RU2250511C1 - Aircraft training complex - Google Patents

Abstract

FIELD: simulation technique for training flight personnel.

SUBSTANCE: proposed training complex includes combat trainer, aircraft simulators and integral system for objective monitoring and estimation of personnel training. Simulator has controls and display systems in trainee and instructor cabins, power plant and systems for starting and monitoring this plant, flight parameter sensors, onboard module of integrated monitoring system and integrated complex of onboard equipment. Integrated monitoring system includes automated working position for operator, equipment for its functioning, recording systems and systems for planning ground and flight training, estimation of level of training and analysis of condition of training equipment.

EFFECT: extended functional capabilities.

2 cl, 1 dwg

Description

The invention relates to means for the professional training of flight personnel and is intended for use in training and training pilots throughout the entire range of tasks related to piloting, navigation and combat use of the aircraft.

Known technical solutions for training facilities (UTK) flight personnel, representing mainly the implementation of their components, namely combat training aircraft (UBS) with on-board simulators (RU 2203200 C1, B 64 C 30/00, 04/27/2003) , data preparation systems for the analysis of piloting results (RU 2179744 C1, G 08 G 5/00, 02/20/2002), flight simulators (GB 2260304 A, G 09 B 9/08, 04/14/1993).

The disadvantages of the known technical solutions are limited functionality that does not allow comprehensive training of pilots.

UTK is also known with the combination of individual components used in the learning process, with their interconnection for solving a wide range of problems (US 5260874 A, G 09 V 9/10, 11/09/1993; US 6319008 B1, G 09 V 9/08, 20.11. 2001).

Closest to the proposed one is the aforementioned aircraft flight control system for flight personnel, which includes airborne navigation systems, specialized and procedural type flight simulators and an integrated objective monitoring system (SOC) and training assessment associated with the aircraft and flight simulators (US 6319008 B1, G 09 V 9 / 08/20/2001).

The disadvantage of this complex is determined by the unsatisfactory training of the pilots, again due to the incomplete range of tasks to be solved during the training.

The technical result provided by the present invention is manifested in increasing the efficiency of training pilots, including for solving some combat missions.

In order to achieve a technical result in an aviation flight control system for flight personnel, which is a combination of airborne flight controllers, specialized and procedural type aviation simulators and integral RMS and training assessment, according to the invention, the airborne flight control system contains controls in the cadet’s cabin, controls in the instructor’s cabin, an integrated system indications in the cadet’s cabin, a comprehensive display system in the instructor’s cabin, the power plant and its launch, monitoring and diagnostics systems, steam sensors flight meters of the aircraft, as well as the on-board module of the integrated objective control system, the inputs of which are connected to the outputs of the said controls, integrated display systems, the power plant and its systems, and an integrated complex of on-board equipment, including the on-board digital computer system of the upper level, the display system information, an integrated navigation, landing, communication and identification system, an integrated control system, airborne controls and an ejection device are expendable x means and interconnected with the mentioned governing bodies, integrated display systems, the power plant and its systems, aircraft flight parameters sensors and the on-board module of the integrated objective control system.

The flight simulator contains a module for the layout of the cockpit with a block of modules of simulators of information display tools at the student’s workplace and a block of modules of simulators of control elements at the student’s workplace, a module of the instructor’s workstation with a block of modules of information display tools at the instructor’s workplace and a block of modules of control tools at the worker the place of the instructor, the block of modules for displaying information in the hull space, the block of modules that imitate acceleration sensations, as well as connected block of program modules of the objective control system, the input of which is connected to one of the outputs of the module of the instructor’s workplace, and the outputs - to the first inputs of the modules of the layout of the cockpit and the instructor’s workplace, and the block of software modules of simulation and control, the input of which is connected to the other output of the module the instructor’s workstation, and the outputs - with the second inputs of the cockpit layout modules and the instructor’s workplace and the inputs of the module for displaying information in the cockpit space and the module block, real those simulating acceleration sensations.

The integrated aviation RNS and training assessment contains an operator’s automated workstation and associated network equipment that provides software operation of the operator’s automated workstation in a local area network in conjunction with objective monitoring systems of a modular design training simulator and combat trainer, as well as a registration and accounting system ground and flight training, planning system for ground and flight training, monitoring system, analysis and assessment of the level of nya preparation and accounting system and analysis of the technical condition of the level of training tools related to automated operator station.

In addition, the technical result is achieved by the fact that in the UBS an integrated complex of on-board equipment is interconnected with control bodies, integrated display systems, a power plant and its systems, aircraft flight parameters sensors and an on-board module of an integrated objective control system with the ability to provide:

take-off and landing training in conditions close to the conditions of their implementation on the main aircraft used in aviation units;

training and improving the skills of piloting the aircraft and navigation day and night in simple and difficult weather conditions;

flying in closed battle formations during the day in terms of visual visibility, in group aerobatics;

acquiring skills in extreme flight regimes during combat maneuvering;

training in actions in special cases of flight in case of aircraft equipment failures, pilot errors in piloting and navigation;

the development of weapons systems and the development of the basics of combat use in operations on ground and air targets, characteristic of the main aircraft used in aviation units and promising;

training in the skills of performing offensive and defensive maneuvers and the use of airborne defense systems in flight, including when flying at low altitudes;

simulation of the operation of airborne survey and sighting systems of the main aircraft used in aviation units, the preparation and use of their weapons;

imitations of a tactical situation with the possibility of setting it and changing it by an instructor, including:

simulation of the situation for working out the tasks of intercepting air targets that use radio countermeasures in combination with various types of maneuver, as well as the tasks of hitting ground targets,

simulating the functioning signals of typical enemy air defense systems and

imitations of launch and guidance of missiles, bombing and firing, imitations of counteraction of the opponent;

acquiring skills of targeted use of weapons on ground and air targets in the conditions of information and fire opposition of the enemy;

development of skills of intercepting air targets autonomously and in a ground guidance system by command;

simulation of controls for setting active and passive interference;

issuance of information to the OMS to simulate the use of standard weapons and perform defensive maneuvering;

flight simulation of air targets in the altitude range of 0.05-32 km with speeds from 0 to 4000 km / h;

simulations of conducting single and group air combat;

combat use of the aircraft in solving the tasks assigned to it during the day at PMU both singly and as part of a group;

control systems and complexes of airborne equipment and weapons at all stages of flight;

maximum reduction of crew load by automating the management of systems operating modes taking into account the real situation;

processing and displaying information received from sensors and subsystems of onboard equipment;

processing and displaying information to the crew necessary to solve all problems;

built-in objective control of the operation of all aircraft systems and crew actions, as well as combat training and simulator operating modes;

the use of unguided weapons;

the use of guided weapons;

determining the location of the aircraft, bringing the aircraft to a given area and returning it to the landing aerodrome;

collecting planes in a group, safe driving in battle formations;

the use of mixed weapons options.

The drawing shows a structural diagram of the proposed educational complex.

UBS 1 contains controls 2 in the cabin of the cadet, controls 3 in the cabin of the instructor, a comprehensive display system 4 in the cabin of the cadet, a comprehensive display system 5 in the cockpit of the instructor, the power plant 6 and its launch, monitoring and diagnosis systems, sensors 7 airplane flight parameters as well as an onboard module 8 of the integrated RNS, the inputs of which are connected to the outputs of the aforementioned 2-7, and an integrated complex of 9 onboard equipment. The latter includes a top-level on-board digital computer system, an information display system, an integrated navigation, landing, communication and recognition system, an integrated control system, on-board controls and an ejection device (not shown) and is interconnected with the said authorities 2- 7 and on-board module 8 of the integrated RNS.

The flight simulator 10 comprises a module 11 of the cockpit layout with a block of modules 12 of imitators of information display devices at the student’s workplace and a block of modules 13 of simulators of controls at the student’s workplace, a module 14 of the instructor’s workstation with a block of modules 15 of information display tools at the instructor’s workplace, and a block of modules 16 controls at the instructor’s workplace, a block of modules 17 for displaying information in the cockpit space, a block of modules 18 that imitate acceleration sensations th, as well as interconnected block of software modules 19 SOK and block software modules 20 simulation and control. The input of the block of software modules 19 is connected to one of the outputs of the module 15 of the instructor’s workplace, and the outputs are connected to the first inputs of the modules 11 of the pilot’s cockpit layout and 14 of the instructor’s workplace. The input of the block of program modules for simulation and control 20 is connected to the other output of the module 14 of the instructor’s workplace, and the outputs are connected to the second inputs of the modules 11 of the cockpit’s cockpit and 14 of the instructor’s workplace and the inputs of the block of modules 17 for displaying information in the cockpit space and the block of modules 18 implementing imitation of acceleration sensations.

The aviation integrated system of the RNS and training assessment 21 contains an automated workstation 22 of the operator and associated network equipment 23 (a system for interfacing with a module 24 for interfacing with an on-board module 8 of an integrated RNS UB 1 and a module 25 for interfacing with a block of program modules 19 RNS simulator 10), providing the software functioning of the automated workstation of 22 operators in the local area network together with the RNS of the flight simulator 10 and UBS 1, as well as the ground and flight registration and accounting system 26 th training, system 27 for planning of ground and flight training, system 28 for monitoring, analyzing and evaluating the level of training, and system 29 for recording and analyzing the level of technical condition of training tools associated with the workstation of 22 operators.

Aircraft UTK with UBS 1 (light multi-purpose aircraft with dual control from the front and rear cockpits) of the Yak-130 type is designed to train flight personnel in solving the following problems:

take-off and landing under conditions close to the conditions of their implementation on the main aircraft used in aviation units;

piloting the aircraft and air navigation day and night in simple and difficult weather conditions;

the implementation of complex types of maneuvers in conditions close to the conditions for their implementation on the main aircraft used in aviation units, in the entire operational range of their altitudes and flight speeds;

flying in closed battle formations during the day under visual visibility and group aerobatics;

actions at extreme flight regimes during combat maneuvering;

actions in special flight cases in case of aircraft equipment failures, pilot errors in piloting and navigation;

reaching angles of attack of up to 35 degrees, entering and correcting deviations when entering stall flight modes, and removing from a tailspin;

the development of on-board equipment and weapons systems, the development of the basics of combat use in operations on ground and air targets, characteristic of the main aircraft used in aviation units and promising fifth-generation aircraft.

The lightweight multi-purpose aircraft with dual control from the front and rear cockpit of UBS 1 provides attacks on ground targets from horizontal flight, from cabrying and diving with angles up to 45 °, as well as attacks from ground targets from diving with angles up to 70 ° and from complex types of maneuvers .

The takeoff and landing characteristics of an aircraft with normal and landing mass ensure its operation from a concrete runway of class III and unpaved airfields.

The flight crew of the light multi-purpose UBS 1 with dual control consists of two people, while it is possible to carry out the flight by one crew member.

To ensure maximum adaptation of the flight crew to the main aircraft used in aviation units of a particular type, UBS 1 has a structural similarity to the cockpits of the cockpits of the aircraft.

In addition, UBS 1 ensures the safe execution of simple, complex and aerobatic maneuvers, and is also equipped with a control system that allows for the inclusion of an active flight safety system in it, and provides reprogrammability to obtain stability and controllability characteristics close to those of aircraft of the type Su-27 and MiG-29.

UBS 1 is equipped with devices, an indication system, control panels that form the information and control field of the cockpit, identical or as close as possible to the main aircraft used in aviation units and promising fifth-generation aircraft, as well as equipment that can simulate the operation mode of on-board sighting systems, modes of preparation and use of weapons included in the weapons systems of the aircraft.

The instructor’s cabin equipment provides flight from take-off to landing, control and duplicate priority control of take-off and landing devices, main systems, aircraft and engine units. In addition, it provides full and continuous monitoring of the readings of instruments and indicators of the student’s cabin, as well as monitoring of the student’s actions with the airplane’s control and visual observation of the student from the instructor’s cabin.

The front cockpit of UBS 1 is equipped with a visibility changing system (SIV) (“curtain” type) with control from the instructor’s cabin for training in instrument flights and flights with a set minimum weather.

In the cabs of UBS 1, ejection seats are installed, equipped with devices that ensure long pilots stay in a working position without noticeable fatigue. In addition, the cabs of UBS 1 are equipped with an air conditioning system that operates from an autonomous on-board air source, allowing you to create an acceptable temperature in the cabs before boarding the crew without starting the main engines or using an external air source. The air conditioning system automatically ensures that the pilots maintain the temperature set by the pilots at all stages of the flight, including taxiing.

The view from the instructor’s cabin provides runway visibility at all stages of take-off, pre-landing planning, when entering and correcting deviations for landing and landing. In the presence of precipitation, visibility conditions from the rear cab are no worse than visibility conditions from the front.

At UBS 1, the cab lantern was opened on the ground without the use of electric or pneumohydraulic systems, as well as access to the cadet’s cabin and instructor for built-in devices.

Normal aircraft combat load includes:

two guided short-range air-to-surface weapons;

two short-range air-to-air guided missiles;

removable cannon mount with ammunition of at least 100 rounds;

device for ejection of spent REP funds.

Aircraft with normal take-off weight in the conditions of ISA has:

maximum flight speed near the ground and at an altitude of not less than 900 km / h;

practical ceiling of at least 10,000 m;

tactical range of action at an altitude of 200 m - at least 260 km;

with an available overload of N 200 m and Vpr 400 km / h - at least 3.5 units;

maximum operational overload without suspensions - +8 ...- 3 units;

takeoff speed at take-off - 190-200 km / h (without suspensions);

landing speed - 180-190 km / h (without suspensions);

take-off and run length for basing on the airfield of the III class.

The UBS is equipped with a power plant, including two turbojet bypass engines (turbofan engines) and an auxiliary turbine engine.

Under conditions of H = 0, M = 0, σin = 1, the ISA turbojet engine has.

Maximum mode:

traction no less than 2500 kgf

specific fuel consumption of not more than 0.64 kg / kgf · h.

Training Mode:

traction no less than 2200 kgf.

Low gas:

traction no more - 120 kgf.

The power plant 6 has an autonomous starting system, which allows for reliable starting of engines on the ground and in the air up to a height of at least 6 km, provides counter-launching and starting from autorotation mode, as well as starting from a ground source. The engine starting system provides a minimum of pilot action when they are launched on the ground and in the air.

The design of the air intake of the power plant 6 ensures the prevention of entry into the inlet channel of the aircraft when testing the engine on the ground, during taxiing, take-off and landing of foreign objects larger than 5 × 5 × 5 mm.

The on-board electronic system for monitoring and diagnosing the power plant 6 provides the monitoring of the operability of each engine, as well as predicting their technical condition in accordance with the adopted system for recording and displaying information on an airplane.

UBS 1 is equipped with 9 attachment points for external suspended objects.

UBS 1 is equipped with a weapon control system that provides:

preparation and launch (discharge) of the selected weapon;

transfer of information on the availability, type and readiness for use of TSA placed at suspension points;

the formation of the necessary locks to ensure safety during the operation and combat use of TSA;

power supply from on-board sources to TSA;

conversion and transmission from the digital computer of the upper level of target designation signals to the TSA.

UBS 1 is equipped with a complex of on-board equipment (BWC), which provides:

take-off and landing training in conditions close to the conditions of their implementation on the main aircraft used in aviation units;

training and improving the skills of piloting aircraft and navigation day and night in simple and difficult weather conditions;

flying in closed battle formations during the day in terms of visual visibility, in group aerobatics;

the acquisition of skills in extreme flight conditions during combat maneuvering;

training in actions in special cases of flight in case of aircraft equipment failures, pilot errors in piloting and navigation;

the development of weapons systems and the development of the basics of combat use in operations on ground and air targets, characteristic of the main aircraft used in aviation units and promising;

training in the skills of performing offensive and defensive maneuvers and the use in flight of airborne defense systems, including when flying at low altitudes;

imitation of the operation of airborne survey and sighting systems of the main aircraft used in aviation units, the preparation and use of their weapons;

imitation of tactical situation with the possibility of its task and change by the instructor, including:

simulation of the situation for working out the tasks of intercepting air targets that use radio countermeasures in combination with various types of maneuver, as well as the tasks of hitting ground targets;

simulation of the functioning signals of typical enemy air defense systems;

simulation of missile launch and guidance, bombing and firing;

imitation of opposition of the opponent;

acquiring skills of targeted use of weapons on ground and air targets in the conditions of information and fire opposition of the enemy;

development of skills of intercepting air targets autonomously and in a ground guidance system by command;

simulation of controls for setting active and passive interference;

the issuance of information to the OMS to simulate the use of standard weapons and perform defensive maneuvering;

flight simulation of air targets in the altitude range 0.05 ... 32 km with speeds from 0 to 4000 km / h;

simulation of conducting single and group air combat;

combat use of the aircraft in solving the tasks assigned to it during the day at PMU both singly and as part of a group;

management of systems and complexes of airborne equipment and weapons at all stages of the flight of the aircraft;

maximum reduction in crew load by automating the management of systems operating modes taking into account the real situation;

processing and displaying information received from sensors and subsystems of onboard equipment;

processing and displaying information to the crew necessary to solve all problems;

built-in objective control of the operation of all aircraft systems and crew actions, as well as combat training and simulator operating modes;

the use of unguided weapons;

the use of guided weapons;

determination of the location of the aircraft, the withdrawal of the aircraft in a given area and its return to the landing aerodrome;

collecting planes in a group, safe driving in battle formations;

the use of mixed weapons options.

The on-board equipment systems of UBS 1 are functionally and algorithmically interconnected and represent a single complex.

The main components of the CCD are:

top-level on-board digital computer system;

information display system;

integrated navigation, landing, communication and recognition system;

integrated management system;

airborne controls;

waste device.

The top-level on-board digital computer system provides the solution to the following tasks:

automatic entry and storage of a combat mission;

collecting information from subsystems and governing bodies;

implementation of correction modes for navigation definitions from newly installed sensors and algorithms for complex information processing;

solving ballistic equations for unguided weapons;

implementation of algorithms for the use of newly installed weapons;

integrated processing of information from sensors;

constant monitoring of the state of on-board systems, reconfiguration of the complex in case of equipment failure;

automated management of MFIs and the formation of separate information frames for it;

information exchange with control systems for weapons on suspension;

Implementation of simulated operating modes of the CCD.

The on-board digital computing system of the upper level includes:

universal computer;

information input devices;

trunk channels of information exchange (ICIE).

Interface blocks and information exchange channels provide:

information exchange on 2-3 redundant multiplex channels in accordance with GOST 26765.52-87;

consistent exchange of information according to GOST 18977-79 and RTM 1495-75;

information exchange on the main parallel interface in accordance with GOST 26765.51-86;

receiving and issuing one-time commands in accordance with GOST 18977-79;

receiving and issuing analog information.

Information Display System (SDI) provides:

displaying a map of the area;

display of flight-targeting display formats in the interests of the use of guided and uncontrolled means of destruction for air and ground targets;

display of navigation and tactical display formats;

indication of the status of aircraft systems and suspensions;

Indication of the necessary information in simulated operating modes of the BWC;

indication of flight and navigation flight parameters in standby modes.

The information display system includes:

indicator on the windshield;

multifunctional color indicators (IFIs);

multifunctional control panels.

The multifunctional indicator of the information display system allows the pilot to select different display modes using the buttons located on the frame of the IFI.

Integrated management system provides:

control of the stabilizer, ailerons and rudders from the control knob and pedals;

control of wing socks, flaps and brake flap;

the required characteristics of stability and controllability of the aircraft in the entire operational area of heights and speeds, angles of attack and overloads;

automatic limitation of the limiting parameters of flight modes;

measuring air parameters and generating signals of current and limit values of altitude and speed parameters;

automatic and director control of the aircraft;

reprogramming stability and controllability characteristics of the aircraft.

On-board controls include:

built-in system control tools;

airborne information-measuring system (IMS) for monitoring and diagnostics;

a data preparation system for analyzing pilot results;

airborne registration device;

television system of objective control.

On-board controls provide:

control of on-board equipment systems from the moment of power supply;

implementation of operational types of training;

reception and registration of flight parametric information containing information on the operation of on-board systems and equipment;

reception and recording of voice (sound) information containing information about crew negotiations between themselves and ground services;

on-board processing of incoming information to monitor crew compliance with flight-operational limitations with recording results on-board drives and issuing to the IFI during post-flight (inter-flight) analysis and maintenance;

saving information registered by a protected drive;

ground-based assessment of the operability of systems and equipment for monitoring and predicting operational status;

assessment of crew actions during the flight;

registration of information indicated on the collimator aviation indicator;

registration of the outside cabin when working on a visually visible target;

registration of the position of controls and readings of instruments located in the student’s cabin.

For the formation of knowledge, skills, and professionally important qualities necessary for flight personnel to master and reliably operate UBS-1 in the entire range of its summer-technical characteristics before the flight, the training simulators include modular aviation simulators.

The structure of flight simulators 10 is based on modern and promising computing and audiovisual equipment with appropriate software. Structurally, simulators 10 and software are designed in a modular manner.

The simulator 10 of the procedural type is designed to familiarize the flight crew with the interior of the cockpit, to formulate a conceptual model of activity and to instill the initial skills in controlling the power plant, aircraft systems and the use of the complex of on-board equipment in preparation for flight and completing the flight mission in accordance with the content of the exercises appropriate training course.

The simulator 10 of the procedural type includes the following components:

the student’s workplace in the form of an airplane cockpit model with simulators of control and indication elements forming the information and control field of the airplane cockpit;

a simplified system of imitation of the camber visual environment (CIVO);

acoustic information simulation system;

simulator computing system with software package;

instructor's workplace;

objective control system;

general exercise equipment.

The simulator 10 of the procedural type provides the following tasks:

familiarization with the interior of the pilot's workplace, the location in the cockpit of the controls, indicators and alarms used to control the power plant, aircraft systems and the complex of on-board equipment and weapons;

the formation of skills to work with controls and displays at crew workplaces (information-control field) in preparation for flight, various flight modes, the operation of the power plant, on-board equipment and aircraft systems (reading indications of information display devices and practicing control actions for aircraft control, its systems and equipment);

familiarization with various flight modes and stages, including in emergency situations, the operating modes of onboard equipment and aircraft systems (the relationship of the values of the corresponding parameters and their permissible values) and the formation of skills in recognizing flight situations;

inculcation of procedural skills to work with aircraft systems and equipment in the main modes of its piloting, including actions in special cases in flight;

development of a sequence of actions when performing specific exercises (the content and sequence of elements of exercises, the nature and sequence of control actions during the exercise, the main controlled parameters at each stage of the exercise and their optimal and acceptable values).

In the management of the educational process, the simulator provides:

setting and changing the initial conditions of the exercise;

control and operational management of learner actions;

automated control, registration and assessment of actions;

a database for everyone trained on the simulator.

The simulator 10 of the procedural type provides modeling of the following on-board systems and equipment of the aircraft in the normal and emergency modes:

the operation of the power plant and general aircraft equipment;

management systems;

flight and navigation complex;

communication facilities;

complex of airborne equipment;

systems and equipment designed to solve combat missions.

The computer system of the simulator 10 provides modeling of the functioning of the systems and equipment of the aircraft. Algorithms and logic of the systems, the characteristic errors of their work, taking into account simulated operating modes, flight conditions and external factors provide mathematical models.

The mockup 11 of the cockpit on the simulator 10 contains the appropriate simulators of control and indication elements, which ensure the pilot's interaction with the systems and equipment of the simulated aircraft. In addition, the standard headset connected via standard connectors is placed at the workplace to reproduce the work of simulators of radio communication equipment, intercom, voice informant, and sound alarm.

The simulator 10 includes the student’s workplace, which is a simplified model of the cockpit.

The composition, appearance, geometric dimensions and placement of simulators of control and display elements in the aircraft cockpit layout correspond to the information-control field of the UBS 1.

The imitation of indicators (both gauge devices and indicators) is carried out by computer synthesis of the corresponding instrument panels on monitors.

The dashboard and panels are imitated using screen masks with control simulators (toggle switches, buttons, etc.). Screen masks in shape and dimensions correspond to the dashboard and panels of the UBS cabin.

The geometric dimensions and placement of simulators of devices, controls, individual panels basically correspond to real equipment. Possible distortions of geometric characteristics caused by the chosen method of their simulation do not introduce false skills in working with the information-control field of the cabin. Unused controls and displays are replaced by layouts.

The simulator of the control post (RUS, pedals and throttle) in terms of size and location repeat the real aircraft controls. Simulation of loads on the RUS and pedals is carried out using spring loaders with the possibility of preliminary control of forces. To simulate the trim effect, the RUS loader is controllable. The ore throttle simulator has a frictional loading system, which corresponds to the real force.

The chair used in the simulator in shape, height and tilt corresponds to a real UBS chair 1.

SIVO simulator 10 of the procedural type provides the formation of a stylized image of the cockpit visual environment in accordance with the tasks being solved and the simulated flight mode, time of day in the following volume:

space in the area of the aerodrome with the visibility of the runway, taxiways, lighting equipment, buildings, landscape of the surrounding area;

a mapped image of the landscape of the underlying surface outside the aerodrome area with the visibility of the terrain, forest areas, rivers, reservoirs, fields, settlements, as well as typical ground targets;

cloudiness, fog, haze;

coupled aircraft, as well as air targets and TSA.

SIVO is single-channel and provides a field of view of at least 60 × 40 ° and a frame rate of at least 50 Hz.

As a reproducing device SIVO can be used a television projector.

The SIVO database provides simulated flight in an area of at least 150 × 150 km with the ability to snap to a real geographical area using a digital map of the area.

A system for simulating acoustic information provides the reproduction of aerodynamic noise, noise from engine operation and aircraft systems in accordance with a simulated flight mode.

The reproduction of acoustic information on a procedural simulator is carried out using standard multimedia tools, including a sound card, appropriate software and speakers.

The computer system of the simulator 10 of the procedural type with the PMO package provides the simulator’s overall functioning, simulates flight dynamics, simulates the operation of the engine, on-board systems and equipment of the aircraft, the complex of on-board equipment (BWC), the complex of aviation weapons (CAV), the aeronautical and tactical situation, and external flight factors . In addition, the PMO simulator provides control and monitoring of the training process.

The architecture of the computing system and the software of the simulator 10 provides for the possibility of its interfacing with another simulator to ensure joint training of two pilots flying in pairs against a single air navigation and tactical background. Pairing is carried out through standard network equipment of a computing system (BC).

To provide training for cadets flying in pairs as a slave simulator 10 in the aircraft, the motion of the leading aircraft along the path set from the instructor’s workstation 14 is simulated.

When paired with another simulator, the aircraft simulated on another simulator acts as the master (slave).

The tactical situation is modeled in a volume that ensures the development of 10 relevant tasks on the simulator.

Workplace 14 instructor provides the following tasks:

turning on, turning off and preparing the simulator 10 for operation, monitoring the performance of systems and the simulator 10 as a whole;

preliminary task of the exercise scenario and input of the necessary initial data;

operational control and management of the flight crew training process, control of the student’s actions, conducting two-way communication with him, playing up the necessary information (for example, performing the functions of a flight leader, etc.);

assessment of student actions;

operational change of the current scenario of the exercise (task of emergency situations, input of failures, etc.).

Hardware RMI simulator 10 can be implemented in the form of a serial PC connected with the aircraft simulator 10. The control process is carried out through a standard display, keyboard and manipulator type “mouse”. Also on the RMI are the on / off bodies of the simulator.

The RNS of the simulator 10 is intended for the implementation of automated objective control and evaluation of the actions of students in the process of training on the simulator 10 with the issuance of an assessment of the quality of each exercise with reflection of deficiencies in preparation and recommendations for their elimination.

The RNC accumulates statistical material for each student according to all training results, generalizes this material and determines the integral assessment with an indication of possible shortcomings in the preparation of each student.

The results of objective control are presented at the RMI both promptly during the training process, and at the end of the training in the form of an integrated assessment indicating the shortcomings at all stages of the exercise.

The results of objective control are documented both on magnetic and paper media.

The software that ensures the functioning of the RNS is implemented in the RMI.

General exercise equipment is designed to ensure the health and normal functioning of both individual systems and the simulator 10 as a whole. It consists of:

power supply system that provides all the simulator systems from the industrial network 220 V, 50 Hz, and conversion to the required type of electricity (constant, alternating voltage, its amplitude and frequency) and quality (permissible deviations), as well as providing emergency protection for the simulator and its systems from overvoltage and other emergency factors;

air conditioning and ventilation system that provides normal operating conditions for the simulator and its systems in terms of temperature, humidity and clean air;

health monitoring system for automated health monitoring and diagnostics of the main systems of the simulator 10.

The simulator 10 of a specialized type is intended for the training and training of flight personnel throughout the entire range of tasks related to the piloting, navigation and combat use of UBS 1 using the on-board instruments, equipment and systems, including actions in special cases in flight. The hardware and software of the specialized type of simulator are made on a modular basis and provide for the possibility of creating an integrated simulator of UBS 1 on their basis.

In this case, the simulator 10 includes:

the student’s workplace in the form of a cockpit model of UBS 1 with simulators of control and indication elements forming the information-control field of the airplane cabin;

visual environment simulation system;

simulator of acoustic information;

simulator of acceleration effects;

instructor's workplace;

simulator computing system with software package;

THE JUICE;

general exercise equipment.

Simulator 10 provides training for the flight crew to solve the following problems:

inclusion, control and preparation for flight of onboard systems and aircraft equipment;

preparation of the power plant for launch, launch, testing on the ground and launch in the air;

taxiing, take-off, climb with visual visibility of the runway, adjacent terrain and the horizon, as well as take-off at night with visual visibility of night start facilities;

piloting the aircraft by instruments and visually in the full operational range of heights, speeds, roll and pitch angles, attack and overload angles using on-board instruments, flight and navigation equipment and systems in manual, director and automatic modes;

performance of simple and complex aerobatics;

making decisions on timely bailouts and its implementation;

air navigation along the route at high, medium and low altitudes, using the navigation systems on board;

two-way communication with ground control centers simulated by interacting aircraft and an instructor;

pre-landing maneuver, landing approach and landing using aerobatic navigation and radio engineering landing equipment, as well as with visual visibility of the runway;

development of actions in case of falling into critical flight modes (corkscrew, stall, etc.), in case of failure of the power plant, aircraft systems and equipment, as well as in the event of other emergency situations;

working out of group flocking as a part of a couple day and night in PMP and beyond the clouds;

search, detection, identification and targeted use of TSA on ground moving and stationary targets;

interception of air targets in free space and on the background of the earth;

conducting maneuverable close air combat;

combat use in the face of opposition from simulated enemy ground and air forces;

counteraction to the attacking forces of the enemy;

analysis of the results of combat use;

conducting group activities;

actions in special cases at the stages of combat use;

decision on timely bailout and its implementation.

The simulator 10 provides the following training opportunities:

task and operational change in the initial conditions of the exercise, external factors simulating a flight task;

control over the actions of students in regular and emergency situations, as well as the operational change in the conditions of a flight task;

entry of failures and control over the actions of students in regular and emergency situations;

repeated testing of individual tasks and phases of flight and combat use under given initial conditions;

stopping the “flight” with freezing the current coordinates and readings on the instruments to analyze the situation and continue the “flight” from this point;

objective (automated) control and assessment of exercises;

creating a database for each student with the ability to process information about the results of training on the simulator.

The simulator 10 provides modeling in the normal and emergency modes of operation of the following on-board systems and equipment UBS 1:

power plant 6;

fuel system;

oil system;

hydraulic system;

power supply systems;

fire fighting equipment;

anti-icing system;

air conditioning and pressure control systems;

aircraft control systems;

automatic control systems;

flight and navigation complex;

radio communication equipment;

light and sound alarm systems;

lighting equipment;

complex of altitude and speed parameters,

radar equipment;

sighting and navigation complex;

weapons control systems;

airborne defense complex.

Modeling the functioning of aircraft systems and equipment is performed in the computer system of the simulator. Mathematical models reflect the algorithms and logic of the operation of these systems, as well as reflect the characteristic errors of their work, taking into account simulated operating modes, flight conditions and external factors.

The computing system with the software package is based on standard serial computing tools and provides:

general functioning of the simulator and the operation of its systems;

modeling in real time the dynamics of the flight of UBS, interacting forces and enemy forces;

real-time simulation of the operation of simulated systems and equipment;

real-time simulation of the tactical environment and external conditions;

management and supervision of the educational process.

The architecture of the computing system of the simulator 10 provides for the possibility of its interfacing with other simulators (and with remote access) to provide the possibility of joint training on a single air navigation background to work out interaction issues when solving various tasks in pairs.

The crew interacts with simulated aircraft systems and equipment through the appropriate control and display simulators located at the student’s workplace on the simulator. The work of simulators of radio communication equipment, intercoms, voice informant, sound alarm are reproduced through a standard headset, connected via standard connectors at the workplace.

The student’s workplace on a specialized-type simulator 10 is a full-size mock-up of the airplane’s cockpit with simulators of control and indication elements forming the information-control field (ICP) of the UBS 1 cockpit.

The design of the layout 11 of the cockpit provides the ability to install it on a dynamic stand of a system for simulating acceleration effects.

The internal geometric dimensions and coloring of the cab layout 11, the location, dimensions and appearance of the control and indication simulators correspond to the real ones. In this case, possible distortions in the geometry of the cockpit caused by the method of reproducing its IUP are minimal and do not create false images in a training flight crew.

Simulators of controls and displays are identical in geometry and appearance to real equipment. Moreover, the images of some means of displaying information can be made by computer synthesis.

Simulators of RUS, pedals and throttle in geometric characteristics and placement are fully consistent with the real ones. The reproducible loads (efforts) on the RUS and pedals correspond to the reproduced flight mode.

The load on the controls is reproduced by using controlled loaders based on torque motors or controlled hydraulic loaders, which also reproduce the trim effect.

The layout of the cockpit 11 is equipped with lighting similar to the lighting of the cockpit of a real aircraft, and a ventilation and air conditioning system that provide normal sanitary and hygienic conditions for training the flight crew.

The simulator visual environment simulation system provides the learner with visibility with a high degree of realism of the image of the cockpit space in accordance with the task and the simulated flight mode, time of day, weather conditions, in the following volume:

space in the area of the aerodrome with the visibility of the runway, taxiways, lighting equipment, buildings, landscape of the surrounding area;

volumetric image of the underlying surface landscape outside the aerodrome area with visibility of the terrain, forest areas, rivers, reservoirs, fields, settlements, as well as typical ground objects;

cloud cover, fog, haze, rain front;

coupled aircraft;

external visual ground and air situation in solving combat missions, with imitation of interacting aircraft, enemy ground and air assets and effects associated with the use of anti-aircraft weapons (traces of missiles, shells, smoke, characteristic destruction of objects and targets after using anti-aircraft weapons, etc. .).

The simulator visual environment simulation system (SIVO) has at least 3 channels and provides a field of view of at least 160 ° × 40 °. The frame rate is not lower than 50 Hz, the resolution is 1280 × 1024 pixels per channel. At least three television projectors, one for each channel, are used as a SIVO reproducing device.

SIVO includes a database of flight simulations in the following areas:

the area of the aerodrome (s) take-off, landing;

route area;

area (s) of piloting.

SIVO includes a database of simulating the underlying surface with a size of at least 150 × 150 km with reference to a real geographical area using a digital map of the area.

A simulator of acoustic information with a fairly high degree of realism reproduces the following noises:

aerodynamic;

runway, taxiway traffic;

work of blood pressure, including abnormal modes of their work;

operation of equipment and systems of a simulated aircraft;

acoustic effects associated with the use of TSA.

The corresponding acoustic information is synthesized by computer means and reproduced by stereo (or multi-channel) speaker systems. The hardware simulators of acoustic information are implemented as separate special blocks based on standard multimedia tools.

To reproduce the acceleration effects on the simulator, an acceleration information simulator based on a dynamic stand can be used as an autonomous hardware-software module. In this case, it is possible to use dynamic stands with a hydraulic or electric drive.

The instructor’s workstation 14 (RMI) is made in the form of a separate hardware and software module, including indicators intended for displaying the information necessary for monitoring the educational process, and the controls through which the instructor enters the necessary information and performs process control functions.

RMI contains the following components:

computer system;

duplicate display organs of simulated aircraft;

SIVO video monitoring device;

monitors displaying information required by the instructor;

controls in the form of appropriate consoles, providing on / off of the simulator and its systems (emergency shutdown);

PC display, keyboard and mouse manipulator for forming tasks, changing scenarios and controlling the training process.

The RMI computer system is connected to the base aircraft of the simulator and processes and submits the required information to the instructors in the required form, and processes the instructor commands.

RMI is designed to solve the following tasks of management and observation of the educational process on the simulator:

turning on, turning off and preparing the simulator for work, monitoring the performance of systems and the simulator as a whole;

preliminary selection of exercise scenario and input of initial data;

operational monitoring and management of the training process, monitoring the actions of trainees, conducting two-way communication with them, the use of game training methods (performing the functions of a flight leader, etc.);

input of the flight mission (configuration, route, combat mission, flight of a single aircraft, in a pair) and the conditions for its implementation (time of day, weather conditions, visibility conditions, combat use area);

task of tactical situation (air, ground targets, fire and other counteraction, etc.);

operational change in the scenario of the current exercise (input failures);

control and adjustment of the learner's actions;

showing the right actions;

playing up the actions of the enemy and the planes of the group

objective control and assessment of the actions of students;

display of control results for the exercises performed.

The simulator 10 includes a RNS designed to provide automated monitoring and evaluation of the actions of students in the training process. The functioning of the RNS is provided by software implemented in the RMI. Estimated actions of the learner formed by the RNC are presented on the RMI indication and recorded on magnetic and paper media.

The RNC accumulates statistical data for each student based on the results of all training sessions, summarizes them and determines the integral score indicating the possible errors of each student. The results of objective control are presented to the RMI promptly during the training and at the end of the training in the form of an integral assessment indicating the errors of each student in all exercises.

General exercise equipment is designed to ensure the health and normal functioning of individual systems and the simulator as a whole. The structure of the general exercise equipment and simulator systems include:

power supply system that provides electricity to all the simulator systems from the industrial (or airfield) network, including the conversion of the industrial network to the desired type (constant, alternating voltage, its amplitude and frequency) and quality (permissible deviations), as well as providing emergency protection for the simulator and its systems from overvoltage and other emergency factors;

air conditioning and ventilation system that provides normal operating conditions for the simulator and its systems in terms of temperature, humidity and clean air;

A system for automated performance monitoring and diagnostics of simulator systems.

UTK contains an integral RNS and training assessment 21.

UBS 1 and ground-based teaching aids are equipped with an interconnected integrated system of objective control (ISOQ) of the actions of the cadet and instructor, with a database of learning outcomes and the level of professional training. ISIC has a two-level construction scheme and consists of the RNC of each TSS (lower level), united by a single information center for management and objective control (upper level). In addition, this system should receive information on the results of the performance of flight missions at UBS 1 from ground-based means of processing flight information according to the data from the UBS 1.

Aircraft RNS and ground TCO RMS provide:

recording the parameters of the exercises and crew actions and their subsequent reproduction for the purpose of demonstration analysis when analyzing the results of the exercises;

recording the functioning parameters of the units and systems of the aircraft, engine, airborne complexes, their safety, including in the event of a flight accident, their subsequent reproduction in order to analyze the condition and performance of aircraft;

processing objective control materials of completed flights, including inter-flight analysis of the completeness and quality of the flight performed and the operation of aviation equipment for a time not exceeding the period of preparation of the aircraft for the next flight, and in-depth analysis with the possibility of demonstrating the entire flight and its fragments with showing parameters and comparing them with reference, showing the deviations and errors in the technique of piloting, navigation, combat use, operation of aircraft;

automatic assessment of the results of the flight crew performing exercises in accordance with the requirements of the applied training (preparation) program and in its entirety;

automated analysis of training results in order to identify erroneous actions of flight personnel;

the implementation of evaluation functions in real-time pace of exercise;

the formation of an integrated assessment of the results of the exercises by the flight crew and the entry of the necessary information on the degree of readiness of the flight crew to the data bank of the information center for control and objective control.

The single information center for management and objective control provides:

control of the sequence of training at all LLPs (theoretical and simulator training) before training on an airplane;

assessment of the readiness of each pilot to switch from one type of training to another, including readiness to practice a task (exercise) on an airplane according to the level of appropriate training in the training class and on simulators;

control of the sequence of development of all tasks (exercises KULP and KBP) in accordance with the training program;

assessment of the readiness of flight personnel to master more complex tasks based on the results of mastering previous tasks;

the formation of a databank for each pilot and student, taking into account the training of the flight personnel (general, by type of flight training, weather conditions, time of day and limitation periods), its replenishment after each training in air and on the ground, as well as the analysis of training taking into account the achieved level, work experience, individual qualities and established limitations;

processing of information obtained by the results of the flight shift (flight time of each pilot, types of flights performed and numbers of exercises, weather conditions and time of day, etc.), the distribution of this information in the form of accounting and reporting documentation for specified categories (from pilot to shelf inclusive);

an integrated assessment of the general level of preparedness of each pilot and student based on the results of all trainings and determination of the degree of readiness to perform more complex exercises;

accumulation of statistical material on the quality of flights performed by each pilot and the possibility of systematizing the deviations, errors by flight stages and groups of reasons with graphic information and printing;

taking into account deviations, errors and prerequisites for flight accidents made by personnel by groups of causes, types and elements of flight, to ensure their analysis in order to develop preventive measures;

creation of a database on flight accidents with a distribution by groups of causes, types of aircraft, types and stages of flights, weather conditions and time of day with the possibility of analyzing and developing preventive measures;

development of options for planned flight tables, taking into account the training of the flight crew and according to the given conditions, with their printing for use in the flight process;

information on the level of technical condition of aviation equipment, prediction of its failures, departure for routine maintenance and repair, calculation of the need to provide spare parts and assemblies.

ISOK 21 is designed to provide constant, formalized automated control of the actions of the cadet and instructor in the process of training and training throughout the entire range of tasks of the Yak-130 combat trainer.

ISOK 21 provides the solution to the following functional tasks:

- control of the sequence of training at all TSS (theoretical and simulator training) before training on the plane;

- assessment of the readiness of each pilot to switch from one type of training to another, including readiness to practice a task (exercise) on an airplane according to the level of appropriate training in the training class and on simulators;

- control the sequence of development of all tasks (exercises KULP and KPB) in accordance with the training program;

- assessment of the readiness of flight personnel to master more complex tasks based on the results of mastering previous tasks;

- the formation of a databank for each pilot and student, taking into account the training of the flight personnel (general, by types of flight training, weather conditions, time of day and limitation periods), its replenishment after each training in the air and on the ground, as well as the analysis of training taking into account the achieved level , work experience, individual qualities and established limitations;

- processing of information obtained by the results of the flight shift (flight time of each pilot, types of flights performed by him and numbers of exercises, weather conditions and time of day, etc.), distribution of this information in the form of accounting and reporting documentation for given categories (from the pilot to the shelf inclusively);

- an integral assessment of the general level of preparedness of each pilot and student based on the results of all trainings and determination of the degree of readiness to perform more complex exercises;

- accumulation of statistical material on the quality of flights performed by each pilot and the possibility of systematizing the deviations, errors by flight stages and groups of reasons with graphic information and printing;

- taking into account the deviations, errors and assumptions made by the personnel for flight accidents according to the groups of causes, types and elements of the flight, to ensure their analysis in order to develop preventive measures;

- Creation of a database on flight accidents with a distribution by groups of causes, types of aircraft, types and stages of flights, weather conditions and time of day with the possibility of analysis and development of preventive measures;

- development of options for planned flight tables, taking into account the training of the flight crew and according to the given conditions, with the conclusion of their printing for use in the flight process;

- information on the level of technical condition of aviation equipment in the interests of predicting its failures, moving away from routine maintenance and repair, calculating the need for spare parts and assemblies.

Field of application of ISOK 21: planning and management of the training process for the preparation of flight personnel using aviation simulators of a modular design and UBS 1 type Yak-130.

ISOK 21 is implemented on the basis of a hardware-software complex consisting of:

- Workstation (AWS) of the operator ISOK 21;

- network equipment to ensure the functioning of the workstation in the local area network (LAN) in conjunction with the flight simulators of a modular design;

- a module for data input from a secure on-board carrier (ZBN) of the Yak-130 type UBK JUICE.

AWS of ISOC 21 operator can be implemented on the basis of a high-performance workstation consisting of:

- 2-processor motherboard based on Intel Pentium 4 processors with a clock frequency of at least 1 GHz;

- RAM capacity of at least 512 MB;

- HDD capacity of at least 80 GB;

- video card for connecting two monitors;

- 19 ’monitors with a resolution of at least 1280 × 1024 pixels;

- network card 100 Mbps.

The workstation of the ISOC 21 operator also includes a printer and an uninterruptible power supply unit, which ensure the operability of the ISOK 21 software in case of a short-term power outage.

ПСО ИСОК 21 can be implemented in the environment of the network operating system Windows 2000.

The ISOK 21 database system operates under the control of the MS SQL Server 2000 database server.

The use of ISOK 21 as intended is organized by a specially trained instructor (operator).

The general organization of work includes the following steps:

- the inclusion and preparation of the ISIS for work,

- work in the mode of maintaining a database of flight personnel,

- work in the mode of maintaining a database on aircraft,

- work in the planning mode of the training process,

- work in the “Debriefing” mode and assess the level of training of flight personnel,

- completion of the work session and turning off ISIC 21.

General procedure for inclusion and preparation for work:

- enable operator workstation;

- load the AWP operating system;

- download the PMC EICU and OK.

The order of inclusion of the operator workstation:

- turn on the uninterruptible power supply device;

- turn on the power of monitors;

- turn on the power of the system unit;

- turn on the printer.

The order of work in the mode of maintaining a database of flight personnel:

- download the software for registration and accounting of the level of training of flight personnel;

- using the PMO menu system, perform the necessary operations to maintain a flight crew database (data entry, data search, data editing);

- if it is necessary to prepare reports, select the appropriate report type in the report generator menu.

The order of work in the mode of maintaining a database of aircraft:

- download the software for accounting and analysis of the state of aviation technology;

- using the PMO menu system, perform the necessary operations on maintaining the AT status database (data entry, data search, data editing);

- if it is necessary to prepare reports, select the appropriate report type in the report generator menu.

The order of work in the planning mode of the training process:

- download the PMO system for planning the training process;

- using the PMO menu system, perform the necessary operations for maintaining the planning system database (data entry, data search, data editing);

- if it is necessary to prepare reports, select the appropriate report type in the report generator menu.

The operating procedure in the “Debriefing” mode and assessing the level of training of flight personnel:

- download the software for monitoring, analysis and assessment of the level of training of flight personnel;

- import data from the database of RNS simulators or from the ZBN UBS 1 Yak-130;

- using the PMO menu system, perform the necessary operations on the reproduction of previously registered flights (using the RNS simulators or on-board RNS UBS 1 Yak-130);

- using the menu of the electronic flight book maintenance mode, enter the necessary data on the results of the training flight (on the simulator or on a real UBS 1 Yak-130);

- if it is necessary to prepare reports, select the appropriate report type in the report generator menu.

General shutdown procedure of ISOC 21:

- complete the implementation of the software;

- terminate the workstation operating system;

- turn off the operator workstation.

The procedure for turning off the operator workstation:

- turn off the power of the printer;

- turn off the power of the system unit;

- turn off the power of monitors;

- turn off the uninterruptible power supply device.

Claims (2)

1. Aviation training complex for flight personnel, which is a combination of combat training aircraft, specialized and procedural type aviation simulators and an integrated system of objective monitoring and training assessment, while the combat training aircraft contains controls in the cadet’s cabin, organs control in the instructor’s cabin, a comprehensive display system in the cadet’s cabin, a comprehensive display system in the instructor’s cabin, a power plant and its launch systems, con monitoring and diagnostics, aircraft flight parameters sensors, as well as an on-board module of an integrated objective control system, the inputs of which are connected to the outputs of the said controls, integrated display systems, a power plant and its systems, and an integrated complex of on-board equipment, including an on-board digital computer system top level, information display system, integrated navigation, landing, communication and recognition system, integrated control system, on-board means to control and discharge device of expendable funds and interconnected with the said controls, integrated display systems, power plant and its systems, aircraft flight parameters sensors and on-board module of the integrated objective control system, the flight simulator contains a pilot’s cockpit module with a block of modules for simulating information display devices on the workplace of the student and the block of modules of simulators of controls at the workplace of the student, the module of the workplace of the instructor with bl lump of modules for displaying information at the instructor’s workplace and block of control tools for modules at the instructor’s workplace, block of display modules for information in the cockpit space, block of modules that imitate acceleration sensations, as well as interconnected block of program modules of the objective control system, the input of which is connected to one of the outputs of the module of the instructor’s workstation, and the outputs - to the first inputs of the modules of the layout of the cockpit and the instructor’s workplace, and the block of software modules imitates aviation and control, the input of which is connected to the other output of the module of the instructor’s workstation, and the outputs are connected to the second inputs of the modules of the pilot’s cockpit and instructor’s workstation and the inputs of the module for displaying information in the cockpit space and the block of modules that imitate acceleration sensations, aviation integrated system objective monitoring and evaluation of training contains the operator’s automated workstation and associated network equipment that provides for the software operation of the car an operator’s workstation in the local area network together with the objective control systems of a modular design flight simulator and combat training aircraft, as well as a registration and accounting system for ground and flight training, a ground and flight training planning system, a monitoring, analysis and assessment system for training and a system for accounting and analysis of the level of technical condition of training facilities associated with the operator’s workstation. 2. The aviation training complex according to claim 1, wherein the integrated combat equipment complex in the combat training aircraft is interconnected with the control systems of the complex display systems of the power plant and its systems, aircraft flight parameters sensors and the onboard module of the integrated objective control system with the possibility of providing training for take-off and landing in conditions close to the conditions for their implementation on the main aircraft used in aviation units, training and improving skills piloting an airplane and navigating day and night in simple and difficult weather conditions, flying in closed battle formations during the day under visual visibility, in group aerobatics, acquiring skills in extreme flight modes during combat maneuvering, learning how to deal with special cases of flight failures equipment, pilot errors in piloting and navigation, mastering weapons systems and working out the basics of combat use in operations on ground and air targets that are characteristic of basic aircraft used in aviation units and prospective ones, training in offensive and defensive maneuvers and the use of airborne defense systems in flight, including when flying at low altitudes, simulating the operation of airborne surveillance and sighting systems of major aircraft used in aviation units, training and the use of their weapons, simulating a tactical situation with the possibility of setting it and changing it by an instructor, including simulating a situation for practicing tasks of intercepting air targets, that use radio countermeasures in combination with various types of maneuver, as well as tasks of hitting ground targets, simulating the signals of the typical air defense systems of the enemy and simulating the launch and guidance of missiles, bombing and firing, simulating the enemy’s countermeasures, acquiring skills of targeted use of weapons on ground and to air targets in the conditions of information and fire opposition of the enemy, to develop skills for intercepting air targets autonomously and in the ground system I am on command, simulating the control of active and passive jamming, issuing information to the weapon control system (LMS) to simulate the use of standard weapons and perform defensive maneuvering, simulating the flight of air targets in the altitude range 0.05 ... 32 km with speeds from 0 to 4000 km / h, simulating the conduct of single and group air combat, the combat use of the aircraft in solving the tasks assigned to it during the day in simple meteorological conditions (PMU), both singly and as part of a group, systems management complexes of on-board equipment and weapons at all stages of the flight of the aircraft, minimizing crew load by automating the management of the operating modes of the systems taking into account the real situation, processing and displaying information received from sensors and subsystems of on-board equipment, processing and displaying information to the crew, necessary for solving all problems built-in objective control of the operation of all aircraft systems and crew actions, as well as combat training and simulator operating modes, the use of uncontrolled weapons, the use of guided weapons, determining the location of an aircraft, taking the aircraft to a designated area and returning him to the landing aerodrome, collecting planes in a group, safely driving in battle formations, and using mixed weapons options.