information distribution and conversion unit 5 and the sash control unit 12, the first inputs - the outputs of single-channel executive units 3 and multi-channel executive units 6, the fifth input-output of the control unit for aviation weapons 18, the eighteenth input-output - with the first input-output of the first control unit for dumping outboard fuel tanks 13, the second inputs-outputs of which are connected through the ninth point of the suspension 9tp with aviation weapons / outboard fuel tanks, the nineteenth input-output - with the first input-output of the second control unit for dumping the outboard fuel tanks 14, the second input-output of which is connected through the tenth point of the suspension 10tp with aircraft weapons / outboard fuel tanks, the twentieth input-output - with the sixth input-output of the control unit by means of destruction weapons 18, the fourth inputs and outputs of the information distribution and conversion block 5 are connected through the seventh 7th, 8th, 8th, 9th, 10th, 10th, 11th and 11th and 12th suspension points of the suspension with aviation weapons, the first outputs of the stand-alone operation panel 10 are connected to the first inputs of the control unit for aviation weapons 18, the second outputs - with the inputs of the first 13 and second 14 control units dumping outboard fuel tanks, the second inputs and outputs of the control unit the mats 12 are connected to the inputs and outputs of the control panel of the shutters 15, the third inputs and outputs are with the mating equipment of the aircraft, the fourth inputs and outputs are with the shutters of the first 1tp, second 2tp, third 3tp, fourth 4tp, fifth 5tp and sixth 6tp suspension points , multi-channel actuating units 6 through analogue signal transmission lines and one-off commands 4, multiplex data transmission channels to aviation weapons 7 and the fifth fifth 5th, sixth 6th, 7th seventh and 8th eighth suspension points connected to the AV by means of defeat means, the inputs of the control panel of aviation means of destruction 17 are connected through the seventh 7tp, eighth 8tp, ninth 9tp and tenth 10tp of the suspension point with aviation means of destruction, the outputs are with the seventh inputs of the control unit of aviation means of destruction 18, the second inputs of the control unit of aviation means of destruction 18 are connected to the mating equipment of the aircraft, the third inputs and outputs through the seventh 7tp, eighth 8tp, ninth 9tp and tenth 10tp suspension points with aviation means of destruction, the fourth input-output - through the multiplexed information exchange channel 19, the seventh 7th, the eighth 8th, the ninth 9th and the tenth 10th point of the suspension with aviation means of destruction, the integrated battery controller 1 and the sash control unit 12 are located on / in the first mounting block 9, the information distribution and conversion unit 5 is located on / in the second mounting unit 16.

Option 4. It differs from option 1 in that the system contains an information transmission line 20.

In this case, in contrast to option 1, the seventh input-output of the integrated autonomous operation controller 1 is connected via an information line 20 to the second inputs and outputs of single-channel executive units 3 and multi-channel executive units 6, the second inputs and outputs of the ground preparation console 11 are connected to the interfaced onboard equipment of the aircraft.

Option 5. It differs from option 1 in that the system comprises a control panel for aviation weapons of destruction 17, a control unit for aircraft weapons of destruction 18, a multiplex information exchange channel 19, an information transmission line 20 and a third mounting block 21.

At the same time, in contrast to option 1, the first input-output of the integrated autonomous operation controller 1 is connected via a multiplex information exchange channel 2 to the aircraft onboard equipment mating, the first inputs and outputs of the first 5 and second 8 information distribution and conversion blocks, the first inputs the outputs of single-channel executive blocks 3 and multi-channel executive blocks 6, the fifth input-output of the control unit for aviation weapons 18, the seventh input-output through a transmission line and information 20 with the mating equipment on board the aircraft, the second inputs and outputs of the single-channel executive units 3 and multi-channel executive units 6, the twentieth input-output - with the sixth input-output of the aircraft weapon control unit 18, the first outputs of the autonomous operation panel 10 are connected to the first the inputs of the control unit for aviation weapons 18, the second outputs - with the mated on-board equipment of the aircraft, multi-channel executive units 6 through lines in front of analog signals and one-time commands 4, multiplex data transmission channels to aviation weapons 7 and fifth 5th, 6th, 6th, 7th and 8th and 8th respectively 8th suspension points are connected to aviation weapons, the input-output of the control panel of aviation weapons 17 is connected to the seventh the input-output of the control unit for aircraft weapons 18, the third inputs and outputs of the control unit for aircraft weapons 18 are connected through the first 1tp, second 2tp, eleventh 11tp and twelfth 12 p suspension points with aviation weapons, the fourth input-output - through the multiplexed information exchange channel 19, the first 1TP, second 2TP, 11th 11TP and 12th 12TP suspension points with aviation weapons, the second inputs and outputs of the ground preparation console 11 are connected to the mating side the equipment of the aircraft, the control unit for aviation weapons 18 is located on / in the third block mounting 21.

The order of the system.

Option 1. Single-channel executive units 3, multi-channel executive units 6, mounting unit 9 with integrated autonomous operation controller 1, first 5 and second 8 information distribution and conversion units, autonomous operation unit 10 and ground preparation unit 11 are placed ( mounted) on board the aircraft.

Ground-based preparation for use (operation) and pre-flight testing (serviceability monitoring) of hardware and software of the aircraft weapon control system are carried out.

By means of the ground preparation console 11, electric power is supplied from the aircraft’s onboard power sources connected to the airfield power supply to electric energy consumers from the control system of aviation weapons.

Occurs:

- in the integrated controller of autonomous work 1 initialization of the pre-installed system and functional software;

- according to the information received from the inputs and outputs of the ground preparation console 11 to the sixth inputs and outputs of the integrated autonomous operation controller 1, as well as to the commands formed by the integrated autonomous operation controller 1, automatic testing and preparation for operation of hardware and software of the aircraft weapon control system : integrated autonomous operation controller 1, single-channel executive units 3, first 5 and second 8 information distribution and conversion units, multi-channel x executive blocks 6;

- by commands from the integrated controller of autonomous work 1 organization of interaction between the control system of aviation weapons and mating equipment on board the aircraft.

The presence and identification of types of aircraft weapons located at the suspension points of the aircraft 1TP-12TP are carried out. Checking the availability and identification of types of aircraft weapons are implemented using the integrated controller of autonomous operation 1, single-channel executive units 3 and multi-channel executive units 6. In this case, in series / in parallel:

- the formation and transmission of commands from the integrated controller of autonomous operation 1 through the first input-output to the first inputs and outputs of single-channel executive units 3 and multi-channel executive units 6 and / or through the eighth, ninth, tenth, eleventh, twelfth, thirteenth, fourteenth, fifteenth, sixteenth and seventeenth inputs and outputs to the corresponding third inputs and outputs of single-channel executive units 3 and / or multi-channel executive units 6;

- receiving commands arriving at the first and / or third inputs and outputs of single-channel executive units 3, performing means of single-channel executive units 3 of the corresponding switching circuits of direct and alternating current, which generate requests for determining the types of aircraft weapons located on the aircraft suspension points transmitted respectively, through the transmission lines of analog signals and one-time commands 4, multiplex data transmission channels to aviation weapons 7, the first 1TP, the second yu 2tp, third 3tp, fourth 4tp, ninth 9tp, tenth 10tp, eleventh 11tp and twelfth 12tp suspension points for aircraft weapons;

- receiving commands arriving at the first and / or third inputs and outputs of the multi-channel actuating units 6, performing means of the multi-channel executive units 6 of the corresponding switching DC circuits that generate requests for determining the presence of aircraft weapons at the aircraft suspension points (if necessary), respectively transmitted through analogue signal lines and one-off commands 4, fifth 5tp, sixth 6tp, seventh 7tp and eighth 8tp suspension points on aircraft I am;

- formation by aviation means of destruction of response signals to requests from the control system of aviation means of destruction that come through the suspension points of the aircraft 1tp - 12tp, transmission lines of analog signals and one-time commands 4 and multiplex data transmission channels to aviation means of destruction 7 into single-channel executive units 3 through the transmission lines of analog signals and one-time commands 4 to multi-channel executive blocks 6 (if necessary);

- receiving response signals from aviation means of destruction by multi-channel executive units 6, generating means of multi-channel blocks of executive 6 information on the presence / absence and type of aircraft means of destruction, respectively, at the fifth 5tp, sixth 6tp, seventh 7tp and eighth 8tp suspension points, its transmission from the first inputs - the outputs of the multi-channel executive units 6 to the first input-output of the integrated controller of autonomous operation 1 and / or from the third inputs and outputs of the multi-channel executive units 6 respectively venno the eighth and seventeenth inputs and outputs of the integrated controller 1, battery life (if necessary);

- receiving response signals from aviation weapons by single-channel executive units 3, generating means of single-channel executive units 3 information on the presence / absence and type of aircraft weapons, respectively, at the first 1tp, second 2tp, third 3tp, fourth 4tp, ninth 9tp, tenth 10tp, eleventh 11tp and twelfth 12tp suspension points, its transmission from the first inputs and outputs of single-channel actuating units 3 to the first input-output of the integrated autonomous controller 1 and / or from the third input a single-channel-output units respectively actuators 3 on the ninth, tenth, eleventh, twelfth, thirteenth, fourteenth, fifteenth and sixteenth input-output integrated controller 1, battery life (if necessary);

- reception, reliability control and processing of information received at the first input-output and / or eighth, ninth, tenth, eleventh, twelfth, thirteenth, fourteenth, fifteenth, sixteenth and seventeenth inputs and outputs of the integrated stand-alone controller 1, execution by means of functional software providing an integrated controller of autonomous work 1 control the presence and identification of types of aircraft weapons with reference to a specific suspension point of the aircraft.

Information about the results of testing and preparation for operation of hardware and software of the aircraft weapon control system from the sixth inputs and outputs of the integrated autonomous operation controller 1 is transmitted to the inputs and outputs of the ground preparation console 11 for indication. By means of the ground preparation console 11, information is displayed on the availability of power supply and the serviceability of the control system for aviation weapons.

Ground-based preparation for use and preflight testing of hardware and software for the aircraft weapon control system is nearing completion. By means of the ground preparation console 11, the control system of aircraft weapons from the onboard power sources of the aircraft is disconnected.

When you turn on the power system of the aircraft before the flight, electricity is supplied to consumers of electric energy from the control system of aviation weapons. Operations are performed similar to ground preparation for the use and preflight testing of hardware and software of the aircraft weapon control system.

Before flight and / or in flight using the controls and indicators of the remote control 10 and interfaced with the control system of aviation means of destruction of onboard equipment of the aircraft:

- the crew of the aircraft selects specific types, sets the modes of preparation and use of aircraft weapons;

- the control system of aviation weapons is carried out operations for the preparation and use of aircraft weapons.

Wherein:

- information about the types, modes of preparation and use of aircraft weapons from the inputs and outputs of the remote control 10 is transmitted to the sixth inputs and outputs of the integrated controller of autonomous work 1;

- in the integrated controller of autonomous work 1, a program is launched that provides the preparation and application of selected types of aircraft weapons for use, the formation of signals about the selected types of weapons with reference to specific suspension points;

- the mating on-board equipment of the aircraft, according to the algorithm, is configured to work with the control system of aviation weapons, specific suspension points and types of aircraft weapons;

- the first 5 and second 8 blocks of the distribution and conversion of information in accordance with commands from the integrated controller of autonomous operation 1 provide reception of information from the mated on-board equipment of the aircraft, received in digital form through the multiplex channel of information exchange 2 to the first inputs and outputs, its conversion to type, ensuring the safe operation of aircraft weapons, distribution between the suspension points of aircraft weapons and transmission from the fourth entrance in outputs through the first 1tp, the second 2tp, the third 3tp, the fourth 4tp, the fifth 5tp, the sixth 6tp, the seventh 7tp, the eighth 8tp, the ninth 9tp, the tenth 10tp, the eleventh 11tp and the twelfth 12tp suspension points in aircraft;

- the first 5 and second 8 blocks of the distribution and conversion of information in accordance with the commands from the integrated controller of autonomous work 1 produces the corresponding switching of information and electrical channels, ensuring the connection of the first inputs and outputs, second and third inputs with fourth inputs and outputs, i.e. mating aircraft equipment with the corresponding aviation weapons located at suspension points;

- the mating equipment on board the aircraft and the control system for aircraft weapons using special algorithms implement operations for the preparation and use of aircraft weapons, while:

a) carrying out information interaction between each other through the multiplex channel of information exchange 2;

b) carrying out information and / or electrical interaction between the integrated autonomous operation controller 1 and the mated onboard equipment of the aircraft through the second and fifth groups of inputs, the third and fourth groups of outputs, between the integrated autonomous operation controller 1 and single-channel executive units 3 through the ninth, tenth, eleventh, twelfth, thirteenth, fourteenth, fifteenth and sixteenth inputs-outputs of the integrated controller of autonomous work 1 - third inputs-output single-channel executive units 3, between the integrated autonomous operation controller 1 and multi-channel executive units 6 through the eighth and seventeenth inputs and outputs of the integrated autonomous operation controller 1 - third inputs and outputs of the multi-channel executive units 6, between the mated on-board equipment of the aircraft and aircraft at the first 1tp, second 2tp, third 3tp, fourth 4tp, fifth 5tp, sixth 6tp, seventh 7tp, eighth 8tp, ninth 9tp, tenth 10tp, eleventh 11tp and twelfth 12tp suspension points, through the second and third inputs, fourth inputs and outputs of the first 5 and second 8 information distribution and conversion blocks;

c) carrying out information and / or electrical interaction between single-channel executive units 3 and aviation weapons located at the first 1tp, second 2tp, third 3tp, fourth 4tp, 9th 9tp, tenth 10tp, 11th 11tp and 12th 12tp suspension points, via transmission lines analog signals and one-time commands 4 and multiplex data transmission channels to aviation means of destruction 7, between multichannel executive units 6 and aviation means of destruction, located on the fifth 5TP, stand 6tp, 7th 7th and 8th 8th suspension points, via analog signal transmission lines and one-off commands 4;

- information about the types of selected (applied) aircraft weapons, from the sixth inputs and outputs of the integrated battery controller 1 is transmitted to the inputs of the battery console 10, where it is displayed.

Option 2. It differs from option 1 as follows.

The first mounting block 9 with the integrated autonomous operation controller 1 installed on it and the sash control unit 12, the second mounting block 16 with the distribution and conversion unit 5 installed on / in it, the first 13 and second 14 outboard fuel tank dump control units, the control panel of the wings 15 are placed (mounted) on board the aircraft.

During ground preparation for the use (operation) and preflight testing (monitoring of serviceability) of hardware and software for the aircraft weapon control system, after the ground preparation console supplies 11 electric power from the aircraft’s onboard power sources, the following additionally occurs:

- according to the information received from the inputs and outputs of the ground preparation console 11 to the sixth inputs and outputs of the integrated autonomous operation controller 1, as well as to the commands formed by the integrated autonomous operation controller 1, automatic testing and preparation for operation of hardware and software of the aircraft weapon control system including an information distribution and conversion unit 5, a sash control unit 12, a first 13 and a second 14 control units for the discharge of outboard fuel tanks;

- receiving commands arriving at the first and / or third inputs and outputs of the multi-channel actuating units 6, performing means of the multi-channel executive units 6 of the corresponding switching DC circuits that generate requests for determining the presence of aircraft weapons at the aircraft suspension points (if necessary), transmitted respectively through the transmission lines of analog signals and one-time commands 4, multiplex data transmission channels to aviation weapons 7, fifth 5tp, sixth 6t , Seventh and eighth 7tp 8TP point suspension on aviation destruction means;

- formation by aviation means of destruction of response signals to requests from the control system of aviation means of destruction that come through the suspension points of the aircraft 1tp - 12tp, transmission lines of analog signals and one-time commands 4 and multiplex data transmission channels to aviation means of destruction 7 into single-channel executive units 3 and multi-channel executive units 6 (if necessary).

Before flying and / or in flight, using the controls and indicators of the autonomous operation panel 10, the sash control panel 15 and the aircraft’s onboard equipment mated to the aircraft’s control system, the crew of the aircraft is carried out including control of the shutters of the aircraft and dumping of suspended fuel tanks.

Wherein:

- commands about dumping the hanging tanks from the outputs of the remote control 10 are transmitted to the inputs of the first 13 and second 14 control units for dumping the hanging fuel tanks and / or from the eighteenth and nineteenth inputs and outputs of the integrated controller of autonomous work 1 - to the corresponding first inputs and outputs of the first 13 and a second 14 outboard fuel tank discharge control units (if necessary);

- in the first 13 and second 14 outboard fuel tank discharge control units, the received outboard tank discharge commands are converted into electrical signals that ensure the safe operation of the aircraft weapon control system, which through the second inputs and outputs of the first 13 and second 14 outboard fuel tank discharge control units , the ninth 9tp and the tenth 10tp are transmitted to the outboard fuel tanks (if necessary);

- leaf control commands from the inputs and outputs of the leaf control panel 15 are transmitted to the second inputs and outputs of the leaf control unit 12 and / or from the first input and output of the integrated autonomous operation controller 1 - through the multiplexed data exchange channel 2 to the first input and output of the leaf control unit 12 and / or from the mating equipment on board the aircraft - to the third inputs and outputs of the sash control unit 12 (if necessary);

- in the sash control unit 12, the received commands for opening the sash are converted into electrical signals that ensure the safe operation of the aircraft weapon control system, which are transmitted through the fourth inputs and outputs of the sash control unit 12 to the sashes of the first 1tp, second 2tp, third 3tp, fourth 4tp, fifth 5tp and sixth 6tp suspension points (if necessary);

- the information distribution and conversion unit 5, in accordance with the instructions from the integrated autonomous operation controller 1, provides reception of information from the mated on-board equipment of the aircraft, received in digital form via the multiplex channel of information exchange 2 to the first input-output, its conversion to a form that ensures safe operation of aircraft weapons, distribution between suspension points of aircraft weapons, and transmission from the fourth inputs and outputs through the saddle muyu 7tp, the eighth 8tp, the ninth 9tp, the tenth 10tp, the eleventh 11tp and the twelfth 12tp suspension points in aircraft weapons;

- the interfaced aircraft equipment and the aircraft weapon control system, using special algorithms, implement the operations of preparing and using aircraft weapons, as well as dumping suspended fuel tanks, while performing information and / or electrical interaction between the integrated autonomous operation controller 1, the distribution unit, and information conversion 5 and the sash control unit 12 through the multiplex channel of information exchange 2, between integra autonomous operation controller 1, the first 13 and second 14 outboard fuel tank discharge control units through the eighteenth and nineteenth inputs-outputs of the integrated autonomous operation controller 1, respectively, the first inputs and outputs of the first 13 and second 14 outboard fuel tank discharge control units, between the mating side the equipment of the aircraft and the leaf control unit 12 through the multiplex channel of information exchange 2 and / or the third inputs and outputs of the leaf control unit 12, between the block distribution and conversion of information 5 and aviation weapons located at the 7th 7th, 8th, 8th, 9th, 10th, 10th, 11th and 12th 12th points of the suspension points, through the fourth inputs and outputs of the information distribution and conversion unit 5, between the sash control unit 12 and the leaves of the first 1tp, the second 2tp, the third 3tp, the fourth 4tp, the fifth 5tp and the sixth 6tp of the suspension points through the fourth inputs and outputs of the sash control unit 12, between the first control unit for the discharge of outboard fuel tanks 13 and a suspended fuel tank located at the ninth 9tp point of the suspension of aircraft weapons through the second inputs and outputs of the first control unit for dumping the suspended fuel tanks 13, between the second control unit for the discharge of suspended fuel tanks 14 and a suspended fuel tank located at the tenth 10tp point of the suspension of the aircraft weapons through the second inputs and outputs of the second control unit dumping outboard fuel tanks 14, between single-channel units executive 3 and aircraft weapons, located at the first 1tp, second 2tp, third 3tp, fourth 4tp, ninth 9tp, tenth 10tp, eleventh 11tp and twelfth 12tp suspension points, through analog signal and single command transmission lines 4 and multiplex data transmission channels to aviation weapons 7, between multi-channel units executive 6 and aviation weapons located on the fifth 5thp, sixth 6thp, 7th 7th and 8th 8th points of the suspension, via analog signal and single command transmission lines 4 and multiplex data transmission channels to aviation means of destruction 7;

- information about the dumping of the suspended fuel tanks from the sixth inputs and outputs of the integrated autonomous operation controller 1 is transmitted to the inputs of the autonomous operation 10, where it is displayed;

- information about the opening / closing of the leaves, from the second inputs and outputs of the control panel of the wings 12 is transmitted to the inputs and outputs of the control panel of the wings 15, where it is displayed.

Option 3. It differs from option 1 as follows.

The first mounting block 9 with the integrated autonomous operation controller 1 installed on it and the sash control unit 12, the second mounting block 16 with the distribution and conversion unit 5 installed on / in it, the first 13 and second 14 outboard fuel tank dump control units, the control panel of the wings 15, the control panel of aviation weapons 17 and the control unit of aviation weapons 18 are located (mounted) on board the aircraft.

During ground preparation for the use (operation) and preflight testing (monitoring of serviceability) of hardware and software for the aircraft weapon control system, after the ground preparation console supplies 11 electric power from the aircraft’s onboard power sources, the following additionally occurs:

- according to the information received from the inputs and outputs of the ground preparation console 11 to the sixth inputs and outputs of the integrated autonomous operation controller 1, as well as to the commands formed by the integrated autonomous operation controller 1, automatic testing and preparation for operation of hardware and software of the aircraft weapon control system including information distribution and conversion unit 5, sash control unit 12, first 13 and second 14 control units for dumping outboard fuel tanks, control unit for aviation weapons 18;

- receiving commands arriving at the first and / or third inputs and outputs of the multi-channel actuating units 6, performing means of the multi-channel executive units 6 of the corresponding switching DC circuits that generate requests for determining the presence of aircraft weapons at the aircraft suspension points (if necessary), transmitted respectively through the transmission lines of analog signals and one-time commands 4, multiplex data transmission channels to aviation weapons 7, fifth 5tp, sixth 6t , Seventh and eighth 7tp 8TP point suspension on aviation destruction means;

- formation by aviation means of destruction of response signals to requests from the control system of aviation means of destruction that come through the suspension points of the aircraft 1tp - 12tp, transmission lines of analog signals and one-time commands 4 and multiplex data transmission channels to aviation means of destruction 7 into single-channel executive units 3 and multi-channel executive units 6 (if necessary).

Before flying and / or in flight, using the controls and indicators of the autonomous operation panel 10, the sash control panel 15, the aircraft weapon control panel 17, and the aircraft’s crew equipment mated to the aircraft weapon control system, the crew of the aircraft is carried out including management of special means of protection of aviation weapons from unauthorized use, aircraft shutters and dumping of outboard fuel tanks.

Wherein:

- commands about dumping the hanging tanks from the outputs of the remote control 10 are transmitted to the inputs of the first 13 and second 14 control units for dumping the hanging fuel tanks and / or from the eighteenth and nineteenth inputs and outputs of the integrated controller of autonomous work 1 - to the corresponding first inputs and outputs of the first 13 and a second 14 outboard fuel tank discharge control units (if necessary);

- in the first 13 and second 14 outboard fuel tank discharge control units, the received outboard tank discharge commands are converted into electrical signals that ensure the safe operation of the aircraft weapon control system, which through the second inputs and outputs of the first 13 and second 14 outboard fuel tank discharge control units , the ninth 9tp and the tenth 10tp are transmitted to the outboard fuel tanks (if necessary);

- leaf control commands from the inputs and outputs of the leaf control panel 15 are transmitted to the second inputs and outputs of the leaf control unit 12 and / or from the first input and output of the integrated autonomous operation controller 1 - through the multiplexed data exchange channel 2 to the first input and output of the leaf control unit 12 and / or from the mating equipment on board the aircraft - to the third inputs and outputs of the sash control unit 12 (if necessary);

- in the sash control unit 12, the received commands for opening the sash are converted into electrical signals that ensure the safe operation of the aircraft weapon control system, which are transmitted through the fourth inputs and outputs of the sash control unit 12 to the sashes of the first 1tp, second 2tp, third 3tp, fourth 4tp, fifth 5tp and sixth 6tp suspension points (if necessary);

- the information distribution and conversion unit 5, in accordance with the instructions from the integrated autonomous operation controller 1, provides reception of information from the mated on-board equipment of the aircraft, received in digital form via the multiplex channel of information exchange 2 to the first input-output, its conversion to a form that ensures safe operation of aircraft weapons, distribution between suspension points of aircraft weapons, and transmission from the fourth inputs and outputs through the saddle muyu 7tp, the eighth 8tp, the ninth 9tp, the tenth 10tp, the eleventh 11tp and the twelfth 12tp suspension points in aircraft weapons;

- commands to control special means of protecting aviation weapons from unauthorized use from the outputs of the control panel of aircraft weapons 17 are transmitted to the seventh inputs of the control unit for aircraft weapons 18, and / or from the first outputs of the remote control 10 - to the first inputs of the control panel of aircraft weapons 18, and / or from the first input-output of the integrated controller of autonomous work 1 through the multiplex channel of information exchange 2 to the fifth input-output the control unit for aviation weapons of destruction 18, and / or from the mated on-board equipment of the aircraft - to the second inputs of the control unit 18, and / or from the twentieth input-output of the integrated controller of autonomous work 1 - to the sixth input-output of the control unit of aircraft weapons of destruction 18 ( if necessary);

- in the control unit for aviation weapons 18, the commands received to control special means of protecting aviation weapons against unauthorized use are converted into information and electrical signals that ensure the safe operation of the control system for aviation weapons and the weapons themselves, which through the third inputs and outputs of the aviation control unit means of defeat 18 and / or the fourth input-output of the control unit of aviation means of defeat Nia 18 by multiplex traffic channel 19 are transferred to the aviation destruction means, placed on the seventh 7tp, 8TP eighth, ninth and tenth 9tp 10tp hardpoints (if necessary);

- the interfaced aircraft equipment and the aircraft weapon control system, using special algorithms, implement the operations of preparing and using aircraft weapons, as well as dumping suspended fuel tanks, while performing information and / or electrical interaction between the integrated autonomous operation controller 1, the distribution unit, and information conversion 5, the control unit of the wings 12 and the control unit of aircraft weapons 18 through the multip information exchange channel 2, between the integrated autonomous operation controller 1, the first 13 and second 14 outboard fuel tank discharge control units through the eighteenth and nineteenth inputs-outputs of the integrated autonomous operation controller 1, respectively, the first inputs and outputs of the first 13 and second 14 discharge control units hanging fuel tanks, between the mated on-board equipment of the aircraft and the sash control unit 12 through the multiplex information exchange channel 2 and / or a third and the inputs and outputs of the sash control unit 12, between the information distribution and conversion unit 5 and aviation weapons located at the seventh 7th, 8th, 8th, 9th, 9th, 10th, 10th, 11th and 11th and 12th suspension points, through the fourth inputs and outputs of the distribution unit and information conversion 5, between the sash control unit 12 and the first 1tp, the second 2tp, the third 3tp, the fourth 4tp, the fifth 5tp and the sixth 6tp suspension points through the fourth inputs and outputs of the sash control unit 12, between the first the outboard fuel tank discharge control window 13 and the outboard fuel tank located at the ninth 9th point of the aircraft weapon suspension through the second inputs-outputs of the first outboard fuel tank discharge control unit 13, between the second outboard fuel tank discharge control unit 14 and the outboard fuel tank located at the tenth 10tp point of the suspension of aircraft weapons through the second inputs and outputs of the second control unit for dumping outboard fuel tanks 14, between the mated onboard equipment the aircraft and the control unit for aviation weapons of destruction 18 through the second inputs of the control unit for aviation weapons of destruction 18, between the integrated controller of autonomous operation 1 and the control unit for aviation weapons of destruction 18 through the twentieth input-output of the integrated controller of autonomous operation 1 - the sixth input-output of the control unit for aviation means of destruction 18, between the control unit of aviation means of destruction 18 and aviation means of destruction placed on the seventh 7th, 8th, 8th, 9th and 10th tenth points of the suspension via the third inputs and outputs of the aircraft weapon control unit 18 and / or the fourth input and output of the aircraft weapon control unit 18 via the multiplex information exchange channel 19, between the single-channel executive units 3 and aircraft weapons located at the first 1tp, second 2tp, third 3tp, fourth 4tp, 9th 9tp, 10th 10tp, 11th 11tp and 12th 12tp suspension points, via analog transmission lines with signals and single commands 4 and multiplex data transmission channels to aviation means of destruction 7, between multi-channel executive units 6 and aviation means of destruction, located at the fifth 5thp, sixth 6thp, 7th 7th and 8th eighth 8th suspension points, through analog signal and single command transmission lines 4 and multiplex data transmission channels to aviation weapons 7;

- information about the dumping of the suspended fuel tanks from the sixth inputs and outputs of the integrated autonomous operation controller 1 is transmitted to the inputs of the autonomous operation 10, where it is displayed;

- information about the opening / closing of the leaves, from the second inputs and outputs of the control panel of the wings 12 is transmitted to the inputs and outputs of the control panel of the wings 15, where it is displayed;

- information on the condition of aircraft weapons located at the 7th 7th, 8th, 8th, 9th and 10th 10th points of the suspension point is fed to the inputs of the aircraft’s weapon control panel 17, where it is displayed.

Option 4. Differs from option 1 as follows.

During ground preparation for the use (operation) and preflight testing (monitoring of serviceability) of hardware and software for the aircraft weapon control system, after the ground preparation console supplies 11 electric power from the aircraft’s onboard power sources, the following additionally occurs:

- organization of interaction between the integrated autonomous operation controller 1, single-channel executive units 3 and multi-channel executive units 6 via an information line 20 through the seventh input-output of the integrated autonomous operation controller 1 - second inputs and outputs of single-channel executive units 3 and multi-channel executive units 6;

- according to the information generated by the means of the ground training console 11 (taking into account the commands received from the mated on-board equipment of the aircraft through the second inputs and outputs of the ground training console 11) coming from the first inputs and outputs of the ground training console 11 to the sixth inputs and outputs of the integrated controller autonomous work 1, as well as teams formed by the integrated controller of autonomous work 1, automatic testing and preparation for operation of hardware and software of the av control system Discount means lesion: the integrated controller 1, battery life, single-channel units actuators 3, the first 5 and the second distribution 8 and converting information blocks multichannel blocks actuators 6.

When checking the availability and identification of types of aircraft weapons located on the suspension points of the aircraft 1TP-12TP additionally occurs:

- the formation and transmission of commands from the integrated controller of autonomous operation 1 through the seventh input-output to the second inputs-outputs of single-channel executive units 3 and multi-channel executive units 6;

- receiving commands received at the first, and / or second, and / or third inputs and outputs of single-channel executive units 3, execution by means of single-channel executive units 3 of the corresponding switching circuits of direct and alternating current, which generate requests for determining the types of aircraft weapons placed on suspension points of the aircraft, transmitted respectively through the transmission lines of analog signals and one-time commands 4, multiplexed data channels to aircraft weapons 7, ne 1tp-hand, second 2m, 3tp third, fourth 4tp, 9tp ninth, tenth 10tp, eleventh and twelfth 11tp 12tp point suspension on aviation destruction means;

- receiving commands arriving at the first, and / or second, and / or third inputs and outputs of the multi-channel actuating units 6, performing means of the multi-channel executive units 6 of the corresponding switching DC circuits that generate requests for determining the presence of aircraft weapons at the aircraft suspension points apparatus (if necessary), respectively transmitted through the transmission lines of analog signals and one-time commands 4, fifth 5tp, sixth 6tp, seventh 7tp and eighth 8tp suspension points on aircraft lesions;

- receiving response signals from aviation means of destruction by multi-channel executive units 6, generating means of multi-channel blocks of executive 6 information on the presence / absence and type of aircraft means of destruction, respectively, at the fifth 5tp, sixth 6tp, seventh 7tp and eighth 8tp suspension points, its transmission from the first inputs - the outputs of the multi-channel executive units 6 to the first input-output of the integrated autonomous operation controller 1, and / or from the second inputs and outputs of the multi-channel executive units 6 to the seventh integrated controller input-output battery life 1 and / or with a third multi-input unit 6 outputs actuators respectively by the eighth and seventeenth inputs and outputs of the integrated controller 1, battery life (if necessary);

- receiving response signals from aviation means of destruction by single-channel executive units 3, generating means of single-channel blocks of executive 3 information on the presence / absence and type of aircraft means of destruction, respectively, at the first 1tp, second 2tp, third 3tp, fourth 4tp, ninth 9tp, tenth 10tp, eleventh 11tp and twelfth 12tp suspension points, its transfer from the first inputs and outputs of single-channel actuating units 3 to the first input-output of the integrated autonomous controller 1, and / or from the second inputs in-outputs of multi-channel executive units 6 to the seventh input-output of the integrated autonomous operation controller 1, and / or from the third inputs and outputs of multi-channel executive units 6 to the ninth, tenth, eleventh, twelfth, thirteenth, fourteenth, fifteenth and sixteenth inputs-outputs integrated battery controller 1 (if necessary);

- reception, reliability control and processing of information received at the first input-output, and / or seventh input / output, and / or eighth, ninth, tenth, eleventh, twelfth, thirteenth, fourteenth, fifteenth, sixteenth and seventeenth inputs-outputs of the integrated autonomous operation controller 1, execution by means of functional software of an integrated autonomous operation controller 1 of monitoring the presence and identification of types of aircraft weapons with reference to a specific suspension point is flying on the apparatus.

Before the flight and / or in flight, the mated onboard equipment of the aircraft and the aircraft weapon control system according to special algorithms implement the operations of preparing and using aircraft weapons, while additionally carrying out information interaction between the integrated autonomous operation controller 1, single-channel executive units 3 and multi-channel units executive 6 via the information line 20 through the seventh input-output of the integrated circuit autonomous work scooter 1 - second inputs and outputs of single-channel executive units 3 and multi-channel executive units 6.

Option 5. Differs from option 1 as follows.

The third mounting block 21 with the control unit for aircraft weapons 18 installed on it and in it and the control panel for aircraft weapons 17 are located (mounted) on board the aircraft.

During ground preparation for the use (operation) and preflight testing (monitoring of serviceability) of hardware and software for the aircraft weapon control system, after the ground preparation console supplies 11 electric power from the aircraft’s onboard power sources, the following additionally occurs:

- organization of interaction between the integrated autonomous operation controller 1, single-channel executive units 3 and multi-channel executive units 6 via an information line 20 through the seventh input-output of the integrated autonomous operation controller 1 - second inputs and outputs of single-channel executive units 3 and multi-channel executive units 6;

- according to the information generated by the means of the ground training console 11 (taking into account the commands received from the mated on-board equipment of the aircraft through the second inputs and outputs of the ground training console 11) coming from the first inputs and outputs of the ground training console 11 to the sixth inputs and outputs of the integrated controller autonomous work 1, as well as teams formed by the integrated controller of autonomous work 1, automatic testing and preparation for operation of hardware and software of the av control system Discount means lesion: the integrated controller 1, battery life, single-channel units actuators 3, the first 5 and the second distribution 8 blocks and converting the information blocks multichannel actuators 6 and aviation destruction means of the control unit 18.

When checking the availability and identification of types of aircraft weapons located on the suspension points of the aircraft 1TP-12TP additionally occurs:

- the formation and transmission of commands from the integrated controller of autonomous operation 1 through the seventh input-output to the second inputs-outputs of single-channel executive units 3 and multi-channel executive units 6;

- receiving commands received at the first, and / or second, and / or third inputs and outputs of single-channel executive units 3, execution by means of single-channel executive units 3 of the corresponding switching circuits of direct and alternating current, which generate requests for determining the types of aircraft weapons placed on suspension points of the aircraft, transmitted respectively through the transmission lines of analog signals and one-time commands 4, multiplexed data channels to aircraft weapons 7, ne 1tp-hand, second 2m, 3tp third, fourth 4tp, 9tp ninth, tenth 10tp, eleventh and twelfth 11tp 12tp point suspension on aviation destruction means;

- receiving commands arriving at the first, and / or second, and / or third inputs and outputs of the multi-channel actuating units 6, performing means of the multi-channel executive units 6 of the corresponding switching DC circuits that generate requests for determining the presence of aircraft weapons at the aircraft suspension points apparatus (if necessary), transmitted respectively through the transmission lines of analog signals and one-time commands 4, multiplex data transmission channels to aviation weapons 7, fifth 5tp, sixth 6tp, seventh 7tp and eighth 8tp suspension points on aircraft weapons;

- receiving response signals from aviation means of destruction by multi-channel executive units 6, generating means of multi-channel blocks of executive 6 information on the presence / absence and type of aircraft means of destruction, respectively, at the fifth 5tp, sixth 6tp, seventh 7tp and eighth 8tp suspension points, its transmission from the first inputs - the outputs of the multi-channel executive units 6 to the first input-output of the integrated autonomous operation controller 1, and / or from the second inputs and outputs of the multi-channel executive units 6 to the seventh integrated controller input-output battery life 1 and / or with a third multi-input unit 6 outputs actuators respectively by the eighth and seventeenth inputs and outputs of the integrated controller 1, battery life (if necessary);

- receiving response signals from aviation means of destruction by single-channel executive units 3, generating means of single-channel blocks of executive 3 information on the presence / absence and type of aircraft means of destruction, respectively, at the first 1tp, second 2tp, third 3tp, fourth 4tp, ninth 9tp, tenth 10tp, eleventh 11tp and twelfth 12tp suspension points, its transfer from the first inputs and outputs of single-channel actuating units 3 to the first input-output of the integrated autonomous controller 1, and / or from the second inputs in-outputs of multi-channel executive units 6 to the seventh input-output of the integrated autonomous operation controller 1, and / or from the third inputs and outputs of multi-channel executive units 6 to the ninth, tenth, eleventh, twelfth, thirteenth, fourteenth, fifteenth and sixteenth inputs-outputs integrated battery controller 1 (if necessary);

- formation by aviation means of destruction of response signals to requests from the control system of aviation means of destruction that come through the suspension points of the aircraft 1tp - 12tp, transmission lines of analog signals and one-time commands 4 and multiplex data transmission channels to aviation means of destruction 7 in single-channel executive units 3 and multi-channel executive units 6 (if necessary);

- reception, reliability control and processing of information received at the first input-output, and / or seventh input / output, and / or eighth, ninth, tenth, eleventh, twelfth, thirteenth, fourteenth, fifteenth, sixteenth and seventeenth inputs-outputs of the integrated autonomous operation controller 1, execution by means of functional software of an integrated autonomous operation controller 1 of monitoring the presence and identification of types of aircraft weapons with reference to a specific suspension point is flying on the apparatus.

Before the flight and / or in flight, using the controls and indicators of the autonomous operation panel 10, the aircraft weapon control panel 17 and the aircraft equipment associated with the aircraft weapon control system, the crew of the aircraft is carried out including management of special means of protection of aviation weapons against unauthorized use.

Wherein:

- teams from the first outputs of the remote control 10 are transmitted to the mating on-board equipment of the aircraft;

- commands for managing special means of protecting aviation weapons from unauthorized use from the input-output of the control panel of aircraft weapons 17 are transmitted to the seventh input-output of the control unit for aviation weapons 18 and / or from the first outputs of the remote control 10 - to the first inputs of the block control of aviation weapons 18, and / or from the first input-output of the integrated controller of autonomous work 1 - through the multiplex channel of information exchange 2 to the fifth the input-output of the control unit for aviation weapons of destruction 18, and / or from the twentieth input-output of the integrated controller of autonomous work 1 - to the sixth input-output of the control unit of aircraft weapons of destruction 18 (if necessary);

- in the control unit for aviation weapons 18, the commands received to control special means of protecting aviation weapons against unauthorized use are converted into information and electrical signals that ensure the safe operation of the control system for aviation weapons and the weapons themselves, which through the third inputs and outputs of the aviation control unit means of defeat 18 and / or the fourth input-output of the control unit of aviation means of defeat 18 through the multiplex channel of information exchange 19 are transmitted to aviation weapons located at the first 1tp, second 2tp, eleventh 11tp and 12th 12tp suspension points (if necessary);

- the mated on-board equipment of the aircraft and the control system of aircraft weapons using special algorithms implement the operations of preparing and using aircraft weapons, while performing information and / or electrical interaction between the mated on-board equipment of the aircraft, an integrated controller of autonomous operation 1, single-channel executive units 3 , multi-channel executive units 6, first 5 and second 8 distribution and conversion units information, the control unit for aviation weapons 18 through the multiplex channel of information exchange 2, between the mated on-board equipment of the aircraft, the integrated controller autonomous operation 1, single-channel executive units 3 and multi-channel executive units 6 through the information transfer line 20, between the integrated controller autonomous operation 1 and the control unit for aviation weapons 18 through the twentieth input-output of an integrated controller avtono I work 1 - the sixth input-output of the aviation weapons control unit 18, between the aviation weapons control unit 18 and the aviation weapons located at the first 1tp, second 2tp, eleventh 11tp and twelfth 12tp suspension points through the third inputs and outputs of the aviation control unit means of destruction 18 and / or the fourth input-output of the control unit of aviation means of destruction 18 by means of a multiplex channel of information exchange 19, between single-channel blocks of executive 3 and aviation weapons located at the first 1tp, second 2tp, third 3tp, fourth 4tp, ninth 9tp, tenth 10tp, eleventh 11tp and twelfth 12tp suspension points, via analog signal and single command transmission lines 4 and multiplex data transmission channels to aviation means of destruction 7, between multichannel executive units 6 and aviation means of destruction located at the fifth 5thp, sixth 6thp, 7th 7th and eighth 8th points of the suspension, through the transmission lines of analog signals and one-time commands 4 and multiplex data transmission channels to aviation weapons 7;

- information about the state of aircraft weapons located at the first 1tp, second 2tp, eleventh 11tp and twelfth 12tp suspension points from the seventh input-output of the aircraft weapon control unit 18 is fed to the input-output of the aircraft weapon control panel 17, which displays indication;

- information about the types of selected (applied) aircraft weapons, from the second outputs of the remote control 10 is transmitted to the mating on-board equipment of the aircraft.

This system compared to the prototype allows you to:

- connect up to two aviation weapons to the executive units, which expands its functionality;

- carry out the dumping of suspended fuel tanks when they are placed on the suspension points of aircraft weapons, which expands its functionality;

- to carry out the opening of the hatch doors before using aircraft weapons when placing suspension points and aircraft weapons inside the fuselage of the aircraft, which expands its functionality;

- manage aviation weapons with special means of protection against unauthorized use, which expands its functionality;

- to ensure the reservation of channels of information exchange between elements of the control system of aviation weapons, mated aircraft equipment and aircraft, which increases the reliability of the operation and fault tolerance of the system;

- carry out pre-flight testing (serviceability monitoring) of hardware and software for the control system of aviation weapons with the conclusion of the test results on the display, which increases its controllability and information content in the conditions of pre-flight training on the ground;

- display information on the status of aircraft weapons and the fuselage flaps of the aircraft, the presence of outboard fuel tanks, the removal of aircraft weapons of destruction locks that protect against unauthorized use, which increases the information content of the system in flight conditions;

- to carry out the installation of components of the system on board the aircraft by means of mounting blocks, which ensures an increase in the degree of its mechanical interface with structural elements of the aircraft.

The use of the invention in aviation technology will expand the range and increase the amount of target load placed on one aircraft, reduce time and improve the quality of pre-flight preparation of the aircraft, successfully perform combat missions that directly depend on the choice of type of aircraft weapons.

Claims (5)

1. The control system of aviation weapons, comprising an integrated controller of autonomous operation, a multiplexed information exchange channel, single-channel executive units, transmission lines of analog signals and one-time commands, a first information distribution and conversion unit, a multiplexed data transmission channel to aviation weapons, characterized in that multichannel executive blocks, a second block for the distribution and conversion of information, a mounting block, a remote control, have been introduced non-operational operation, a ground-based training console, the first input-output of the integrated controller of autonomous operation connected via a multiplex information exchange channel with the mated aircraft equipment, the first inputs and outputs of the first and second information distribution and conversion units, the first inputs and outputs of single-channel executive and multi-channel executive units, the second and fifth groups of inputs, the third and fourth groups of outputs - with interfaced onboard equipment of the training apparatus, sixth inputs and outputs - with inputs and outputs of the stand-alone remote control and ground preparation console, the eighth and seventeenth inputs and outputs - with third inputs and outputs of multi-channel executive units, which in turn are through analog signal and single command transmission lines and, accordingly, the fifth, sixth, seventh and eighth suspension points are connected to aviation weapons, the ninth, tenth, eleventh, twelfth, thirteenth, fourteenth, fifteenth and sixteenth inputs and outputs are connected with third inputs and outputs of single-channel executive units, which in turn are through analog signal and single command transmission lines, multiplex data transmission channels to aviation weapons and, accordingly, the first, second, third, fourth, ninth, tenth, eleventh and twelfth suspension points are connected to aviation means of destruction, the second and third inputs of the first and second blocks of the distribution and conversion of information are connected to the mating on-board equipment of the aircraft, and the fourth inputs and outputs - through the first, second, third, fourth, fifth, sixth, seventh, eighth, ninth, tenth, eleventh and twelfth points of suspension with aviation weapons, an integrated controller of autonomous operation, the first and second information distribution and conversion units on / in the mounting block, information, mechanical and electrical interfaces of the elements of the aircraft weapon control system located on / in the mounting block, with mating avionics tion machine, actuating single-channel units, executive units multichannel, remote battery life, the remote ground training and aviation destruction means via the mounting unit. 2. The aircraft weapon control system according to claim 1, characterized in that the information distribution and conversion unit, the sash control unit, the first and second outboard fuel tank discharge control units, the sash control panel, the first and second mounting units, the first are additionally introduced the input-output of the integrated controller of autonomous operation is connected via a multiplex channel of information exchange with the mated on-board equipment of the aircraft, the first inputs and outputs of the unit distribution and conversion of information and the control unit for the valves, the first inputs and outputs of single-channel blocks of actuators and multi-channel blocks of actuators, the eighteenth input-output - with the first input-output of the first control unit for dumping outboard fuel tanks, the second inputs and outputs of which are connected through the ninth suspension point with aviation means of destruction, the nineteenth input-output - with the first input-output of the second control unit dumping outboard fuel tanks, the second inputs and outputs of which are connected s through the tenth point of the suspension with aviation weapons, the fourth inputs and outputs of the distribution and information conversion unit are connected through the seventh, eighth, ninth, tenth, eleventh and twelfth points of the suspension with aviation weapons, the outputs of the remote control are connected to the inputs of the first and second outboard fuel tank discharge control units, the second inputs / outputs of the sash control unit are connected to the inputs / outputs of the sash control panel, the third inputs / outputs are connected to interfaced aircraft equipment, the fourth inputs and outputs - with shutters of the first, second, third, fourth, fifth and sixth suspension points, multi-channel executive units via analog signal and single command transmission lines, multiplex data transmission channels to aviation weapons and, accordingly, the fifth , the sixth, seventh and eighth suspension points are connected to aircraft weapons, the integrated battery controller and the sash control unit are located on / in the first The mounting block, the information distribution and conversion unit is located on / in the second mounting block. 3. The aircraft weapon control system according to claim 1, characterized in that it further includes: an information distribution and conversion unit, a sash control unit, a first and second outboard fuel tank discharge control unit, a sash control panel, a first and second mounting unit, a remote control control of aircraft weapons, a control unit for aircraft weapons and a multiplex channel for information exchange, with the first input-output of an integrated autonomous controller soy inen through the multiplex channel of information exchange with mated aircraft equipment, the first inputs and outputs of the information distribution and conversion unit and the leaf control unit, the first inputs and outputs of single-channel executive and multi-channel executive units, the fifth input-output of the aircraft weapon control unit, eighteenth input-output - with the first input-output of the first control unit dumping outboard fuel tanks, the second inputs and outputs of which connected through the ninth point of the suspension with aviation weapons, the nineteenth input-output - with the first input-output of the second control unit dumping outboard fuel tanks, the second inputs and outputs of which are connected through the tenth point of the suspension with aircraft weapons, the twentieth input-output - with the sixth the input-output of the control unit for aviation weapons, the fourth inputs and outputs of the distribution and information conversion unit are connected through the seventh, eighth, ninth, tenth, single, respectively the ninth and twelfth suspension points with aviation weapons, the first outputs of the autonomous operation console are connected to the first inputs of the aircraft weapons control unit, the second outputs are with the inputs of the first and second control units for dumping outboard fuel tanks, the second inputs and outputs of the sash control unit are connected to the inputs - the outputs of the sash control panel, the third inputs and outputs - with the mating equipment of the aircraft, the fourth inputs and outputs - with the sashes of the first, second, third , the fourth, fifth and sixth points of the suspension, multi-channel actuator blocks through the transmission lines of analog signals and one-time commands, multiplex data transmission channels to aircraft weapons and, accordingly, the fifth, sixth, seventh and eighth suspension points are connected to aircraft weapons, the inputs of the aviation control panel means of destruction are connected through the seventh, eighth, ninth and tenth points of the suspension with aviation means of destruction, the outputs are with the seventh inputs of the aviation control unit means of destruction, the second inputs of the aircraft weapon control module are connected to the mating equipment of the aircraft, the third inputs and outputs through the seventh, eighth, ninth and tenth suspension points with aviation weapons, the fourth input-output through the multiplex information exchange channel, the seventh, eighth, ninth and tenth suspension points with aviation weapons, an integrated battery controller and the sash control unit are located on / in the first unit In the mounting block, the information distribution and conversion unit is located on / in the second mounting block. 4. The aircraft weapon control system according to claim 1, characterized in that an information transmission line is additionally introduced, the seventh input-output of the integrated autonomous operation controller being connected via an information transmission line to the second input-outputs of single-channel executive and multi-channel executive blocks, second the inputs and outputs of the ground training console are connected to the mating equipment of the aircraft. 5. The aircraft weapon control system according to claim 1, characterized in that an aircraft weapon control panel, an aircraft weapon control unit, an information exchange multiplex channel, an information transfer line and a third mounting unit are introduced, the first input-output of an integrated controller autonomous operation is connected through the multiplex channel of information exchange with the mated on-board equipment of the aircraft, the first inputs and outputs of the first and W of the information distribution and conversion blocks, the first inputs and outputs of the single-channel executive blocks and the multi-channel executive blocks, the fifth input-output of the aircraft weapon control unit, the seventh input-output - through the information transmission line with the aircraft onboard equipment being interfaced, the second input-outputs of single-channel executive blocks and multi-channel executive blocks, the twentieth input-output - with the sixth input-output of the aircraft control unit lesions, the first exits of the autonomous operation console are connected to the first inputs of the aircraft weapon control unit, the second outputs are connected to the aircraft onboard equipment, multichannel executive units via analog signal and single command transmission lines, multiplex data transmission channels to aircraft weapons and, accordingly, the fifth , the sixth, seventh and eighth points of the suspension are connected to aircraft weapons, the input-output of the aircraft control panel the defeat is connected to the seventh input-output of the aircraft weapon control unit, the third inputs and outputs of the aircraft weapon control unit are connected through the first, second, eleventh and twelfth suspension points with the aircraft weaponry, the fourth input-output is via the multiplex information exchange channel, the first, second, eleventh and twelfth points of the suspension with aviation weapons, the second inputs and outputs of the ground preparation console are connected to the mating side turn dovaniem aircraft control unit aviation destruction means arranged on / in the third mounting unit.

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