RU71012U1 - COMPLEX FOR TESTING A SHIP WEAPON CONTROL SYSTEM - Google Patents

Abstract

The utility model relates to integrated test systems, namely, systems for debugging and repairing a ship weapon control system in a factory environment. The objective of the utility model is to ensure high reliability and reliability of the results of a comprehensive verification of the ship’s weapon control system. To achieve the claimed technical result, in the complex for testing a ship’s weapon control system containing standard and imitation equipment, the standard equipment includes a remote control connected to a device for converting guidance signals from a rocket launcher (RPU) and to a device for converting guidance signals from individual guidance objects ( SPE), which are based on actuators of servo systems, the first and second data input devices in SPE, connected by without a signal switch with a SPE guidance signal conversion device, as well as a SPE firing circuit switching device connected to the handheld device, a SPE angular rotation data output device of the SPE and an analog signal reception and conversion device based on actuating mechanisms of tracking systems, the input of one of which is connected to the output of the device for issuing data of the angular turn of the PA OIN, and the inputs of the others are connected to the corresponding outputs of the analog signals of the complex simulators of external systems on which target designation data of underwater and surface targets and course and speed data of your ship are formed, the outputs of the analog signal reception and conversion device are connected to the first group of inputs of the analog signals of the remote control, the second group of inputs of the analog signals of which are connected to the outputs of the tracking actuators RPU guidance signal conversion device systems and SPE guidance signal conversion device, output of a complex simulator of external systems, on which the digital data of the angles of the side and keel pitching of his ship is generated, connected via a digital communication channel to the handheld device, the outputs of the RPU guidance signal conversion device, on which the signals of the horizontal and vertical pointing angles are formed, and the inputs to which the signals of the full horizontal and vertical guidance, taking into account the side and keel pitching of your ship, connected to the corresponding inputs and outputs of the gyroscopic system simulator

stabilization, and the outputs of the device for converting the guidance signals of the RPU according to the signals of the full angles of horizontal and vertical guidance are connected to the inputs of the simulator of the full guidance angles, which, like the simulator of the gyroscopic stabilization system, is made on the basis of rotating transformers with scales, while working out the passage of the control signals of the circuits firing, the corresponding outputs of the RPU guidance signal conversion device are connected to the RPU firing circuit simulator, and the corresponding outputs of the devices and the switching of the SPE firing circuits is connected to the simulator of the SPE firing circuits.

Description

The utility model relates to integrated test systems, namely, systems for debugging and repairing a ship weapon control system in a factory environment.

Known complexes of control and verification equipment [1, 2], designed to test in the factory the on-board systems of an unmanned aerial vehicle. Known devices contain standard equipment of the product under test, simulation equipment, a control panel, a switching device containing a control point switch, a command switch and a signal switch, as well as a control system control device, an electrical equipment control device, and a self-control device integrated into a local network with a control panel based on electronic computers.

Known systems cannot be used to test ship weapon control systems, as built taking into account the specifics of the tested product.

Closer in completeness of control coverage of the composite devices of the product analogues were not identified.

The objective of the utility model is to ensure high reliability and reliability of the results of a comprehensive verification of the ship’s weapon control system.

To achieve the claimed technical result, in the complex for testing a ship’s weapon control system containing standard and imitation equipment, the standard equipment includes a remote control connected to a device for converting guidance signals from a rocket launcher (RPU) and to a device for converting guidance signals from individual guidance objects ( SPE), which are based on actuators of servo systems, the first and second data input devices in SPE, connected by without a signal switch with a SPE guidance signal conversion device, as well as a SPE firing circuit switching device connected to the handheld device, a SPE angular rotation data output device of the SPE and an analog signal reception and conversion device based on actuating mechanisms of tracking systems, the input of one of which is connected to the output of the issuing device

data of the angular reversal of the PA OIN, and the inputs of the others are connected to the corresponding outputs of the analog signals of a complex simulator of external systems, on which target designation data of underwater and surface targets and course and speed data of your ship, the outputs of the device for receiving and converting analog signals are connected to the first group of analog inputs signals of the console device, the second group of inputs of analog signals of which are connected to the outputs of the actuators of the tracking systems of the device is converted the RPU guidance signals and the SPE guidance signal conversion device, the output of a complex simulator of external systems, on which the digital data of the angles of pitch and pitching of the ship is generated, is connected via a digital communication channel to the handheld device, the outputs of the RPU guidance signal conversion device, on which the signals are generated angles of horizontal and vertical guidance, and inputs to which signals of the full angles of horizontal and vertical guidance are received taking into account the side and keel pitching and your ship, connected to the corresponding inputs and outputs of the simulator of the gyroscopic stabilization system, and the outputs of the device for converting RPU guidance signals by signals of the full angles of horizontal and vertical guidance are connected to the inputs of the simulator of full guidance angles, which, like the simulator of the gyroscopic stabilization system, is based on rotating transformers with scales, while for developing the passage of control signals of the firing circuits, the corresponding outputs of the conversion device RPU guidance signals are connected to the RPU firing circuit simulator, and the corresponding outputs of the SPE firing circuit switching device are connected to the SPE firing circuit simulator.

The essence of the utility model is illustrated by drawings, on which are presented:

figure 1 - structural diagram of the complex,

figure 2 is a structural diagram of a remote control device,

figure 3 is a structural diagram of a device for converting guidance signals RPU,

figure 4 is a structural diagram of a device for converting guidance signals SPE and input devices to SPE,

5 is a structural diagram of a device for receiving and converting analog signals.

Figure 1 structural diagram of the repair shop are indicated:

1 - remote control,

2 - device conversion signal guidance missile launcher (RPU),

3 - a device for converting signals of individual guidance objects (SPE),

4 - signal switch

5, 6 - the first and second data input devices in the SPE,

7 - device switching circuits firing SPE

8 - data output device angular rotation of the launcher (PA) SPE,

9 - device for receiving and converting analog signals,

10 - a comprehensive simulator of external systems, made on the basis of a microprocessor module interfaced with a remote terminal and with peripheral devices of a centralized input-output of digital and analog signals,

11 - simulator of a gyroscopic stabilization system, made on the basis of rotating transformers with scales,

12 - simulator of the full guidance angles of the RPU in the vertical and horizontal planes (hereinafter referred to as the simulator of full guidance angles), based on rotating transformers with scales,

13, 14 - simulators of firing circuits RPU and PA OIN, respectively, made on the basis of relay circuits with indicators.

According to figure 1, the complex for testing a ship’s weapon control system (product) contains standard equipment designed to control the firing of bomb weapons from a rocket launcher and the firing of guided projectiles (objects of individual guidance) from a multi-tube launcher, and simulation equipment.

The remote control device 1, which is part of the standard equipment, is connected to a complex simulator 10 of external systems via a digital communication channel, through which the digital data of the angles “θ _K ” and “ψ _K ” of the side and keel pitching of his ship are transmitted with a parallel code.

In addition, at the outputs of the analog signals of the complex simulator 10, target designation data (distance “D _CPU ”, “D _TsN ” and heading angle “q _CPU ”, “q _TsN ” target of underwater and surface targets) are generated, in real equipment coming from ship’s sonar and radar stations, as well as data on the current speed

“V _S ” of their ship, in real equipment coming from the lag, and course data K _{S of} their ship, in real equipment, coming from the gyroscopic stabilization system.

The outputs of the indicated analog signals of the simulator 10, as well as the output of the device 8 for outputting data “A _f ” of the angular rotation of the SPE launcher, are connected to the corresponding inputs of the standard device for receiving and converting analog signals, which contains, as will be discussed below, a group of actuating mechanisms (IM) tracking systems (SS) that convert the input signals to voltages whose phase is shifted relative to the reference voltage by an angle proportional to the angle of rotation of the actuator shaft. The outputs of the device 9 by the signals "D _CPU ", "D _TsN ", "q _CPU ", "q _TsN ", "V _S ", "K _S ", "A _f " are connected to the corresponding inputs of the first group of inputs of the analog signals of the remote control one.

In addition, in standby mode at the corresponding outputs of device 9, the SPE guidance data is generated — the angle α of the SPD divergence in the salvo (signal “input α _RES ”), the target angle q _{bt of the} target side (signal “input q _btPEЗ ”), the angle ω of the guidance of the gyroscopic instrument SPE (signal “input ω _RES ”) and the distance D _{div of the} discrepancy between SPEs in the salvo (signal “input D _divРЭЗ ”), which are transmitted to the corresponding inputs of the standard device 3 for converting the SPE guidance signals. In addition, the device 9 in the main mode of operation receives from the remote control 1 the signal “N _SPE ” for inputting the depth of the SPE and transmits it to the corresponding input of the switch 4 signals, and in standby mode generates a signal “N _SPEED ” and transmits it to the switch four.

The outputs of the remote control device 1, on which in the form of control voltages the calculated data of the angles of vertical and horizontal guidance of the rocket launcher are generated (signals "input UVN", "input UGN") are connected to the corresponding inputs of the device 2 converting guidance signals RPU, the outputs of the remote control, which in the form of control voltages, the calculated data of the angle α of the divergence of the SPE in the salvo, the course angle q _{bt of the} side of the target, the angle ω of the guidance of the gyroscopic device of the SPE, the distance D _{div of the} divergence of the SPE in the volley are formed e (signals “input α”, “input q _bt ”, “input ω”, “input D _div ”) are connected to the corresponding inputs of the device 3 converting signal signals guidance SPE.

The outputs of device 2, on which the signals “BIF _UGN ”, “BIF _UVN ” of the actual angular position of the IM SS shafts are formed, and the outputs of device 3, on which

the signals "BIFα", "BIF _bt ", "BIFω", "BIFD _div " of the actual angular position of the shafts of the corresponding actuators are generated, connected to the second group of inputs of the analog signals of the remote control 1.

The outputs of the “UVN”, “UGN” signals generated by the IM SS of the RPU guidance signal conversion device 2 are connected to the inputs of the simulator 11 of the gyroscopic stabilization system, in which the values of the full pointing angles in the vertical and horizontal plane (“PUVN”, “PUGN”) are generated taking into account onboard and pitching. These signals are transmitted through the device 2 to the inputs of the simulator 12 full angles of guidance RPU.

The outputs of the IM SS device 3, on which control voltages are generated (signals “Ctrl n. Q _bt ”, “Ctrl n. Ω”, “Drive n. D _div ”), are connected through 4 signal switch with corresponding inputs of the first data input device 5 in the SPE, and the output of the signal "Ex. n N _SPE "connected through the switch 4 to the corresponding input of the second device 6 data input into SPE.

Data input devices 5, 6 are also based on actuators of servo systems, the control signals "α _K ", q _btK "," ω _K "," D _divK "of the actual position of the shafts of which are transmitted to the console 1 and displayed on the scales of the front panel .

The input of the discrete signals of the remote control device 1, to which the signals "Availability BO" of the presence of ammunition in the RPU is received, is connected to the corresponding output of the device 2 for converting the guidance signals of the RPU, and the inputs to which the signals "Availability of SPE" the presence of ammunition in the multi-tube launcher of the SPE, connected to the corresponding outputs of the device 7 switching firing circuits SPE.

The outputs of the remote control 1, on which discrete signals are generated "Ex. CA SPE "control the firing circuits SPE connected to the corresponding control inputs of the switch 4 signals, and the outputs on which the signals are formed" On. CA SPE "switching on the firing circuits of the corresponding SPEs are connected to the inputs of the firing circuit switching device 7, which in normal conditions commutes the executive power supply circuits to the electromagnets assigned to the volley of the SPV launcher tubes. In the proposed complex upon receipt of the control signal "On. TsS "voltage 27 direct current is supplied to

relay circuits simulating 14 SPE firing circuits, including corresponding indicators.

The outputs of the discrete signals of the remote control device 1, on which for the assigned RBU are formed in the form of a three-phase sequence of pulses data of the depth of immersion (fuse response) of bombs (Signal "N _BO "), as well as the command "On. CA BO "inclusion of the firing circuits, connected to the corresponding inputs of the device 2 conversion signal guidance RPU. The outputs of the signals generated in the device 2 upon receipt of the control signals "N _BO " and "On. CA BO ", connected to the simulator 13 firing circuits RPU, in which, through relay circuits, the corresponding indicators are turned on.

On Fig 2 structural diagrams of the remote control device 1 are indicated:

15 - a device for receiving and processing data from information sources,

16 is a device for generating firing data,

17 - display device and data input (remote terminal),

18 is a control device

19 is a digital input-output device (DAC),

20 - multi-channel digital tracking system (MCCS),

21 - two-input random access memory (RAM), implemented in the form of a module "Electronics C5-2205" connected to the unit for interfacing lines

22 - communication adapter,

VMP-1-1, VMP-1-2 - the first internal trunk of the device,

VMP-2-1, VMP-2-2 - the second internal trunk of the device,

23 - the first micro-computer (MEW), implemented in the form of a microprocessor module "Electronics C5-2200",

24 - the second MEM, implemented as a module of the microprocessor "Electronics C5-2200",

25 - block debugging programs

PZU-18 - read-only memory (ROM) of the control device, implemented as a module "Electronics S5-2213M2",

VIM-18 - the internal interface line of the control device 18,

IPC - serial line trunk,

26 - the third MEM, implemented as a module of the microprocessor "Electronics C5-2200",

CVV-26 - block registers CVV MEWM 26,

OZU-15 - RAM ("Electronics C5-2205") of the device 15,

PZU-15 - ROM ("Electronics S5-2213M2") device 15,

VIM-15 - internal interface highway device 15,

27 is a block conversion of parallel codes (26-bit parallel code to 16-bit parallel code),

28 - the first unit for receiving analog signals and supplying power to contactless induction phase shifters (BIF) (hereinafter referred to as the first unit for receiving analog signals),

29 - the first multichannel phase-code converter (8-bit binary code),

30 - the fourth MEVM, implemented as a module of the microprocessor "Electronics C5-2200",

OZU-16 - RAM ("Electronics C5-2205") of the device 16,

PZU-16 - PZU ("Electronics S5-2213M2"),

VIM-16 - the internal interface of the device 16,

31 - block arithmetic multipliers,

32 - fifth MEWM, implemented as a module of the microprocessor "Electronics C5-2200",

OZU-17 - RAM ("Electronics C5-2205") of the device 17,

PZU-17 - ROM ("Electronics S5-2213M2") of the device 17,

VIM-17 - internal interface highway of the device 17

33 - block pairing with indicators,

34 - CVM module, implemented as a module of functional CVV “Electronics C5-2202”

35, 36 - front panels of the remote terminal,

37, 38 - CV modules ("Electronics C5-2202"),

39 - a block for converting a binary code into a three-phase sequence of pulses (hereinafter referred to as a block for converting a binary code),

40 - block switching electrical circuits through relays and circuits with galvanic isolation (hereinafter referred to as the block switching electrical circuits),

VIM-19 - the internal interface line of the device 19,

41 - CV module ("Electronics C5-2202"),

42 - multichannel unit for generating control signals of an asynchronous motor (HELL) of the tracking system (in the form of a 10-bit parallel code),

43 - multi-channel code-voltage converter (MPKN),

44 is a second block receiving analog signals,

45 - second multi-channel phase-to-code converter (to 16-bit parallel code)

VIM-20 - the internal interface line of the device 20,

46 - CV module ("Electronics C5-2202"),

47 - front panel.

The console device 1 is made in the form of a multi-machine computing system, providing the formation of calculated guidance data based on information received from a complex simulator of 10 external systems, entering these data into the weapon with working out the values of the mismatch between the calculated and actual values of the position of the actuating mechanisms of the tracking systems, and generating signals shooting control.

The composition of the computing devices of the remote control device 1 includes a device 15 for receiving and processing data from information sources, a device 16 for generating firing data, and a device for displaying and inputting data 17, connected by means of the first internal highway VMP-1-1 to each other, with a two-input RAM 21, forming the common memory field of the computing system of the device, and with a communication adapter 22, as well as a control device 18 connected to the second inputs-outputs of the RAM 21 and the adapter 22 via the second internal trunk of the VMP-2-1.

The CVC device 19 connected to the VMP-1-2 trunk, and the MCCS 20 connected to the VMP-2-2 trunk are structurally combined into a separate device and connected to computing devices 15, 16, 17, 18 through a communication adapter 22 that performs hardware pairing the internal highways VMP-1-1 and VMP-2-1 with their continuation VMP-1-2 and VMP-2-2.

The device 15 for receiving and processing data from information sources is based on the third MEWM 26, which is connected to VPM-1-1, and also through the internal interface line of the VIM-15 device OZU-15, ROM-15 is connected to the parallel code conversion unit 27 whose input from the complex

the simulator 10 receives digital data of the angles θ _to and ψ _{to the} side and pitching of his ship. In addition, the device 15 contains a series-connected first multi-channel block 28 for receiving analog signals and a first multi-channel converter 29 phase-code, the outputs of which are connected to the digital input-output registers MEWM 26. The inputs of block 28 form the first group of inputs of the analog signals of the remote control 1, on which receive the signals of the distance and heading angle of underwater and surface targets (“D _P ”, “D _H ”, “q _CPU ”, “q _TSN ”), speed “V _s ” and course “K _S ” of their ship and hardware angle “A _f ” company PA OIN.

The firing data generating device 16 is based on the fourth MEWM 30, which is connected to the first VMP-1-1 internal trunk of the device and connected via the VIM-16 internal trunk to OZU-16, PZU-16 and arithmetic multiplier unit 31.

The console terminal 17 is made on the basis of the fifth MEWM 32, which is connected to the first internal trunk of VMP-1-1 and, through VIM-17, is connected to OZU-17, PZU-17 and to the interface unit 33 with indicators. In addition, the device includes a DVR module 34 connected to the VMP-1-1, the inputs and outputs of which are connected to the front panels 35, 36 of the console terminal.

On the front panel 35 there are buttons for starting the device, initial debugging start and program start. In the center of the panel are three gas discharge indicators (screens), each of which displays alphanumeric information. Under the indicator there is a typesetter, with the help of which a call to the service information screens is made, as well as a button that forms a command for displaying information in automatic mode, and a button for entering non-standard information.

The front panel 36 is used to manually enter data in all operating modes of the device. Data entry is provided by ADDRESS, NUMBER dials with indication of the dialing result on the screen.

The control device 18 comprises a first MEW 23, connected via a serial line trunk (MPC) to a second MEW 24, a third MEW 26, a fourth MEW 30 and a fifth MEW 32, and also through a program debugging unit 25 connected to the VIM-18 trunk to which are connected the second MEM 24 and PZU-18 and which, in addition, is connected to the internal highways VIM-15, VIM-16,

VIM-17 devices 15, 16, 17. MEWM 24 is connected via a second internal trunk of the device VMP-2-1 with two-input RAM 21 and a communication adapter 22.

The CVC device 19 comprises CVC modules 37, 38, 46 connected to the internal trunk of the device VMP-1-2, which is connected to the VMP-1-1 through the communication adapter 22. The CVC module 37 is connected via the VIM-19 trunk to the binary code conversion unit 39, the output of which is connected to the circuit switching unit 40, the corresponding inputs and outputs of which are also connected to the CVC module 38. The external inputs of the unit 40 form the inputs of the presence of ammunition ("Availability BO", "The presence of SPE") remote control device 1, and the external outputs form the outputs of the device 1 according to the input signal of the depth of immersion ("N _BO "), and the signal to turn on the firing circuit RPU ( “On. RPU CA”), transmitted to the RPU guidance signal conversion device 2, as well as on the control signal of the SPE firing circuits (“Exercise CA SPE”) and ON signals of the ON firing circuits (“On. CA SPE”), transmitted respectively to the control input of the switch 4 signals and control inputs of the device VA 7 switching circuits firing SPE.

The DVC module 46 is connected to the front panel 47, on which are located the power-on buttons, the start and debug mode buttons, the weapon selection and salvo production buttons, as well as the selsyn scale for monitoring data entered into device 5 “α _K ”, “q _btK ” , "Ω _K ", "D _divK " and the scale for manual input of stroke depth data SPE "N _SPE ".

The multi-channel digital tracking system 20 comprises a CVM module 41 connected to the VPM-2-2, which is connected via a communication adapter 22 to the VMP-2-1, and connected by means of the VIM-20 to the block 42 for generating control signals for asynchronous motors of the tracking systems, a multi-channel converter 43 code-voltage and with a second multichannel converter 45 phase-code. The inputs of the multi-channel phase-code converter 45 are connected to the outputs of the second analog signal receiving unit 44, the inputs of which form the second group of inputs of the analog signals of the remote control 1, to which feedback signals “BIFugn” are received from the contactless induction phase shifters (BIF) of the actuators of the tracking systems of the device 2 ”,“ BIFuvn ”, and feedback signals“ BIFα ”,“ BIFq _bt ”,“ BIFω ”,“ BIFD _div ”are received from the BIF actuators of the tracking systems of device 3. The outputs of the multi-channel Converter 43 code-voltage form the outputs of the signals "Input UGN", "Input UVN" transmitted by the remote control device

2, and the outputs of the signals "input α", "input q _bt ", "input ω", "input D _div " transmitted by the remote control device to the device 3.

Figure 3 of the structural diagram of the device 2 conversion signal guidance RPU indicated:

48 is a device for generating a signal to prohibit shooting, made in the form of a mechanical device connected to a power drive of the RPU. On the device are set using the cams of the shooting sector, taking into account the location of deck superstructures. In the event that the RPU leaves the zone of the permitted sector, the device generates a fire prohibition signal;

49 - a source of secondary power (IVEP) DC,

50 - switching unit stepper motors (SH),

51 - block switching executive circuits,

52 - block switching firing circuits,

53 - emergency release switching unit,

54 - block matching electric scales,

55-UGN - executive mechanism for processing the signal "UGN" (horizontal pointing angle),

55-UVN - executive mechanism for processing the signal "UVN" (angle of vertical guidance),

56 - power amplifier of an induction motor (UMAD),

57 - asynchronous electric motor (HELL), for example, type DA-402,

58 - a scale of angular reference located under the cover of the device,

59 - rotary transformer (VT) sensor,

60 _GO - non-contact induction phase shifter (BIF) of rough reading (GO),

60 _TO - Beef accurate reading (TO).

According to figure 3, the input signal "Input N _BO " device 2 is the control input of the switch 50 of the stepper motors, the power input of which is connected to IVEP 49, and the outputs forming a three-phase circuit (φ ₁ , φ ₂ , φ ₃ ) of the power of the stepper motors are connected with the corresponding inputs of the simulator 13 RPU firing circuits. In real equipment, by means of stepper motors, the values of immersion depth (bomb detonator actuation) are introduced into the bombs.

IVEP 49 is also connected to the power input of the Executive circuit switching unit 51, the control input of which forms the signal “On. CA "device 2, and the output is connected to the power inputs of the block 52 switching firing circuits, the outputs of which, forming the power supply circuit of the igniter and electronic ballast RPU, are connected to the corresponding inputs of the simulator 13 firing circuit RPU. The input and output of the “Presence” signal of block 52 form the input and output of the device 2 of the same name, and the “Presence” signal is generated by pressing the corresponding buttons on the panel of the simulator 13 RPU firing circuits.

The input and output of the block 52 by the signal of the prohibition of firing “Zapr.” Are connected respectively to the output of the device 48 for generating the signal of the prohibition of firing and the control input of the block 51 for switching the executive circuits. The output of block 52 by the turn-on signal of the RPU (“On RPU”) is connected to the corresponding inputs of the block 53 and the block 54 for matching the electric scales, the outputs of which according to the signals “PUGN”, “PUVN”, which form the outputs of the same name 2, are connected to the inputs of the simulator 12 full angles of guidance RPU.

The power input of the emergency release switching unit 53 is connected to the battery, and the power output is connected to the power circuits of the RPU and igniter.

The inputs of block 54 by the signals "PUGN", "PUVN" are connected to the outputs of the simulator 11 of the gyroscopic stabilization system, the inputs of which are connected by the signals "UGN", "UVN" to the outputs of the actuators 55-UGN and 55-UVN.

The actuator 55-UGN (55-UVN) contains an induction motor 57, on the shaft of which there is a VT sensor 59, the output of which forms the output of the signal "UGN"("UVN"), and non-contact induction phase shifters 60-GO, 60-TO, the output of which forms the output of the signal "BIF _UGN "("BIF _UVN ") for testing the actuator 55-UGN (55-UVN). The input of the actuator 55-UGN (55-UVN), which receives the signal “input UGN” (“input of the UVN”) from the remote control 1, is the input of the power amplifier 56 of the induction motor, the output of which is connected to the control input of the induction motor 57. Position the shaft of the induction motor is controlled on a scale of 58 angular reference located under the cover of the device 2.

In Fig.4 structural diagrams of the device 3 conversion signal guidance of the SPE and devices 5, 6 data input into the SPE are indicated:

61-α, 61-q _bt , 61-ω, 61-D _div - actuators for processing signals “input α” (angle of divergence of SPE in a salvo), “input q _bt ” (course angle of the side of the target), “input ω” (angle of pointing the gyro of the SPE) and “input D _div ” (distance of the discrepancy between the SPE in the salvo), respectively,

62 - power amplifier induction motor,

63 - asynchronous electric motor (type DA-402),

64 - a scale of angular reference located under the cover of the device 3,

65 - VT sensor

66 - BT receiver

67-GO, 67-TO - non-contact induction phase shifters of coarse and accurate reading, respectively,

68 - amplifier

69 - relays with normally closed and normally open contacts,

70 - amplifier

71-α, 71-q, 71-ω, 71-D _div are the actuators for inputting the values α, q _bt , ω, D _div into SPEs, respectively,

72 - electric motor (type ADP-1263),

73 - scale angular reference

74 - selsyn sensor (type BD-160A), electrically connected to the selsyn receiver (type BS-151A), which is mechanically connected to a scale located on the front panel 47 of the console device 1,

75 - spindle SPE kinematically (using cardan rollers) connected to the motor shaft 72,

76 - BT receiver, electrically connected with a rotating transformer-sensor 65,

77 - electric motor (type ADP-1263),

78 - scale angular reference

79 - spindle SPE kinematically (using cardan rollers) connected to the shaft of an electric motor 77,

80 - VT receiver, electrically connected to the rotor winding of the VT sensor, which is connected through a gearbox to the scale H of the front panel 47 of the remote control 1.

According to figure 4, the device 3 converting signal guidance of the SPE contains four identical actuators 61-α, 61-q _bt , 61-ω, 61-D _div , by

which are working out the guidance signals of the SPE, and an amplifier 70 that generates a control voltage ("Str. N"), which sets the depth of the SPE.

Each of the actuators 61-α, (61-q _bt , 61-ω, 61-D _div ) contains an induction motor 63 and an asynchronous motor power amplifier 62, through which a control voltage is supplied to the control winding of the induction motor 63 (signal “input α "), Generated in the MCCS 20 of the console device 1, or, in standby mode, the signal" input α res. ", Generated, as will be shown below, in the device 9 for receiving and converting analog signals. The input circuit of the control signal “input α” is connected to the UMAD input 62 through normally closed contacts of the relay 69, and the input circuit of the signal “input α res.” Is connected through the BT-receiver 66 in series and normally open relay contacts 69. The outputs installed on the motor shaft 63 non-contact induction phase shifters 67-GO, 67-TO, forming a voltage whose phase is proportional to the angle of rotation of the shaft AD 63, form the output of the control signal "BIF α"("BIF q _bt ", "BIF ω", "BIF D _div ") transmitted to the МЦСС 20 console device 1. Signal output of VT-sensor Ika 65 mounted on the shaft of the AD 63 is connected to the input of the amplifier 68, the output of which is formed by the control voltage n α ", which through the switch 4 of the signals is transmitted to the device 5 data input in the SPE.

The input devices 5, 6 in the SPE under standard conditions are installed directly on the corresponding pipe of the multi-tube launch apparatus of the SPE, from which the corresponding SPE is launched.

The data input device 5 contains four identical actuators 71-α, 71-q _bt , 71-ω, 71-Dd _iv , intended for inputting the corresponding guidance data into the SPE.

Each actuator 71-α (71-q _bt , 71-ω, 71-D _div ) contains an electric motor 72, the shaft of which is kinematically connected with the spindle 75 SPE for inputting guidance data. The control winding of the motor 72, to which the signal "Ex. n α ”(“ Exercise q _qt ”,“ Exercise q ”,“ Exercise D _div ”), is connected to the output of amplifier 68 of the corresponding actuator 61-α (61-q _bt via the 4-way switch , 61-ω, 61-D _div ) of the device 3. The BT-receiver 76, of the actuator 71 is electrically connected to the BT-sensor 65 of the actuator 61 through a switch 4, in which the signal passage "α"("q _bt " is closed, “Ω”, “D _div ”) when the signal “Ex. CA SPE ".

The selsyn sensor 74, mounted on the shaft of the engine 72, generates a control signal "α _K "("q _btK ", "ω _K ", "D _divK "), which is transmitted to the selsyn receiver front panel 47 of the remote control, which deploys the control scale at an angle corresponding to the position of the motor shaft 72.

The device 6 data input in the SPE is designed to enter the value of the depth of the SPE. The device 6 contains an electric motor 77, the shaft 78 of which is kinematically connected with the spindle 79 for entering the stroke depth of the SPE. A BT receiver 80 is installed on shaft 78, the input of which is connected to the input of the switch 4 of the same name by the signal “input Н _ОИН ” when the signal “Ex. TsS ", and the output of the signal" N "is connected through a switch 4 to the input of the amplifier 70 of the device 3. The output of the amplifier 70, on which the control voltage is generated" Ex. n N "through the switch 4 is connected to the control winding of the motor 77.

In Fig.5 structural diagram of a device 9 for receiving and converting analog signals are indicated:

81 - Executive mechanism for processing data q _CPU heading angle of the underwater target,

82 - actuator data mining D _{P the} distance of the underwater target,

83 - actuator data mining q _CN directional angle of the surface target, made similar to the IM 81,

84 - actuator data mining D _{N the} distance of the underwater target, made similar to the IM 82,

85 - Executive mechanism for processing data V _{S the} speed of his ship, made similar to the IM 82,

86 - Executive mechanism for processing data K _S course of his ship, made similar to the IM 82,

87 - actuator data mining A _{f the} angular turn of PA SPE in the plane of the deck,

88 - remote control manual data input,

89 - block switching guidance signals,

90 - block switching control signals firing circuits,

91 - VT sensor kinematically associated with a scale for manual data entry q _bt course angle of the side of the target,

92 - VT sensor kinematically associated with the scale of manual data input Ddiv distance of the discrepancy of the SPE in a salvo,

93 - VT sensor kinematically associated with the scale of manual data input Δω increment of the pointing angle of the gyroscope SPE,

94 - VT sensor kinematically associated with a scale for manual data entry α of the angle of divergence of the SPE in a salvo,

95 - VT sensor kinematically associated with the scale of manual data input H stroke depth SPE,

96 is a gearbox through which the shaft of the actuator of the device 8 is connected with the shaft of the starting device SPE,

97 - VT sensor mounted on the shaft of the device IM 8, kinematically connected with the scale of the angular reference data A _{f the} hardware angle of the SPD launcher in the deck plane,

HELL - asynchronous electric motor,

BIF-GO, BIF-TO - non-contact induction phase shifters of coarse and accurate reading, respectively,

VT _DAT - rotating transformer sensor,

VT _PR - rotating transformer receiver,

UMAD is an asynchronous motor power amplifier.

According to figure 5, the inputs of the analog data q _CPU , D _P , q _TSN , D _N V _S , K _S entering the device 9 for receiving and converting analog signals from the simulator 10 are formed by the input windings of the VT-receivers of the actuators 81-86. The mismatch voltage from the rotor winding of the VT receiver is fed to the UMAD input, the output of which is connected to the control winding of an asynchronous electric motor, on the shaft of which there is a VT sensor connected to the supporting system, a VT receiver and BIF units. The outputs of the BIF blocks, forming the output voltage of a sinusoidal shape, the phase of which is shifted relative to the reference voltage by an amount proportional to the angle of rotation of the HELL shaft, form the information outputs of the device 9 connected to the first group of inputs of the analog signals of the remote control 1.

IM 87, designed to process the signal “A _f ”, is made similarly to IM 81. The input of the VT-receiver IM 87 is connected to the output of the VT-sensor 97 of the device 8 for outputting data of the angular rotation of the PA SPE, which is mounted on a shaft connected via a gearbox

96 with the shaft of the SPD launcher. The outputs of the BIF IM 87 blocks are connected to the inputs of the console device 1.

The manual data input panel, coming in from device 9, contains BT-sensors 91-95 mounted on shafts that are kinematically connected with the data input scales “q _bt ”, “D _div ”, “Δω”, “α”, “Н” . The outputs of the VT sensors 91-94 are connected to the normally open contacts K _{1 of the} relay of the block 89, and the output of the sensor 95 is connected to the normally open contacts K _{2 of the} relay of the block 89, the winding Р of which is included in the control signal circuit “On. PP ", formed by pressing the backup mode enable button (not shown) located on the remote 88. The signal circuits K _{1 are} connected to the outputs of the contacts K ₁ input q _bt res., Input D _div res., Input Δω res." , “Input α res.”, Which are transmitted to the actuators of device 3, and the output signal of contacts K _{2 is} connected to the signal “input Н _ОИН ” signal transmitted through switch 4 to data input device 6. The input of normally closed contacts K _{2 is} connected to the signal circuit "N _SPE ", which is formed at the corresponding output of the console device 1 in the main mode of operation.

The inputs of the block 90 switching signals of control of the firing circuits are connected to the corresponding buttons of the remote control 88 (not shown), its outputs according to the signals "Ex. CA SPE "connected to the control inputs of the switch 4, and the outputs of the signals" On. CA SPE "- with the control inputs of the device 7 switching firing circuits.

The health check of the firing control system (product) is carried out by the diagnostic and troubleshooting software under the control of an operator using the controls located on the front panels 35, 36 and 47 of the remote control.

The interaction between the components and devices of the product is as follows.

Communication between devices 15-20 of the console device is carried out along two internal trunk lines of the device (VMP-1 and VMP-2). Information is transmitted between MEWs 26, 30, 32, data is transmitted from one MEWM to another through a two-input RAM 21, which is connected to VMP-1 by one input-output and by VMP-2 by the other. Two-input RAM 21 is a common memory field of the entire network of computers.

On the VMP-1 highway, MEVMs 26, 30, 32 are connected through the registers of the modules 34, 46 of the CVM, to the controls on the front panels, through the registers of the CVM of the MEVM 26 are connected to the device 9 for receiving and converting analog signals, through the registers

CVC modules 37 through VIM-19 are connected to the binary code to three-phase pulse train 39, and through the registers of the CVC module 38, through the circuit switching unit 40, they are connected to the RPU guidance signal conversion device 2 and the SPE firing circuit switching device 7. On the highway VMP-2, MEWM 24 is connected to the devices of the MCCS 20.

MEWM 26, 30, 32 on the VMP-1 trunk are active subscribers, the rest of the devices are passive. MEWM 30 upon requests from active subscribers (MEWM 26, 32) transfers control of the trunk to the latter. On the VMP-2 highway, the only active subscriber is MEWM 24, which controls the exchange on this highway.

In addition, the console device uses the inter-machine serial channel of the IPC. When issuing IPC data, its work is provided by both hardware and software.

The tasks solved by the console device are distributed according to their functional purpose.

MEWM 23 together with device 17 and program debugging unit 25 provides autonomous control and debugging of device programs by writing information to RAM cells and programmatically accessible registers, reading from RAM cells, ROM, setting various instrument operating modes, connecting individual test programs, etc. . The results of autonomous control are displayed on the indicators and screens of the front panel 35 of the remote control.

MEWM 26, together with the parallel code conversion unit 27, the analog signal reception unit 28, the multi-channel phase-to-code converter 29, RAM-15 and ROM-15 provides the reception and formation of arrays of converted quantities coming from the complex simulator 10 via digital and analog communication channels and transferring them to a common memory field (two-input RAM 21).

MEWM 26 also outputs to the block 39 the depths of immersion of the bombs, corresponding to the time of immersion of the bombs, for subsequent output in the form of a three-phase sequence of pulses into the device 2 for converting the guidance signals of the RPU, which commutates the power supply circuit of the stepper motors of the RPU.

MEWM 30 together with block 31 of arithmetic multipliers, OZU-16 and PZU-16 provides the generation of bombardment data from RPU against an underwater target, guided projectiles (SPE) on underwater or surface targets, as well as on

two targets at the same time (for underwater targets - with bomb weapons, for surface targets - with guided projectiles).

MEWM 32 together with OZU-17, ROM-17 provides a dialogue with the operator.

The screens of the three indicators of the front panel 35 display the initial data from the ship's support systems (simulated by a complex simulator 10), information on the presence and condition of the weapon coming from the RPU guidance signal conversion device 2 and the SPE firing circuit switching device 7, recommendations to the operator for manually entering information , depending on the stage of the computational process, and the results of solving problems.

All information displayed on the screens is divided into display pages and displayed automatically or manually. The symbol and the number of the product malfunction are displayed on the first line of the first page, the MEM number blinking with a frequency of 1 Hz is displayed on the second line, which indicates its serviceability, and the name of the product operation mode, recommendations to the operator are displayed on the third line. The second and third pages display information about the availability of ammunition in the RPU and the stages of solving the problems of firing bomb weapons from the RPU. The fourth page contains information on the availability and type of SPE, the fifth contains recommendations to the operator when entering data manually, the sixth page is for calling up RAM and ROM cells for display, the seventh page contains information about the distance to the target, the angle between the course of your ship and the bearing line to the target , signal of loss of target, etc.

MEWM 24 together with OZU-18 and PZU-18 organizes the output of digital information, prepared by the tasks of organizing the appropriate type of shooting, to the device МЦСС 20 for converting it into analog and further output to devices 2 and 3.

When the product is turned on in the main operating mode by the console device 1, control signals are generated that are transmitted through the device 3 to the SPE launcher for initialization of the SPIN spindles, as well as input signals of the initial explosion depth and the installation are transmitted through the device 2 to the RPU.

Targeting data q _CPU , D _П , q _ЦН , D _Н information sources (underwater and surface targets) and data on heading K _S and speed V _{S of} your ship, generated by complex simulator 10, are fed to actuators 81-86, and data A _f about the position of the PA SPE, formed by the device 8 enter the executive

the mechanism 87 of the device 9 for receiving and converting analog signals (see figure 5).

In the actuators 81-87, voltages proportional to the q values of the _CPU , D _P , q _TsN , D _H , K _S , V _S , A _f , are supplied to the input windings of the VT receivers. The mismatch voltage from the rotor winding of the VT receiver (turned on according to the SCWT circuit) is supplied to the asynchronous motor power amplifier (UMAD), where it is amplified and fed to the winding of the asynchronous electric motor (HELL). The rotor of the engine rotates until the mismatch angle between the VT sensor and the BT receiver of the supporting system is worked out. From the coarse and accurate reference unit BIF connected to the BT receiver through the reducer, a sinusoidal voltage, the phase shift of which relative to the reference voltage is proportional to the angle of rotation of the VT receiver shaft, is supplied to the analog signal receiving unit 28 and power is supplied to the transmitter unit 1 transmitter. From block 28, the indicated voltages are supplied to a multichannel phase-code converter 29, which converts the phase shift into an 8-bit parallel binary code and transfers it to the DEC registers of the MEW 26. When two-counted signals were entered into the MEW 26, The order of information is removed from two single-count channels and coordinated programmatically.

The digital data generated by the simulator 10 (the values of the angles of the onboard and pitching keels θ _K , ψ _K ) are transmitted via a digital channel to the code conversion unit 27, which provides the conversion of a 26-bit parallel code into a 16-bit parallel code and writes information to cells of RAM-15, from which the entire array of information converted to the VIM-15 trunk is transmitted to two-input RAM 21.

From the simulator of 14 SPE firing circuits through the SPF firing circuit switching device 7, information on the availability of ammunition is received in the electrical circuit switching unit 40 of the remote control device 1 and is stored on the registers of the 38 CVV module. MEWM 30 on the VMP-1 trunk line through the adapter 22 polls the programmatically accessible registers of the CV module 38 and writes the input information to the two-input RAM 21. The presence signals of the SPE are simulated by the relay circuits of the simulator 14.

Similarly, using the same devices of the remote control device 1, the two-input RAM 21 receives through the block 52 switching firing circuits of device 2 information about the presence of bombs in the RPU generated by the relay circuits of the simulator 13 firing RPU.

From the two-input RAM 21 via the VMP-1 highway, information enters the MEWM 32, which generates signals for displaying information on the screens of the front panel 35.

Based on the information and recommendations displayed on the screens, the operator can approve the recommendation or enter new information. The result of solving functional problems, depending on the type of target and type of weapon is:

determination of the elements of the movement of the target;

generation of SPE guidance data (values of α, q _bt , D _div , ω for two pipes of a multi-tube PA);

generation of RPU guidance data (UGN, UVN values);

prohibition of shooting if the target is unattainable or there are no normal launch conditions;

display on the screens of indicators of the firing data, as well as the state of the weapon and ammunition;

passing volley.

When firing a SPE, the operator connects the input data to solve the firing problem. According to the operator’s commands, the initial data from the two-input RAM 21 is supplied to the MEWM 30, which, together with the devices located on the VIM-16 highway, solves the firing problem and enters the results into the two-input RAM 21.

The result of solving the SPE firing problem is the values of α, q _bt , D _div , ω along the two tubes of the SP SPM assigned to the volley and the control signals of the firing circuits. The developed values are displayed on the indicator screen and entered into the weapon only after the operator issues the appropriate command. After issuing the command, MEWM 24 polls the two-input RAM 21 and then through the adapter 22 transfers the data to the MCCS 20 to the registers of the CVM module 41.

The module 41 CVC interfaces the highways VMP-2 and VIM-20. A multi-channel converter 43 code-voltage, an asynchronous motor control signal generating unit 42, an analog signal receiving unit 44 and a multi-channel phase-to-code converter 45 organize a functional unit of a multi-channel digital servo system that provides reception and conversion of a 13-bit binary code into control signals of actuators 2, 3.

The interaction of devices included in the MCCS 20 is carried out under the control of MEWM 24 through the programmatically accessible registers of the module 41 DEC. Under the control of MEWM 24, the developed values α, q _bt , D _div , ω are introduced into the RAM of block 42. Reception

and the conversion of information about the actual position of the shafts of the actuators 61 of the device 3, as well as the formation of the supply voltage BIF 67 coarse and accurate counting for each value is carried out by the block 44 receiving analog signals. After conversion in the multi-channel converter 45 phase-code information about the actual position of the actuators is recorded in the RAM unit 42, which compares the values of the generated values with the actual position of the actuators, generates a control code to work out the mismatch for each value and passes it to the input of the multi-channel converter 43 code voltage. In MPKN 43, the codes are converted into direct current control signals (“input α”, “input q _bt ”, “input D _div ”, “input ω”) and fed to the inputs of power amplifiers 62 of induction motors, where they are amplified and fed to the control windings asynchronous electric motors 63. HELL 63 rotates the shaft until the voltage at the input of the AMAD becomes minimum. In this case, the BT sensor 65 of each actuator 61 will be rotated by an angle equal to that required for input into the SPE.

The BT sensors 65 of the actuators 61 are electrically connected to the VT receivers 76 of the actuators 71 of the SPE data input device 5, which are connected in the switching device 4 by firing chain control signals. In this case, the signal from the BT receiver 76 is supplied to the BT sensor 65 and then to the amplifier 68. From the output of the amplifier 68, the control voltage ("Ctrl n. Α", "Ctrl q q _bt ", "Ctrl N D _div "," Exercise. ω ") is supplied to an electric motor 72, which rotates the shaft of the servo system until the voltage at the input of amplifier 68 becomes minimal. In this case, the BT receiver 76 and the sync sensor 74 of each actuator 71 will be rotated through an angle equal to that entered into the actuators 61 of the device 3.

Control of input values α, q _bt , D _diw , ω is carried out according to the scales located on the front panel 47 of the remote control. Each scale is kinematically connected with the synchro-receiver, which is electrically connected with the synchro-sensor 74 of the device 5. The choice of a specific device 5 is made by the switch in accordance with the launcher tube assigned to the volley.

On the front panel 47, according to the scales of N _SPE connected through a gearbox with VT sensors, the depth of the SPE is set for each designated SPE. From rotor windings of VT sensors, voltage is supplied through normally closed

K2 contacts of the switching unit 89 of the guidance signals of the device 9 to the BT receiver 80 of the data input device 6, which is connected in the switch 4 by the firing chain control signals. The signal from the rotor winding of the BT receiver is supplied to the amplifier 70 of the device 3. From the output of the amplifier 70, the control voltage H is supplied to an electric motor 77, which rotates the shaft of the servo system until the voltage at the input of the amplifier 70 becomes minimal. In this case, the BT receiver 80 of the tracking system will be rotated by an angle equal to the angle set on the scale H of the _{SPE of} device 1. The depth of immersion in the SPE is entered using cardan rollers connecting the line of the tracking system to the 79 ION spindle.

A positive result of preparation for firing and data entry is indicated by the light on the ready indicator on the front panel of the device 1. Connection of the executive firing circuits is made from the front panel 47 by setting the switch “Ex. CA SPE ”, while in the device 7 switching the firing circuits, the executive circuits are connected to the electromagnets of the launcher tubes assigned to the salvo, and in the switch 4 of the signals are connected, as discussed above, the VT-receivers 76, 80 and the input of the guidance signals reversing the shafts is performed actuators of devices 5 and 6. If there is a recommendation on the device indicator screen 1 for a salvo, the “On. CA SPE ", while under normal conditions, the voltage of 27 V DC is applied to the electromagnets to start the SPE, and in the proposed complex, these voltages are displayed on the simulator panel of 14 SPE firing circuits.

When firing from RPU, the operator, by setting the appropriate switches, connects the input data to solve the firing problem. According to the operator’s commands, the initial data from the two-input RAM 21 via the VMP-1-1 highway is sent to the MEWM 30, which, together with the devices located on the VIM-16 highway, solves the shooting problem and enters the results into the two-input RAM 21.

The result of solving the firing problem is the values of the angles of horizontal and vertical guidance of the RPU (UGN, UVN), the depth N of the _BO of the bombings and the control signals of the firing chains. The generated values are displayed on the indicator screen and entered into the weapon only when you press the data entry button.

At the same time, MEWM 24 polls the two-input RAM 21 and then, through the communication adapter 22, transfers the UGN, UVN values to the MCCS to the registers of the CVC module 41.

The principle of working out the calculated values of the UGN, UVN values by the actuators 55 of the device 2 is similar to the principle of working off the values by the actuating mechanisms of the device 3.

To generate full guidance angles (PUGN, PUVN), the voltages from the VT sensors 59 of device 2, proportional to the UGN, UVN values, are supplied to the rotating transformers of the gyroscopic stabilization system simulator 11, where they are summed with voltages proportional to the ship’s onboard and keel pitch, which are set with using scales of rotating transformers. Further, the signals obtained as a result of the summation, proportional to the PUGN, PUVN, are fed through the block 54 matching the electric scales to the VT-receivers of the simulator 12 full guidance angles and are controlled on their scales.

To enter the calculated values of N _{BO the} depth of immersion (fuse operation) of the bombs produced by the MEWM 30 and transferred to the two-input RAM 21, the MEWM 26 polls the two-input RAM 21 and through the communication adapter 22, enters the value of the N _BO into the registers via the VMP-1-2 line module 37 CVM. Module 37 implements the VMP-1.2 and VIM-19 highways and transfers the calculated values to the binary code conversion unit 39, which converts the 8-bit binary code corresponding to the value of the immersion depth N _BO into a three-phase pulse train.

The generated pulses are fed into the device 2 to the relay windings of the step switching power supply unit 50, through the contacts of which under normal conditions three-phase power supply circuits of the step motors are fed, which enter values into the bombs. In the proposed complex, these voltages are applied to the inputs of the relay circuits of the simulator 13 RPU firing circuits.

To ensure the safety of firing of bomb weapons, a prohibition signal generation device 48 is used, which is mechanically connected to the RPU power drive. The device 48 is set using the cams of the shooting sector, taking into account the location of deck superstructures. If the RPU goes beyond the sector area, the device 48 generates a fire prohibition signal.

Switching firing circuits during the production of volley is carried out using block 51 switching Executive circuits and block 52 switching firing circuits. The signal “On. CA RPU ", while the voltage of 27 V DC through blocks 51, 52 is supplied to the squibs and electric fuses

bombs. Ignition commands are given at a predetermined interval, and, depending on the firing range and pointing angle, on one or two squibs of the engine. The results of the passage of teams are displayed on the front panel of the simulator 13 firing circuits RPU.

The emergency release of bombs is controlled using block 53 by turning on the emergency release buttons according to the number of RBU guides that are on the front panel of block 53. The voltage during emergency release is supplied from the battery.

The operation of the product in standby mode is carried out using the working bodies of the remote control 88 of the manual data input in the device 9.

At the same time, the data of target designation, heading and speed of your ship from the complex simulator 10 are processed by actuators 81-86 of device 9 and displayed on the scales of actuators.

Based on the readings of the scales of the actuators 81-86, the operator sets the scales 91-95 to the marks of the calculated values. The solution to the shooting problem is reduced to the development of the pointing angle of the gyroscopic instrument of the SPE by adding the analog values q _C , A _f and Δω. After selecting the launcher tube, the guidance data is transmitted through the switching unit 89 of the guidance signals to the BT receivers 66 of the actuators 61, from which through the normally open contacts of the relay 69 to the control winding UMAD 62. The control signal including the relay 69 is generated by pressing the corresponding button on the front the panel of the block 88 (the power circuit of the signal circuits for simplicity is not shown in figure 5).

The inclusion of firing circuits is carried out through the block 90 switching control signals CA.

As discussed above, when the system is in the main (automatic) mode, information about the progress and completion of the stages of the computational operations is displayed on the indicator screen, and if a malfunction occurs, the number of the faulty unit and recommendations to the operator on troubleshooting are displayed.

Diagnostics of faults when the product is turned on is carried out by the test control system programs, which includes the test control and diagnostics organization program, which is connected by the initial start-up program of each resident software computer and transfers control to the central control controller in the computer 32 and the monitoring controller in the computer 24, 26 and 30, and also

programs for test control of the computer, test control of the interface device with information sources, test control of the arithmetic accelerating module, test control of the trunk device, test control of the depth input device and test control of the digital tracking system.

During the operation of the product, fault diagnostics are provided by the program of failures and failures (OSO), which is implemented in the form of a programmable plug-in, and any task that fixes the failure generates a fault number in the general register and makes an unconditional transition to the OSO start address. At the end of the testing of the CCA, in each case, it is ensured that the product continues to function or is stopped to replace the failed module or unit. The CCA program is connected by those tasks that, in the process of solving, fixed a failure or failure. Any task that fixes a failure transfers control to the CCA switch, which captures the status of the MEWM service registers and control cells in two-input RAM, and then connects a specific CCA processor using the number recorded in the general register. If the CCA switch does not detect a malfunction existing in this MEM, then the MEM is dynamically stopped, and the malfunction is displayed on the screen.

When the remote control unit is offline checked, after the test check is completed and the device readiness message appears, they check the operability of the controls by sequentially pressing the number and switch buttons and checking the correctness of the codes that appear on the indicator. To check the operation of indicators, press the address and enter buttons until the control image appears.

When checking the pairing of the product with information sources, the input data specified by the simulator 10 are read on the scales of actuators 81-86 and if the error in working out any value exceeds the permissible value, the corresponding unit of the device 9 is adjusted.

The verification of the conversion of analog signals input from device 9 is carried out by setting the scales of actuators 81-86 to a predetermined position and comparing the entered values with their values displayed on a specific indicator page, which the operator calls by entering the indicator number and page number.

Checking the pairing of the product with simulator 10 via a digital channel is carried out by entering codes corresponding to certain values of roll and pitching (5.6 ° θ _K for and 2.8 ° for ψ _K ), which are displayed on a specific display page called up by the operator during normal operation .

Checking the correctness of the conversion by the remote control of the guidance data entered into devices 2 and 3 is carried out in the following order.

Set the angle scale of the actuators 55 of the device 2 and actuators 61 of the device 3 to zero. On the indicator switch, dial the number 2 corresponding to the indicator number, the number 8 corresponding to the display page number and press the enter button, after which page 8 should appear on the screen of the second indicator. Using the address switch, enter the number 75 and control the appearance of the first indicator on the 6th line of the screen dialed address 75 and the pattern corresponding to it. Enter the number of the called MEWM 24 using the number switch, controlling the appearance of the first indicator on the 6th line and on the 1st line of the second indicator of the dialed number of the called MEWM. Enter the number 76 using the address switch, controlling the change of address 75 on the screen of the first indicator to the dialed address 76 and the corresponding template. Enter the decimal code of the starting hexadecimal address using the number switch, controlling the input of the decimal code on the 9th line of the first indicator and the appearance on the 6th line of the first indicator and on the first line of the second indicator of the dialed starting address. Then, in the same order, the address 78 and the new decimal code of the hexadecimal address are sequentially entered, the next address 77 is entered, and then the number 7 is entered and the number is entered on the 9th line of the screen of the first indicator, etc. During the verification process, code changes are constantly monitored. If there is no change in the code, the steps for connecting the conversion program are repeated. Next, the contents of the cells corresponding to the position of the scales are read and, if it differs from the indicated, loosen the screws of the stator mounting unit for the BIF of the corresponding servo system and, slowly turning the stator, achieve the indication of the corresponding codes for phase shifters of a coarse and accurate reading.

Checking the joint operation of devices 9, 3, 5 and 6 in the standby mode of firing of SPEs is carried out by installing on the scales 91-95 of the remote control 88 manually entering data of the corresponding values of the input values and reading the rotation angles on the scales of devices 5, 6. If there is an error in working out any parameter exceeds admissible

value, adjust the kinematic lines of rotating transformers and selsyn.

Thus, the proposed complex for testing a ship’s weapon control system has wide functional capabilities and provides high reliability of the results due to the control coverage of both individual devices and devices, and their interaction during joint work in the main and standby modes.

The industrial applicability of the utility model is determined by the fact that the proposed complex can be manufactured in accordance with the above description and drawings on the basis of well-known components and technological equipment and used for complex verification of the ship’s weapon control system.

Bibliography

1. RF patent No. 2205441 for invention, IPC G05B 23/02, publication May 27, 2003.

2. RF patent No. 56662 for utility model, IPC G05B 23/02, publication September 10, 2006.

Claims (1)

A complex for testing a ship’s weapon control system, containing standard and simulation equipment, characterized in that the standard equipment includes a remote control connected to a device for converting guidance signals from a rocket launcher (RPU) and to a device for converting guidance signals from individual targeting devices (SPE) which are made on the basis of actuators of servo systems, the first and second data input devices in the SPE, connected via a signal switch to the device the SPF of the SPE guidance signal conversion, as well as the SPF firing circuit switching device connected to the handheld device, the SPE angular turn data output device (PA) of the SPE and the analog signal reception and conversion device based on actuating mechanisms of the tracking systems, the input of one of which connected to the output of the device for issuing data of the angular turn of the PA SPE, and the inputs of the rest are connected to the corresponding outputs of the analog signals of a complex simulator of external systems, on which Target designation data of underwater and surface targets and heading and speed data of your ship are generated, the outputs of the analog signal reception and conversion device are connected to the first group of inputs of the analog signals of the remote control, the second group of inputs of analog signals of which are connected to the outputs of the actuators of the tracking systems of the guidance signal conversion device RPU and SPE guidance signal conversion devices, output of a complex simulator of external systems on which digital signals are generated data of the angles of the onboard and keel pitching of his ship, connected via a digital communication channel to the handheld device, the outputs of the RPU guidance signal conversion device at which the horizontal and vertical guidance angles are generated, and the inputs to which the signals of the full horizontal and vertical guidance angles are received side and keel pitching of your ship, connected to the corresponding inputs and outputs of the gyroscopic stabilization system simulator, and the outputs of the signal conversion device The RPU guidance by signals of the full angles of horizontal and vertical guidance is connected to the inputs of the simulator of full guidance angles, which, like the simulator of the gyroscopic stabilization system, are made on the basis of rotating transformers with scales, while for processing the passage of signals from the control of the firing circuits, the corresponding outputs of the signal conversion device guidance RPU connected to the simulator of firing circuits RPU, and the corresponding outputs of the switching device of the circuit of firing SPE connected to the simulator c ephes firing SPE.