RU29901U1 - Group flight training complex - Google Patents

Description

2002134276

eleven

MILITARY TRAINING VOMPLZHS GREGVOGO TRAINING

B64 F 7/00 oleznaya-yedoyo- ® refers to the field of aviation technology, in particular, to Equipment and devices for training and training of flight crews, leveling of flight crews (F) of flying machines (M) in all areas of the PRAYING YES., INCLUDING yo dch} shn m5 There are known l-flight-airborne complexes (LS), representing the codot compatibility of ground-based airborne facilities providing research and development of aircraft using semi-natural and mathematical modeling methods. The following fixed assets are part of the DMK: an experienced aircraft or a specially equipped flying laboratory; means for collecting onboard and external trajectory measurements; Computers of preliminary processing and express analysis of information; real-time computing systems; means of data transmission on the land-board and borf-emdn lines (radio telemetry channel, radio command line, radio communication equipment, television channel); Means of accompanying semi-natural modeling. . On the ground, the LS shone are provided with radiometric information received from the aircraft and from means of external measurements. External trajectory information is generated using radar tools. Li i-I (I is performed when direct information links are established between the computer and other systems, which are part of the cochlex. Information processing computer performs the functions of translating the parameters transmitted via the external trajectory channel into physical values, sorting and displaying these parameters with the necessary the speed of information transmission and processing, Semi-scale modeling tools are used to develop on-board systems, develop flight experiment techniques, and train flight personnel. Allows you to conduct certification flight tests, training and training of flight personnel with the condition of overload tolerance when the flight load is about 1 hour. The closest analogue is the well-known complex of means for monitoring and controlling the flight experiment, which includes means for external trajectory and radio station measurements, satellite communications and navigation systems 2. EMpleks equipped with laboratory aircraft with measuring, communication and information processing with a command post, system the theme of managing the summer experiment. In addition, the complex is equipped with a ground command post with communication facilities, a flight test processing center and uses an equipped runway with flight support facilities for laboratory laboratories, an air traffic control system with a control panel, a fixed and PO system. ) measuring points. Such an AE-T complex does not provide KG training for training flight personnel under the conditions of bo $ u, liiHOU riocA j KiU, orbit 1 Sordkl ON CA / IOLET -NoCUTtiAb. .. The task of developing a utility model is to create a flight model., W of the crews to the HALL-HOUSE GO prL & leIlL prL. 4s ORBYTALIOGO KRABLE AND A PLANE-BEAR TPL, LTK is intended for training flight crews, providing scientific research, carrying out zero-moon airborne gear (BO) (avionics), modeling of airborne, TUSADGI bPEITA bIogo KGo (5 DBA91 ON S / AMOAeT-H eS1D TEL. TAICOC MODULATED and TRAILING AoA: e4сн- Cut in the conditions of acceleration of biological loads, as close as possible evaluation of the pilot’s performance under high congestion conditions. ITK POM0Sh0T to instill in the pilot the correct behavioral and orientational skills when exposed to accelerating sensations, provides regular training. The task is achieved in that in the flight training complex, including means for external trajectory and radio telemetry measurements, external trajectory measurements (VTI), radio engineering systems (RTS), landing radar complex (PRZ), short-range navigation system (RSBN), instru mental landing system, DKI (ILS), microwave landing system (MNO), television landing system, satellite navigation system (ONO), carrier aircraft, air traffic control system with control center, control panel for communications, satellite communications system (SOS) , a connected flight experiment control system (SUDE), EM modeling of the dynamics of the V03.11 EAR ship, navigation aids, equipped runway with flight aids, ANDLOGO ORDER, communications, information processing and display, a computer processing center, flight test results from a computer to determine the results of eruptions, a ground-based complex of centrifuge equipment has been introduced with its own computer for processing measurement results, consisting of the actual mechanism 1; an electric drive with cabs and drives ; governing bodies (in a cabin with) and control of an overload; simulators of visual orientation of the pilot; life support systems; equipment of me, tsitsinsky control; connected to the control panel of the centrifuge, which in turn is connected to the control panel of the instructor of the SUD, connected to a single local subsystem 5-1 Yri, the central computer for processing the results of flight tests of the computer center is connected to the mini-computer for processing the results of measurements of ground-based facilities in the local computer network. The creation of such a complex provides the following technical and economic advantages. The complex uses information tools and training systems, combined into a single automated system, to obtain integral estimates due to the application of i-th methods based on calculation, modeling and flight tests. The structure of the CERO5LU1S1NLG classification C) and on-board equipment (BO) using the complex allows to achieve significantly the degree of completion of the training cycle and training the flight crew, reduce their volume and terms, reduce the complexity and costs of flight tests (G). Indeed, trainings and a trainer for the flight crew, conducted with the help of this complex a, are adequate to the requirements for professionally skilled pilots. Trainings conducted with the help of this complex help minimize unproductive time and material costs, losses from factors of adverse weather conditions, time of year and day during flights in different regions of the globe. Attention. The invention is illustrated in FIG. I, in which the pinch block is a schematic diagram of the proposed test a, and FIG. 2 is a block diagram of a complex centrifuge complex. The figure I shows: -COSIGEDIU I Airplane - M with the flight-navigation complex installed on it. 2. Communication satellites that are part of the satellite communications system (CCG). 3.Satellites of the navigation system (SNA). 4. Pseudosatellite. 5. Control and correction station (KKS) SNA. 6. The satellite navigation system of external trajectory measurements (VTI). 7. A measuring instrument of exact time. 8. ESh modeling, processing and analysis of the results. 9. The next communication node. JHfA AEHiAa 10.System of airborne traction. (ATC). 11. The control panel of the air traffic control system. 12. Computer processing the test results. 13. A complex of centrifuge equipment. 14.Pilot visual orientation simulator. 15. Life support system. 16. Medical control equipment. 17. Computer simulation and processing of experimental results. 18. The control panel of the centrifuge complex. 19. Centrifuge mechanisms with cab and power drives. 20. Controls installed in the cab and overload control.

23. The control point of the summer experiment (PULE) with a control panel and an instructor display,

24. Computer simulation. Flight flight test engineer engineer.

25. Computer simulation and processing of test results.

26. A computer for collecting information and processing information from a computer center.

27. The system of external tractor measurements (VTI) - optoelectronic system Opal.

28. MS system (course-glide path beacons).

29.System of meteorological service and meteorological sounding.

30. The system of lighting equipment of the airfield.

31. Landing radar complex (PRZ).

32. MIC microwave system.

33. The runway (VSH1) of the aerodrome.

34. Computer processing the test results of radio equipment.

35. Television Landing System (STP).

36. Short-range navigation system (ROBN).

37. Aircraft --An A log ORBIT

38. PMAOAGAZHIO-Nayigam, South KOMHAEIC I (flHlcJ dnAlogd-Kor dya

39.System of air signals (SHS).

40. Radio receiver of the long-range navigation system (RSDN).

41. Radio receiver system MS.

42. Automatic control system (ACS).

43. On-board computer.

44. A radio receiver of a short-range navigation system (RSBN).

45. Remote control with display screen, with a system for recording measurements.

.47. Inertial Navigation System (ANN).

48. Radio receiver for communication of data transferring (LS),

49. Radio transponder.

50. RTS funds complex.

In FIG. 2 shows 51-power centrifuge drives, 52-power beams, 53-54 - pilots' cabins (capsules) installed in cardan (for group training) suspensions 55 and 56.

57.58 - counterweights.

59.60 - cable mechanisms.

61.62 - hydraulic drive cabs.

On Earth, a control and correction station (KKS) - 5 with Alpdrd) swarm pseudo-satellite .; 4, which are part of CHG, are connected with navigation satellites -3 and airborne receiver -46 installed on M-I. KKS-5 is connected with the VTI-ONS-6 block of external trajectory measurements, as well as with the exact time meter -7, and a mini-computer - 8 processing and analysis of measurement results, the input of which is in its own eye. For VTI-ONS-6, and the output is from a computer-26 computing center, a personal computer-34 data processing radio engineering landing equipment. In addition, the exact time meter -7 is connected to a ground communication center (NS) -9, a visual orientation simulator 14, medical control equipment 16, a control centimeter / cm / 18 centrifuge, an external trajectory measurement system 27, and RTS 50 equipment, ПУ1Э-23.

The ground communication node of the satellite communication system (CCC) -2 is radio-technically connected to the airborne 1/1 connected receiver 48 via a data line (LCD) with a centrifuge control panel 18, with an ATC-10 control system connected to an ATC-11 control panel, and minicomputer - 12 processing results F, connected to a computer -26 computing center and computer-34 data processing RTS-50. C NUO-9 is connected to the receiver L1SCH-48 LA-1, with a control panel 11ULE-23, with the UVD-10 system; controls for 20 aircraft and overload control are installed in the cab-21 equipment complex, which also includes visual orientation simulators 14, a life support system 15, and medical control equipment 16. All of these subsystems are connected to computer-17 modeling and testing of experimental results. The complex of equipped centrifuge 13 contains a control panel 18 connected to the centrifuge mechanisms 19 with a cabin 21 and power drives in the cabins, where control and overload controls 20 are installed with an electric loading system of controls, a visual orientation pilot 14, life support system 15, medical equipment control 16, computer-17 modeling and processing of test results, connected to block5I 14.15D6. Control panel: I -23 PULE-22 are connected to the VTY-27 system radio-technically - through the control panel, a centrifuge 18 and BUS-9, with a data transmission line (ZhC) - 48 on the LA-16, with a weather monitoring system -29, with: RVM; simulation -24 data of the aircraft, and then with the computer -25 modeling and processing of test results, which in turn is connected to the computer -26 of the computing center and the RTS-50 system, which includes PRLK -31, television landing system (STP) - 35, RSBN -36, ZhS-32 system, ILS-28 system. The VTI Opal system is optically coupled to BC-I. On board the BG-I, which includes the GHG -46 receiver, the INS -47, ZhD -48 inertial navigation system, the ROBE -44 receiver, the CBG -39 air signal system, the RODI -49 receiver, the MO -41 receiver, automatic control system (SAU) -42 and a remote control with a display with a registration system of ivemerii -45 are connected to the on-board computer -43, SVS -39 MI pa, 1 is technically connected to the RT -50 of the earth.

The orbital GHG-3 in conjunction with the ground -4.5.6 and on-board equipment -46 sets the location of M1.57 in a given coordinate system. As a reference radionavigation reference point with a known coordinate w at the moment time-i is used for, given in time and space with a certain accuracy, the satellite trajectory. The satellite trajectory -3 in time is given by periodically updated ephemeris (calculated values of c) in a single time system, and their values are entered into the storage device of the satellites, which are transmitted together with the signal W: exact time.

sleep -3,4,5 and BTI-SNS-6 continuously determine the location and velocity vector of the aircraft LA-I on the earth's surface and in the surface space by the pseudo rangefinding method. When measuring navigation parameters (pseudoranges and radial pseudoranges) in four directions, on four satellites, navigation satellites, measured; of satellite orbital parsethers, the on-board cabin of time being spent with respect to system time, the coordinates and the velocity vector of the aircraft -I are calculated. At the same time, the time is also linked to the system sleep scale, carried out in the exact time meter - 7, i.e. the signal received from the -3 satellite is compared with the signal of the local time frequency standard. The equation of the navigation parameter has the form:

D-L (-. F- ().)).

where DC L 7 is the systematic measurement error, is the discrepancy between the time standards for LA -I and satellite. nike sleep -3, G is the propagation velocity of the radio waves.

Yrzhvyazka to a common time of the actual values of the parameters measured in the VTI-SNS-6, is carried out in the exact time meter -7. The input generator block -7 includes a reference generator, a synchronization device, and a current-time counter binding, a device for forgating synchronization signals, marks and current time codes, and an output pairing device. The information from block -7 is sent to NUS-9, to the air traffic control system -10, to PU13 -22, to visual orientation simulator 14, medical control equipment 16 and RTS -50. Testing using NUS-9 airborne communication systems, in which LGSH 9 ... 48 was introduced, has its own characteristics. If telephone channels were evaluated by the articulation team, then the digital channels of the SD are evaluated instrumentally, with THIS the parameters of the digital channels are set to probable value l1. In the LI process, a test is transmitted in real time from the BUS-9, the information is transmitted, the airborne complex receives it and relayes it to the NS-9. On the ground, the received test signal is compared with the transmitted one and the reliability of the test signal is evaluated. The operation of the ground-based NUS-9 is controlled by a computer -12 connected with the ATC-10, which forges the test of the signal for transmission, compares the received message with the transmitted one, estimates its quality, computes the reliability of message reception, compares it with the normative value.yash1 and registers the result. Shni-computer -12 is connected to computer -26 of the data processing center. In real time, the estimation of the LC 9 ... 48 takes place with the correction of the flight experiment when there is a need to change its parameters, which increases the efficiency of the satellite. The satellite communication system (CCC) -2, in addition to the satellite orbital system, includes the LCD-48 transceiver station , which is part of the NUS -9. : j

There are real data bases (DBs) about existing and forecast levels of demand and throughput. The databases use models that accurately predict channel congestion and time. The on-board system interacts with the equipment for organizing the flow of traffic, forming trajectories that fully meet the needs of the user and the conditions of limiting the throughput of the system. Better connectivity to ME5UO is provided by ATC and flow management services.

The automatic machine from the ATC ATC allows you to reconcile the actions of the earth and BG in order to improve tactical management. When the user considers it necessary to make changes to the flight plan, between the onboard flight control system and the ground tactical control system using the 9 ... 48 LPS, a new flight path is coordinated that meets the user's goals: -

; . Similarly, changes are made to the flight plan by the tactical command (land). These reconciliation processes include dialogue between the pilot and the air traffic controller. This air traffic control system -13 helps to increase the capacity of aerodromes, eliminates conflict situations when landing approaches at neighboring airports, and ensures the independent functioning of every airport.

Using the ATC-13 test center:

-created a single continuum of airspace with transparency for the user border1 ®;

- introduced with the help of bj. The air-to-ground debug when discussing a flight plan;

- flight safety is increased, delays are reduced, and the throughput capacity of airspace and airports is increased; : .- t-flexible routing is carried out, and -cenital adjustment of the air routes in accordance with the changing weather and conditions of heavy traffic; - the perfect organization of flights eliminates excessive levels of overload / congestion, reduces the workload of dispatchers. The ATC-10 system with a remote control - screen -I, which, in turn, is connected to the Misht-computer -17 of processing the results of experiments associated with the computer -26 of the information processing center. Centrifuge 19 is a ground-based installation that simulates real-life accelerations and is used for training pilots and astronauts, as well as for testing various airborne aircraft equipment, Centrifuge-19 is a stand, figure 2, on which 52.53 (group training) is located in the cockpit person (and equipment). The powerful engines of §1, which rotate the centrifuge 19, make it possible to create centripetal accelerations. Depending on the position of the human body, acceleration affects him in various directions. The centrifuge 19 is equipped with measuring equipment 16, the devices are in negotiation, the LA1 control tool, 20. The centrifuge 19 is used to train the vestibular apparatus, record biopotentials and other important physiological indicators of a person (blood pressure, saturation of the inhaled and exhaled air; carbon dioxide by gas and oxygen), evaluated in the apparatus control. Overload is a critical flight factor that has a certain effect on the human body. Long overloads arise in maneuverable flight - pilot overloads (1Sh). SHT is characterized by direction, duration and repeatability of action. The direction is opposite to the directional acceleration vector to negative. In flight, longitudinal overloads along the head - pelvis are most often encountered. Overloads are distinguished in the direction ibQbgjs4m E of the relative main axis of the person: longer, transverse, lateral W. The action of W is subjectively perceived as an increase in body weight and is accompanied by a more difficult sensation of movement and movement of the extremities, and there is visual impairment (gray: and black shroud) , sometimes there are unpleasant and even pain. Exposure to Ш is characterized by increased hydrostatic blood pressure and heterogeneous deformation of various organs, which leads to increased, 1y displacement of blood into the lower half of the body and especially to the vessels of the abdominal cavity, to a decrease in blood flow and its; oxygen enrichment in the lungs, reduction of blood flow in the vessels of the brain and eyeball, increased excitability of the central nervous system. These pairs of meters are recorded in 16 mecidin control equipment, the anti-overload suit and oxygen equipment are included in the equipment 15, For conducting air HOti: according to:: dd 1s1D - - two cabins are installed on the centrifuge 13 - capsules 54 and 55 in 2-degree gimbal suspensions. Cardan suspensions provide 1 "staff of angles of tar1ga; ka and roll, cabins are located one above the other on two parallel beams. Change of the overload vector from half-solid to the negative day of each cab is carried out by moving it along the guide mounted on the beams 52. Moving them is accompanied by a change in the position of the balances 52 and 57, which are driven by a system of cables 59 and 60, and moveable by electrohydraulic drives 61.62, The effect of Coriolis accelerations on pilots i MneHewpu, TGYA Turning the cabbage most of the work Most of the centrifuge axis is located and only at high loads are transferred to the edge of the beam, Transient processes are unavoidable LA ki are provided by varying the speed of beams and peremescheshem them cabins capsules with the pilots. Each cabin is a centrifuge capsule that contains: At the moment of touching, controls are (aircraft and engine control knob (RCD, ORE), with trim mechanism and electromechanical loading system; - instrument panel; - multi-function displays; - windshield indicator (s) ); - remote controls, controls;. target designation system (. Щ); - pilot seat. Extra-cabin conditions are provided by projectors that provide the image directly on the screen - capsule shell; the pilot field is 60 horizontally and 40 ° vertically, The cockpit (capsule) of pilots 53 and 54 contains the experimental VO cockpit, levers and controls, electrical sensors fixed to them, an information display system; when control bodies are deflected, the signals from the sensors go to the inputs of the ZVM. a self-contained computer simulation in a closed loop, reproducing the effect of the external environment, parameters and setpoints on instruments and controls, visualization devices relatively hollow: the formation of heaven and earth when performing maneuvers. In the cockpit are controls, steering wheel, pedals., Control knob, gas sector associated with mechanisms / loading, reproducing the magnitude and gradient of effort on the control levers. If you install electric sensors installed in all channels, you give voltages proportional to the deviations of the corresponding rudders. These signals are fed to a computer, which implements the equations of motion of the aircraft, characteristics and flight modes. The output voltage of the computer 2 and 25 reproduces the parameters of the angular

position visualizations BG 1, recording devices, information collection devices.

The unitation of the functioning of on-board systems using the technical means of a controlled flight experiment is due to the large amount of information entering the SUEL-22. Means of collecting and transmitting information SULZ-22 include:

airborne radio-telemetric systems by means of communication with LA-1;

ground external trajectory systems 9-18-23;

command information transmission lines aboard the LA-1;

external trajectory measurement systems coming from -27 optical devices and RTS -50 radio engineering systems associated with an accurate time meter;

 - accompanying simulation -24. Experimenters ’workstations - the control panel -23 of the SULE contains a display system in the form of a series of graphic and alphanumeric displays, means of documenting information, plotters, printing devices, means of transmitting control commands on board the LA-I, communication means with the interacting service 1a 9-13, which provides summer experiment, flight manager. A computer -25 modeling and processing of LI results is connected with a computer -26 for collecting information and a computer center. Graphic and alphanumeric displays allow you to observe on-screen the process of performing re.zhimov, to control the values of individual parameters. Displays allow you to display paA leggings as functions of two variables, which makes it possible to adjust the flight program, perform intensive maneuvers, etc. Issuing the display of the current flight parameters of the aircraft -I, assists operators in making emergency decisions at the pace of flight.

the determination of the flight path of the HE and the determination of the spatial orientation of its axes is resolved with the help of the kinoteod station station (CTO), when the range D, az11m is measured; rm A and elevation angle for coordinates of the center of mass of the airborne forces (X.jj determines the flight altitude

НпОА When using electron-optical systems (EOS) (OPM), laser reflectors are installed on BG, the probe-generating signal is generated by the laser in the form of a coherent radiation beam, to increase the directivity of its radiation, it is collided by the transmitting system. BG reflected radiation is collected

receiving optical system, passed through uvkbandnogo

interference optical filter to reduce background illumination

and converted to photosensitive. element in an electrical signal. The amplified signals from the input terminal of the receiving unit enter the mining unit, into which the reference signal is also supplied. The received and reference signal allows the I3x to lose the range of the propagation time of the signal to VO and vice versa. In the VTI-27 calculator, the angular and linear coordinates of VO -I are simultaneously measured. VTI tools based on CGS and EOS are used in assessing r v:: landing characteristics of navigation and navigation parameters. The external trajectory meter -27, which records the trajectories of take-off and landing, of the aircraft deck, is connected to the console; tons of PULZ -23 and further in the computer -25.

Ground-based radio systegles -50 navigation and landing include PRLK -31, a television system. landing -35, instrumental landing system MS-28, microwave system.me landing MS, radio-technical system for navigation navigation RSVN -36.

The PRZ was assigned to control the landing approach by determining the coordinates of the I-I - elevation angle, course angle, incline range, as well as solving air traffic control tasks. The PRLK is built on the principle of the sub-channel tracking radar with conical scanning

beam of the antenna, which creates a radio signal zone in space. When the angular position of the VO-I changes, an error signal appears in space, which ensures automatic tracking of the antenna behind the VO. The basis of the creation is a radiol: the radiation printers of a radar station operating in the long wavelength range.

The parabolic mirror of an antenna forlags the given radiation pattern. The conical viewing mechanism causes the radiation pattern to rotate in space relative to the axis, as a result of which an equal-signal zone is formed. If the VO is on the equal-signal zone, then the reflected pulses will be of the same frequency; if not, then they will be promoted in amplitude. The modulation depth determines the degree of deviation from the equal-signal zone, and the phase shift relative to the reference voltage generator, with the frequency of which rotates the cone view, the angular direction is the mismatch of the antenna axis. The generation of signals of the existing mismatch proportional to the amplitude occurs in the tracking and angle measuring equipment, in the calculation body, the data are converted from the spherical coordinate system to the right angle, the deviation of the aircraft from the given path along the height H to the side deviation A2 is determined. , current range information 2

The system of television posadai (STP) -35 is a system for monitoring and measuring the trajectory, moving; 1st aircraft in the area of the aerodrome. OTP -35 allows video monitoring of the flight of the aircraft LA-I during take-off, landing, and flight over the airfield during taxiing along the runway with transmission and registration of the image on the VCR, measuring the position and trajectory of the JIA. STP -35 allows you to remotely provide; inspection of the aircraft at the WIN, observation of the runway in conditions of limited visibility, to control the external components of the aircraft on the take-off run (mileage) to decide on the continuation

takeoff and landing, which helps to improve flight safety.

STP -35 allows you to measure the position of the aircraft in the form of a dimensional figure, and not a single point, which is important when measuring at short ranges, when the linear -dimensions M significantly exceed the limiting measurement errors. In this case, it becomes necessary to register the position of the previously adopted reference point of the image at 1A,

STP-35 is built on the basis of a tube, for example, VIDRShON, which automatically measures the coordinates of VO at the same time, coinciding with the direction of personnel and horizontal scans. If the image is BG on er: the wound of the television receiver is offset by an amount of X in rV /.

risontal and - vertically, then at the focal length of the lens F the image shift by distance I means that the sun

shifted in the horizontal plane relative to the longitudinal axis of the transmitting tube by an angle, g X / F similarly in the vertical plane - on jTQJifJt tjfJ (- У /. Automatic measurement of the BG offset along the ХгУ axes allows the determination of the angles Л and iU relative to the axis of the television 1Ш1лера allows using the control device rotate the camera to keep the image in the field of view.The trigger scheme for measuring the video pulse in the horizontal and vertical axes is the measurement of coordinates

X, Y

The course-glide path beacons KRM and GRM of the MG instrument system use a double-amplitude pinch, simulation, and emit two types of signals. One of them is the promo carrier frequency signal, 11 is amplitude-tuned with a low frequency j. The directivity characteristic of this radiation is such that two lobes are formed, separated by the plane of the landing course., The modulating voltages in both lobes are in the off-line, and the coefficients of the modulation depth are the angular coordinate measured from the runway axis (for CRM). The phase of the modulating voltage of this radiation, when passing through the plane of the landing course, changes to 180, this is nsJjy eHHe of a variable phase. The second radiation is the same; the voltage of frequency m, in which the phase is constant, at any point in the current, is the radiation of Hiie of the constant phase and in phase with the modulating voltage of the signal of the variable phase in the one of the petals. , “The technical means of the meteorological slang and meteorological radar -29, and used in the interests of meteorological support for flights, include instruments, equipment and installations designed for measuring meteorological parajutes (elements near the ground and at heights for detecting dangerous phenomena weather), as well as for reception, (collection and transmission) of meteorological information. Basic 1. Yes, the requirements for the installation of devices and the placement of equipment is to ensure the continuity and accuracy of parameter measurements, information collection and transmission. System -29 includes a pulsed light height meter for lower cloud cover at any time of the year or day, the principle of operation of which is to measure the travel time of the light pulse from the transmitter to the lower edge of the reservoirs (similar to previous 7de1u); visibility recorder - based on the definition of the welt / area of attenuation of the luminous flux. measuring instrument for wind direction, tegherature and relative humidity B03.iiyxa, atmospheric pressure; JG instruments for determining atmospheric parameters at altitudes when a koi, shlex temperature - wind sounding of the atmosphere using a radiosonde or wind sounding using a radio pilot is carried out. In addition, the -29 system includes equipment for detecting dangerous weather phenomena, determining the location of foci of thunderstorms and rainfall, the horizontal and vertical length of these foci, as well as the direction and speed of their movement; for cloud exposure / measurement, measurements from the upper and lower boundaries, such as cloud & precipitation, us intensity, cloud water content, hazard rating

icing of aircraft by pulsed radar in the centimeter and millimeter 1/1 meter ranges; superlaw wave ra.d11olokats1№ monopulse automatic thunderstorm, thunderstorm cybelengator (PAG-1) to determine the direction (azimuth) of the source of electromagnetic radiation from thunderstorm lightning. Lighting equipment of airfield BShtipovoe. PIX OF ANODEG CARRIER AND ANALOGUE have

SOHAASOVANNCHK5 ..

Elements of the satellite’s orbit, which can be read with constant accuracy by the MFN.JL1 for 1-2 hours, are transmitted from the satellite with an interval to all consumers. In elementary orbit and airborne time, the Cartesian coordinates XSK of the satellite are shown for any predetermined (current). point in time. And already by the distance .it1 to three satellites located at the calcareous points of space, it is determined by the location of the nuclear weapon. Using the values of speed and range of up to three satellites, the aircraft’s ground speed vector and flight altitude are calculated.

The signal, satellites are emitted in two frequency ranges for consumers with authorized access (increased measurement accuracy) and available for any consumer. To increase the accuracy characteristics, a differential method of determining the location coordinates is used, the essence of which is to identify and take into account, as corrections, the highly correlated error components of napaivieTpOB navigation using ground control correction stations TZhS -5. On IxKG -5, the coordinates are determined using the consumer equipment and compared with the geodetic reference data. Then the corresponding consumer is calculated by the ITO of the given area, which allows them, by introducing amendments, to increase the accuracy of the navigation definition.

ANN -47 platform or strapdown type. . provides the calculation of the coordinates of the location M and flight altitude by integrating the measured accelerometer accelerations. Setting the inertial system & w for 01ooler period (84.4 min)

provides construction of an irreplaceable accelerated vertical rail in

flying

The Be platform platform system (B11NS) provides for the determination and delivery to the consumer of M after using 2 parsletters: geographical coordinates, directional speed and components of ground speed., Angular positions of aircraft, angular speeds accelerating, vertical speed and altitude,

BSHS -47, in comparison with the platform, provides for the determination of a large number of JIA paratrograms, is built on the basis of laser gyroscopes, provides their higher reliability and low time of the emergency pump.

RSBN -36-And P1zhemnik -44 measures the pr / linear distance 02. and the aj-zut A of the beacon on the aircraft. For this NW / flying onboard

the transmitter emits pulses that are re-emitted by a terrestrial beacon. By BpeMem-joiviy prom. / s Meddu measured / g and accepted

the pulse is determined by the distance T) 0.5, where O is the propagation velocity of the radio waves. To measure the angle / 4g, the antenna of the beacon has a narrow diagonal of the directional direction, which can be imagined as a half-plane passing through the local vertical for the lighthouse and rotating around this vertical at a constant and known speed. The omnidirectional antenna of this half-plane of the plane of Meri, Diana (in its Northern direction) emits a signal that is received on M. The second signal is received on board when the aircraft. falls into the plane of the radiation pattern. By temporarily 1L5 interval 7 between the two impulses E1 mosho judge about avi1 / 3tv A g. RSBN gives a signal D range; spans in real: navigation swing: T) NA-. ,, D

RSDN-40 provides the measurement of two differences Dg and Dg

vjp

J, rch information in this library are the time delays TI2 and TI3 of the arrival of the LA pulses from the main station and the slave radio stations. Be, a foolish radio station emits an impulse received on an aircraft and on a Kaada from the slave radio stations. CHILD -40 generates signals of geographical coordinates of latitude and longitude LCD -48 - the digital signal transmission line 5 is connected to the radio transponder. SAIOLETA-I 5E1LTBLA PRI In the I1C-41 system of the instrument approach, the course and glide deviations of the ON -I zones of r and the deviations of the KZFS at the time of the flight of the far and near driving radio stations are determined, including: lonography from the approach trajectory, as well as n T Sihfr d D OBO -39 gives a signal of relative height: mn, absolute height M (4, number M. Formation of reference values for the navigation and aerobatic parameters of the aircraft (location coordinates, components of speed, altitude, course, track angle, angle, drift, etc. ) is carried out by distortion Of the intrinsic signals of ANN -47, estimates of their errors are obtained: using the Kalgan filter, when using the IT data -3 ... 46 as redundant information, information is controlled and restored at a resistance level of up to 50, and they are synchronized. the reference values of the navigation parameters and the forecast mode, in the absence of sleep information -46, a dynamic cascade of dynamic smoothing of estimates is used (due to the processing of information in easy and reverse time) to increase accuracy and form / g Set reference values at all stages of flight.

graphic display on the display panel -45 results processing, as well as the issuance of the results processing for printing PI plotter. GAU PLANE-A nl LOGA rdeotutzet Vreet | : IME fto ASUiHOro ZACKOLD GL POMDKGI,

SPG -42 HAS T1LPOV NE CTpvjKTSpA jpAsbTAET ALSO YEZhME.

The registration system, implemented on the -45 remote control, is designed to accumulate information about the results of express processing of irtformady at the pace of an experiment with a subsequent post-long-term express analysis and a BTsVM -43 LA-I, taking into account a large circle of tasks and various Requirement depending on the stages of the flight and the composition of the measured parameters, their accuracy and polling frequencies. The information on the VO test systems is secured on magnetic carriers and in databases (DB) based on magnetic recording equipment for recording digital streams from multiplexed CMM channels. The equipment contains a program for receiving, converting, selecting parameters, thinning, as well as measuring transducers, input / output devices, control and interface cards, a magnetic recorder, a tape recorder, and a magnetic disk. Communication with the tested on-board equipment and electrical coordination of the control of the signal carrier and digitalization of the signals of the sensors of the on-board systems is carried out according to the ARlbJC -429 standard. (training and education of flight personnel). A continuous cycle of work on the assessment of onboard equipment includes technical means and related work that must be performed with a strict technical approach to their organization and conduct. Theme: under and under the model, bench work is carried out in the same real: th time when conducting J.

The conformity assessment of training and learning characteristics, as required by normative documentation, is carried out according to the accuracy characteristics of the systems; according to the accuracy characteristics of aircraft navigation; by the quality of automatic control; by meteorological parameters landing; on fail-safety; ergonoshke (usability, installation, indication, loading); by assessing the impact of external influences on the pilot's work (heat, vibration, food not in U 8, electrostatics); software program for providing digital BO systems; according to meteorological support; for operational manufacturability.

Complex Ж is an automated system in which part of operations, in particular measurements, are performed automatically, and a person takes part in the execution of others. VO, M -I, the test object, is not present in an environment that exerts agitating agents on it. exposure. In the process of trashing, estimates of the operator of the object are found, i.e. complex of its characteristics.

To measure the ISCOAX characteristics, which are the components of the operator, a measurement field is constructed, which is a list of measured parameters, based on which the characteristics of the aircraft are relaxed or indirectly determined. The sensors convert the measured physical parameters into electrical signals, which, using the means of collecting information, are in turn converted into a multidimensional signal, transmitted to the processing center -26, and after the transformations during processing, estimates of the measured physical quantities are obtained. Based on the results of the processing with the use of an identification apparatus, spectrally correlative and statistical processing, estimates of the characteristics of the flight crew and aircraft are determined and its correct functioning is evaluated.

Management training and multi-level training:

the described control of the program of the 1-million training session, carried out on the basis of processing the results of the experiment after it has been carried out: and in the FLIGHT TEMP.

Claims (1)

Flight training complex of group training, including means for external trajectory measurements and radio telemetry measurements, external trajectory measurement system (VTI), radio engineering equipment (RTS), landing radar system (PRLK), short-range navigation system (RSBN), instrumental landing system (ILS) , microwave landing system (MLS), television landing system (TSP), satellite navigation system (CHC), air traffic control system (ATC) with control center, control panel communications, satellite communications system (CCC), a coherent flight experiment control system (CLE) associated with an aircraft dynamics computer, navigation aids, an equipped runway with flight support facilities, a carrier aircraft with measuring instruments , navigation, communication and information display processing, a computer center for processing flight test results with a processor (computer) for processing measurement results, an analogue aircraft of an orbital ship, characterized in that it introduced a complex of centrifuge equipment, a system with its own mini-computers for processing measurement results, including the centrifuge mechanism itself with the cockpits of pilots and drives, controls (in the cabs) and overload control, visual orientation simulators, life support systems, medical control equipment, life support systems, connected with the control panel of the centrifuge, which, in turn, is connected with the remote control instructor SULE connected to a single local area network.