RU2267163C2 - Complex training system for aviation specialists - Google Patents

Abstract

FIELD: aeronautical engineering; vocational training of pilot personnel and ground services pertaining to flight control.

SUBSTANCE: proposed system includes computer complex. Central server of this complex is connected in parallel with functionally-oriented servers of local nets. Local nets connect computer complex with working positions of trainee and specialists: pilots, instructor, flight director, landing zone director, ground control group and inspector. Provision is made for operator's position for servicing the computer complex. Storage of central server contains base array of initial data, real process simulating unit with simulating devices and trainee monitoring unit.

EFFECT: maximum realistic conditions in training pilot personnel.

5 cl, 10 dwg

Description

The invention relates to aeronautical engineering, namely, an integrated training system designed for joint professional training of aviation specialists involved in the implementation, organization and management of flights: flight personnel and interacting with it during the flight operations of ground services.

There is a well-known unified multifunctional flight simulator containing a local computer network, a unified workplace (RM) for an instructor, a set of unified RM trainees in an instructor's flight group, a collective use screen, a flight information input device, a training script database, and a training results database. The local computer network contains software modules for the implementation of training scenarios, objective monitoring of the student and objective monitoring of the instructor / 1 /.

The disadvantages of the known device include the fact that the public screen does not allow to individualize the learning process and, therefore, significantly narrows the range of tasks.

The existing database of training scenarios does not allow making training interactive, making changes to it during the course of training depending on the decisions made by each student and their impact on other students.

In addition, in the well-known simulator, the nomenclature of the Republic of Moldova does not allow expanding the range of tasks for the interaction of various ground services and command personnel engaged in flight support.

RM pilots containing the student’s display modules and the student’s training modules do not allow developing the skills necessary for working in a real flight, and lead to the danger of educating “virtual specialists”.

A comprehensive training system for aviation specialists is known, containing from 2 to 8 aircraft (LA), equipped with RM installed on ball platforms of dynamic simulators moving in two or three planes, with personal computers, mechanical and electrical parts, and a control room with the RM of the control ground service and the local area network with the output of the picture in one virtual field of events to a common overview screen for all RM / 2 / - a prototype.

The known system provides for the simultaneous training of several crews and dispatch personnel of the ground control service on individual simulators equipped with RM, equipped with real instruments and equipment with discrete and continuous control elements connected by contact devices to the local computer network.

A disadvantage of the known training system is the low probability of its practical implementation, for example, the implementation of a common viewing screen for 2-8 helicopters is difficult not only because of its large dimensions, but also requires special equipment to darken it in daytime training, which significantly increases costs not only to create a complex, but also to operate it. In addition, such training conditions do not meet the conditions of real flights.

The rotation of each helicopter mounted on a ball bearing, carried out by 6 winches, will lead to greater energy consumption of the control system of all RM (2-8) trainees and will require the installation of additional equipment for its implementation. And fixing the helicopters on a platform located at the center of gravity of the centered fuselage of each helicopter, due to the limited length of the cable, will not allow rotation around each axis at large angles, which also does not allow to bring the training conditions closer to real ones.

Thus, the known device of an integrated training system is difficult to implement, not effective enough, because it does not allow to bring training conditions closer to the actual flight conditions. To create speeds and accelerations close to real, it is necessary to create great efforts that will lead to an increase in the already energy-intensive dynamic simulator and the integrated system as a whole and a significant increase in the cost of its operation.

In addition, in the well-known training system, the range of jobs is limited, for example, jobs are not provided for the inspector and other management personnel.

The task of the invention is to maximize the training and interaction of specialists of flight crews and various ground services, including command personnel to the real conditions of flight training, while minimizing the cost of training and operating an integrated training system.

The task is achieved by the fact that in the known device, an integrated training system for aviation specialists containing workstations (RM) of the ground control service, one or more RM of trained pilots equipped with individual simulators in real cockpits of aircraft installed on dynamic platforms with the ability to move in 2-3 planes equipped with control devices with discrete controls, valves and continuous controls associated with contact devices with a computing local area network in one virtual field of events and outputting information to visualization devices, the contact devices of continuous control units are made in the form of sensors, each of which is connected in series with the controller system, and the comprehensive training system is additionally equipped with a computing complex containing an operator’s PM with individual visualization device equipped with a central server with information input / output devices and storage devices om, which includes an array of source data bases, a unit for modeling real processes with simulation devices, and an objective control unit for students managing information exchange between local networks connecting the computer complex with the students of RM through parallel communication of the central server with functionally oriented servers of local networks of the RM of trained pilots, RM of the ground control service, for example, the RM of the flight manager, the RM of the landing zone leader, the RM of the ground control group and the RM instructor as well as the local network of the RM inspector, while the local networks include computer modules for implementing training scenarios and visualization devices connected in series with the servers, made in the form of individual screens or a system of monitors, and information is exchanged in local networks and between functionally oriented servers through a central server.

Each server of the RM pilot’s local network, which contains the modeling and control unit for the dynamic model of the aircraft, the control unit for the dynamic platform, the radio control unit, is connected in parallel with the information input / output device with the computing modules of the onboard visualization system for the cockpit space, the computing module of the instrument display system, and the control panel and engine noise simulators and an armament control system computing module, with discrete controls set Lena's dashboard messages, some of which is designed as a screen with holes on the perimeter and indicators located in front of one or more devices monitors display systems and control cabin armature.

The instructor’s server, which contains the modeling and control unit for the dynamic model of the aircraft and the radio communication control unit, is installed with the possibility of parallel connection with one of the PM’s servers and with the computing modules of the onboard visualization system of the cockpit space, the computing module for displaying instruments, controlling the cabin fittings and simulating engine noise, the armament control system computing module, while the instructor’s workplace is equipped on an individual simulator in a real cabin LA and controls further comprise a control input of educational failure.

The control ground service server, comprising the radio communication control unit and the aerodrome lighting equipment control unit, is connected in parallel with the computational modules of the short-range navigation radio system, the ground control group control system, the radio landing and weather control systems.

The flight director’s RM is equipped on an individual simulator with a long-range radar indicator, an indicator of a short-range navigation system, a command radio communication system, and an aerodrome lighting control system.

The RM of the head of the landing zone is mounted on an individual simulator and is equipped with indicators of the radar landing system, a command radio communication system, a control system for lighting equipment of the airfield, and a weather information display system.

The RM of the ground control group is designed as a simulator equipped with long-range radar indicators and command radio communications.

The central server is connected in series with the visualization system and the printing device of the class of flight debriefing and analysis of objective control equipment.

The presence of the indicated essential features in the claimed invention, first of all, the interconnection of the computer computing complex with the workplaces of flight crew and ground crew specialists located in real aircraft cabins equipped with real control bodies allows:

- expand the number of tasks to be solved and increase the efficiency of training through effective and high-quality training of flight personnel at all stages of the flight, acquiring the development and strengthening of combat skills both singly and as part of an aircraft group, and working out interactions when conducting combat operations between aircraft crews and a group of ground (combat) control;

- bring training conditions as close as possible to real conditions, conduct interactive comprehensive training on combat operations as part of aviation units, followed by analysis of each stage of operations;

- expand the composition and number of trained aviation specialists and training tasks from narrow and single to complex in the entire complex;

- to develop the skills of interaction between various services, including the acquisition, development and strengthening of combat management skills of both single aircraft and the group of aircraft, interactions between members of the combat operations control group;

- significantly reduce the cost of training by reducing the energy intensity of dynamic flight platforms, using simple design solutions of simulators of the components of the proposed system, including the relationship of the electromechanical and computer parts of the training system.

The proposed device is illustrated by drawings.

Figure 1 is a schematic diagram of an aviation integrated training system;

Figure 2 - schematic diagram of the connection of the central server with functionally oriented servers;

Figure 3 is a schematic diagram of the registration of the position of the continuous control;

Figure 4 - the computing module of the system of mapping devices with simulators of real discrete controls;

Figure 5 is a section aa in figure 4;

6 - individual flight simulator RM pilot;

Fig.7 is a side view of Fig.6;

Fig. 8 is an algorithm for the functioning of a computing complex using the example of the occurrence of a control action on a RUS in a pilot's cabin;

Fig.9 is a diagram of the implementation of communications between discrete controls in the cockpit and the cockpit of the instructor;

Figure 10 is an adaptive simulator loading continuous controls.

The proposed comprehensive training system for aviation specialists contains simulators with equipped RM students as part of a computer complex that directly implements the process of converting information and managing the training and simulator of aviation specialists of various profiles (see figure 1).

The computing complex VK contains a central server 1, which is included with the individual screen 2 of the visualization tools CB and input / output devices 3 in the PM 4 operator. Server 1 is connected in parallel with input-output devices 5, 6, 7, 8, 9 with functionally oriented servers: 10 local network of RM pilots 11 (from 1 or more RML), server 12 of the local network of instructor PM 13, server 14 of the local control LAN services, in particular, the PM of the flight manager 15, the RM of the landing zone leader 16, the RM of the ground control group 17, and also the inspector’s local network RM 18. At the same time, with the central server 1, forming a parallel local network, the PM 19 class of analysis of the means of objective control of the RNS and flight debriefing with the CB 20 and the printer 21 are connected in series.

The RM of trained pilots are flight simulators 11 with dynamic platforms 22 and real aircraft cabins installed on them. The instructor’s RM is equipped with an individual flight simulator 13. The control ground service RM is located on individual simulators, respectively:

PM flight manager 15, head of landing zone 16, RM ground control group 17.

The central server 1, which controls the exchange of information in an integrated training system between local networks, contains a memory device, including an array of source databases 23, a block for modeling real processes 24 with simulation devices 25, and an objective control unit for students 26 (Fig. 2).

Functionally oriented servers 10, 12, 14 that control the exchange of information in local networks: individual flight simulators 11, 13, individual simulators 15, 16, 17, and also PM 18 are connected by individual computing modules VM 27-39 to the visualization system CB, in including on-board visualization system BSV 41-46, made in the form of three screens, individual SV 47-50, made in the form of monitors.

Moreover, continuous controls 51, 52 (for example, RUS control sticks, pedals) are remotely connected by displacement sensors 53, each of which is connected in series through the controller system 54 to computing modules VM 30, BM 35 of the instruments and cabin fittings. In parallel with the sensors 53, switches 55 are connected to the controller system 54 (FIG. 3).

Cabins 56 simulators (figure 3) are equipped with control devices 57, valves and discrete controls 58 in the form of taps, buttons and other organs corresponding to the real ones, and are mounted on shields, some of which are made in the form of a screen 59 with holes 60 around the perimeter of the devices and indicators 57 located in front of the monitors 61 (see Fig. 4, 5). This implementation of discrete controls allows you to arrange them like in a real cockpit of an aircraft and, accordingly, develop the skills of working with real controls with trained pilots and instructors.

LA 56 cabins are mounted on dynamic platforms 22 with the possibility of angular movement in two planes with specified dynamic characteristics by electric motors of drives 62, 63 in pitch and roll, depending on the movement of the aircraft 51, 52 control stick in the cabin of the trained pilot 56. To reduce energy consumption and improve performance in the drives 62, 63 of the platforms 22 use cable wiring (not shown) (see Fig.6, 7). The rotation of the shaft of the electric motors of the drives 62, 63 is set by the controller system 54 depending on the rotation of the control handle of the aircraft 51, 52, fixed, for example, by optoelectronic displacement sensors 53.

The server 10 of the flight simulators 11 contains a modeling and control unit for a dynamic model of aircraft LA 64, a control unit for a dynamic platform 65, a control unit for radio communication between the pilots RM 66. The individual pilots BM27, VM28, VM29 on-board visualization systems BVS 41, 42 43 in-cab space. VMZO is a computational module of the instrument display system 57, control of the cockpit fittings 58 and noise simulation of aircraft engines LA 67 and VM31 by the computational module of the armament control system 68.

The instructor’s PM is an individual simulator 13 including a real aircraft cockpit, which has a separate connection with each simulator 11 of trained pilots, carried out by the central server 1. The controls 52 include the training failure input panel 69. The instructor server 12 allows you to switch any cockpit 56 included in the flight simulators 11 for themselves, to control the actions of the pilot when working with fittings in the cockpit 56 and the correctness of the exercises, intervene in the control process of the aircraft, indicating errors in the technique of pilots mania and air navigation. The server 12 is connected in parallel with the servers 10 through the central server 1. The server 12 contains a block for modeling and controlling the dynamic model LA 70, a radio control unit 71. In this case, visual information is displayed on the on-board visualization means BSV 44-46 by computational modules BM 35-39. The instructor's local network includes a computational module for the instrument display system, control of the cabin fittings, and noise simulation of aircraft engines BM 35 and VM 36 of the weapon control system.

The flight director’s RM is equipped with the simulator 15. The simulator 15 module 37 includes long-range circular radar units 72, 73 that allow viewing airspace at various scales, a short-range navigation system 74, a command radio communication system 75, and an aerodrome lighting control system 76, wherein the individual visualization tool CB 47 is connected in series with the computing module BM 37 of the short-range navigation system and server 14.

The RM of the head of the landing zone is equipped on the simulator 16 with individual means of visualization of SV 48 and is connected in series with the computing module 38 of the radio engineering system for landing and monitoring the meteorological situation, which includes the block of the radar landing system 77, the command radio communication system 78, the control system for lighting equipment of the airfield 79, and the information display system meteorological conditions 80.

The PM of the ground (combat) control group is a simulator 17 with an individual visualization tool 49 connected in series with the computing module 39 of the control system of the ground control group and the server 14. The module 39 contains an all-round radar viewing unit 81, command radio communications 82 for controlling the aircraft and implementation of interaction between members of combat crews.

The server 14 of the control ground service includes a radio control unit 83 and a control unit for lighting equipment of the airfield 84.

Inspector’s PM 18 is equipped with an individual visualization system CB 50, BM 40 and appropriate equipment for monitoring the actions of: flight crews 85, ground control service 86, instructor 87. The inspector’s local network is directly connected to central server 1 via a serial connection BM 40 for controlling parameters training system of the RM inspector 18.

The central server 1 is connected in series with the CB 20 of the class of debriefing and analysis of means of objective control 19 and the printer 21.

When training aviation specialists, a comprehensive training system ensures the implementation of the following steps:

- the stage of the pre-flight check of the equipment’s operability, its preparation for flights, the development of skills for working with real controls;

- stage of setting the task;

- the stage of practical development of training processes at all stages of the flight, acquisition, development and strengthening of combat skills, both singly and as part of an aircraft group;

- the stage of developing interaction in the conduct of hostilities between crews and the managing ground service;

- the stage of analysis and analysis of the results of flights.

The operator with PM 4 enters the initial conditions and initial data for completing the task of input 3 of the central server 1: exercise number, geographical area, weather conditions, time of day and year, parameters of the radio navigation situation of the flight area, complex configurations for training, simulation parameters of the likely enemy - dynamic objects and others. An operator with PM 4 monitors the state of the entire computing complex, issuing sound and light signals in the event of an emergency.

Flight management is carried out by the flight manager from his PM 15. He also manages the movement of aircraft in the near and far zones, generates the flows of aircraft approaching the landing, and controls the movement in the landing zone. The flight manager exercises the skills of interaction with the flight crews of the ground control service, for example, a combat control group. Analysis of the air and meteorological conditions is carried out on RM 15 flight manager.

The servers 10 of the individual flight simulators 11 determine the position of each aircraft in space (coordinates and flight altitude) and transmit this information to the individual servers 10 of the other flight simulators 11, the instructor server 12 and the control ground service server 14.

At the stage of practical development of educational processes, the information necessary for the student is issued to the individual CB computing module of each RM.

RM pilots equipped with flight simulators 11 allow testing of equipment and fittings of cabin 56 before flight, preparation for launch, launch and engine control on the ground and in flight.

Depending on the flight mission, pilots taxi, take off, climb, all types of flights, perform aerobatics. Improving the skills of individual aircraft navigation and in the flight group, pre-landing descent, approach visually and using radio engineering and navigation aids, the use of special equipment.

The functioning of the integrated training system is illustrated by the example of the occurrence of control actions when the pilot rejects in the cockpit 56 of one of the individual simulators 11 of the aircraft control stick RUS, which is a continuous control 51 (see Fig. 8). The displacement sensor along the pitch or roll 53 registers the movement of the RUS 51. Next, the signal in electrical form enters the controller system 54, where it is converted into a control signal for the VC computing complex. In this form, the signal enters the input of the server 10 of the individual simulator 11. In the server 10, the signal enters the modeling and control unit of the dynamic model of the aircraft 64. Block 64, solving the equation of motion of a specific aircraft, outputs the parameters of the newly established movement of the aircraft, in this example change in flight altitude, in the form of control signals to the computing modules of the local computing system 30 or other servers 10, which convert these signals, depending on the algorithm embedded in them, into control signals for use tional devices.

Computing modules VM 27, 28, 29 provide a control signal to the on-board visualization system BSV 41, 42, 43, and accordingly, the signal changes the display of the cockpit space.

The dynamic platform control unit LA 65 of the server 10 provides a control signal to the controller system 54, which controls the electric motors 62, 63. When the motor shaft 62, 63 is rotated by a predetermined angle, the cable wires of the drives 62, 63 are tensioned and the dynamic platform 22 is rotated with the cabin 56 , respectively, in pitch or roll.

The same signal from the server 10 of the individual simulator 11 is issued to the server of the instructor 12, in the case when the server 10 of this simulator 11 is connected to the server of the instructor 12. In this case, the control signal from the server 12 is supplied to the VM 32, 33, 34, which the turn gives control signals to the on-board visualization system BSV 44, 45, 46. BM 35 generates control signals for the display system of the monitoring devices. The control signal supplied to the drive RUS 52 of the instructor simulator 13 moves the instructor RUS 52 by an amount equal to the deviation of the RUS 51 of the trained pilot.

From the server 10 of the individual simulator 11, the signal is sent to the central server 1, where block 23 solves navigation problems, for example, determining the location of an aircraft in space at the current time (aircraft coordinates: geographical latitude, longitude, and flight altitude). Navigation information in the form of control signals is fed to the input of the server 14.

From the server 14 of the control ground service, information is supplied to the corresponding computing modules VM 37, 38, 39, which receive, process and issue control signals to the flight manager 47, 48, 49 PM, ground control group, and landing zone manager.

From the central server 1 through the VM, in which the information is processed and issued for analysis in a form convenient for presentation to the RM inspector 18, it is sent to monitor the actions of all participants in the training (training).

Between the servers of the instructor 12 and the trained pilots 10, information is transmitted in both directions as follows (Fig. 9).

The signal about the position of the OS 51 in the cockpit of the trained pilot through the server 10 and the central server 1 is supplied to the server of the instructor 12. The server 12 provides control signals to the loading mechanism of the OS 88, which operates in two modes.

The first is that upon receipt of a command from the pilot’s server 10 of the pilot 11, the OS loading mechanism 88 is an actuator that, by means of electric drives 89, 90 and cable wiring 91, moves the OS 52 in the instructor’s cockpit 92 simultaneously moving the OS in the cockpit 56 of the trained pilot (Fig. 10).

The second - when the op-amp 52 is rejected by the instructor, the loading mechanism 88 loads these op-amps according to the algorithm embedded in the corresponding VK unit and the corresponding loading of the controls of the real aircraft.

The signals about the position of the OS 51 in the cockpit of a trained pilot, being transformed in the VMZO into signals providing the operation of instrument simulators and engine noise simulators through servers 10, individual flight simulators 11, central server 1 and instructor server 12 are sent to VM 32, 33, 34 , 35 and are issued from them in the form of control signals to the visualization of the cockpit space, an engine noise simulator, instruments and controls of the instructor's cabin.

The following signals can be sent from the server 12 PM 13 instructor to the server 10 of the pilot.

The signal from the selection switch of the cabin 93 of the controlled pilot through the server 1 is sent to the server 10 of the individual simulator 11, where the selected individual server 10 of the required cabin 56 is connected to the instructor server 12. Further, all signals to the instructor server are received only from this server 10 until the moment of a new switch .

The signal about the entry of the training failure comes from the console 69 of the input of training failures through the server 12, server 1 to the corresponding server 10, then through VM 30 to the instruments and fittings of the cabin 56 of the trained pilot.

The signals about the position of the OS 52 in the instructor’s cabin 92 are received through the server 12, to the server 1 and then to the corresponding server 10 of the individual simulator 11. The server 10 issues control signals to the loading mechanism 88 of the OS 51, which moves the electric drives 89, 90 and the cable wiring 91 OS 51 in the cockpit of a trained pilot synchronously moving OS 52 in the cockpit of the instructor 92.

The final stage of the training is carried out in the class of flight debriefing and analysis of objective control 19, the visualization system 20 of which is connected in series with the central server 1, the storage device of which contains a block for modeling real processes 23 and a block for objective control of students 25. In this case, parameters, for example, the position of the aircraft at a particular point in time for conducting OK and other parameters for the implementation of training flights, diagrams, diagrams, trajectories of the aircraft, etc., necessary for conducting Zbor flights are reproduced on NE 20 class or printed in paper form on the printer 21.

A prototype of the proposed device of an integrated training system for aviation specialists is made up of flight simulators with a dynamic platform that provides angular movement of the cabin from -45 degrees. up to +45 degrees. in pitch and roll.

To accommodate an integrated training system with four RM pilots and an RM ground control service, a room of 230 square meters is required. and a height of 4 m. The power consumption of the complex is 65 kW, the power source is a 3-phase current of 380V, 50Hz.

The proposed device of an integrated training system for aviation specialists allows training with a different combination of RM nomenclature and the number of trainees.

The tests showed that the presence of an integrated training system as part of the aviation unit can significantly increase the level of training of the flight crew and the ground services interacting with it.

Literature

/ 1 / Patent RU 2087037, G 09 B 9/08, dated June 28, 94, op. bull. No. 25 dated 08/10/97.

/ 2 / Utility model RU No. 10479, G 09 B 9/08, dated 08/14/98, op. bull. No. 7, 07/16/99 - prototype.

Claims (5)

1. A comprehensive training system for aviation professionals, containing workplaces of the ground control service, one or more workplaces of trained pilots equipped with individual simulators in real cockpits of aircraft installed on dynamic platforms with the ability to move by electric drives in 2-3 planes equipped control instruments and discrete controls, valves and continuous controls with electric loading drives connected by contact devices with computing modules of the corresponding local network of workplaces in one virtual event field and outputting information to visualization devices, characterized in that the integrated training system is supplemented by a computing complex equipped with a central server with a storage device including an array of source data bases, a block for modeling real processes with simulation devices and an objective control unit for students, parallel connected with input-output devices with functional orientation localized servers of local networks: workplaces for trained pilots, workplaces of the ground control service, for example, the workplace of the flight manager, the workplace of the head of the landing zone, the workplace of the ground control group and the workplace of the instructor, as well as the local network of the workplace of the inspector a server of a local network of workplaces for pilots, comprising a block for modeling and control of a dynamic model of an aircraft, a control unit for a dynamic platform, a radio control unit , in parallel, is connected by an information input / output device to the computing modules of the on-board visualization system of the cockpit space, the computing module of the instrument display system, control of the cabin fittings and engine noise simulators and the armament control computer module, and the dynamic platform electric drives and continuous control loading actuators, kinematically connected via cable wiring respectively to the dynamic platform and controls continuous operations, remotely connected by displacement sensors, each of which is connected in series through the controller system to the computing modules of the corresponding local workstation network, the instructor server, which contains the modeling and control unit for the dynamic model of the aircraft and the radio control unit, is installed with the possibility of parallel connection through the central a server with one of the servers of the pilot’s workplaces and with computing modules for the on-board visualization system cabin space, a computing module for displaying devices, controlling the cabin fittings and simulating engine noise, a computing module for the weapon control system, while the instructor’s workstation is equipped with an individual simulator in a real cockpit of the aircraft, and the controls are supplemented by a training failure input panel, a ground control service server comprising a radio communication control unit and an aerodrome lighting control unit, connected in parallel with computing modules of the short-range radio engineering system, the ground control group control system, the radio-electronic landing and weather control system, and the central server is connected in series with the visualization system and a printing device of the class of flight debriefing and analysis of objective control tools and is equipped with an operator workstation with an individual visualization device. 2. The comprehensive training system according to claim 1, characterized in that the discrete controls at the pilots' workplaces and the instructor's workplace are installed on the instrument panels, some of which are made in the form of a screen with holes around the perimeter of the instruments and indicators, located in front of the monitors of the instrument display system and control cabin fittings. 3. The comprehensive training system according to claim 1 or 2, characterized in that the flight director’s workstation is equipped on an individual simulator with a long-range radar indicator, an indicator of a short-range navigation system, a command radio communication system, and an aerodrome lighting control system. 4. The comprehensive training system according to claim 3, characterized in that the workplace of the head of the landing zone is mounted on an individual simulator and equipped with indicators of the radar landing system, a command radio communication system, an aerodrome lighting control system, and a weather information display system. 5. The comprehensive training system according to claim 1, characterized in that the workplace of the ground control group is made in the form of a simulator equipped with long-range radar indicators and command radio communications.

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