RU2184683C1 - Multi-functional two-seat highly-maneuverable tactical-purpose aircraft - Google Patents

Abstract

FIELD: aircraft manufacture; tactical aviation for detection, and destruction of air, surface and ground targets. SUBSTANCE: unlike conventional designs, proposed aircraft is equipped with multi-functional pilot's console, display processor, TV observation camera, multi- functional operator's console, operator's display processor and computing logic modules for coordination of tactical operations, coordination of training operations, coordinated air-to-air cooperation, coordinated air-to-surface cooperation and coordinated air-to-air-to-surface cooperation which are connected to information exchange channel by means of inputs and outputs. Proposed aircraft possesses extended functional capabilities and fighter-trainer, interceptor, bomber, attack aircraft, reconnaissance aircraft, ECM aircraft in space-and-time coordination. EFFECT: enhanced efficiency. 1 dwg

Description

 The invention relates to the field of aircraft construction, in particular to tactical aircraft, performing the detection and destruction of air, surface and ground targets.

 Of the well-known modern domestic and foreign two-seat multifunctional tactical aircraft, the closest analogue is the aircraft described in the book of M.A. Levina, V.E. Ilyin's "Modern Fighters", Moscow, HOBBIKNIGA, 1994. , p. 204-210, aircraft F / A-18F "Hornet", comprising a glider, propulsion system, means of mechanization; all-aircraft equipment, the crew emergency escape system, the aircraft and propulsion control system, the communications equipment complex, the parameters monitoring and registration system, the navigation and navigation equipment complex, the sighting and sighting system, the telecommand guidance system, the weapon and passive countermeasure control system, a set of weapons and passive countermeasures, a range of electronic countermeasures, multifunctional pilot indicators and operator, indicators of the pilot and operator on the windshield, indicator of the helmet-mounted target designation system of the pilot, means of operational control of the pilot and operator, on-board computer system, including the computing and logical modules of the integrated database, the formation of navigation and flight parameters, the formation of target designation and application parameters, the formation of parameters displayed information, input-output-control information exchange interconnected along the highway of computer exchange and with the on-board equipment through an information exchange channel.

 With an appropriate set of weapons and countermeasures, a multifunctional aircraft performs the functions of a fighter, attack aircraft, interceptor, bomber, operational reconnaissance, and jammer. However, in dangerous combat rapidly changing situations, the combination of the aforementioned functions must be performed in a coordinated manner, and the crew can work out difficult combat situations only with training in flight under real evolutions and overloads.

 The objective of the invention is to expand the functionality of a two-seat highly maneuverable tactical aircraft and, as a consequence, increase the efficiency of its use.

 This result is achieved in that a multi-functional, highly maneuverable tactical aircraft containing interconnected inputs and outputs through the channel of information exchange glider, propulsion system, means of mechanization; all-aircraft equipment, the crew emergency escape system, the aircraft and propulsion control system, the communications system, the parameter monitoring and registration system, the navigation and flight monitoring system, the sighting and sighting system, the telecommand guidance system, the weapon control and passive countermeasures system, a set of weapons and passive countermeasures, a range of electronic countermeasures, multifunctional pilot indicators, and pilot indicator on the windshield, helmet-mounted target designation indicator, pilot operational controls, multifunctional operator indicators, operator indicator on the windshield, operator’s operational controls, on-board digital computer system including interconnected logic-logical modules of the integrated computer-aided exchange databases, the formation of navigation and flight parameters, the formation of target designation and application parameters, parameters for displaying information, input-output-control of information exchange, the other input-output of which is the input-output of the on-board computer system, is additionally equipped with connected inputs and outputs to the information exchange channel of a multifunctional pilot’s panel, pilot’s display processor, television camera’s internal camera, multifunctional operator panel, operator’s display processor, and inputs connected to the on-board digital computer system s-outs to the pipeline computing exchange computationally coordination logic modules warfare, coordination of training activities coordinated interaction of air-air, air-coordinated interaction surface coordinated interaction air-to-air surface.

The drawing shows a block diagram of a multifunctional two-seat highly maneuverable aircraft, where
1 - a glider, a propulsion system of a means of mechanization PDUM,
2 - general aircraft equipment CCA,
3 - emergency exit system by the crew of the SAPS,
4 - control system for the aircraft and propulsion system SUMS,
5 - a set of communication tools KSS,
6 - a system for monitoring and recording parameters SKRP,
7 - a set of navigation and flight control aids KNPS,
8 - a complex of sighting and sighting equipment COPS,
9 - telecommand guidance system TKSN,
10 - control system of weapons and passive counteraction SUSP,
11 - a set of weapons and passive counteraction KSPP,
12 - a set of means of electronic countermeasures KSRP,
13 - channel information exchange KIO
14 - multifunctional pilot indicators MFIL,
15 - pilot indicator on the windshield ILLS,
16 - indicator helmet-mounted targeting system INSC,
17 - multifunctional pilot MPPL,
18 - operational management of the pilot SOUL,
19 - display processor pilot DPL,
20 - multifunctional indicators of the operator MFI,
21 - the indicator of the operator on the windshield IOLS,
22 - the inside camera of the television review of VTKO,
23 - multifunctional operator console MFPO,
24 - means of operational management of the operator SOUO,
25 - display processor operator DPO,
26 - bots digital computer system BTsVS,
27 - computational logic module (VLM) of the integrated database HBS,
28 - VLM formation of navigation and flight parameters FNPP,
29 - VLM input-output-control information exchange of the WSIS,
30 - VLM formation of target designation parameters and the application of FTPs,
31 - VLM forming parameters of the displayed information FOI,
32 - line computing computing MBO,
33 - VLM coordination of combat operations of the CVBD,
34 - VLM coordinated interaction of air-to-air HVAC,
35 - VLM coordinated interaction of the air-surface KDVP,
36 - VLM coordinated interaction of the air-air-surface VVVP,
37 - VLM coordination of the training activities of KUTD.

 PDUM 1 includes the design of an aircraft with a propulsion system based on two double-circuit forced turbojet engines with narrowing-expanding adjustable nozzles and mechanization means - landing gear, horizontal and vertical tail, means of deflecting the engine nozzle when changing the direction of the thrust vector. The interconnection of the actuators of the mechanization means with the interacting equipment is carried out through the input-output PDUM 1 according to KIO 13.

 OCO 2 includes an electro-remote control system for mechanization, providing increased aerodynamic characteristics, providing the specified characteristics of stability and controllability; hydraulic system for the release and cleaning of the chassis, emergency and starting braking of the wheels of the chassis; fire alarm system and fire extinguishing means in engine compartments; power supply system for aircraft equipment with direct and alternating current; an air conditioning, cooling and pressurization system to maintain a predetermined temperature and pressure in the cockpit, in the pressure suits of the pilot and operator, and in interconnected instruments and equipment requiring cooling and pressurization; fuel system, lighting equipment inside the cabin, illumination of the runway and the designation of the dimensions of the fighter and its flight direction.

 CAPS 3 includes ejection seats for the pilot and operator, pyrotechnic means for dumping the flashlight and ejection of seats and the device for generating a cyclogram for opening the main and stabilizing parachutes after the ejection according to the data received at the input / output of the SAPS 3 from KNPS 7 through KIO 13 until the ejection.

 SASD 4 according to the data received at the input-output through KIO 13 from the interacting equipment in manual, semi-automatic and automatic control modes generates control signals and their output through KIO 13 to actuators of mechanization devices PDUM 1. At the same time, the combination of control means of mechanization of the aircraft and propulsion system provides the implementation of super-maneuvers such as "bell", "cobra", "hook" and their spatial combinations.

 KCC 5 provides two-way radiotelephone communication between crew members, telecode communication between interacting aircraft and ground control and guidance points, information exchange is carried out through KCC 5 input-output via KIO 13.

 SKRP 6 interacts with KIO 13 with all on-board equipment, providing its control and registration on information media in the current time of the main parameters for subsequent decryption and analysis on ground-based equipment.

 KNPS 7 includes physically dissimilar (inertial, air, radio, satellite) information systems and sensors of state parameters of the aircraft, forming the coordinates of the location, components of speeds and angular velocities, components of accelerations and overloads, components of air speeds; angles of course, roll, pitch, attack and slip; signals from the input-output KNPS 7 KIO 13 are fed to the inputs and outputs of the interacting equipment.

 COPS 8 includes physically heterogeneous (radar with a synthesized antenna array, optical radar, laser, television, thermal imaging, sight - helmet-mounted target designation system) systems and sensors for viewing the environment, fixing, identifying and tracking air, ground and surface moving and stationary targets; the parameters of the relative motion of the aircraft relative to the goals, the characteristics of the identified targets from the input-output of COPS 8 via KIS 13 are supplied to the inputs and outputs of the interacting equipment.

 TKSN 9 provides the use of weapons from the composition of the KSPP 11 with television and radar homing heads that have an output on a television signal and a command radio signal, which from the input-output of the TKSN 9 through KIO 13 enter the input-output of the interacting equipment.

 SUSP 10 provides the distribution of target designation signals to weapons, the formation of commands for the preparation and launch of weapons and passive counteraction, the issuance of commands about the state of the system and tools as part of the KSPP 11. SUSP 10 operates in automatic, manual, emergency, test and training modes interaction, the exchange of signals with interacting equipment is carried out through the input-output of the EMS 10 according to KIO 13.

 KSPP 11 contains means of destruction - small arms and cannons, guided, homing and unguided air-to-air missiles, guided, homing and uncontrolled air-to-surface missiles, guided, homing and uncontrolled bombs, passive countermeasures - false thermal and radar targets, the exchange of signals with interacting equipment is carried out through the input-output of the KSPP 11 according to KIO 13.

 KSRP 12 provides for fixing the facts of aircraft detection by enemy radar (ground and air) stations, direction finding of radio-emitting and heat-emitting targets, formation of active radar jamming radiation, signal exchange with interacting equipment is carried out through the KSRP 12 input-output by KIO 13.

The composition of MFIL 14 includes "k" multifunction indicators (MFIs) based on color liquid crystal screens (LCD). MFIs 20 include “n” MFIs. The number of "k" and "n" is determined by the dimensions of the cockpit and the MFI, the location of the pilot relative to the front wall of the cockpit and, accordingly, the dimensions of the optimum-visible part of the information-control field. Information is displayed on screens in a single time (lags are less than natural delays in changing images and changing current data) with the current situation. The LCD displays the incoming monochrome and color signographic, television, cartographic and mixed information. All "k" and "n" MFIs can operate in the same and different display modes, set automatically or by crew members pressing softkeys:
- indicator of tactical situation,
- indicator of vertical situation,
- indicator of sighting tools,
- indicator of electronic countermeasures,
- indicator of complex informational signaling,
- indicator of training modes,
- indicator of a television review camera.

 The multifunctional buttons-keys framing the LCD are automatically assigned (with highlighting of the names) according to the display modes and are used to manually select sub-modes in accordance with the purpose.

 Thus, at MFIL 14 and MFIO 20, the set airplane operating modes are displayed, the state of all on-board equipment is displayed with the ability to automatically and manually select and change the indication operating modes of PDUM 1 and all interacting equipment for controlling and presenting information in various situations (preparation, take-off, landing, route flight, combat modes).

 ILLS 15 and IOLS 21 are collimator indicators for displaying navigation, piloting, sighting and tactical information on a translucent screen against the background of the surrounding space visible through the windshield and translucent screen.

 The ISSC 16 is a monocular or binocular optical system for displaying visible space with the imposition of standard data similar to those displayed on the indicators on the windshield with target designation data input to the output of the ISSC 16 by KIO 13.

 VKTO 22 is an in-cab video camera that captures a television image of the cabin space against the background of information frames of ILLS 15. The television signal from the input-output of VKTO 22 according to KIO 13 is fed into the interacting equipment, in particular, when IOLS 21 is implemented on the basis of MFIs, television display signals visible on ILLS 15, VKTO 22 is removed and transmitted through KIO 13 to the LCD of the multifunctional indicator simulating IOLS 21.

SOUL 18 and SOUO 24 include control knobs for mechanization of the aircraft and the propulsion system with mounted guns of the cannon mounts, a pointing arm for aiming the crosshair at the chosen target and launching weapons and passive countermeasures. Additionally introduced MFPL 17 and MFPO 23 contain:
- engraved mode buttons corresponding to the airplane operating modes (PDG - preparation, NAV - navigation, BR - combat mode, etc.), on-board equipment operation mode (KSS - communication equipment complex, KOPS - sighting and sighting equipment complex, etc.), when turned on, the remote control becomes a means of controlling the corresponding mode or equipment,
- engraved buttons for entering alphanumeric source data during the preparation and in flight and the formation of executive teams (VVD - input, KNT - self-monitoring, etc.),
- an information panel framed by nameless multi-function buttons corresponding to the components of the aircraft and onboard equipment operating modes, fixed by engraved mode buttons, the information panel is divided into parts corresponding to the multi-function button located nearby, the purpose of which is highlighted on the indicated part of the information panel, for example, in the mode , indicated by the "PDG" mode button, the nameless multi-function buttons are indicated by the inscriptions "CONTROL", "ALARM CA "," Exercises "et al.
- a hint board displaying the name of the selected mode and hints to crew members of the “ENTER PPM” type - enter the intermediate route point, “ON.COPS” - turn on the complex of sighting and sighting devices, etc.

 MFPL 17 and MFPO 20 interact with on-board equipment through their inputs and outputs on KIO 13.

 DPL 19 and DPO 25 are standard high-speed digital computers that provide the current formation of information frames for display means - MFIL 14, MFI 20, INSC 16, ILLS 15, IOLS 21, display of television frames with VKTO 22; The interaction of the DPL 19 and DPO 25 with the on-board equipment is carried out through their inputs and outputs according to KIO 13.

BTsVS 26 is a dual or built computing system based on modern high-speed digital computers that provide the reception, processing and delivery of information in almost real time. BTsVS 26 contains executed on standard elements of computer technology computing logic modules (VLM):
- VLM VVUO 29 - carries out, through one input-output, data reception, conversion and transmission of data to the interacting equipment according to KIO 13, the other input-output of VVUO 29 is connected to MVO 32, which provides computational and information exchange between all VLM BTsVS 26,
- VLM OBD 27 is a long-term storage device that stores the initial operational data of the flight route, brought from portable carriers of flight missions, the initial long-term data on the ballistic characteristics of weapons and passive countermeasures, data from the digital aeronautical map of the area of operations, alignment characteristics of on-board equipment, model model parameters goals, model parameters of combat training modes, graphical symbols of generalized information and other parameters, necessary s for computing processes in the MWM BTSVS 26 and the functioning of interacting on-board equipment,
- VLM FNPP 28 carries out complex processing of information from KNPS 7, KOPS 8 with initial data from OBD 27 and generates navigation and flight parameters for all flight modes from pre-flight preparation to landing, which from the input-output of FNPP 28 through MVO 32 go to the inputs- the outputs of the interacting VLM BTsVS 26, including in VVUO 29 for transmission through KIO 13 to the interacting equipment,
- VLM ФПЦП 30 carries out complex processing of information received from COPS 8, КСРП 12, ТКСН 9, КНПС 7, КСПП 11 and generates aiming parameters and commands for all flight modes for all means from the structure of КСПП 11, which are from the input-output of ФПЦП 30 through the MVO 32 enter the interacting VLM BTsVS 26, including in the WSIS 29 for transmission through KIO 13 to the interacting equipment,
- VLM FOI 31 according to the data obtained by MVO 32 from OBD 27, FNPP 28, FPTsP 30, from interacting equipment through KIO 13 and VVUO 29, generates generalized functional displayed information, alphanumeric information, television information, information of the aeronautical map, the signals of which input-output FOI 31 through the MVO 32 VVUO 29, KIO 13 are fed to the inputs and outputs of the DPL 19 and DPO 25, forming frames of the displayed information in the necessary combinations and formats for display on the MFI 14, MFI 20, ILLS 15, IOLS 21, INSC 16 In this case, IOLS 21 can be performed at the IFI, information image frames for which are formed in the DPO 25 on the television image VKTO 22.

 Additionally, the logic and logic modules KVBD 33, KVVV 34, KVVP 35, VVVP 36, KUTD 37, introduced into the BCVS 26, are implemented on standard elements of computer technology - interconnected processor and memory with input-output to the MBO 32, while the processor and memory can be part of a combined processor and a combined storage device as part of the BCVS 26.

 During the flight, KOPS 8 and KSRP 12 review the airspace and the earth's surface, fix, track and select chains and landmarks, the location coordinates and characteristics of which through KIO 13, VVUO 29, MVO 32 enter the OBD 27, where the detected many landmarks are recorded and goals, including those entered before the flight.

In VLM KVBD 33 in connection with COPS 8, KSRP 12, KNPS 7, OBD 27 is carried out
- analysis of the target situation and ranking of goals by degree of danger (priority of threats) and by degree of importance (necessity of defeat at various degrees of danger),
- the purpose of the type of interaction - "air-air", "air-surface", "air-air-surface"; signals of the type of interaction from the input-output of the CVBD 33 through the MVO 32 are received in the KVVV 34, KVVP 35, VVVP 36, FOI 31 and through VVUO 29, KIO 13, DPL 19, DPO 25 on MFIL 14, MFIO 20 for indicating to the crew.

In accordance with the designated type of interaction in the VLM KVVV 34, KVVP 35, VVVP 36 in conjunction with other VLM BTsVS 26 and on-board equipment through VVUO 29 according to KIO 13 on the basis of optimization of the functional of minimum losses and maximum damage is carried out
- the distribution of goals and means of locating them for the pilot and operator,
- the distribution of means of COPS 8, KSRP 12 for targets followed, - the distribution of means of destruction and passive counteraction of KSPP 11 for use on targets to be hit,
- the purpose and operational change of the operating order of radio-emitting and radio-receiving means KNPS 7, KOPS 8, KSRP 12,
- the appointment of the application of active countermeasures from the KSRP 12,
- the appointment of maneuvers (including super-maneuvers) and methods for their execution (manual, semi-automatic, automatic) at various stages of the selected interaction,
- assignment of modes and sub-modes of operation of the display means MFIL 14, MFI 20, ILLS 15, IOLS 20, INSC 16.

 Commands and signals in accordance with the generated cyclograms from the inputs and outputs KVVV 34, KVVP 35, VVVP 36 through the MVO 32 are fed to the interacting VLM BTsVS 26 and through the VVUO 29, KIO 13 to the inputs and outputs of the interacting equipment.

For example, when intercepting a DVC - a long-range important aerial target (bomber, a group of enemy bombers), using COPS 8 an attacking fighter of the enemy (a dangerous airborne target of the OVC) was detected in the computational and logical modules of the KVBD 33, KVVV 34
- solves the task of targeting the DCC - the operator, the DCC - the pilot,
- means of target tracking are assigned - a radar station from the structure of KOPS 8 to the operator, a helmet-mounted targeting system of the NSC from the composition of KOPS 8 to the pilot,
- the means of destruction from the composition of the KSPP 11 are assigned — medium and long-range air-to-air missiles with an active radar or thermal homing head — to the operator; short-range highly maneuverable air-to-air missiles for meeting on overtaking and intersecting courses and cannon armament for a pilot,
- means of passive counteraction (false thermal targets) from the composition of the KSPP 11 are assigned to the pilot,
- indication modes MFIL 14, ILLS 15, MFI 20, IOLS 21, INSC 16 are assigned in which data on targets and means of destruction and passive counteraction are concentrated in the optimal field of view of the pilot and operator,
- a method and procedure for performing a maneuver or over-maneuver is assigned, in which the pilot-controlled aircraft is in a more favorable position relative to the DEC, and the operator continues (or has already completed) combat work in the DEC.

 The calculation of the launch of weapons and passive counteraction is carried out in FTP 30, the launch is carried out by crew members by issuing commands from SOUL 18 and SOUO 24 through KIO 13 and SUSP 10 to the input-output of KSPP 11.

 Thus, the aircraft simultaneously performs the functions of a long-range air interceptor, a highly maneuverable air melee fighter with the implementation of jamming - false thermal or radar targets.

For example, when escorting an NSC from COPS 8 and attacking an important ground target of the VSC (a railway junction with anti-aircraft defense air defense systems - a radar detection and jamming system, anti-aircraft missile systems), KSRP 12 recorded the fact of aircraft detection by air defense systems, and radar from of the composition of COPS 8, an attacking unaffected ground-to-air missile (NARZ) was found in KVBD 33, KVVP 34:
- the task of target allocation of the VSC to the operator, NARZ to the pilot,
- means are assigned to support targets of IOLS 21 (with the display of a television image from VKTO 22) to the operator,
- assigned means of destruction from the KSPP 11 - bomber weapons and short-range air-to-surface missiles with a passive homing television - to the operator for working at the VSC, passive countermeasures (false thermal and radar targets) - to the pilot to distract the attacking NARZ to false target,
- a maneuver or super-maneuver is prescribed, in which the VSC is defeated and the NARZ is withdrawn (with loss of location contact).

 The calculation of the launch of weapons and passive counteraction is carried out in FTP 30, the launch is carried out by crew members by issuing commands from SOUL 18, SOUO 24 through KIO 13, SUSP 10 to the input-output of the KSPP 11.

 If NARZ is not detected, the pilot performs the work at the VSC, the operator is assigned to work with KSRP 12 — preparing and launching air-to-surface missiles with passive homing radar and placing active radar radiation on air defense systems. By means of VKTO 22, SKRP 6, the state of the VSC is recorded after defeat for further operations, operational data from VKTO 22 through KIO 13, KSS 5 are transmitted to interacting aircraft and ground control points.

 Thus, the aircraft simultaneously performs the functions of an attack bomber, directors of active and passive interference and performs operational reconnaissance operations.

For example, if an enemy attack fighter — OVC — is found in long-range programmed ground (surface) targets of a DZTs, a radar from the COPS 8 at a long range, in VVBD 33, VVVP 36
- the target distribution of the remote control center is carried out to the operator, the DEC pilot,
- Means of tracking radar targets from the COPS 8 are assigned to the pilot, TKSN 9 to the operator,
- the means of destruction are assigned from the KSPP 11 - long-range air-to-air missiles with thermal or radar homing heads to defeat the DEC with a pilot, long-range air-to-surface missiles with a telecommand guidance system for guidance and launch by the operator’s remote sensing center,
- MFIL 14, ILLS 15, MFIO 20, IOLS 21, INSC 16 operating modes are assigned in which data on targets and means of destruction are concentrated in the optimal field of view of the pilot and operator.

 The operator on TKSN 9 through the SOUO 24 guides (and starts according to the data from the FTP 30) the selected means of destruction to a given target, in FULL NAME 31 determines the moment of launch, a television image of the earth's surface (and targets on it) transmitted from the television output means of destruction of remote sensing centers through KIO 13 is transmitted to SKRP 6 for recording and through KSS 5 to ground points for operational decisions.

 The pilot carries out work at the DEC, according to the calculation in FPTsP 30, the use of weapons at the DEC is carried out.

 Thus, the aircraft simultaneously performs the functions of a long-range attack bomber, fighter-interceptor and operational reconnaissance.

 When working on a remote control center, situations are possible of detecting an aircraft by airborne reconnaissance aircraft from Avax type aircraft or by radar stations of the enemy’s ground defense systems, then the aircraft performs the functions of a long-range attack bomber, jammer and operational reconnaissance of ground (surface) and air targets.

 When conducting training operations, the transition to which is carried out by issuing commands from the controls (buttons-keys) to MFIL 14, MFIO 20, teams of typical educational-training situations are formed - preflight simulator, ground simulator, air simulator coming through KIO 13, VVUO 20 in KUTD 39 and in the interacting equipment, transferred to the training state.

 During preflight training in KUTD 37, according to OBD 27, in accordance with the entered mission, models of the aircraft’s movement at all stages of the flight and motion models and characteristics of the programmed targets are formed. In the interaction of the VLM BTsVS 26 and the interacting equipment, a flight is carried out along the programmed route from take-off to landing, checking the use of the specified means of destruction and counteraction against the set targets in the set modes of manual, semi-automatic or automatic control, the results of the training are recorded on SKRP 6, and crew members control and fulfill their actions, while through KSS 5 the process and the results of the training can be simultaneously transmitted to the ground training and planning point flight missions.

 In the ground-based simulator mode, at the ground-based planning and preparation point for flight tasks, a task for a training flight is formed with the introduction of imitating operational situations entered in OBD 27. In KUTD 37, according to the OBD 27, a model of the object’s movement and model of movement and characteristics of the set targets are formed received in the CVBD 33, which, depending on the simulation situation, assigns the operation of the KVVV 34, KVVP 35 or VVVP 36. In the interaction of the VLM BTsVS 26, the on-board equipment and the PDUM 1 transferred to the ground-based simulator mode, flying flight with the work of crew members and subsequent verification of the quality of its performance according to records on SKRP 6 or operational verification at ground control points in connection with the aircraft through KSS 5.

 In the "air simulator" mode, a flight is carried out in accordance with the flight task entered in the OBD 27, including with imitation of operational situations. In KUTD 37, according to HBS 27, models of movement and characteristics of targets are formed for which the operation of the KVVV 34, KVVP 35 or VVVP 36 is assigned to the KVBD 33. In the interaction of the VLM BTsVS 26, the on-board equipment transferred to the "air simulator" mode, a flight simulation with the work of crew members with subsequent verification of the quality of their performance according to the records on SKRP 6 or operational mutual verification and verification at ground control points interconnected with the aircraft through KSS 5.

 MFIL 14, ILLS 15, INSC 16, MFP 17, SOUL 18, DPL 19, MFI 20, IOLS 21, VKTO 22, MFPO 23, SOUO 24, DPO 25 in conjunction with the on-board equipment and the BCVS 26 KIO 13 provide high situational awareness crew and form an operational information-indicating control computer center that allows crew members in dangerous, rapidly changing modes to simultaneously interact and simultaneously independently implement the concept of situation management such as "detected-hit-evaded retaliation", "detected-evaded-struck" , "obna uzhil-hit attack-recorded results. "

 Thus, the examples of technical implementation show the achievement of the result in terms of expanding the functionality of a multifunctional two-seat maneuverable aircraft that performs the coordinated functions of a combat and combat training fighter, interceptor, bomber, attack aircraft, operational reconnaissance and jammer in spatial and temporal coordination, which significantly increases the effectiveness of its use.

Claims (1)

 A multi-functional, highly manoeuvrable tactical aircraft, containing interconnected inputs and outputs via the glider information exchange channel, a propulsion system and mechanization equipment, general-purpose equipment, an emergency crew exit system, an aircraft and propulsion control system, a communications system, a parameter monitoring and registration system, navigation and flight aid complex, sighting and sighting system, telecommand guidance system, si the theme of controlling weapons and passive countermeasures, a set of weapons and passive countermeasures, a range of electronic countermeasures, multifunctional pilot indicators, pilot indicator on the windshield, helmet-mounted target designation system, operational pilot control tools, multifunctional operator indicators, operator indicator on the windshield, Operator’s on-line controls, on-board digital computer system including interconnected input-outputs on the highway of computational exchange, the logic modules of the integrated database, the formation of navigation and aerobatic parameters, the formation of target designation and application parameters, the formation of parameters of the displayed information, input-output-control of information exchange, the other input-output of which is input-output on-board computer system, characterized in that it is additionally equipped with connected inputs and outputs to the information exchange channel multifunctional remote ohm pilot, pilot display processor, in-cab television review camera, multi-function operator’s console, operator’s display processor and integrated on-board digital computing system, connected inputs and outputs to the computer exchange line, logical and logical modules for coordinating combat operations, coordinating training action, coordinated air-to-air interaction, coordinated air-to-surface interaction, coordinated air-air-surface interactions.