RU2450306C1 - Automated system for controlling carrier-rocket preparation - Google Patents

Abstract

FIELD: information technology.

SUBSTANCE: system has four automated workstations for operators, two communication devices with a fibre-optic information link, fifteen units for determining functional readiness, seven devices for communication with the object - technological equipment, eleven devices for triggering actuating elements, eight discrete information input/output units, five control and communication devices, a hardware-software control subsystem panel, two network-based system switches, four primary electric power distribution devices, a device for remote control of primary electric supply to a mobile command post, a device for remote control of primary power supply to the launch installation, four secondary electric power distribution devices for different models of carrier-rocket families, four devices for powering actuating elements and carrier-rocket systems, five software simulators, four uninterrupted power supply devices connected though a suitable set of connections.

EFFECT: broader functional capabilities owing to automated flight preparation of a carrier-rocket family consisting of models of different classes.

11 cl, 30 dwg, 1 tbl

Description

The invention relates to complex products of automation and computer technology, it can be used in the automation of objects that are important and dangerous operating conditions mainly in the rocket and space industry.

Known automated redundant control system for refueling a cryogenic overclocking unit (1), which contains a system-wide communication line, devices for online data change, an initial priority exchange device, local control devices, communication devices with an object-subsystem for working with components, communication devices with an object - refueling technological equipment , blocks for determining functional readiness, actuator start-up devices, switching-functional matrixes of emergency l in local situations, a local console, communication devices with a fiber-optic communication line, while the priority exchange device consists of a central processor, a communication device, a system bus and an operator’s workstation, each local control device contains a central processor, an operator’s workstation and a system a bus, communication devices with an object-subsystem of work with components contain a system bus, an input-output unit for discrete information, an intrinsic safety barrier group and a communication apparatus with the object - the process equipment each contain a system bus, an input-output unit of digital information, a group of intrinsic input-output unit of analog information and the analog signals unit normalization interconnected set of external and internal connections.

However, the above system (1) has a number of disadvantages, since situations may arise in it that lead to a temporary loss of control due to a failure of the central processor included in the local control device, and cases of slowing down of the system and exit from the technological process due to processor congestion and Communication device buffers overflow due to unlawfully large flow of analog information.

The closest in technical essence to the claimed invention is an automated redundant control system for refueling a cryogenic booster unit (ARSUZ KRB) (RF patent No. 2216760 C2 IPC G05B 17/02 of 11/13/2001), containing a system-wide communication line, devices for online data change ( UOID), an initial priority exchange device (UNOP), local control devices (LUU), communication devices with a fiber-optic information transmission line (US VOLPI), communication devices with an object-subsystem of work with components p of an argon unit (USOR), a device for communication with an object - technological equipment (USO TO) for refueling and component supply, functional readiness determination units (BOFG), actuator triggering devices (USE), a local console, a discrete input / output unit for monitoring device status launch of actuating elements and communication with the central flight training system (BVVDI-K), freelance control stations (IEDs), watchdog timer blocks (BST), variable information input control unit (BRVI), variable-frequency blocks h polling rates (BCHI), blocks for determining the accuracy of inputted analog information (BODAI), adaptive information input blocks (BAVI), BST consists of an encryption unit and an indication of the status of the controllers of the central processing unit's local area network (USHIK), a unit for counting time (SPM), and an adjustable unit failure signal delay (URZ), VCA consists of a control backup center (URC), a node for interfacing with a system-wide communication line, a node for interfacing with a system bus, interconnected by a combination of external and internal links, the LUU consists of an automaton EventLog operator position (ARMO) and a central processing unit (CPU).

However, the above system (2) also has a number of disadvantages that do not allow it to be used as a universal automated control system for the preparation of a family of launch vehicles. The most important of them are as follows:

- onboard launch vehicle systems are not provided with special currents when they are located at the start in the pre-launch period;

- the control of the operability of communication circuits with control objects (LV and ground processing equipment) is not fully ensured: there is no verification of the correct resistance of the circuits of actuating elements, determination of the galvanic separation of elements of the control object and their connections;

- there is no remote control without redundant inclusion of system parts necessary for the preparation of different LV models;

- there is no uninterrupted power supply for the preparatory cycle, when the power supply to the system is not from guaranteed power systems;

- there is no special automated workplace for the engineer, which provides reconfiguration of the system of the required equipment volume for the prepared LV model and frees the operators of control subsystems from collecting and diagnosing malfunctions of their own equipment;

- structure highways network exchange not exclude the presence of collisions while accessing the common link between the individual devices of the system, which significantly slows the forwarding information (to avoid collision is required network load is not more than 30%).

The problem solved by this invention is the implementation of automated preparation for flight of a family of launch vehicles (LV), consisting of models of different classes.

The invention provides remote reconfiguration of control equipment, allowing to work without any problems with any model of this LV family and perform the basic functions of preparing the LV for flight: refueling with various rocket fuel components, temperature control during the refueling period.

Due to the special danger of working with rocket fuel components (CRT) and to avoid emergency situations, equipment to ensure high reliability of the formation of control commands and trouble-free operation is reserved. The guaranteed supply of primary AC power during the test period is carried out by introducing uninterruptible power supplies into the control equipment, and during the period of connection to the system, it must be carried out from the guaranteed power supply system of the spaceport.

The technical solution to the problem lies in the fact that in an automated control system for the preparation of launch vehicles (ASUP RN), which contains automated workstations of operators (ARMO), communication devices with a fiber-optic transmission line (UFOLPI), blocks for determining functional readiness (BOFG) , communication devices with an object - technological equipment (USO), actuators for actuating actuators (USIE), discrete information input-output blocks (BVVDI), while the input-outputs of the optical signals of the first USOLPI are connected to the optical signal input-outputs of the second USOLPI, the first-fourth, sixth, tenth and fourteenth subgroups of the fifth group of ACS LV inputs from the first poles of the executive elements of the control object, the control subsystem of the elements and systems of the launch vehicle through the first-fourth subgroups, control subsystems refueling the first component of rocket fuel (SRT) through the sixth subgroup, control subsystems refueling the second SRT through the tenth subgroup, thermostat subsystems (TST) through four the twentieth subgroup is connected to pairs - the second group inputs of the corresponding BOFGs and the second group inputs of the first-seventh USO, the fifth, seventh-ninth, eleventh-thirteenth and fifteenth subgroups of the fifth group of inputs of the automated control system of control systems from the first poles of the executive elements of the control object, the fueling control subsystem of the first SRT through the fifth, seventh and eighth subgroups, fueling control subsystems of the second SRT through the ninth, eleventh and twelfth subgroups, TST subsystems through the thirteenth and fifteen the first subgroups are connected to the second group inputs of the corresponding BOFGs, the first group inputs of the second, sixth and tenth ultrasound detectors are connected to the first group outputs of the fifth-seventh USO, respectively, the fifth to fifteenth subgroups of the first group of ACSN outputs to the second poles of the actuating elements, the fueling control subsystem of the first SRT through the fifth to eighth subgroups, the fuel supply control subsystems of the second SRT through the ninth to twelfth subgroups, the TST subsystems through the thirteenth to fifteenth subgroups are connected respectively essentially with the first group outputs of the first to eleventh ultrasonic energy sources, the first to fourth, sixth, tenth and fourteenth subgroups of the sixth group of inputs of the automated control system for the control system of the rocket from the discrete sensors of the control object, the subsystem for controlling elements and systems of the launch vehicle through the first to fourth subgroups, the fueling control subsystem for the first SRT through the sixth subgroup, the fuel supply control subsystems of the second SRT through the tenth subgroup, the TST subsystems through the fourteenth subgroup are connected to the first group inputs, respectively, of the first of the seventh USO, the third groups of inputs of the first, third and fourth USO are connected respectively to the first or third subgroups of the seventh group of inputs of the automated control system of the PH from analog sensors, five additional control and communication devices (CCS) have been introduced, the first CCC with external adjacent systems on an external command paragraph (CPSU), the second CCS - with elements and systems of launch vehicles, the third CCC - with the technological equipment for refueling the first SRT, the fourth CCL - with the technological equipment for refueling the second MCT, the fifth CCL - with the technological TST equipment and external ground-based systems, a control panel for a hardware and software control subsystem (PSC APS), two network system switches (SSC), four primary power distribution devices (URPEP), the first URPEP - VKP equipment, the second UREP - equipment in the starting structure, control equipment for the distribution of secondary power supply and the control system, the third UREPP - equipment of the launch facility, providing power to the systems and actuators of the launch vehicles, the fourth UREPP - equipment start-up on the structure providing power supply to the executive elements of the technological equipment of the control object — fueling control and temperature control subsystems, the VKP primary power supply remote control device (UDUPEP-VKP), the primary power supply remote control remote control device (UDUPEP-SS), four secondary power distribution devices (URVEP ) for various models of the carrier rocket family, the first URVEP for the base model (BM) of the launch vehicle, the second URVEP for I have additional equipment for the second model of the launch vehicle (DM2), the third URVEP for the additional equipment of the third model of the launch vehicle (DM3), the fourth URVEP for the additional equipment of the fourth model of the launch vehicle (DM4), four power supply devices for actuating elements and systems (UZIES) , five software simulators for the corresponding UUS, four uninterruptible power supply devices (UBEP) for the corresponding UREP, the first group input-output of the automated control system of the launch vehicle from the inputs and outputs of the adjacent automated control system of those biological processes of ground equipment (ACS TP NO), the first group input of the automated process control system of the spacecraft from the guaranteed power supply system (SEC) of the cosmodrome, the second group input of the automatic control system of the spacecraft from the ground measurement system (SNI), the third group input of the automatic control system of the spacecraft from the single time system (SEV) are connected respectively, to the second, fourth, sixth and eighth group inputs and outputs of the first CCS, the first group input of which is connected to the first group output of the first UREP, the group inputs and outputs of the first to fifth software simulators are connected to the tenth group inputs and outputs of the corresponding CCS, the group inputs of the first to fifth software simulators are connected to the group outputs of the corresponding CCS, the ninth group input-output of the first CCC is connected to the first group input-output of the first CCK, the second to sixth group inputs and outputs of which are connected respectively to the group inputs and outputs of the first to fourth ARMO and to the first group input and output of the PSK APS panel, the group inputs of the first to fourth ARMO, the first SSK and the PSK APS panel are connected respectively to the second - the sixth and ninth group outputs of the first URPEP, the thirty-ninth group input-output of the first SSK is connected to the first group input-output of the first UVOLPI, the output of the first URPEP is connected to the first inputs of UDUPEP-VKP and the first UVOLPI, the third group input-output of UDUPEP-VKP is connected to the second group input-output of the first FIRM, the first group input-output of the UDUPEP-VKP is connected to the second group input-output of the PSK APS console, the first output of the first UBEP is connected to the second input of UDUPEP-VKP, the first group input-output of the first UBE connected to the first group input-output of the first URPEP, whose second group input-output is connected to the second group input-output of UDUPEP-VKP, the group output of the first SSK is connected to the first group input of UDUPEP-VKP, the first inputs of the second UVOLPI and UDUPEP-SS are connected to the output of the second URPEP, the first group input-output of the second USVOLPI is connected to the thirty-ninth group input-output of the second SSK, the second group input-output of the second UVOLPI is connected to the fourth group input-output of UDUPEP-SS, the first-third group inputs the passages of which are connected respectively with the second group inputs and outputs of the second-fourth UREPP, the first group input and the second-fourth inputs of the UDUPEP-SS are connected respectively to the first group output of the second SSK and to the first outputs of the second-fourth UBEP, the first group input of the second SSK is connected to the tenth group output of the second UREPP, the first-fourth group outputs of which are connected to the first group inputs of the first-fourth UREP, respectively, the fifth-eighth group outputs of the second UREP are connected to the first group output of the fourth URPEP is connected to the first group inputs of the first-fourth ultrasound device of the technological equipment of the fueling subsystem of the first SRT, the second the group output of the fourth UREP is connected to the first group inputs of the fifth to eighth ultrasonic ultrasonic sensors of the technological equipment of the fueling subsystem of the second K T, the third group output of the fourth UREPP is connected to the first group inputs of the ninth to eleventh ultrasonic measuring devices of the technological equipment of the TST subsystem, the first group inputs and outputs of the second and fourth UBEP are connected to the first group inputs and outputs of the second and fourth UREP, the first and fourth group inputs and outputs the second SSK are connected to the first group inputs and outputs, respectively, of the first to fourth URVEP, the eighth to eleventh group inputs and outputs of the second SSK are connected to the first group inputs and outputs am, respectively, of the first to fourth BOFG, the twelfth group input-output of the second SSK is connected to the ninth group input-output of the second CCS, the thirteenth to sixteenth group inputs and outputs of the second SSK are connected to the first group inputs and outputs of the fifth to eighth BFG, the seventeenth group input is the output of the second SSK is connected to the ninth group input-output of the third CCS, the eighteenth to twenty-first group inputs and outputs of the second SSK are connected to the first group inputs and outputs of the ninth to twelfth o BOPG, the twenty-second group input-output of the second SSK is connected to the ninth group input-output of the fourth CCS, the twenty third to twenty-fifth group inputs-outputs of the second SSK are connected to the first group inputs-outputs of the thirteenth to fifteenth BOFG, the twenty-sixth group input is the output of the second SSK is connected to the ninth group input-output of the fifth CCS, the twenty-seventh to thirtieth group inputs and outputs of the second SSK are connected to the first inputs and outputs of the first to fourth UZIES, thirty first to three the twenty-fourth group inputs and outputs of the second SSK are connected to the first group inputs and outputs of the first-fourth ultrasound, respectively; the thirty-fifth to thirty-eighth group inputs and outputs of the second SSK are connected to the first group inputs and outputs of the fifth to eighth ultrasound, fifth to seventh group inputs the outputs of the second SSK are connected to the first group inputs and outputs, respectively, of the ninth to eleventh ultrasound, the first and second outputs of the first URVEP connected to the first and second inputs of the first USO, respectively this output of the first URVEP is connected to the first inputs of the first, fifth, ninth and thirteenth BOPG, the fourth and fifth outputs of the first URVEP are connected respectively to the first and second inputs of the first BVVDI, the sixth and seventh outputs of the first URVEP are connected to the first and second inputs of the fourth BVVDI, eighth and the ninth outputs of the first URVEP are connected respectively to the first and second inputs of the seventh BVVDI, the first and second outputs of the second URVEP are connected respectively to the first and second inputs of the second USO, the third output is second The first URVEP is connected to the first inputs of the second, sixth, tenth and fourteenth BOFG, the fourth and fifth outputs of the second URVEP are connected respectively to the first and second inputs of the fifth USRO, the sixth and seventh outputs of the second URVEP are connected to the first and second inputs of the sixth USO, the eighth and ninth, respectively the outputs of the second URVEP are connected respectively to the first and second inputs of the seventh USO, the first and second outputs of the third URVEP are connected respectively to the first and second inputs of the third URES, the third output of the third URVEP is connected nen with the first inputs of the third, seventh, eleventh and fifteenth BOFG, the fourth and fifth outputs of the third URVEP are connected respectively to the first and second inputs of the second BVVDI, the sixth and seventh outputs of the third URVEP are connected respectively to the first and second inputs of the fifth BVVDI, the eighth and ninth outputs of the third URVEP connected respectively to the first and second inputs of the eighth BVVDI, the first and second outputs of the fourth URVEP are connected respectively to the first and second inputs of the fourth USO, the third output of the fourth URVEP under it is connected to the first inputs of the fourth, eighth and twelfth BOFG, the fourth and fifth outputs of the fourth URVEP are connected respectively to the first and second inputs of the third BVVDI, the sixth and seventh outputs of the fourth URVEP are connected to the first and second inputs of the sixth BVVD, the first, third, fifth and seventh the group inputs and outputs of the second CID are connected to the first group inputs and outputs of the first to fourth CCD, the second, fourth, sixth and eighth group inputs and outputs of the second CSC are connected respectively to the fourth subgroups of the fourth group of inputs and outputs of the automated control system for the launch vehicle with sequential codes of the systems of the first to fourth models of the carrier rocket family, the first group outputs of the first to fourth ultrasonic sensors are connected to the first group inputs of the corresponding BOFGs and, respectively, to the first and fourth subgroups of the second poles of the actuating elements of the first the group output of the automated control system of the launch vehicle in the subsystem for controlling the elements and systems of the launch vehicle, the second group inputs and outputs of the first and fourth ultrasonic sensors are connected to pairs - the fourth the main inputs of the corresponding BOFGs and to the corresponding first to fourth subgroups of the third group input-output of the automated control system of the control system for power supply to the systems of the first and fourth models of the carrier rocket family, the first group inputs of the first to seventh USO are additionally connected to the third group inputs of the first, fourth, sixth, tenth and fourteenth BOFG, the second group inputs of the first to fourth UZIES are connected to the first group outputs of the corresponding USO, the third group inputs of the first, third and four of this USO are additionally connected to the fifth group inputs of the corresponding BOFGs, the first, third, fifth and seventh group inputs and outputs of the third CCS are connected to the first group inputs and outputs of the first BVVDI, fifth USO, second and third BVVDI, the first group inputs of the fifth to fifteenth BOFG additionally connected respectively to the first group outputs of the first to eleventh ultrasound, the first group outputs of the first to eighth BVVDI connected to the first group inputs respectively of the first, third to fifth, of the seventh-ninth and eleventh ultrasound detectors, the first group inputs of the first to eighth BVVDI are connected respectively to pairs - the fifth, seventh, ninth, eleventh-thirteenth and fifteenth subgroups of the sixth group input of the automated control system of pH from discrete sensors and the third group inputs of the fifth, seventh, seventh and seventh eleventh-thirteenth and fifteenth BOFG, the second group inputs of the fifth, seventh-ninth, eleventh-thirteenth and fifteenth BOFG are additionally connected to the second group inputs respectively Actually, the first to eighth BVVDI, the first, third, fifth, and seventh group inputs and outputs of the fourth CID are connected respectively to the first group inputs and outputs of the fourth BVVDI, the sixth CIRCU, the fifth and sixth BVVDI, the first, third, and fifth group inputs and outputs of the fifth CID are connected respectively, to the first group input-output of the seventh BVVDI, the eighth group input of the automated control system of the control system from the system for measuring the parameters of the technological object (SIPTO), the first group inputs and outputs of the seventh USVO and eighth BVVDI, the second group input - the output of the ASUP RN from the ground-based automated control system of the launch vehicle (NASU RN) is connected to the second group input-output of the seventh BVVDI and the fourth group input of the thirteenth BOFG, the third group output of the ASUP RN to the single time system (SEV) at the starting position is connected to the second group output of the seventh BVVDI and to the fifth group input of the thirteenth BOFG.

In the automated control system for control systems, the control panel for the hardware and software control subsystem (PSK APS) contains three monitors, three system units, three universal keyboards, three mouse buttons, three network switches, two automatic transfer switches, three USB port switches, and three network adapters from USB output and a printer, the first and second power supply networks of the first group input of the PSA APS remote control are connected respectively to the first and second inputs of two reserve input machines, the output of the first machine is connected to the first input of the first network switch, to the first inputs of the first and third system units, the first and third monitors, the first and third USB port switches, the output of the second machine is connected to the first inputs of the second and third network switches, the printer, the second monitor, the system unit and the port switch, the first and second buses of the first group input the outputs of the PSK APS console are respectively connected to the first inputs and outputs of the first and second switches, the first inputs and outputs of the first to third system units are connected to the first inputs and outputs of the first and third monitors Orov, the second inputs and outputs of the first-third system units are connected to the first inputs and outputs of the first to third network adapters, the third and fifth inputs and outputs of the first and third system units are connected respectively to each other and to the corresponding first inputs and outputs of the first to third port switches, the second inputs and outputs of the first to third network adapters are connected respectively to the first and third buses of the second group I / O of the PSK APS console, the second inputs and outputs of the first and second network switches are connected are connected respectively with the sixth and seventh input-output of the first system unit, the third inputs and outputs of the first and second network switches are connected to the sixth and seventh inputs and outputs of the second system unit, the fourth inputs and outputs of the first and second network switches are connected to the sixth and seventh, respectively the inputs and outputs of the third system unit, the fifth inputs and outputs of the first and second network switches are connected respectively to the first and second inputs and outputs of the third network switch, the third input-output of which th connected to the input-output of the printer, the first-third universal keyboard connected to a second input-output respectively first through third switch ports, the first to third manipulators "mouse" coupled to the third input-output respectively first through third switch ports.

In the automated control system for control systems, the control unit for communication and control of the control system contains two network switches, three bus lines, a fault collection unit, a central processor, a multi-channel power supply MIEP and three multi-channel interface cards MIK, the first, third, fifth and seventh group inputs / outputs of the control system have two buses of the local area network, the first of which are connected respectively to the seventh, sixth, fifth and fourth inputs and outputs of the first network switch, the second buses of these inputs and outputs are connected to the seventh, respectively The fifth, fourth and fourth inputs and outputs of the second network switch, the input-output of the fault collection unit is connected to the first inputs and outputs of the first and second network switches, the first inputs of the first and second network switches are connected to the second bus of the first group input of the CCS, the first bus of the first group the UUS input is connected to the MIEP input, both buses, the first and second, are connected to the corresponding buses of the first group input of the central processor, the first group inputs of the first and second network switches are connected to the group m MIEP output, which is also connected by a bus of one of the output ratings to the input of the fault collection unit, the second group input-output of the UCS, as well as the fourth, sixth and eighth inputs and outputs, consists of three subgroups of inputs and outputs connected respectively to the first group inputs-outputs of the first-third MIC, three subgroups of inputs and outputs of the fourth group input-output of the CCS are connected to the second group inputs and outputs of the first-third MIC, three subgroups of the inputs-outputs of the sixth group input-output of the CCC are connected respectively However, with the third group inputs and outputs of the first to third MICs, three subgroups of inputs and outputs of the eighth group input-output of the MCS are connected respectively to the fourth group inputs and outputs of the first and third MICs, the first and third subgroups of the second group input and output, and the corresponding subgroups of the second group the input of the central processor through the bus input / output lines are connected respectively to the fifth group inputs-outputs of the first to third MICs, the first and second buses of the third group input-output of the central percent The essors are connected respectively to the second inputs and outputs of the first and second network switches, the third inputs and outputs of which are connected respectively to the first and second buses of the ninth group input-output of the CCS, the first and second buses of the input-output of the tenth group input-output of the CCC are connected to the first group the input / output of the central processor, the first group output of the central processor is connected to the first group output of the control system, the first outputs of the first and third MICs and the second MIEP output are connected to the corresponding buses of the first load ppovogo input node failure collection.

In the automated control system for control systems, the primary power distribution device UREPP contains an automatic transfer switch input switch, a control mode switch, two phase control relays, two network switches, two electric contactors, two contact groups of the corresponding electric contactors, two secondary power supply sources of IWEP, twenty individual automatic machines, two emergency switching units , the first bus power supply of the first group input UREPP connected to the first inputs of the first relay phase control, the first node emergency switch of the first network switch and with the input of the first IVEP, the second mains supply bus of the first group input of the UREP is connected to the first inputs of the second phase control relay, the second emergency switching node, the second network switch and to the input of the second IVEP, the input bus of the first group input-output UREP connected to the second inputs of the first and second emergency switching nodes, the output bus of the first group input-output URPEP connected to the output of the ATS, the first and second inputs of which are connected respectively to ne the outputs of the first and second network switches, the second outputs of which are connected and connected to the "ABP connected" bus of the subgroup of the status outputs of the second group input-output URPEP, the outputs of the first and second phase monitoring relays are connected respectively to the buses "Norm 380/220 V1" and " Norm 380/220 B2 "subgroup of the outputs of the states of the second group input of the UREP, the first output of the first IHEP is connected to the bus" IWEP1 is on "of the subgroup of the outputs of the states of the second group input-output of the UREP and combined with the first output of the second IWEP, which it is connected to the bus "IVEP2 included" subgroups of the state outputs of the second group input-output URPEP, the combined outputs of the first and second IVEP are connected to the second inputs of the first and second electric contactors and to the bus of the positive pole of the output UREPP of the standby DC voltage, the second outputs of the first and second IVEP combined and connected to the first input of the control mode switch and to the negative pole bus of the first output of the URPEP of the standby DC voltage, the input bus of the second group input command yes, the output of the control mode switch is connected to the second input of the control mode switch, the second and third outputs of which are connected respectively to the "Remote control" and "Local control" buses of the subgroup of state outputs of the second group input-output control loop, the first output of the control mode switch is connected to the first inputs of the first and the second electric contactors, the outputs of which are galvanically connected to the second inputs of the respective contact groups, the output of the first emergency switching unit is connected to the first input of the contact group and to the input of the ninth individual machine, the output of the second emergency switching unit is connected to the input of the second contact group and to the input of the nineteenth individual machine, the outputs of the ninth and nineteenth individual machines are connected to the first and second buses of the ninth group output of the standby AC voltage, the first outputs the first and second contact groups are connected respectively to the bus "Enabled 220 V 1" and "Enabled 220 V 2" subgroups of the outputs of the status of the second group input-you UREPP, the second outputs of the first and second contact groups are respectively connected to the inputs of the groups of individual machines of the first group of the first to eighth, tenth machines and the second group of the eleventh to eighteenth, twentieth machines, the outputs of the first to eighth and tenth individual machines are connected to the first buses, respectively, of the first of the eighth and tenth group outputs of the UREP, the outputs of the individual automata of the eleventh to eighteenth and twentieth are connected to the second buses of the first to eighth and 10th group outputs of UREPP.

In the automated control system for control systems, the network system switch SSK contains four network switches, two multichannel power sources MIEP, two circuit breakers, the first buses of the first to twenty-fourth group I / O of the SSK are connected to the corresponding inputs and outputs of the first network switch, the first buses of the twenty-fifth to thirty-eighth group inputs and outputs are connected to the corresponding first to fourteenth inputs and outputs of the second network switch, the second buses of the first to twenty-fourth group inputs and outputs CCK with are connected to the corresponding inputs and outputs of the third network switch, the second buses of the twenty-fifth to thirty-eighth group inputs and outputs of the CCK are connected to the corresponding first to fourteenth inputs and outputs of the fourth network switch, the twenty-fifth inputs and outputs of the first and second network switches are combined and connected to the first the bus of the thirty-ninth SSK I / O, the twenty fifth inputs and outputs of the third and fourth network switches are combined and connected to the second bus of the thirty-ninth SSK I / O, the first bus the first group input of the SSK is connected to the input of the first circuit breaker, the second bus of the first group input of the SSK is connected to the input of the second circuit breaker, the first output of the first circuit breaker is connected to the inputs of the first and second MIEP, the first output of the second circuit breaker is connected to the second inputs of the first to fourth switches network, the output of the first MIEP is connected to the first inputs of the first and second switches of the network and with the bus "MIEP 1 is on" of the first group output SSK, the output of MIEP connected to first inputs of the third and fourth switches and to network bus "included MIEP 2" of the first group output CCK second outputs of the first and second circuit breakers respectively connected to buses "Enabled feeder 1" and "Enabled feeder 2 '.

In the automated control system for control systems, the remote control device for primary power supply at the remote command post UDUPEP-VKP contains three network switches, three elements of galvanic isolation of power supply EGREP, a node of the majority of VME elements, three interface relay modules IRM, six input / output modules MVV, the first input UDUPEP-VKP connected to the inputs of the first to third EHEC, the output of the first EHEC is connected to the inputs of the first and second MVV and the first network switch, the output of the second EHED is connected to the inputs of the third and fourth MVV and the second comm network tator, the output of the third EDGE is connected to the inputs of the fifth and sixth MVV and the third network switch, the first group input of the UDUPEP-VKP is connected to the group inputs of the first, third, and fifth MVV, the inputs and outputs of which are connected to the fourth inputs and outputs of the first and third switches network, three subgroups of the first group input-output UDUPEP-VKP are connected to the fifth input-output, respectively, of the first-third network switches, a subgroup of inputs of the second group input-output UDUPEP-VKP is connected to the first sub memory inputs of the second, fourth and sixth MVV, a subgroup of outputs of VME connected to the buses of the subgroup of outputs of the second group input-output UDUPEP-VKP, the first to third group inputs of VME connected respectively to the second group outputs of the first to third IRM, group inputs and first group outputs of the first Third IRM are connected respectively to group outputs and second subgroups of group input, respectively, of the second, fourth and sixth MVV, inputs and outputs of the second, fourth and sixth MVV are connected to third inputs and outputs respectively, first and third switches in the network, a second input UDUPEP-ACP is connected to the second input-output of the first switch network, the first input-output of the first-third switches network connected respectively to the first to third sub-groups of the third group IO inputs-outputs UDUPEP-MAC.

The primary power supply remote control device in the start-up facility of the UDUPEP-SS contains three network switches, three galvanic isolation elements of the power supply of the EGREP, three nodes of the UME majority elements, nine IRM interface relay modules, twelve MVV input-output modules, the first input of the UDUPEP-SS is connected to the inputs EGREP, the output of the first EGREP is connected to the inputs of the first network switch and the first to fourth MVV, the output of the second EGREP is connected to the inputs of the second network switch and the fifth to eighth MVV, the third output of the first EGREP is connected to the inputs of the third network switch and the ninth to twelfth MVV, the first group input of the UDUPEP-SS is connected to the group inputs of the first, fifth and ninth MVV, the outputs of which are connected to the fifth inputs-outputs of the first and third network switches, the second and fourth inputs UDUPEP-SS are connected respectively with the ninth, eighth and seventh inputs-outputs of the first network switch, a subgroup of inputs of the first group input-output UDUPEP-SS is connected to the first subgroups of inputs of the second, sixth and tenth MVV, pa outputs of the first VME is connected to a subgroup of outputs of the first group input-output UDUPEP-SS, a subgroup of inputs of the second group input-output of UDUPEP-SS is connected to the first subgroup of inputs of the third, seventh and eleventh MVV, the group of outputs of the second VME is connected to a subgroup of outputs of the second group input -output UDUPEP-SS, a subgroup of inputs of the third group input-output UDUPEP-SS is connected to the first subgroups of inputs of the fourth, eighth and twelfth MVV, the group of outputs of the third VME is connected to the subgroup of outputs third of the first group input-output UDUPEP-SS, the first-third group inputs of the first VME are connected respectively to the second group outputs of the first, seventh and fourth IRM, the first and third group inputs of the second VME are connected respectively to the second group outputs of the fifth, second and eighth IRM, the first the third group inputs of the third VME are connected respectively to the second group outputs of the third, sixth and ninth IRM, the group inputs and the first group outputs of the first-third IRM are connected respectively to the group outputs the second subgroups of inputs of the second-fourth MVV, respectively, the group inputs and the first group outputs of the fourth-sixth IRM are connected respectively to the group outputs and the second subgroup of inputs of the sixth-eighth MVV, respectively, the group inputs and the first group outputs of the seventh-ninth IRM are connected respectively to the group outputs and the second subgroups of inputs of the tenth to twelfth MVV, respectively, the inputs and outputs of the second-fourth MVV are connected respectively to the fourth, third and second inputs-outputs the first network switch, the inputs and outputs of the sixth-eighth MVV are connected respectively to the fourth, third and second inputs and outputs of the second network switch, the inputs and outputs of the tenth to twelfth MVV are connected to the fourth, third and second inputs and outputs of the third network switch, the first inputs - the outputs of the first to third network switches are connected, respectively, with the first and third subgroups of the fourth group input-output UDUPEP-SS.

The secondary power distribution device URVEP contains two network switches, three multi-nominal low-voltage power sources MIEP-N, an electric contactor, a time relay, three peripheral processors, three discrete data normalizers, three FSU control signal formers, a majority of VME elements, ten electric power sources, three bus lines M1, M2, M3, the first subgroup of the group input of the UREP is connected to the first inputs of the time relay, electrical contactor and tenth IED, the second subgroup of RUREP group input is connected to the second inputs of the time relay, the electric contactor and the tenth IED, the first and second outputs of the time relay are connected respectively to the third and fourth inputs of the electric contactor, whose first output is connected to the first inputs of the first to ninth IEDs, the second output of the electric contactor is connected to the second inputs of the first -the ninth IEP, the outputs of the first to third MIEP-N are connected respectively to the first to third bus highways, the first highway is connected to the group inputs and outputs of the first peripheral processor, ND D, FSU and with the first input of the first processor, the second highway is connected to the group inputs and outputs of the second peripheral processor, NDD, FSU and the first input of the second processor, the third highway is connected to the group inputs and outputs of the third peripheral processor, NDD, FSU and the first the input of the third processor, the first inputs and outputs of the first to third peripheral processors are connected respectively to the second and fourth inputs and outputs of the first network switch, the second inputs and outputs of the first to third peripheral processors are connected s, respectively, with the second-fourth inputs and outputs of the second network switch, the inputs of both network switches and the first-third MIEP-N are connected to the output of the tenth IED, the group output of the tenth IEP is connected to the tenth subgroup of the group inputs of the first to third NII, the group inputs of the first to ninth IEDs are connected respectively to the first to ninth subgroups of the VME output, group outputs of the first to ninth IEDs are connected respectively to the first to ninth subgroups of the group inputs of the first to third NDIs, group outputs of the first to third FS U are connected respectively to the first or third group inputs of VMEs, the outputs of the first to ninth IES are connected respectively to the first to ninth outputs of the URVEP, the first inputs and outputs of the first and second switches of the network are connected respectively to the first and second subgroups of the input and output of the URVEP.

The power supply device for the actuating elements and systems of the ultrasonic electric power station contains an automatic transfer switch for automatic transfer switch backup, a secondary power supply source for electric power supply, an input-output module MVV, two power sources for electric power supply, four electronic keys, the first subgroup of the first group input of the electronic power supply connected to the first inputs of the automatic power supply, first and second electric power supply, the second subgroup of the first group input of the UZIES is connected to the second inputs of the ATS, the first and second IES, the output of the ATS is connected to the input of the IES, whose output is connected to the inputs of the MVV and the first to fourth electronic keys, four the outputs of the group output states of the first IED are connected to the corresponding first-fourth inputs of the MVV group input, the outputs of the positive and negative voltage poles of the first IED are multiplied and connected by multiconductor buses to the first group output and the second group input of the ultrasonic generator, the first and second inputs of the group input of the first IED are connected respectively, with the outputs of the first and second electronic keys, the inputs of which are connected respectively to the first and second outputs of the group output MVV, in e four status outputs of the group output of the second IED are connected respectively to the fifth or eighth inputs of the MVV group input, the outputs of the positive and negative voltage poles of the second IED are multiplied and the multi-wire busbars are connected respectively to the subgroup of outputs and the subgroup of inputs of the second group input-output of the UZIES, the first and second inputs the group input of the second IED are connected respectively to the outputs of the third and fourth electronic keys, the inputs of which are connected respectively to the third and fourth output It is output MBB group, a group of input-output LEV connected to the second input-output of the group UZIES.

A communication device with an object - USOTO technological equipment, contains three multi-nominal low-voltage power sources MIEP-N, three peripheral processors, three bus lines M1 ÷ M3, three normalizers of discrete data of NDD, three shapers of control signals of FSD, three multi-channel analog-to-digital converters of MACP, k intrinsic safety barriers of discrete BIDS signals, p IEC majority key elements, m INAI intrinsically safe analog information normalizers, the first input of the USOE is connected to the first inputs Ami of the first-third MIEP-N, the first-third NDD, the first-third FSD and the first-third MACP, three subgroups of the first group input-output USO are connected respectively to the pairs - the first and second inputs-outputs of the first-third peripheral processors, the second input USO is connected to the second inputs of the first-third NDD, the first inputs k BIDS and the first inputs m INAI, the outputs of the first and third MIEP-N are connected to the corresponding bus lines M1 ÷ M3, the group inputs and outputs of the processors and their first inputs are connected respectively to by a third or third bus line, the first NDD, FSU and MATsP group inputs and outputs are connected to the first bus line, the second NDD, FSU and MatsP group inputs and outputs are connected to the second bus line, the third NDD, FSU and MatsP group inputs and outputs are connected to of the third bus line, the inputs from the first to the k-th first group input of the USO are connected to the inputs of the corresponding first - k-th BIDS, the outputs of which are connected to the corresponding inputs of the group input of the first-third NDI, inputs from the first to the p-th second group The first input of the USO is connected to the fourth inputs of the corresponding first - pth IEC, the outputs of which are connected to the corresponding outputs of the group output of the USO, the outputs from the first to the pth first to third FSO are connected to the first to third inputs of the corresponding IEC so that any n the first-third FSU output is connected respectively to the first-third inputs of the n-th IEC, the inputs from the first to the m-th of the third group input are connected to the inputs of the first - m-th INAI, each output of which is connected to the corresponding input the first to third Matzpen.

The functional readiness determination unit BOFG contains a bus line, a multi-nominal power supply source MIEP, a processor, a measuring power supply source IIEP, four electronic keys, a driver for FSU control signals, two switches for analogue UAS signals, a node for operating modes of the OAI, four measuring transducers, a multi-channel analog-to-digital converter MATsP, controlled voltage divider UDN, the first input of the BOFG is connected to the inputs of IIEP and MIEP, the first and second outputs of IIEP connected respectively to the first input of the UDN and the first input of the first electronic key, the output of which is connected to the eighth input of the UDN, the second input of the first electronic key is connected to the first single output of the first group output of the FSU, the group output of the MIEP is connected to the bus line M1, the group input-output of the processor and its first input is connected via a bus line to the group inputs and outputs of the FSU and the MASP and their second inputs, the first input-output of the processor is connected to the input-output of the BOFG, the first to fifth group inputs of the BOFG are connected respectively to the first to fifth subgroups of inputs of the second group input of the first and second UAN, the first group outputs of which are connected respectively to the first and second subgroups of the outputs of the first group output of the FSU, the outputs of the first and second UAN are connected respectively to the first and third inputs of the OAI, the first to fifth outputs of which are connected respectively, with the third-seventh inputs of the UDN, the second input of the OCR is connected to the bus of the BOFG housing, the first group input of the OCR is connected to the sixth group input of the BOFG, the second group input of the OCR is connected to the third under the group of outputs of the first group output of the FSO, the first group input of the UDI is connected to the fourth subgroup of the outputs of the first group output of the FSU, the first output of the UDN is connected to the second input of the fourth measuring transducer, the output of which is connected to the fourth single input of the first group input of the MACP, the first input of the fourth measuring transducer is connected to the eighth single output of the first group output of the FSU, the third input of the fourth measuring transducer is connected to the third inputs of the first or third measuring transducers, the first input of the second electronic key and the second output of the UDN, the first input of the first measuring transducer is connected to the fifth single output of the first group output of the FSU, the output of the first measuring transducer is connected to the third single input of the first group input of the MACP, the third output of the UDN is combined with the output of the second electronic key and connected to the second input of the first measuring transducer, the first input of the second measuring transducer is connected to the sixth single the output of the first group output of the FSU, the second inputs of the second to fourth electronic keys are connected respectively to the second and fourth single outputs of the first group output of the FSU, the first input of the third electronic key is connected to the fourth output of the UDN, the fifth output of which is combined with the output of the third electronic key and connected to the second input of the second measuring transducer, the output of which is connected to the second single input of the second group input of the MACP, the first input of the third measuring transducer p it is connected to the seventh single output of the first group output of the FSU, the output of the third measuring transducer is connected to the first single input of the first group MASP, the second input of the third measuring transducer is connected to the seventh output of the UDN, the sixth output and the second input of the UDN are connected respectively to the first input and the output of the fourth electronic key .

Introduction of five control and communication devices, a PSK APS console, two network system switches, four primary power distribution devices, two primary power remote control devices, four secondary power distribution devices, four power supply devices for executive elements and systems into an automated control system for the preparation of launch vehicles a booster rocket, five software simulators, four uninterruptible power supply devices and the corresponding combination of It, known and newly introduced, for connecting the blocks and devices included in the restrictive and distinctive parts of the formula, does not allow the redundancy of the equipment necessary to control the preparation of all models of the carrier rocket family, allows you to more fully determine the functional readiness of the system's communications with the control objects, and verify the correctness regular work programs for preparing launch vehicles for launch, to coordinate the work of related systems at the remote command post and at the launch position, allows for Preparing launchers do not expend energy resource means boosters, provides remote control by including parts of the system.

The operation of the system will be clear from the drawings presented in figures 1-30:

figure 1 presents a diagram of an automated control system for the preparation of launch vehicles;

figure 2 presents a diagram of a workstation operator;

figure 3 presents a diagram of the remote control PSK APS;

figure 4 presents a diagram of a control and communication device (CCS);

figure 5 presents a diagram of a central processor from a control and communication device;

figure 6 presents a diagram of a software simulator;

figure 7 presents a diagram of a primary power distribution device (URPEP);

on Fig presents a diagram of an uninterruptible power supply (UBEP);

figure 9 presents a diagram of a network system switch (SSK);

figure 10 presents a diagram of a device for remote control of primary power at a remote command post (UDUPEP-VKP);

figure 11 presents a diagram of a device for remote control of primary power in a launch facility (UDUPEP-SS);

on Fig presents a diagram of a communication device with a fiber optic data transmission line (USVOLPI);

on Fig presents a diagram of a device for the distribution of secondary power supply (URVEP);

on Fig presents a block diagram determining the functional readiness (BOFG);

on Fig presents a diagram of a device for powering the Executive elements and systems of the launch vehicle (UZIES);

on Fig presents a diagram of a device for launching actuating elements of technological equipment (USIE);

on Fig presents a diagram of a communication device with an object - technological equipment (USO);

on Fig presents a diagram of a block input-output discrete information (BVVDI);

on Fig presents a diagram of an intrinsically safe normalizer of analog information from the USOTO (INAI);

on Fig presents a diagram of the intrinsic safety barrier of discrete signals from the structure USOTO (BIDS);

on Fig presents a diagram of a power source (IEP);

on Fig presents a diagram of the node modes of operation from the unit for determining the functional readiness (OA);

on Fig presents a diagram of a controlled voltage divider from the composition of the determination of functional readiness (UDN);

on Fig presents a diagram of a normalizer of discrete data from the composition of USO and BVVDI (NDD);

on Fig presents a diagram of a driver of control signals from the composition of USO and BVVDI (FSU);

on Fig presents a diagram of a multi-channel analog-to-digital Converter from the composition of USOTO (MASP);

on Fig presents a diagram of a majority element - a key from the composition of USOTO and BVVDI (IEC);

on Fig presents a graph diagram of the algorithm reconfiguration of the system;

on Fig presents a graph diagram of the mode of electrical checks of the base module;

on Fig presents a graph diagram of the General mode of electrical checks for all models of the family of launch vehicles.

The automated control system for the preparation of launch vehicles (ASUP RN) (Fig. 1) contains four automated workstations of operators (ARMO) 2-1 ÷ 2-4, two communication devices with a fiber optic data transmission line (USVOLPI) 8-1, 8-2, fifteen blocks of determination of functional readiness (BOFG) 12-1 ÷ 12-15, seven communication devices with the object - technological equipment (USO) 13-1 ÷ 13-7, eleven devices for launching actuating elements (USE) 16-1 ÷ 16-11, eight blocks of input-output of discrete information (BVVDI) 15-1 ÷ 15-8, five devices communications and communications (CCS) 1-1 ÷ 1-5, the first CCC 1-1 - with external adjacent systems, the second CCC 1-2 - with the elements and systems of launch vehicles, the third CCC 1-3 - with the technological equipment for refueling the first component of rocket fuel (CRT), the fourth УУС 1-4 - with the technological equipment for refueling the second КРТ, the fifth УУС 1-5 - with the technological equipment for thermostating and external ground systems at the starting position, the PSK APS 10 console, two network system switches (SSK) 6-1, 6-2, four primary power distribution devices UR ЭП 4-1 ÷ 4-4, the first УРПЭП 4-1 - equipment of the remote command post (VKP), the second УРПЭП 4-2 - the equipment in the launch facility, the control equipment for the distribution of secondary power supply and the УУС 1-2 ÷ 1-5, the third UREPP 4-3 - equipment of the launch facility, providing power to the systems and actuators of the launch vehicles, the fourth UREP 4-4 - equipment of the launch facility, providing power to the actuators of the process equipment of the control object - fueling and temperature control subsystems, primary control power supply remote control device VKP (UDUPEP-VKP) 7, primary launch remote control power supply device (SS) (UDUPEP-SS) 11, four secondary power distribution devices (URVEP) for various models of the carrier rocket family, the first URVEP 9- 1 for the base model (BM), the second URVEP 9-2 for the additional equipment of the second model of the launch vehicle (DM2), the third URVEP 9-3 for the additional equipment of the third model of the launch vehicle (DM3), the fourth URVEP 9-4 for the additional equipment of the fourth model of the launch vehicle (DM4), four power supply devices for actuating elements and systems of the launch vehicle (UZIES) 14-1 ÷ 14-4, five program simulators (PI) for the corresponding control devices 3-1 ÷ 3-5, four uninterruptible power supply devices (UBEP) for the corresponding UREPP 5-1 ÷ 5-5, the inputs and outputs of the optical signals 4 of the first USVOLPI 8-1 are connected to the inputs and outputs of the optical signals 4 of the second UVOLPI 8-2, the first-fourth, sixth, tenth and fourteenth subgroups of the fifth group of inputs 8-1 ÷ 8-4, 8-6, 8-10 and 8-14 ACS from the first poles of individual elements (IE) of the control object, the subsystem “LV elements and systems” through the first and fourth subgroups 8-1 ÷ 8-4, the control subsystem “TO 1 KRT” through the sixth subgroup 8-6, the control subsystem “TO 2 KRT” through the tenth subgroup 8-10, thermostat subsystems “TO TST” through the fourteenth subgroup 8-14 are connected to pairs - the second group inputs 4 of the corresponding BOFGs 12-1 ÷ 12-4, 12-6, 12-10 and 12-14 and the second group inputs 6, respectively, USO 13-1 ÷ 13-7, fifth, seventh-ninth, eleventh-thirteenth and fifteenth subgroups of the fifth group of inputs 8-5, 8-7 ÷ 8-9, 8-11 ÷ 8-13 and 8-15 of the automated control system of the launch vehicle from the first poles of the IE of the control object, the control system for refueling the first SRT through the fifth, seventh and eighth subgroups 8-5, 8- 7, 8-8, fueling control subsystems of the second SRT through the ninth, eleventh and twelfth subgroups 8-9, 8-11 and 8-12, thermostatting subsystems through the thirteenth and fifteenth subgroups 8-13 and 8-15 are connected to the second group inputs 4 the corresponding BOFGs 12-5, 12-7 ÷ 12-9, 12-11 ÷ 12-13 and 12-15, the first group inputs 3 of the second, sixth and tenth USI 16-2, 16-6 and 16-10 are connected to the first group outputs 5 respectively, the fifth-seventh USOUT 13-5 ÷ 13-7, the fifth-fifteenth subgroups of the first group of outputs 9-5 ÷ 9-15 ACSN of the LV to the second poles of the IE, the fueling control subsystem of the first SRT “TO 1 KRT” through the fifth-eighth subgroup 9 -5 ÷ 9-8, fueling control subsystems of the second SRT “TO 2 KRT” through the ninth to twelfth subgroups 9-9 ÷ 9-12, thermostatting subsystems “TO TST” through the thirteenth to fifteenth subgroups 9-13 ÷ 9-15 are connected respectively with the first group outputs 4 of the first to eleventh ultrasonic ultrasonic analysis 16-1 ÷ 16-11, the first-fourth, sixth, tenth and fourteen I am the subgroup of the sixth group of inputs of the automated control system for the control systems of the pH 10-1 ÷ 10-4, 10-6, 10-10 and 10-14 from the discrete sensors (DD) of the control object, the subsystem "elements and systems of the LV" through the first and fourth subgroups 10-1 ÷ 10-4, the control subsystem “TO 1 KRT” through the sixth subgroup 10-6, the control subsystems “TO 2 KRT” through the tenth subgroup 10-10, the thermostat subsystems “TO TST” through the fourteenth subgroup 10-14 are connected to the first group inputs 4 respectively of the first-seventh USO 13-1 ÷ 13-7, the third group of inputs 7 of the first, third and fourth USO 13-1, 13-3 and 13-4 are connected with Accordingly, with the first-third subgroups of the seventh group of inputs of the automated control system of the control system RN 11-1 ÷ 11-3 from analog sensors (YES), the first group input-output 1 of the automatic control system of the control system RN from the group of inputs and outputs of the adjacent automated process control system for ground equipment ), the first group input 2 of the control system of the LV from the guaranteed power supply system (SEC) of the cosmodrome, the second group input 3 of the automatic control system of the LV from the ground-based measurement system (SNI), the third group input 4 of the automatic control system of the LV from the single time system (SEV) are connected respectively to the secondthe fourth 4, sixth 6 and eighth 8 group inputs and outputs of the first UUS 1-1, the first group input 10 of which is connected to the first group output 3 of the first UREP 4-1, group inputs and outputs 2 of the first to fifth software simulators 3-1 ÷ 3 -5 are connected to the tenth group inputs and outputs 11 of the corresponding CCS 1-1 ÷ 1-5, group inputs 1 of the first to fifth software simulators 3-1 ÷ 3-5 are connected to the first group outputs 12 of the corresponding CCS 1-1 ÷ 1-5 , the ninth group input-output 9 of the first CCS 1-1 is connected to the first group input-output 1 of the first CCK 6-1, sec the sixth group inputs-outputs 2-6 of which are connected respectively to the group inputs-outputs 2 of the first to fourth ARMO 2-1 ÷ 2-4 and to the first group input-output 2 of the PSK APS 10 panel, group inputs 1 of the first to fourth ARMO 2-1 ÷ 2-4, group input 40 of the first SSK 6-1 and group input 1 of the PSK APS 10 panel are connected respectively to the second-sixth 4 ÷ 8 and ninth 11 group outputs of the first UREP 4-1, the thirty-ninth group input-output 39 of the first SSK 6-1 is connected to the first group input-output 2 of the first USVOLPI 8-1, the output 12 of the first URPEP 4-1 is connected to the first inputs 1 UDUPEP-VKP 7 and the first USVOLPI 8-1, the third group input-output 6 UDUPEP-VKP 7 is connected to the second group input-output 3 of the first UVOLPI 8-1, the first group input-output 3 UDUPEP-VKP 7 is connected to the second group input-output 3 of the PSK APS 10 console, the first output 1 of the first UBEP 5-1 is connected to the second input 5 of UDUPEP-VKP 7, the first group input-output 2 of the first UBEP 5-1 is connected to the first group input-output 2 of the first UREP 4-1, whose second group input-output 13 is connected to the second group input-output 4 UDUPEP-VKP 7, group output 41 p the first SSK is connected to the first group input 2 UDUPEP-VKP 7, the first inputs 1 of the second UVOLPI 8-2 and UDUPEP-SS 11 are connected to the output 12 of the second URPEP 4-2, the first group input-output 2 of the second UVOLPI 8-2 is connected to thirty the ninth group input-output 39 of the second SSK 6-2, the second group input-output 3 of the second USVOLPI 8-2 is connected to the fourth group input-output 9 of UDUPEP-SS 11, the first-third group input-outputs 3 ÷ 5 of which are connected respectively the second group inputs and outputs 13 of the second to fourth UREPP 4-2 ÷ 4-4, the first group input 2, W the fourth fourth inputs 6 ÷ 8 of the UDUPEP-SS are connected respectively to the first group output 41 of the second SSK 6-2 and to the first outputs 1 of the second and fourth UBEP 5-2 ÷ 5-4, the first group input 40 of the second SSK 6-2 is connected to the tenth group output 14 of the second UREPP 4-2, the first-fourth group outputs 3 ÷ 6 of which are connected to the first group inputs 10 of the first-fourth UREP 9-1 ÷ 9-4, the fifth-eighth group outputs 7 ÷ 10 of the second UREP 4-2 connected to the first group inputs 10, respectively, of the second to fifth CCS 1-2 ÷ 1-5, the first to fourth group outputs 3 ÷ 6 of the third UREPP 4-3 connected to the first group inputs 1, respectively, of the first-fourth UZIES 14-1 ÷ 14-4, the first group output 3 of the fourth UREP 4-4 connected to the first group inputs 1 of the first-fourth UZIE 16-1 ÷ 16-4, the second group output 4 of the fourth UREP 4-4 is connected to the first group inputs 1 of the fifth to eighth UZIES 16-5 ÷ 16-8, the third group output 5 of the fourth UREP 4-4 is connected to the first group inputs 1 of the ninth to eleventh UZIE 16-9 ÷ 16-11, the first group inputs and outputs 2 of the second-fourth UBEP 5-2 ÷ 5-4 are connected to the first group inputs-output am 2, respectively, of the second-fourth UREPP 4-2 ÷ 4-4, the first-fourth group inputs-outputs 1 ÷ 4 of the second SSK 6-2 are connected to the first group inputs-outputs 11, respectively, of the first-fourth UREP 9-1 ÷ 9-4 , the eighth to eleventh group inputs and outputs 8 ÷ 11 of the second SSK 6-2 are connected to the first group inputs and outputs 2, respectively, of the first to fourth BOFG 12-1 ÷ 12-4, the twelfth group input-output 12 of the second SSK 6-2 is connected to the ninth group input-output 9 of the second UUS 1-2, the thirteenth to sixteenth group inputs and outputs 13 ÷ 16 of the second CCK 6-2 sub are connected to the first group inputs-outputs 2, respectively, of the fifth to eighth BOFG 12-5 ÷ 12-8, the seventeenth group input-output 17 of the second SSK 6-2 is connected to the ninth group input-output 9 of the third CCS, the eighteenth to twenty-first group inputs are outputs 18 ÷ 21 of the second CCK 6-2 are connected to the first group inputs-outputs 2, respectively, of the ninth to twelfth BOFG 12-9 ÷ 12-12, the twenty second group input-output 22 of the second CCK 6-2 is connected to the ninth group input-output 9 the fourth UUS 1-4, twenty-third to twenty-fifth group inputs-outputs 23 ÷ 25 W SSK 6-2 connected to the first group inputs and outputs 2, respectively, of the thirteenth to fifteenth BOFG 12-13 ÷ 12-15, the twenty-sixth group input-output 26 SSC 6-2 is connected to the ninth group input-output 9 of the fifth CCS 1-5 , twenty-seventh-thirtieth group inputs-outputs 27 ÷ 30 of the second SSK 6-2 are connected to the first inputs-outputs 2, respectively, of the first - fourth UZIES 14-1 ÷ 14-4, thirty-first-thirty-fourth group inputs-outputs 31 ÷ 34 are connected with the first group inputs and outputs 2, respectively, of the first or fourth ultrasonic radiation detector 16-1 ÷ 16-4, thirty-five the fifth-thirty-eighth group inputs and outputs 35 ÷ 38 of the second SSK 6-2 are connected to the first group inputs and outputs 2, respectively, of the fifth and eighth ultrasonic detectors 16-5 ÷ 16-8, the fifth and seventh group inputs and outputs 5 ÷ 7 of the second SSK 6 -2 are connected to the first group inputs and outputs 2, respectively, of the ninth to eleventh ultrasonic detectors 16-9 ÷ 16-11, the first 1 and second 2 outputs of the first URVEP 9-1 are connected respectively to the first 1 and second 3 inputs of the first USO 13-1, the third output 3 of the first URVEP 9-1 is connected to the first inputs 1 of the first 12-1, fifth 12-5, ninth 12-9 and thirteenth 12-13 BOFG, the fourth 4 and fifth 5 outputs of the first URVEP 9-1 are connected respectively to the first 1 and second 3 inputs of the first BVVDI 15-1, the sixth 6 and seventh 7 outputs of the first URVEP 9-1 are connected respectively to the first 1 and second 3 inputs of the fourth BVVDI 15- 4, eighth 8 and ninth 9 outputs of the first URVEP 9-1 are connected respectively to the first 1 and second 3 inputs of the seventh BVVDI 15-7, the first 1 and second 2 outputs of the second URVEP 9-2 are connected respectively to the first 1 and second 3 inputs of the second USO 13-2, the third output 3 of the second URVEP 9-2 is connected to the first inputs 1 of the second 12-2, the sixth 12-6, des that 12-10 and fourteenth 12-14 BOFG, the fourth 4 and fifth 5 outputs of the second URVEP 9-2 are connected respectively to the first 1 and second 3 inputs of the fifth USTO 13-5, the sixth and seventh 7 outputs of the second URVEP 9-2 are connected respectively to the first 1 and second 3 inputs of the sixth USPO 13-6, the eighth 8 and ninth 9 outputs of the second URVEP 9-2 are connected respectively to the first 1 and second 3 inputs of the seventh USPO 13-7, the first 1 and second 2 outputs of the third URVEP 9-3 are connected respectively, to the first 1 and second 3 inputs of the third USTO 13-3, the third output 3 of the third URVEP 9-3 connected to the first my inputs 1 of the third 12-3, the seventh 12-7, the eleventh 12-11 and the fifteenth 12-15 BOFG, the fourth 4 and fifth 5 outputs of the third URVEP 9-3 are connected respectively to the first 1 and second 3 inputs of the second BVVDI 15-2, the sixth 6 and seventh 7 outputs of the third URVEP 9-3 are connected respectively to the first 1 and second 3 inputs of the fifth BVVDI 5-5, the eighth 8 and ninth 9 outputs of the third URVEP 9-3 are connected respectively to the first 1 and second 3 inputs of the eighth BVVDI 15- 8, the first 1 and second 2 outputs of the fourth URVEP 9-4 are connected respectively to the first 1 and second 3 inputs of the fourth USOT About 13-4, the third output 3 of the fourth URVEP 9-4 is connected to the first inputs of the fourth 12-4, eighth 12-8 and twelfth 12-12 BOFG, the fourth 4 and fifth 5 outputs of the fourth URVEP 9-4 are connected respectively to the first 1 and the second 3 inputs of the third BVVDI 15-3, the sixth 6 and the seventh 7 outputs of the fourth URVEP 9-4 are connected respectively to the first 1 and second 3 inputs of the sixth BVVDI 15-6, the first 1, third 3, fifth 5 and seventh 7 group inputs the outputs of the second UUS 1-2 are connected to the first group inputs-outputs 2, respectively, of the first-fourth USO 13-1 ÷ 13-4, second 2, fourth 4, sixth 6 and eighth 8 group inputs and outputs of the second CCS 1-2 are connected respectively to the first to fourth subgroups of the third group of inputs and outputs 13-1 ÷ 13-4 of the control system of the launch vehicle with serial codes of systems of the first to fourth models of the carrier rocket family, the first group outputs 4 of the first to fourth UZIES 14-1 ÷ 14-4 are connected to the first group inputs 3 of the corresponding BOFGs 12-1 ÷ 12-4 and, respectively, with the first and fourth subgroups of the second poles of the actuating elements of the first group output 9-1 ÷ 9- 4 ASUP RN in the subsystem “elements and systems of RN”, WTO The first group outputs 5 of the first-fourth UZIES 14-1 ÷ 14-4 are connected to pairs - the fourth group inputs 6 of the corresponding BOPGs 12-1 ÷ 12-4 and to the corresponding first-fourth subgroups of the second group output 12-1 ÷ 12-4 ACS LV for power supply of systems of the first and fourth models of the carrier rocket family in the subsystem “LV elements and systems”, the first group inputs 4 of the first-seventh USO 13-1 ÷ 13-7 are additionally connected to the third group inputs 5, respectively, of the first and fourth 12-1 ÷ 12-4, sixth 12-6, tenth 12-10 and fourteenth 12-14 BOFG, first group inputs 3 of the first to fourth UZIES 14-1 ÷ 14-4 are connected to the first group outputs 5 of the corresponding USTO 13-1 ÷ 13-4, the third group inputs 7 of the first 13-1, third 13-3 and the fourth 13-4 USO connected to the fifth group inputs 7 corresponding 12-1, 12-3 and 12-4 BOFG, the first 1, third 3, fifth 5 and seventh 7 group inputs and outputs of the third CCS 1-3 are connected to the first group inputs and outputs 2, respectively, of the first BVVDI 15-1, fifth USVO 13-5, second and third BVVDI 15-2 and 15-3, the first group inputs 3 of the fifth to fifteenth BOFG 12-5 ÷ 12-15 will supplement are connected respectively to the first group outputs 4 of the first to eleventh ultrasonic ultrasonic sensors 16-1 ÷ 16-11, the first group outputs 5 of the first to eighth BVVDIs 15-1 ÷ 15-8 are connected to the first group inputs 3 respectively of the first 16-1, third to fifth 16-3 ÷ 16-5, seventh-ninth 16-7 ÷ 16-9 and eleventh 16-11 UZIE, the first group inputs 4 of the first-eighth BVVDI 15-1 ÷ 15-8 are connected respectively with pairs - fifth 10-5, seventh-ninth 10-7 ÷ 10-9, eleventh-thirteenth 10-11 ÷ 10-13 and fifteenth 10-15 subgroups of the sixth group input 10 of the automated control system of the RN from discrete sensors DD third group inputs 5, respectively, of the fifth 12-5, seventh-ninth 12-7 ÷ 12-9, eleventh-thirteenth 12-11 ÷ 12-13 and fifteenth 12-15 BOFG, second group inputs 4 of the fifth 12-5, seventh-ninth 12-7 ÷ 12-9, eleventh-thirteenth 12-11 ÷ 12-13 and fifteenth 12-15 BOFG are additionally connected to the second group inputs 6, respectively, of the first to eighth BVVDI 15-1 ÷ 15-8, the first 1, third 3, the fifth 5 and seventh 7 group inputs and outputs of the fourth CCS are connected respectively to the first group inputs and outputs 2 of the fourth BVVDI 15-4, sixth USO 13-6, fifth and the sixth BVVDI 15-5 and 15-6, the first-third 1-3 and the fifth 5 group inputs and outputs of the fifth CCS 1-5 are connected respectively to the first group input-output of the seventh BVVDI 15-7, the eighth group input 14 of the control system a system for measuring parameters of a technological object (SIP TO), the first group inputs and outputs 2 of the seventh and eighth BVVDIs 15-7 and 15-8, the second group input-output 6 of the automatic control system of the LV from the ground NASU of the LV connected to the second group input-output 8 of the seventh BVVD 15-7 and the fourth group input 6 of the thirteenth BOFG 12-13, the first output 7 of the automated control system of the LV in the system At present, SEV is connected to the first output 7 of the seventh BVVDI 15-7 and the second input 7 of the thirteenth BOFG 12-13.

The automated workstation of operator 2 (Fig. 2) contains two network switches 17-1 and 17-2, three monitors 18-1 ÷ 18-3, three system units 19-1 ÷ 19-3, three universal keyboards 20-1 ÷ 20-3, three “mouse” manipulators 21-1 ÷ 21-3, two automatic transfer switches 22-1 and 22-2, three USB port switches 23-1 ÷ 23-3.

The PSK APS 10 remote control (Fig. 3) contains three monitors 18-4 ÷ 18-6, three system units 19-4 ÷ 19-6, three universal keyboards 20-4 ÷ 20-6, three mouse manipulators 21-4 ÷ 21-6, three network communicators 17-3 ÷ 17-5, two automatic transfer switches 22-3, 22-4, three USB port switches 23-4 ÷ 23-6, three network adapters from the USB output 24-1 ÷ 24-3, printer 36, two power supply networks 1-1 and 1-2 of the first group input 1 are connected respectively to the first 1 and second 2 inputs of the two reserve input machines 22-3 and 22-4, the output 3 of the first machine 22-3 is connected to the first input 1 of the first network switch 17-3, to the first inputs 1 of the first and the third system units 19-4 and 19-6, the first and third monitors 18-4 and 18-6, the first and third switches of the USB ports 23-4 and 23-6, the output 3 of the second machine 22-4 is connected to the first inputs 1 the second and third network switches 17-4 and 17-5, the printer 36, the second monitor 18-5, the system unit 19-5 and the USB port switch 23-5, the first and second buses 2-1 and 2-2 of the first group input outputs 2 of the PSA APS console are respectively connected to the first inputs and outputs 2 of the first and second switches 17-3 and 17-4, the first inputs and outputs 2 of the first and third system units 19-4 ÷ 19-6 are connected to the first inputs-outputs 2, respectively, of the first-third monitors 18-4 ÷ 18-6, the second inputs-outputs 3 of the first-third system units 19-4 ÷ 19-6 are connected to the first inputs-outputs 1, respectively, of the first-third network adapters 24- 1 ÷ 24-3, the third-fifth inputs and outputs 4-6 of the first-third system units 19-4 ÷ 19-6 are connected respectively to each other and to the corresponding inputs and outputs of 2 USB port switches 23-4 ÷ 23-6, the second inputs-outputs 2 of the first-third network adapters 24-1 ÷ 24-3 are connected respectively to the first-third buses 3-1 ÷ 3-3 of the second group input yes-outputs 3 of the control panel of the PSA APS, the second inputs and outputs 3 of the first and second switches of the network 17-3 and 17-4 are connected respectively to the sixth 7 and seventh 8 inputs and outputs of the first system unit 19-4, the third inputs and outputs 4 of the first and the second network switches 17-3 and 17-4 are connected respectively to the sixth 7 and seventh 8 inputs and outputs of the second system unit 19-5, the fourth 5 inputs and outputs of the first and second switches of the network 17-3 and 17-4 are connected respectively to the sixth 7 and the seventh 8 inputs and outputs of the third system unit 19-6, the fifth 6 inputs and outputs of the first and second to network switches 17-3 and 17-4 are connected respectively to the first 2 and second 3 inputs-outputs of the third network switch 17-5, the third input-output 4 of which is connected to input-output 2 of the printer 36, the first and third universal keyboards are connected to the second inputs and outputs 3, respectively, of the first-third switch ports 23-4 ÷ 23-6, the first and third manipulator "mouse" 21-4 ÷ 21-6 connected to the third inputs and outputs 4, respectively, of the first-third switch ports 23-4 ÷ 23 -6.

The control and communication device UUS1 (Fig. 4) contains two network switches 17-5 and 17-6, three bus lines M1 ÷ M3, a fault collection unit 25-1, a central processor 26, a multi-nominal power supply (MIEP) 28-1, and three multichannel interface cards (MICs) 27-1 ÷ 27-3, the first 1, third 3, fifth 5 and seventh 7 group inputs / outputs of the UCS have two buses of the local area network, the first buses of which are 1-1, 3-1, 5-1 and 7-1 are connected respectively to the seventh 8, sixth 7, fifth 6 and fourth 5 inputs and outputs of the first network switch 17-5, the second buses of these inputs - outputs 1-2, 3-2, 5-2, and 7-2 are connected respectively to the seventh 8, sixth 7, fifth 6, and fourth 5 inputs and outputs of the second network switch 17-6, input and output 2 of the fault collection node 25 1 is connected to the first input-output 2 of the first and second switches of the network 17-5 and 17-6, the first inputs 1 of the first and second switches of the network 17-5 and 17-6 are connected to the second bus 10-2 of the first group input 10 of the CCS, the first the bus 10-1 of the first group input 10 of the UCS is connected to the input 1 of the MEP 28-1, both buses 10-1 and 10-2 are connected, in addition, to the corresponding buses of the first group input 3 center processor 26, the first group inputs 9 of the first and second switches of the network 17-5 and 17-6 are connected to the group output 2 of the MEP 28-1, which is also connected by a bus of one of the ratings of output 2 to the input 1 of the fault collection node 25-1, the second group input-output 2 of the UCS consists of three subgroups of inputs / outputs, connected respectively to the first group inputs / outputs 1 of the MIC 27-1 ÷ 27-3, three subgroups of the inputs and outputs of the fourth group input-output 4 of the UCS are connected to the second group inputs outputs 2 MICK 27-1 ÷ 27-3, three subgroups of inputs and outputs of the sixth group input-output 6 CCC are connected respectively to the third group input-output 3 MIC 27-1 ÷ 27-3, three subgroups of the inputs and outputs of the eighth group input-output 8 CCM are connected respectively to the fourth group inputs-outputs 4 MIC 27-1 ÷ 27-3, the first-third subgroups 4-1 ÷ 4-3 of the second group input-output 4 and the corresponding inputs 6-1 ÷ 6-3 of the central processor 26 through the bus I / O lines M1 ÷ M3 are connected respectively to the fifth group inputs - outputs 5 MICK 27-1 ÷ 27-3, the first and second buses 5-1 and 5-2 of the third group input-output the odes of the central processor 26 are connected respectively to the second input-output 3 of the first and second network switches 17-5 and 17-6, the third input-output 4 of which are connected respectively to the first and second buses 9-1 and 9-2 of the ninth group input-output 9 CCS, the first and second input / output buses 11-1 and 11-2 of the tenth group input-output 11 of the CCC are connected to the first group input-output 2 of the CPU 26, the first group output 1 of the CPU 26 is connected to the first group output 12 of the CCC , the first outputs 6 MIK 27-1 ÷ 27-3, the second output 3 MEP 28 -1 are connected to the corresponding buses 3-1 ÷ 3-4 of the first group input 3 of the fault collection node 25-1.

The central processor 26 (Fig. 5) contains two network switches 17-7 and 17-8, a fault collection unit 25-2, five multi-nominal power supplies MIEP 28-2 ÷ 28-6, three processors for centralized data processing 29-1 ÷ 29-3, power management device 30.

Software simulator 3 includes a processor for centralized data processing 29-4 and a multi-channel interface card 27-4.

The primary power distribution device UREPP 4 (Fig. 7) contains an automatic transfer switch ABP 22-5, a control mode switch 31, two phase monitoring relays 32-1, 32-2, two network power switches for batteries 33-1, 33-2, two electrical contacts 34-1, 34-2, two contact groups of the corresponding electrical contacts 35-1, 35-2, two sources of secondary power supply IVEP 37-1, 37-2, twenty individual automatic machines 38-1 ÷ 38-20, two emergency units switching 39-1, 39-2, the first bus power supply 1-1 of the first group input 1 UREP connected to the first input odes 1 of the first phase monitoring relay 32-1, the first failover node 39-1, the first network switch 33-1 and the input 3 of the first IVEP 37-1, the second bus power supply 1-2 of the first group input 1 UREP connected to the first inputs 1 the second phase monitoring relay 32-2, the second failover node 39-2, the second network switch 33-2 and to the input 3 of the second IVEP 37-2, the input bus 2-1 of the first group input-output 2 of the UREP is connected to the second inputs 2 of the first and the second failover nodes 39-1 and 39-2, the output bus 2-2 of the first group input-output 2 UREP connected to the output 3 of the ATS 22-5, the first 1 and second 2 inputs of which are connected respectively to the first outputs 2 of the first and second network switches 33-1 and 33-2, the second outputs 3 of which are combined and connected to the bus 8 “ABP is connected” subgroup of outputs 13-2 of the state of the second group input-output 13 of the UREP, outputs 2 of the first and second monitoring relays of phases 32-1 and 32-2 are connected respectively to buses 3 and 9 “Norm 380/220 1” and “Norm 380/220 2 "subgroup of outputs 13-2 of the state of the second group input 13 UREPP, the first output 1 IVEP 37-1 connected to the bus 4 “IWEP 1 enabled” subgroup of outputs 13-2 of the state of the second group input-output 13 UREPP and combined with output 1 IWEP 37-2, which is also connected to the bus 7 “IWEP 1 enabled” subgroup of outputs 13-2 state of the second group input output 13 UREPP, the combined first outputs of IVEP 37-1 and 37-2 are connected to the second inputs of 2 electrocontactors 34-1, 34-2 and the bus "+" of the first output 12 UREPP standby DC voltage, the second outputs 2 IVEP 37-1 and 37-2 are combined and connected with the first input 1 of the control mode switch 31 and with the bus “-” of the first output 12 of the URP DC standby voltage input, input subgroup 13-1 of the second group input-output command 13 UREPP is connected to the second input 2 of the control mode switch 31, the second 4 and third 5 of which outputs are connected respectively to the buses 2 "Remote control" and 1 "Local control "A subgroup of outputs 13-2 states of the second group input-output 13 UREPP, the first output 3 of the control mode switch 31 is connected to the first inputs 1 of the first and second electrical contactors 34-1 and 34-2, the outputs 3 of which are galvanically connected to the input 4 contact groups 35-1 and 35-2, respectively, the output 3 of the emergency switching unit 39-1 is connected to the input 3 of the contact group 35-1 and to the input 1 of the individual machine 38-9, the output 3 of the emergency switching unit 39-2 is connected to the input 3 of the contact group 35-2 and with the input 1 of the individual machine 38-19, the outputs of 2 individual machines 38-9 and 38-19 are connected to the first and second buses 11-1, 11-2 of the group output 11 of the standby AC voltage, the outputs 1 contact groups 35-1 and 35-2 are connected respectively to buses 5 and 6 “220 V 1 on” and “220 V 2 on” subgroups the outputs of the 13-2 states of the second group input-output 13 of the UREPP, the outputs of 2 contact groups 35-1 and 35-2, respectively, are connected to the inputs of the groups of individual machines 38-1 ÷ 38-8, 38-10 and 38-11 ÷ 38- 18, 38-20 outputs of 2 individual automatic machines 38-1 ÷ 38-8, 38-10 are connected to the first buses 3-1 ÷ 10-1, 14-1, respectively, of the first-eighth 3 ÷ 10 and tenth 14 group outputs of URPEP, outputs individual machines 38-11 ÷ 38-18, 38-20 are connected to the second buses 3-2 ÷ 10-2, 14-2, respectively, of the first to eighth 3 ÷ 10 and tenth 14 group outputs of the UREP.

The uninterruptible power supply unit UBEP 5 (Fig. 8) comprises an emergency switching unit 39, an inverter 40, a battery unit 41, a rectifier 42, a monitoring unit 43, and a filter 44.

The network system switch CCK 6 (Fig. 9) contains four network switches 17-16 ÷ 17-19, two multi-channel power sources MIEP 28-11 and 28-12, two circuit breakers 45-1 and 45-2, the first buses of the first of the twenty-fourth group I / O CCK 1-1 ÷ 24-1 connected to the corresponding inputs and outputs of the first switch of the network 17-16, the first buses of the twenty fifth to thirty-eighth group I / O CCK 25-1 ÷ 38-1 connected to the corresponding first - fourteenth inputs and outputs of the second network switch 17-17, second buses of the first twenty hours of the fourth group input-output SSK 1-2 ÷ 24-2 are connected to the corresponding inputs and outputs of the third network switch 17-18, the second buses of the twenty-fifth to thirty-eighth group inputs and outputs of the SSK 25-2 ÷ 38-2 are connected to the corresponding first - fourteenth inputs and outputs of the fourth network switch 17-19, twenty-fifth inputs and outputs of the first and second network switches 17-16 and 17-17 are combined and connected to the first bus 39-1 of the thirty-ninth input-output CCK, twenty-fifth inputs and outputs the third and fourth network switches 17-18 and 17-19 are combined and connected to the second bus 39-2 of the thirty-ninth input-output CCK, the first bus 40-1 of the first group input 40 CCK is connected to input 1 of the first circuit breaker 45-1, the second bus 40-2 of the first group input 40 CCK is connected to input 1 of the second circuit breaker 45-2, the output 2 of the first circuit breaker 45-1 is connected to the inputs 1 of the first and second MIEP 28-11 and 28-12, the output 2 of the second circuit breaker 45-2 is connected to the second inputs 27 of the first to fourth switches of the network 17- 16 ÷ 17-19, output 2 MIEP 28-11 connected to the first inputs 26 to mmutators of the network 17-16, 17-17 and with bus 41-1 “MIEP 1 is on” of the first group output SSK 41, output 2 of MIEP 28-12 is connected to the first inputs 26 of the network switches 17-18, 17-19 and to bus 41 -2 “MIEP 2 is on” of the first group output SSK 41, the second outputs 3 of the first and second circuit breakers 45-1 and 45-2 are connected respectively to buses 41-3 and 41-4 “Feeder 1 is on” and “Feeder 2 is on” .

Remote control device for primary power supply at the remote command post UDUPEP-VKP 7 (Fig. 10) contains three network switches 17-9 ÷ 17-11, three galvanic isolation elements of power supply EGREP 46-1 ÷ 46-3, the unit of majority elements UME 47- 1, three interface relay modules IRM 48-1 ÷ 48-3, six input / output modules MVV 49-1 ÷ 49-6, the first input 1 of the UDUPEP-VKP is connected to the inputs 1 of the EGREP 46-1 ÷ 46-3, output 2 EGREP 46-1 is connected to the inputs 1 MVV 49-1, 49-2 and the network switch 17-9, output 2 EGREP 46-2 is connected to the inputs 1 MVV 49-3, 49-4 and the network switch 17-10, input 2 EGREP 46-3 p connected to inputs 1 MVV 49-5, 49-6 and network switch 17-11, the first group input 2 UDUPEP-VKP is connected to group inputs 2 MVV 49-1, 49-3, 49-5, outputs 4 MVV 49-1 , 49-3, 49-5 are connected to the fourth inputs of 5, respectively, network switches 17-9 ÷ 17-11, buses 3-1, 3-2, 3-3 of the first group input-output 3 UDUPEP-VKP are connected to the fifth inputs- outputs 6, respectively, of the network switches 17-9 ÷ 17-11, a subgroup of inputs 4-1 of the second group input-output 4 UDUPEP-VKP is connected to the first subgroup of inputs 2-1 MVV 49-2, 49-4, 49-6, group of outputs 4 VME 47-1 is connected to buses 4-2 of the subgroup of outputs in of the next group input-output 4 UDUPEP-VKP, group inputs 1, 2, 3 UME 47-1 are connected respectively to group outputs 3 IRM 48-1 ÷ 48-3, group inputs 1 and group outputs 2 IRM 48-1 ÷ 48- 3 are connected respectively with group inputs 3 and subgroups of inputs 2-2 respectively MVV 49-2, 49-4, 49-6, inputs and outputs 4 MVV 49-2, 49-4, 49-6 are connected to the third inputs-outputs 4 respectively, the network switches 17-9 ÷ 17-11, the second input 5 UDUPEP-VKP is connected to the second input-output 3 of the network switch 17-9, the first inputs and outputs 2 of the network switches 17-9 ÷ 17-11 are connected respectively to the first 6-1 minutes, the second 6-2, the third group of the third 6-3 buses IO inputs-outputs 6 UDUPEP-MAC.

The remote control primary power supply in the launch pad UDUPEP-SS (Fig. 11) contains three network switches 17-12 ÷ 17-14, three elements of galvanic isolation of power supply EGREP 46-4 ÷ 46-6, three nodes of major elements UME 47-2 ÷ 47-4, nine interface relay modules IRM 48-4 ÷ 48-12, twelve I / O modules MVV 49-7 ÷ 49-18, the first input 1 of UDUPEP-SS is connected to the inputs 1 of EGREP 46-4 ÷ 46-6 , the output 2 of the EDGE 46-4 is connected to the inputs 1 of the network switch 17-12, MVV 49-7 ÷ 49-10, the output 2 of the EDGE 46-5 is connected to the inputs 1 of the switch of the network 17-13, MVV 49-11 ÷ 49-14 exit 2 EGREP 46-6 is connected to the inputs 1 of the network switch 17-14, MVV 49-15 ÷ 49-18, the first group input 2 UDUPEP-SS is connected to the group inputs 2 MVV 49-7, 49-11, 49-15, outputs 4 MVV 49-7, 49-11, 49-15 are connected to the fifth input-output 6 of the network switches 17-12 ÷ 17-14, respectively, the inputs 6 ÷ 8 of the UDUPEP-SS are connected respectively to the eighth 9, seventh 8 and sixth 7 inputs - the outputs of the network switch 17-12, a subgroup of inputs 3-1 of the first group input-output 3 UDUPEP-SS is connected to the first subgroup of inputs 2-1 of MVV 49-8, 49-12, 49-16, the group of outputs 4 of VME 47-2 is connected with tires 3-2 subgroups of the outputs of the first group input-output 3 UDUPEP-SS, a subgroup of inputs 4-1 of the second group input-output 4 UDUPEP-SS is connected to the first subgroup of inputs 2-1 MVV 49-9, 49-13, 49-17, group of outputs 4 VME 47- 3 is connected to buses 4-2 of the subgroup of outputs of the second group input-output 4 UDUPEP-SS, a subgroup of inputs 5-1 of the third group input-output 5 of UDUPEP-SS is connected to the first subgroup of inputs 2-1 MVV 49-10, 49-14, 49-18, the group of outputs 4 UME 47-4 is connected to buses 5-2 of the subgroup of the outputs of the third group input-output UDUPEP-SS, group inputs 1 ÷ 3 UME 47-2 are connected respectively to g uppp outputs 3 IRM 48-4, 48-10, 48-7, group inputs 1 ÷ 3 VME 47-3 are connected respectively to group outputs 3 IRM 48-8, 48-5, 48-11, group inputs 1 ÷ 3 VME 47-4 are connected respectively to group outputs 3 of IRM 48-6, 48-9, 48-12, group inputs 1 and group outputs 2 of IRM 48-4 ÷ 48-6 are connected respectively to group outputs 3 and a subgroup of 2-2 group inputs 2 respectively MVV 49-8 ÷ 49-10, group inputs 1 and group outputs 2 IRM 48-7 ÷ 48-9 are connected respectively to group outputs 3 and subgroups 2-2 of group inputs 2 respectively MVV 49-12 ÷ 49-14, group inputs 1 and g UPP outputs 2 IRM 48-10 ÷ 48-12 are connected respectively to group outputs 3 and subgroups 2-2 of group inputs 2, respectively MVV 49-16 ÷ 49-18, inputs and outputs 4 MVV 49-8 ÷ 49-10 are connected respectively to inputs and outputs 5, 4 and 3 of the network switch 17-12, inputs and outputs 4 MVV 49-12 ÷ 49-14 are connected respectively to the inputs and outputs 5, 4 and 3 of the network switch 17-13, inputs and outputs 4 MVV 49- 16 ÷ 49-18 are connected respectively to the inputs and outputs 5, 4 and 3 of the network switch 17-14, the inputs and outputs of 2 switches of the network 17-12 of the network 17-12, 17-13 and 17-14 are connected respectively to the first or third subgroups 9-1, 9-2 and 9-3 fourth group input-output 9 UDUPEP-SS.

A communication device with a fiber-optic information transmission line USVOLPI 8 (Fig. 12) contains five transceivers-converters "copper-glass" and "glass-copper" 50-1 ÷ 50-5.

The secondary power distribution device URVEP 9 (Fig. 13) contains two network switches 17-20, 17-21, three multi-nominal power sources MIEP-N 63-1 ÷ 63-3, an electric contactor 34-3, a time relay 51, three peripheral processors 52-1 ÷ 52-3, three normalizers of discrete data NDD 53-1 ÷ 53-3, three former of control signals FSD 54-1 ÷ 54-3, node of the majority elements UME 47-5, ten power sources IEP 56-1 ÷ 56-10, three bus lines M1 ÷ M3, subgroup 10-1 of group input 10 of URVEP connected to the inputs of 1 time relay 51, electric contactor 34-3, IEP 5 6-10, a subgroup 10-2 of the group input 10 of the UREP is connected to the inputs 2 of the time relay 51, the electric contactor 34-3, IEP 56-10, the outputs 3 and 4 of the time relay 51 are connected respectively to the inputs 3 and 4 of the electric contactor 34-3, whose output 5 is connected to inputs 1 of IEP 1 ÷ IEP 9, output 6 of electric contactor 34-3 is connected to inputs 2 of IEP 1 ÷ IEP 9, outputs 3 of MIEP 63-1 ÷ 63-3 are connected respectively to bus lines M1 ÷ M3, highway M1 is connected with group input-output 4 of peripheral processor 52-1 and its input 1, input-output 2 - NDD 53-1, FSU 54-1, highway M2 connected to group input-you run 4 of the peripheral processor 52-2 and its input 1, inputs and outputs 2 NDD 53-2, FSU 54-2, the highway M3 is connected to the group input-output 4 of the peripheral processor 52-3 and its input 1, inputs and outputs 2 NDD 53-3, FSU 54-3, inputs and outputs of 1 peripheral processors 52-1 ÷ 52-3 are connected respectively to inputs and outputs 3 ÷ 5 of a network switch 17-20, inputs and outputs of 2 peripheral processors 52-1 ÷ 52-3 connected respectively to the inputs and outputs 3 ÷ 5 of the network switch 17-21, inputs 1 of the network switches 17-20, 17-21 and inputs 1 of MIEP-N 63-1 ÷ 63-3 are connected to output 5 of IEP 56-10, group output 4 IEP 56-10 s it is connected with a subgroup of 1-10 group inputs 10 NDI 53-1 ÷ 53-3, group inputs 3 of IEP 56-1 ÷ 56-9 are connected respectively to subgroups of output UME 47-5 4-1 ÷ 4-9, group outputs of 4 IEP 56-1 ÷ 56-9 are connected respectively with subgroups 1-1 ÷ 1-9 NDD 53-1 ÷ 53-3, group outputs 1 FSU 54-1 ÷ 54-3 are connected respectively to group inputs 1-3 UME 47-5 , outputs 5 of the IES 56-1 ÷ 56-9 are connected respectively to the outputs 1-9 of the URVEP, the inputs and outputs of 2 switches of the network 17-20 and 17-21 are connected respectively to the subgroups 11-1 and 11-2 of the input-output 11 of the URVEP.

The functional readiness determination unit BOFG 12 (Fig. 14) contains a M1 bus line, a multi-nominal power supply MIEP 28-9, a processor 29-4, a measuring power supply IIEEP 57, four electronic keys 58-1 ÷ 58-4, an FSU control signal generator 54-4, two switches of analog signals CAS 59-1, 59-2, operation mode unit УРР 61, four measuring transducers 64-1 ÷ 64-4, multi-channel analog-to-digital converter MACP 65-1, controlled voltage divider UDN 60, input 1 BOFG is connected to inputs 1 of MIEP 28-9 and IIEP 57, outputs 2 and 3 IIEP 57 are connected respectively to the inputs 1 of the UDN 60 and the electronic key 58-1, the output 3 of the electronic key 58-1 is connected to the input 16 of the UDN 60, the input 2 of the electronic key 58-1 is connected to the output 1-4 of the FSU 54-4 output 2 MIEP 28-10 is connected to the bus line M1, the group input-output 4 of the processor 29-4 and its input 1 are connected via the bus line M1 to the group inputs-outputs 3 of the Matsp 65-1 and FSU 54-4 and their inputs 2 , input-output 2 of processor 29-4 is connected to input-output 2 of BOFG, group inputs 3 ÷ 7 BOFG are connected respectively to pairs of group inputs 3-1 ÷ 3-5 KAS 59-1 and 59-2, group inputs KAS 59-1 and KAS 59-2 are connected respectively to outputs 1-1 and 1-2 of FSU 54-4, outputs 1 of KAS 59-1 and KAS 59-2 are connected respectively to inputs 6 and 10 of URR 61, outputs 1 ÷ 5 of which are connected respectively to inputs 11–15 of UDN 60, input 7 of the URR 61 is connected to the bus of the BOFG body, group input 8 of the URR is connected to the input 8 of the BOFG, group input 9 of the URR 61 is connected to the group output 1-3 of the FSU 54-4, the group input 10 of the UDN is connected to the group output 1-5 of the FSU 54-4, the output 2 of the UDN 60 is connected to the input 3 of the fourth measuring transducer 64-4, whose output 1 is connected to the input 1-4 of the MACP 65-1, input 2 of the meter the transducer 64-4 is connected to the output 1-12 of the FSU 54-4, the input 4 of the measuring transducer 64-4 is connected to the corresponding inputs of the measuring transducers 64-1 ÷ 64-3, the input 1 of the electronic key 58-2 and the output 3 of the UDN 60, input 2 of the measuring transducer 64-1 is connected to the output 1-9 of the FSU 54-4, the output 1 of the measuring transducer 64-1 is connected to the input 1-3 of the MATs 65-1, the output 4 of the UDN 60 is combined with the output 3 of the electronic key 58-2 and connected to input 3 of the measuring transducer 64-1, input 2 of the measuring transducer 64-2 connected to the output 1-10 of the FSU 54-4, input odes of 2 electronic keys 58-2 ÷ 58-4 are connected respectively to outputs 1-6 ÷ 1-8 of FSU 54-4, input 1 of electronic key 58-3 is connected to output 5 of UDN 60, output 6 of which is combined with output 3 of electronic key 58-3 and connected to the input 3 of the measuring transducer 64-2, the output 1 of which is connected to the input 1-2 of the MACC 65-1, the input 2 of the measuring transducer 64-3 is connected to the output 1-11 of the FSU 54-4, the output 1 of the measuring transducer 64-3 is connected to input 1-1 of the MACC 65-1, input 3 of the measuring transducer 64-3 is connected to output 9 of the UDN 60, output 7 and input 8 of the UDN 60 are connected respectively enno to the input 1 and the output of the electronic key 3 58-4.

The device for powering the actuating elements and systems of the ultrasonic ultrasonic control system 14 (Fig. 15) contains an automatic transfer switch reserve ABP 22-3, a secondary power source. IVEP 37-7, input-output module MVV 49-19, two power sources IEP 56-11 and 56-12, four keys 58-5 ÷ 58-8, subgroup 1-1 of group input 1 of the ultrasonic amplifier connected to inputs 1 of ATS 22 -3, IEP 56-11, IEP 56-12, subgroup 1-2 of the group input 1 of the UZIES is connected to inputs 2 of the ATS 22-3, IEP 56-11, IEP 56-12, the output of 3 ATS is connected to the input 1 of the IES 37- 7, whose output 2 is connected to the inputs 1 MVV 49-19, the first and fourth keys 58-5 ÷ 58-8, the outputs 4-1 ÷ 4-4 of the group output of the IED 56-12 are connected to the corresponding inputs 1-4 of the group input 2 MVV 49-19, outputs 5-1 and 5-2 of IEP 56-12 are multiplied and connected with multi-wire buses with Responsibly to the group output 4 of the UZIES and to the group input 3 of the UZIES, the inputs 3-1 and 3-2 of the group input 3 of the IEP 56-12 are connected respectively to the outputs 2 of the keys 58-5 and 58-6, the inputs 3 of which are connected respectively to the outputs 3 -1 and 3-2 of group output 3 MVV 49-19, outputs 4-1 ÷ 4-4 of IEP 56-11 are connected respectively to inputs 2-5 ÷ 2-8 of group input 2 MVM 49-19, inputs 3-1 and 3-2 IEP 56-11 are connected respectively to the outputs of 2 keys 58-7 and 58-8, the inputs 3 of which are connected respectively to the outputs 3-3 and 3-4 of group output 3, the outputs 5-1 and 5-2 of IEP 56- 11 propagated and connected respectively to odgruppam outputs 5-1 and 5-2 of the group inputs input-output 5 UZIES, group input-output 4 MBB 49-19 group connected to a second input-output of 2 UZIES.

The actuator actuator actuator UZIE 16 (Fig. 16) contains an automatic transfer switch ABP 22-4, a secondary power supply 37-10, an input-output module MVV 49-20, two keys 58-9 and 58-10, a power supply 56-12.

A communication device with an object - technological equipment USOTO 13 (Fig. 17) contains three multi-nominal low-voltage power sources MIEP-N 63-4 ÷ 63-6, three peripheral processors 29-5 ÷ 29-7, three bus lines M1 ÷ M3, three normalizers of discrete data NDD 53-4 ÷ 53-6, three shapers of control signals FSU 54-5 ÷ 54-7, three multi-channel analog-to-digital converters MAZP 65-2 ÷ 65-4, k barriers of intrinsic safety of discrete signals BIDS 66 -1 ÷ 66-k, p of the majority elements - keys IEC 62-5 ÷ 62-p + 5, m intrinsically safe normalizers analog of INAI information 67-1 ÷ 67-m, the input 1 of the USO is connected to the inputs 1 of MIEP-N 63-4 ÷ 63-6, the inputs of 2 NDI 53-4 ÷ 53-6, FSU 54-5 ÷ 54-7, and the MAC 65-2 ÷ 65-4, three subgroups 2-1 ÷ 2-3 of the group input-output 2 of the USO are connected respectively to the pairs of inputs and outputs 2 and 3 of the peripheral processors 29-5 ÷ 29-7, the input 3 of the USO is connected to the inputs 3 NDD 53-4 ÷ 53-6, BIDS 66-1 ÷ 66-k, INAI 67-1 ÷ 67-m, outputs 2 MIEP-N 63-4 ÷ 63-6 are connected to the corresponding bus lines M1 ÷ M3, group inputs - the outputs of 4 processors 29-5 ÷ 29-7 and their inputs 1 are connected respectively to the bus lines M1 ÷ M3, NDD 53-4 group input-output 4, FSU 54-5 and MAT 65-2 group inputs / outputs 3 are connected to the bus line Ml, NDI 53-5 group input / output 4, FSU 54-6 and MATsP 65-3 group inputs and outputs 3 are connected to the bus line M2, NDD 53-6 group input -exit 4, FSU 54-7 and MACP 65-4 group inputs-outputs 3 are connected to the bus line M3, inputs 4-1, 4-2 ... 4-k group input 4 USO connected to inputs 1 of the corresponding BIDS 66-1 ÷ 66-k, the outputs 2 of which are connected to the corresponding inputs of the NDD 53-4 ÷ 53-6, the inputs 6-1, 6-2 ... 6-p of the group input 5 USO are connected to the inputs 5 of the corresponding IEC 62-5 ÷ 62-p + 5, outputs 4 which are connected to the corresponding outputs 5-1, 5-2 ... 5-r group output 5 USO, outputs 1-1, 1-2 ... 1-r FSU 54-5 ÷ 54-7 are connected to the inputs 1, 2, 3 of the corresponding IEC 62-5, 62-6 ... 62-p + 5 in such a way that the output 1-n of the FSD 54-5 ÷ 54-7 is connected respectively to the inputs 1, 2, 3 of IEC 62-n + 5, inputs 7-1 , 7-2 ... 7-m group input 7 CIRCUIT connected to the inputs 1, respectively, INAI 67-1 ÷ 67-m, each output 2 of which is connected to the corresponding inputs of the MACP 65-2 ÷ 65-4.

The input-output unit for discrete information BVVDI (Fig. 18) contains three multi-nominal power supply sources MIEP 63-7 ÷ 63-9, three processors 29-8 ÷ 29-10, three normalizers for discrete data NDP 53-7 ÷ 53-9, three shaper control signals 54-8 ÷ 54-10, the majority element 47-5, "p-1" of the majority key elements 62-n + 1 ÷ n + p.

The intrinsically safe analog information normalizer 67 from the INOI USOE structure (Fig. 19) contains an input stabilizing unit 68-1, a normalized signal isolation element 69-1, a galvanic isolation isolation unit 70-1, and an output converter 71.

The intrinsic safety barrier of discrete signals 66 from the USODO BIDS structure (FIG. 20) comprises an input stabilizing unit 68-2, a normalized signal galvanic isolation element 69-2, a power isolation galvanic isolation unit 70-2, and a digital signal output repeater 72.

The power source 58 of the IEP (Fig. 21) contains two rectifier modules 73-1 and 73-2, two conjunctors 74-1, 74-2.

The node operating modes 61 OAF from the BOFG (Fig) contains nine relay contacts 75-1 ÷ 75-9.

A controlled voltage divider 60 UDN from the BOFG (Fig.23) contains six resistors 76-1 ÷ 76-6 and two electronic switches 58-11 and 58-12.

The discrete data normalizer 53 NDD from the USOTO and BVVDI compositions (Fig. 24) contains 2k input elements of galvanic isolation 77-1 ÷ 77-2k, an electronic key 78 for supplying test elements, a shaper 79 of test packages, an undervoltage unit 80-1, a microprocessor 81 -1, indication element 82-1.

The FSU control signal generator 54 from the USOTO and BVVDI compositions (Fig. 25) contains a power isolation element 46-8, a voltage reduction unit 80-2, a microprocessor 81-2, an indication element 82-2, an output key unit 84, “n” output relays 85-1 ÷ 85-n, node 87 feedback element, delay element 86, "n" contact groups 88-1 ÷ 88-n output relays.

The multi-channel analog-to-digital converter 65 of the MACP from the USOTO structure (Fig. 26) contains an element 46–9 of a galvanic isolation of a power supply, a voltage-reducing unit 80-3, a microprocessor 81-3, a multi-input analog-to-digital converter 91, and an indication element 82-3.

The majority element is the IEC key 62 from the USOTO and BVVDI compositions (Fig. 27) contains six normally open relay contacts 92-1 ÷ 92-6.

The scheme of the system reconfiguration algorithm (Fig. 28) contains the following notation for functional nodes and conditional vertices.

94 - beginning of the system reconfiguration mode

95 - is the input voltage ~ 380/220 V from the switchboard supplied?

96 - turn on URPEP 1, URPEP 2, remote control PSK APS, SSK 1, SSK 2, UDUPEP-VKP, UDUPEP-SS

97 - Sub-test application software?

98 - enable AWP 1 ÷ AWP 4, UUS 1-UUS 5, software simulators (PI) 1 ÷ 5

99 - is work being done with the base model (BM)?

100 - carry out BM electrical check mode?

101 - enable URVEP1, include in URVEP1 IEP 3

102 - analysis of the task of carrying out work with BM (the work of the control subsystems PSU and regular work):

102-1 - operation of CCP elements and systems BM

102-2 - the work of PSU to refuel the first SRT

102-3 - the work of PSU to refuel the second SRT

102-4 - work of PSU on TST

102-5 - work with ground technological systems

102-6 - regular operation of the automated control system of the launch vehicle with BM

103 - turn on AWP 1, UUS 2, UREP 3, URVEP 1, IEP 1,2

104 - turn on AWP 1, AWP 2, УУС 2, УУС 3, УРПЭП 4, УРВЭП 1, ИЭП 4,5

105 - turn on AWP 1, AWP 3, УУС 2, УУС 4, УРПЭП 4, УРВЭП 1, ИЭП 6, 7

106 - AWP 1, AWP 4, УУС 2, УУС 5, УРПЭП 4, УРВЭП 1, ИЭП 8, 9

107 - turn on AWP 1 ÷ AWP 4, UUS 3 ÷ UUS 5, UREP 1, 2, 4, URVEP 1, IEP 4 ÷ 9

108 - work with removal from the facility?

109 - turn on AWP 1 ÷ AWP 4, UUS 1-UUS 5, PI 1, URVEP 1, IEP 1, 4, 6, 8

110 - turn on AWP 1 ÷ AWP 4, UUS 1-UUS 5, UREP 3, 4, URVEP 1, IEP 1, 2, 4-9

111 - is work being done with model 2 (M2)?

112 - to conduct a sub-mode of M2 electric checks?

113 - enable URVEP 1, URVEP 2, IEP 3 in each

114 - analysis of the task of carrying out work with M2 (the work of control subsystems PSU and regular work)

114-1 - operation of CCP elements and systems M2

114-2 - the work of PSU to refuel the first SRT

114-3 - PSU work on refueling the second SRT

114-4 - work of PSU on TST

114-5 - work with ground technological systems

114-6 - regular operation of the automated control system of the launch vehicle with M2

115 - turn on AWP 1, UUS 2, UREP 3, URVEP 1, 2, IEP 1, 2 in each

116 - enable AWP 1, AWP 2, UUS 2, UUS 3, UREP 4, URVEP 1, 2, IEP 4, 5 in each

117 - turn on AWP 1, AWP 3, UUS 2, UUS 4, UREP 4, URVEP 1, 2, IEP 6, 7 in each

118 - turn on AWP 1, AWP 4, UUS 2, UUS 5, UREP 4, URVEP 1, 2, IEP 8, 9 in each

119 - turn on AWP 1 ÷ AWP 4, UUS 3-UUS 5, UREPP 4, URVEP 1, 2, IEP 4 ÷ 9 in each

120 - work with removal from the object?

121 - turn on AWP 1 ÷ AWP 4, UUS 1 ÷ UUS 5, PI 1, URVEP 1, 2, IEP 1, 4, 6, 8 in each

122 - turn on AWP 1 ÷ AWP 4, UUS 1 ÷ UUS 5, UREP 3, 4, URVEP 1, 2, IEP 1, 2, 4 ÷ 9 in each

123 - is work being done with model 3 (M3)?

124 - conduct a submode of M3 electrical checks?

125 - turn on URVEP 1 ÷ 3, IEP 3 in each

126 - analysis of the task of carrying out work with M3 (the work of the CSP control subsystems and regular work)

126-1 - operation of CCP elements and systems of the Ministry of Health

126-2 - the work of PSU to refuel the first SRT

126-3 - PSU work on refueling the second SRT

126-4 - work of PSU on TST

126-5 - work with ground technological systems

126-6 - regular operation of the automated control system of the launch vehicle with M3

127 - turn on AWP 1, UUS 2, UREP 3, URVEP 1 ÷ 3, IEP 1, 2 in each

128 - turn on AWP 1, AWP 2, UUS 2, UUS 3, UREP 4, URVEP 1 ÷ 3, IEP 4, 5 in each

129 - turn on AWP 1, AWP 3, UUS 2, UUS 4, UREP 4, URVEP 1 ÷ 3, IEP 6, 7 in each

130 - turn on AWP 1, AWP 4, УУС 2, УУС 5, УРПЭП 4, УРВЭП 1 ÷ 3, IEP 8, 9 in each

131 - turn on AWP 1 ÷ AWP 4, UUS 3 ÷ UUS 5, UREPP 4, URVEP 1 ÷ 3, IEP 4 ÷ 9 in each

132 - work with removal from the facility?

133 - turn on AWP 1 ÷ AWP 4, UUS 1 ÷ UUS 5, PI 1, URVEP 1 ÷ 3, IEP 1, 4, 6, 8 in each

134 - turn on AWP 1 ÷ AWP 4, UUS 1 ÷ UUS 5, UREP 3, 4, URVEP 1 ÷ 3, IEP 1, 2, 4 ÷ 9 in each

135 - is work being done with model 4 (M4)?

136 - system failure to locate model type

137 - to conduct a submode of M4 electric checks?

138 - enable URVEP 1 ÷ 4, IEP 3 in each

139 - analysis of the task of carrying out work with M4 (the work of control subsystems PSU and regular work)

139-1 - operation of CCP elements and systems M4

139-2 - the work of PSU to refuel the first SRT

139-2 - PSU work on refueling the second SRT

139-4 - work of PSU on TST

139-5 - work with ground technological systems

139-6 - regular operation of the automated control system of the launch vehicle with M4

140 - turn on AWP 1, UUS 2, UREP 3, URVEP 1 ÷ 4, IEP 1, 2 in each

141 - turn on AWP 1, AWP 2, UUS 2, UUS 3, UREP 4, URVEP 1 ÷ 4, IEP 4, 5 in each

142 - turn on AWP 1, AWP 3, UUS 2, UUS 4, UREP 4, URVEP 1 ÷ 4, IEP 6, 7 in each

143 - turn on AWP 1, AWP 4, УУС 2, УУС 5, УРПЭП 4, УРВЭП 1 ÷ 3, IEP 8, 9 in each

144 - turn on AWP 1 ÷ AWP 4, UUS 3 ÷ UUS 5, UREP 4, URVEP 1 ÷ 3, IEP 4 ÷ 9 each, URVEP 4, IEP 4-7

145 - work with removal from the facility?

146 - turn on AWP 1 ÷ AWP 4, UUS 1 ÷ UUS 5, PI 1, URVEP 1 ÷ 3, IEP 1, 4, 6, 8 in each, URVEP 4, IEP 1, 4, 6

147 - turn on AWP 1 ÷ AWP 4, UUS 1 ÷ UUS 5, UREP 3, 4, UREP 1 ÷ 3, IEP 1, 2, 4 ÷ 9 each, UREP 4, IEP 1, 2, 4 ÷ 7

148 - the end of the reconfiguration mode, permission to implement modes of work with the CSP and the system

The scheme of the algorithm for electrical checks BM (Fig) contains the following notation for functional nodes and conditional vertices.

149 - the beginning of the operation of the mode of electrical checks of the communication system with BM PH

150 - input voltage ~ 380/220 VAC applied?

151 - turn on UREPEP 1, UREPEP2, PSK APS, SSK 1, SSK 2, UDUPEP-VKP, UDUPEP-SS, URVEP 1, IEP 3, USVOLPI 1, 2

152 - permission to conduct electrical checks of the system’s communications with the LV was obtained?

153 - from the PSK APS remote control, enter the number of verified actuating elements of IE in the address counter [СЧ А] = N

154 - measure (using BOFG 1) the insulation resistance of the current IE R _from IE

155 - the value of R _from IE is normal?

, находящееся не в норме156 - record the value in the repair report

abnormal

157 - measure (using BOFG 1) the resistance of the circuit IE R _c IE

в норме?158 - value

fine?

159 - write in the repair protocol the resistance value R _c IE, which is not normal

, схемно не связанных между собой160 - measure the mutual resistance of the circuits

not schematically interconnected

в норме?161 - resistance

fine?

, находящееся не в норме162 - record the value in the repair report

abnormal

163 - increase the contents of the IE address counter by one

164 - the contents of the IE address counter are equal to the limit value equal to the number of IE = N?

165 - enter the counter addresses of discrete sensors [MF A] = M

166 - measure the insulation resistance of the circuit of the discrete sensor R _from DD

167 - Is the insulation value of the discrete sensor circuit normal?

168 - write in the repair report the value of the circuit R _{from the} DD, which is not normal

169 - measure the mutual resistance of the circuits of discrete sensors, circuitry unconnected

в норме?170 - value

fine?

171 - write in the repair report the value of the mutual resistance, which is not normal

172 - increase the contents of the counter address DD [SC A] by one

173 - the contents of the address counter DD is equal to the limit value [SC A] DD = M?

174 - enter the counter counter addresses of the sensors analog [SC A] YES = P

175 - measure the insulation resistance of the circuit YES R _from YES

176 - Is the insulation resistance value R _of YES normal?

177 - write in the repair report the value of R _from YES, which is not normal

178 - measure the value of the circuit resistance YES R _c YES

179 - the value of R _C YES is normal?

180 - write in the repair report the value of R _C YES, which is not normal

текущего ДА с остальными элементами БМ РН181 - measure mutual resistance

current YES with the remaining elements of the BM RN

в норме?182 - mutual resistance

fine?

, находящееся не в норме183 - record the value in the repair report

abnormal

184 - increase the contents of the address counter YES [SC A] YES by one

185 - the contents of [Sch A] YES is equal to the limit value of P?

186 - enter the limit value [SCh A] BS equal to S in the counter of information channels of on-board systems

187 - to verify the health of information channels (IR) of on-board computer systems by exchanging test messages between the UUS 2 and systems

188 - are the results of the health check of information channels positive?

189 - record in the repair report the numbers of channels and systems that do not give positive results

190 - increase the content of the number of information channels on-board systems by one

191 - the contents of the counter numbers of the information channels of the on-board systems is equal to the limit value [SC A] IR = T

192 - visualization of the repair protocol. The end of the mode of electrical checks of the communication system with BM RN.

The scheme of the algorithm of electric checks, common to all models of LV (Fig), contains the following notation for functional nodes and conditional vertices.

193 - the beginning of the mode of electrical checks for all pH models

194 - turn on the PSK APS, UREPEP 1, UREPEP 2, SSK 1, SSK 2, UDUPEP-VKP, UDUPEP-SS, USVOLPI 1, 2, URVEP 1 ÷ 4, IEP 3 for each remote control

195 - enable BOFG 1, 5, 9, 13, check for BM: IE, DD, YES, information channels of on-board computer systems

196 - is there a transition to a higher model?

197 - enable BOFG 1, 2, 5, 6, 9, 10, 13, 14; check for DM2: IE, DD, YES, information channels of onboard computer systems

198 - enable BOFG 1, 2, 3, 5, 6, 7, 9, 10, 11, 13, 14, 15; check for DM3: IE, DD, YES, information channels of onboard computer systems

199 - turn on BOFG 1 ÷ 15; check for D4: IE, DD, YES, information channels of onboard computer systems

150 - input voltage ~ 380/220 VAC applied?

152 - permission to conduct electrical checks of communications systems with a LV is obtained?

99 - is work being done with the base model (BM)?

111 - is work being done with model 2 (M2)?

123 - is work being done with model 3 (M3)?

135 - is work being done with model 4 (M4)?

136 - system failure to locate model type

200 - end of the test mode for communication of the automated control system of the control system with all models, permission to switch to work with the control system and the system

Automated control system for the preparation of launch vehicles operates as follows.

At the initial moment of work in the automated control system of the launch vehicle, a reconfiguration is organized, i.e. the inclusion of the necessary equipment to work with the serviced model of launch vehicles.

There are four models in the family of launchers serviced by the automated control system of the launcher: the basic model of the launcher of the light class BM, model M2, model M3 and model M4 of the launcher of heavy class.

To work with the BM model in the automated control system of the RN, a set of equipment is included, indicated by the BM set; for model M2, the equipment set consists of a BM set and additional equipment DM2; for the M3 model, the equipment set consists of the M2 set (BM + DM2) and additional DM3 equipment; for the M4 model, the equipment set consists of the M3 set (BM + DM2 + DM3) and additional DM4 equipment.

At the beginning, when the ACS RN supplies 5 input three-phase AC voltage ~ 380/220 V to the group input from the distribution board of the power system of the cosmodrome, a set of resident equipment is needed to carry out the reconfiguration.

At the remote command post the PSK APS 10, UDUPEP-VKP 7 and USVOLPI 8-1 switch on. УРПЭП 4-1 is brought into the state of "Readiness". In the launch facility, UDUPEP-SS 11 and USVOLPI 8-2 are included. UREPP 4-2 ÷ 4-4 are given in the state of "Readiness".

The input AC voltage supplied to the input of the control system RN can be supplied from two voltage sources.

In the preparatory commissioning period, voltage is supplied to the system input from two networks of conventional power supply of SES. In this case, the system equipment works in conjunction with uninterruptible power supply devices UBEP 5-1 ÷ 5-4, which are connected to the corresponding UREP 4-1 ÷ 4-4.

During normal operation, voltage from two networks of the guaranteed power supply system of the SECS of the cosmodrome is supplied to the input of the automated control system for the launch vehicle. During this operation, the UBEP 5-1 ÷ 5-4 are disconnected from the UREP 4-1 ÷ 4-4 using their own manual controls.

Upon receipt of the supply voltage to the input 5 of the control system RN it is fed to the group inputs 1 URPEP 4-1 ÷ 4-4 (Fig.7). In each URPEP, the mains voltage from the first network through input 1-1 is supplied to the inputs 1 of the RKF 32-1 phase monitoring relay, UAP 39-1 emergency switching unit and PPB 33-1 battery power switch of its UBEP and by input 3 to the input of the secondary source power supply IVEP 37-1.

The voltage from the second network at input 1-2 is supplied to inputs 1 of the RKF 32-2, UAP 39-2, PPB 33-2 and at input 3 to the input of IVEP 37-2.

From outputs 2 of the RKF 32-1 and 32-2, the signals 3 and 9 “Norm 380/220 V1” and “Norm 380/220 V2” are issued to the output bus of states 13-2, indicating the presence of voltages at all phases of the input voltage and finding the mains voltage is normal in magnitude, from the outputs 1 of the IVEP 37-1 and 37-2 the signals 4 and 7 “IVEP 1 on” and “IVEP 2 on” are issued. From outputs 2 of PPB 33-1 and 33-2, the network voltages of network I and network II are fed to inputs 1 and 2 of the automatic transfer switch ABP 22-5. The combined outputs 3 PPB 33-1 and 33-2 give on the output bus status 13-2 signal 8 "ABP connected."

In addition, the combined outputs 2 of the IVEP 37-1 and 37-2 are connected to the input of the control switch of the switchgear 37, which can be in the state of local control and remote control, manually set by its controls. Depending on the control mode, signals 1 and 2 “Local control” or “Remote control” are issued to the status bus.

The set of signals 1 ÷ 4, 7 ÷ 9 from bus 13-2 of each UREPP is transmitted respectively to group input-output 4 UDUPEP-VKP 7 from URPEP 4-1 and to group inputs-outputs 6-8 UDUPEP-SS, respectively, from UREPP 4- 2 ÷ 4-4.

From the outputs 3 of the UAP 39-1, the voltages of the networks I and II go to the input of 3 contact groups 35-1 and 35-2 and to the inputs 1 of the individual automatic machines 38-9 and 38-19, forming at the output 11 of the UREP 4-1 the standby voltage of the alternating current 220 V.

From the outputs 1 and 2 of the IVEP 37-1 and 37-2, respectively, the combined chains of the positive and negative poles arrive: from outputs 1 to the inputs 2 of the electric contactors 34-1 and 34-2 and to the positive poles of the group outputs 12 of the UREP 4-1 and 4- 2, from outputs 2 in addition to the previously mentioned input 1 of the switchgear 37 and to the negative poles of group outputs 12 URPEP 4-1 and 4-2. A standby DC power supply voltage = 24 V is formed. A standby voltage ~ 220 V from the output 11 of the URPEP 4-1 is supplied to turn on the PSK APS 10 console by input 1. The standby voltage = 24 V from the outputs 12 of the URPEP 4-1 and 4-2 includes at the inputs 1 UDUPEP-VKP, USVOLPI 8-1 and 8-2, UDUPEP-SS 11.

The system is ready to turn on the equipment necessary for working with a particular model of the PH family.

Before turning on the necessary set of devices and functional blocks for working with a given model, the application software of the system software is checked, which will subsequently make it possible to implement all the necessary debugging modes in the commissioning and standard cycles of preparing a given LV model.

Verification of software for any model requires the inclusion of the following set of devices that provide for “dry refueling”: ARMO 2-1 ÷ 2-4, SSK 6-1 and 6-2, UUS 1-1 ÷ 1-5 with software simulators 3-1 ÷ 3-5. At the same time, the resident devices are already included: PSK APS 10 console, UREPEP 4-1 and 4-2 with their UBEP 5-1 and 5-2, UDUPEP-VKP 7, UDUPEP-SS 11, USVOLPI 8-1 and 8-2.

The inclusion of devices "dry refueling" is organized using the remote control PSK APS and UDUPEP 4-1 and 4-2. The inclusion of CCK is provided by power supply. Power supply to CCK 6-1 is supplied from the output 8 of the included UREPP 4-1, to SSK 6-2 - from the output 14 of the UREPP 4-2. ARMO 2-1 ÷ 2-4 prepared by supplying power from the outputs 4 ÷ 7 UREPP 4-1, their inclusion is made by the operator. The CCS is prepared by supplying power; they are turned on via the network through the CCK. UUS 1-1 is prepared by supplying power from output 3 of UREPP 4-1. UUS 1-2 ÷ 1-5 prepared by supplying power from the outputs 7 ÷ 10 UREP 4-2.

The inclusion of CCS is organized after the inclusion of CCK 6-1 and 6-2. Devices are turned on by commands from the PSK APS 10 remote control. The CCS 1-1 of communication with adjacent systems is turned on through input-output 1 of the CCC 6-1 at their ninth input-output 9. The CCS 1-2 ÷ 1-5 are turned on alternately from the PSK APS 10 through SSK 6-1, USVOLPI 8-1 and 8-2, SSK 6-2.

УУС 1-2 subsystems for controlling elements and on-board systems of the LV is switched on from input-output 12 ССК 6-2, УУС 1-3 subsystems for controlling refueling 1 КРТ - from input-output 17, УУС 1-4 subsystems for controlling refueling 2 КРТ - from input - exit 22, УУС 1-5 of the TST subsystem and communication with adjacent systems at the starting position - from input / output 26 of CCK 6-2.

Software simulators 3-1 ÷ 3-5 of the corresponding CCS 1-1 ÷ 1-5 are included from their CCS. Software simulators 3-1 ÷ 3-5 in the "dry" gas station play the role of control objects for the CCS 1-1 ÷ 1-5.

The definition of the model of the PH family affects the composition of the software; the corresponding routines are connected. Modes of operation with a particular LV model are set with ARMO 2-1 and transmitted to the remaining ARMO and UUS 1-1 ÷ 1-5 through CCK 6-1, USVOLPI 8-1 and 8-2 and CCK 6-2.

After checking the correctness of the software, the system hardware is reconfigured. Reconfiguration consists in supplying primary and secondary power supply voltage to devices and functional blocks of BOFG, USOTO, BVVDI, UZIES, UZIE.

Subscribers of primary power supply UREPP 4-1 ÷ 4-4 and secondary power supply URVEP 9-1 ÷ 9-4 are presented in table 1.

It should be noted that BOFG 12-1 ÷ 12-15 is used only in the mode of electric checks of communications of control objects (launch vehicle and ground processing equipment for refueling and thermostating) with automatic control system of the launch vehicle. The participation of devices and functional blocks is marked with a “+” sign, non-participation - with a “-” sign, those parts of UREP that are not involved in the system in any mode are marked with a space.

Before debugging modes and regular work with the participation of control objects, the mode of electrical checks of communications of the automated control system for control systems with technological objects of control and elements and systems of the control system is performed.

The following elements and systems are checked:

- discrete sensors;

- Signals of joining the connections of the elements of the object and individual parts of the system;

- analog temperature sensors such as thermistors TSP;

- analog potentiometric pressure sensors for traffic rules;

- Executive elements IE type electric pneumatic valves EPK;

- multi-wire power bus systems;

- buses of serial codes of LV systems.

Types of electrical checks carried out in the automated control system of the RN:

- measurement of insulation resistance;

- measurement of circuit resistance;

- check the integrity of the circuit;

- measurement of resistance between various elements (galvanic separation).

The principle of electrical checks is the measurement of resistances in the BOFG measurement circuit (Fig. 14). It is necessary to connect two poles of the measured resistance. To measure insulation resistance, the second pole is the equipment case; for other electrical checks, the second poles of the objects being checked are used from the elements being tested. A comprehensive check of all the connections of the elements being checked consists in sequentially checking the resistance of all contacts of the object relative to the second pole. For example, for the IE actuator, this is a measurement of the resistances R _{+ 1-1} , R _{+ 2-1} , R _-2-1 , which should be equal in a normal situation

R _{+ 2 + 1} = R _{+ 1-1} , = R _pc + R _IE , R _-2-1 = 0 (short circuit),

where R _PC - the resistance of the supply circuits from the control system to the IE and from the IE to the control system. The resistance R _{IE is} usually equal to several tens of ohms.

Measurement scheme BOFG 12 consists of a measuring power supply source IIEP 57, a control voltage divider UDN 60, an operating mode unit УРР 61, electronic switches 58-1 ÷ 58-4, measuring transducers 64-1 ÷ 64-4, a multi-channel analog-to-digital converter 65 -one. The control signal generator 54-4 and the processor 29-4 control the measurement and conversion circuit and process the result to output it at input-output 2 in CCK 6-2.

The first pole of the measured object is connected from the output of the analogue switch CAS 59-1 to the input to the OAI 61. The second pole of the object to be tested is connected to the measurement circuit from the output of the CAS 59-2 to the input 10 of the OAI 61.

The second measurement pole for checking the insulation resistance R _{of is} connected to the housing through input 7 of the OAI.

The eighth input 8 of the BOFG 14 is connected to the input 8 of the OA for possible checks of the resistance of the object relative to other common wires in the system, except for the housing.

The following set of devices is involved in the system for electric checks: UREPEP 4-1, UREPEP 4-2, UDUPEP-VKP 7, UDUPEP-SS 12, UVOLPI 8-1 and 8-2, PSK APS 10, included as a resident part after submission input voltage ~ 380/220 V to input 5 of the automated control system of the launch vehicle and switched on using the PSK APS SSK 6-1, 6-2, URVEP 9-1, 9-2, as well as BOFG 12. The number of switched on BOFGs and their numbers depend on Served pH Model. In the description of the operation of the automated control system of the launch vehicle, the M2 model will be considered. For M2, the following BOFG 12 is turned on using UREP 9-1 and 9-2: 12-1, 12-2, 12-5, 12-6, 12-9, 12-10, 12-13, 12-14.

In addition to conducting electrical checks of the connections between the elements of the control objects and the elements themselves, the pH systems are checked. Part of the checks, which consists in measuring the insulation resistance of the screens of the connection wires of the systems, is carried out in a series of electrical checks of elements. Additionally, the systems are checked algorithmically by analyzing the information coming from the PH systems. To initiate the operation of the systems and analyze their information, it is necessary to include in addition to the equipment of electrical inspections UUS 1-2 and UZIES 14-1 and 14-2. Power to these devices is supplied from the already included UREP 4-2 and included UREP 4-3. Commands for turning on UREPP 4-3, UUS 1-2, UZIES 14-1 and 14-2 are given from the PSK APS 10 remote control via UDUPEP-VKP 7, UVOLPI 8-1, 8-2, UDUPEP-SS 11 (for UREPP 3 ) and through SSK 6-1, USVOLPI 8-1, 8-2 (network channels), SSK 6-2 (for UUS 1-2 and UZIES 14-1 and 14-2). With CCK 6-2, from its input-output 12, a command is issued to turn on the CCS 1-2 at input-output 9. With CCK 6-2, from its inputs-outputs 27 and 28, commands are issued to turn on, respectively, UZIES 14- 1 and 14-2.

Using the same inputs and outputs, the state of switched-on devices is analyzed. They must be on standby. Otherwise, their unavailability status is transmitted to the PSK APS console to make a decision on restoring the operability of the connected devices.

In UUS1 (figure 4), information is exchanged with CCK 6-2 on two network buses 9-1 and 9-2. The command from the PSK APS 10 remote control is supplied to the inputs and outputs 4 of the network switches 17-5 and 17-6 and from there, via inputs and outputs 3 to the inputs and outputs 5-1 and 5-2 of the central processor 26.

Information from the CCS in the central processor (Fig. 5) at the inputs and outputs 5-1 and 5-2 is received at the inputs and outputs 5 of the network switches 17-7 and 17-8 and transmitted from them to the processors 29-1 ÷ 29-3 at the inputs and outputs 6-8.

In UZIES (Fig. 15), information is exchanged with SSK 6-2 through group input-output 2 via buses 2-1 and 2-2. In the I / O module 49-19, information is collected on the state of the IEDs 56-11 and 56-12 by their outputs 4-1 ÷ 4-4 and depending on the state of the IEDs 56-11 and 56-12, a power-on command can be issued to them from group output 3 MVV for subgroups 3-1 and 3-2 on IEP 56-12 and for subgroups 3-3 and 3-4 on IEP 56-11. The states of the IED (Fig. 21) can be: 4-1 "Fault 1" corresponding to the fault of the rectifier module MB 73-1 included in the IEP 56; 4-2 - “Readiness”, which is formed on the conjuncture 74-2 by the presence of two signals “Readiness” of rectifier modules 73-1 and 73-2; 4-3 - "Enabled" after turning on both MB 73-1 and 73-2; 4-4 - “Malfunction 2”, corresponding to the malfunction of module 73-2 included in IEP 56.

If at least one signal “Malfunction 1” or “Malfunction 2” is issued, then the operator of the PSK APS remote control is notified, and the further actions - to continue working or restore the MB to work — are accepted by the operator of the PSK APS remote control.

After turning on the UZIES 14-1 and 14-2, the output voltage of the LV systems for the subgroups 12-1 and 12-2 of the group output 12 of the automatic control system of the LV is supplied to the system equipment for the BM and DM2 model via multi-wire power buses. УУС 1-2 receives information from systems and by its analysis is convinced of serviceability or malfunction of LV systems.

Operation in normal operation of the automated control system of the launch vehicle is described for the M2 model. The reason for this is that the total system equipment used to control the preparation of the M2 model consists of the sum of devices and blocks for the BM model and additional equipment DM2. The equipment for the BM model is similar to the equipment for additional equipment DM3 and DM4. However, the equipment for DM2 differs from similar sets of devices and functional blocks. Firstly, DM2 equipment for the launch vehicle does not contain analog sensors. Secondly, DM2 equipment for refueling and temperature control process equipment should be protected from communication circuits with the control object passing through the explosive zone. Therefore, the description of the equipment of the automated control system for the control system of the BM and additional equipment DM2 is representative of the description of the control system of the control system.

In the normal operating mode for the M2 model, the following control systems for RN are included: UREPP 4-1 ÷ 4-4, URVEP 9-1 and 9-2, ARMO 2-1 ÷ 2-4, remote control panel APS 10, USVOLPI 8-1 and 8-2, UDUPEP-VKP 7, UDUPEP-SS 11, SSK 6-1 and 6-2, USOTO 13-1, 13-2, 13-5 ÷ 13-7, BVVDI 15-1, 15-4, 15 -7, UZIES 14-1 and 14-2, UZIE 16-1, 16-2, 16-5, 16-6, 16-9, 16-10.

Information about the status of discrete DD sensors and SS docking signals is input into the system through subgroups 10-1, 10-2, 10-5, 10-6, 10-9, 10-10, 10-13, 10-14 of group input 10 in ASUP PH. It arrives at the group inputs 4 USTO 13-1, 13-2, 13-5 ÷ 13-7 and BVVDI 15-1, 15-4, 15-7.

In USO 13 (Fig.17), the information through the inputs 4-1, 4-2 ... 4-k goes to the inputs of the intrinsic safety barriers of the discrete signals BIDS 66-1, 66-2 ... 66-k. BIDS 66 (Fig.20) are grouped into four circuits in one housing. They include a stabilizing unit 68-2 for 4 inputs, an EGR 69-2 galvanic isolation element for 4 inputs, a discrete signal output repeater 72 for 4 circuits, and a 70-2 galvanic isolation unit.

The set of these nodes and their connections provide galvanic isolation of the incoming signals and the supplied power supply, which in the event of an emergency with communications of discrete signals from the DD and SS ensure the safety of the automated control system of the LV in the discrete data path.

The technological equipment for controlling the fueling and thermostating for the BM included in M2 is located in the non-hazardous area and does not have analog sensors, therefore, signals from subgroups 10-5, 10-9, 10-13 are sent to the inputs 4 of the corresponding BVVDI 15-1, 15- 4, 15-7. In BVVDI 15 (Fig. 18), the information through the inputs 4-1, 4-2 ... 4-k goes to the inputs 1-1, 1-2 ... 1-k of the normalizers of discrete data NDD 53-4 ÷ 53-9.

In USO 13, the information from the outputs of BIDS 66 also goes to the inputs 1-1, 1-2 ... 1-k NDD 53-4 ÷ 53-6.

In further communications and devices involved, the paths for the passage of discrete information and its processing are identical.

From the output of NDD 53 (for USTO 53-4 ÷ 53-6, for BVVDI 53-7 ÷ 53-9) information is transmitted via bus lines M1 ÷ M3 to processors 29 (for USOTO 29-5 ÷ 29-7, for BVVDI 29 -8 ÷ 29-10). From the output of the processors through the group input-output 2, the information processed in accordance with the calculation algorithms is sent to the corresponding CCS1: from the inputs-outputs 2 of the USOUT 13-1 and 13-2 - to the USS 1-2, from the inputs and outputs 2 of the USOU 13-5 and BVVDI 15-1 - in UUSO 1-3, from the inputs and outputs 2 of USTO 13-6 and BVVDI 15-4 - from UUSO 1-4, from the inputs and outputs 2 of USTO 13-7 and BVVDI 15-7 - in UUS 1-5.

From the inputs and outputs 9 UUS 1-2 ÷ 1-5 information through SSK 6-2 and 6-1, passing USVOLPI 8-2 and 8-1, is distributed in SSK 6-1 in the corresponding ARMO: from UUS 1-2 - in ARMO 2-1, from UUS 1-3 - in ARMO 2-2, from UUS 1-4 - in ARMO 2-3, from UUS 1-5 - in ARMO 2-4. If through any channels there is information about the malfunction of the DD or SS, it is transferred to the PSK APS 10 console to diagnose the malfunction.

Information from analog sensors is entered into the system through a subgroup 11-1 of group input 11 in the automated control system of the pH. She arrives at the group input 7 USO 13-1. In USO 13 (Fig.17), the information goes through inputs 7-1, 7-2 ... 7-m to the inputs of intrinsically safe normalizers of analog information INAI 67-1, 67-2 ... 67-m. INAI 67 (Fig. 19) are grouped according to two schemes in one building. They include an input stabilizing unit 68-1 for two inputs, an galvanic isolation element EGR 69-1 for 2 inputs, an output converter 71 for two circuits and a galvanic isolation unit for power 70-1.

A set of these nodes and their connections provide galvanic isolation of the incoming signals and the supplied power supply. As shown in table 3, the incoming signals from the sensors TSP and SDA are fed by four inputs. From the INAI output 67-1, 67-2 ... 67-m normalized in the range of 0-10 V and explosion-proof signals that ensure the safety of the automated control system of the LV in the analog information path are fed to the inputs 1-1, 1-2 ... 1-m of the module multi-channel analog-to-digital converter MATsP 65-2 ÷ 65-4.

MADC 65 (Fig. 26) contains an element of a multi-channel ADC 91, to the inputs 2-1, 2-2 ... 2-m of which the input information from the outputs of INAI 67-1, 67-2 ... 67-m, a reduction circuit 80-3 voltage, element 46-9 galvanic isolation of power supply EGREP, microprocessor 81-3, element 82-3 indication EI. At the input 2 to the MACP, power is supplied, at the input / output 3, a connection is established with the processor. At the service input-output 4 in the preparatory period, information is entered into the microprocessor MKP 81-3. Having received the input signal “Readiness” from the MACP 91, the MCP issues an “Read” command on the output 2 of the MACP 91. On command, the codes from the output of the 4 MACP enter the input 3 of the MCP.

From the inputs and outputs 3 of the MACP 65-2 ÷ 65-4, respectively, through the bus lines M1 ÷ M3, information in a digital code is fed to the inputs and outputs of 4 processors 29-5 ÷ 29-7 in USO 13-1. From the inputs and outputs of processors 2 and 3 through the input-output 2 USOUT 13-1, the information goes to the UUS 1-2, and then through the CCK 6-2, 6-1, USVOLPI 8-2, 8-1 in ARMO 2-1 . The issuance of control commands for LV elements and systems is carried out from USOTO 13-1, UZIES 14-1, BVVDI 13-2, UZIES 14-2 with control from UUS 1-2. The control commands for the fueling subsystem of the first SRT are organized using BVVDI 15-1, UZIE 16-1, USOE 13-5, UZIE 16-2 under control from UUS 1-3. The control commands for the refueling subsystem of the second SRT are organized with the help of BVVDI 15-4, UZIE 16-5, USOTO 13-6, UZIE 16-6 under the control of UUS 1-4. The control commands for the thermostat subsystem are organized using BVVDI 15-7, UZIE 16-9, USOTO 13-7, UZIE 16-10 under the control of UUS 1-5.

The issuance of single commands is set with ARMO for the subsystem for controlling elements and systems of the LV - with ARMO 2-1, for the subsystem for controlling the fueling system of the first KRT - with ARMO 2-2, for the subsystem for controlling the fueling system of the second KRT - with ARMO 2-3, for the subsystem for controlling the temperature control - with ARMO 2-4. With ARMO, teams through CCK 6-1, USVOLPI 8-1, 8-2, CCK 6-2 are transmitted to the appropriate CCS. If any mode is launched, then only the mode launch command is issued from the AWP to the UCS, and control commands are generated by the programs in the UCS. From the UUSO to USTO 13 and BVVDI 15, the teams arrive at group inputs-outputs 1 and 3 (for M2) and arrive at group inputs-outputs 2. In USOTO and BVVDI, processors 29 are transmitted through bus lines M1 ÷ M3 to FSU 54 .

FSU 54 (FIG. 25) contains a galvanic isolation element for power supply EGREP 46-8, a voltage reduction circuit SPN 80-2, a microprocessor MKP 81-2, an indication element EI 82-2, a node 84 of the UVK output keys, output relays 85-1 ÷ 85-n, delay element 86, feedback element node 87, contact groups 88-1 ÷ 88-n of output relays, fuse 89, diode 90. Group output 1-1 ... 1-p of contact groups contains two outputs: direct 1- 1-1 ÷ 1-1-n and feedback 1-2-1 ÷ 1-2-n.

The outputs of the contact groups are supplied to the majority elements of the contact 62 (Fig.27), which majorize the team of three FSU 54.

After switching on the FSU at input 2 and receiving input / output 3 commands for issuing the MCP 81-2 issues a group of commands from its register of commands for outputs 3-1 ÷ 3-n received at the output key node of the UVK. The “Issue” command from the output 2 of the MCP 81-2 gates the UVK 84 and transmits the corresponding signals to the output relays 85. When contact groups 88 of the relay 85 operate, the signals from the feedback outputs 1-2-1 ... 1-2-n with a delay of τ by the delay element 86 is recorded in the feedback register of the MCP 81-2 at the inputs 4-1 ÷ 4-n by the command to the input 5 of the MCP.

Often, before the regular work with real control objects, the operation mode “with removal from the object” is performed.

For this purpose, separately formed commands for switching on the inputs of USOTO and BVVDI with separate power sources in URVEP 9-1 ÷ 9-4 are provided.

Removal from an object means that information from control objects does not enter the system and the system does not issue control commands to control objects.

This is achieved by the fact that in IWEP 1 ÷ 4 IEP 56-2, 56-5, 56-7, 56-9 are not included. This ensures that power is not received at INAI 67-1 ÷ 67-n and at BIDS 66-1 ÷ 66-k. At the inputs of the NDD 53-4 ÷ 53-6 and at the inputs of the MACP 65-2 ÷ 65-4, zero information is received from the outside, which will eventually be transferred to the corresponding ARMO. In NDD 53 (Fig. 24), it is possible to work with information arriving either externally from inputs 1-1 ÷ 1-k through input elements 77-1, 77-3 ... 77-2k-l, or by internal test signals from input elements 77-2, 77-4 ... 77-2k from the shaper 79 test packages FTP. If there is no voltage at input 3 from microprocessor 81-1 from NDD, commands are issued for output 3 of MCP 81-1 “test mode”. From the output of the key 78, power is supplied to the EGR 77-2, 77-4 ... 77-2k. Shaper 79 test parcels, receiving the command "test parcels" from the output 4 of the MCP 81-1, received at input 2 of the shaper 79, gives signals to the inputs of the EGR 77-2, 77-4 ... 77-2k. NDD works on test packages that are recorded in the MCP 81-1 and transmits the input codes to the MCP 81 or BVVDI via the input-output 6 of the MCP through the M1 ÷ M3 bus lines test codes. Through the service input-output 8 of the MCP 81-1, the work program is recorded in the debug preparatory period from the input-output 5 of the VAT.

In order not to issue commands from the automated control system of the launch vehicle in the mode of detachment from the facility, the UZIES 14-1, 14-2, UZIE 16-1, 16-2, 16-5, 16-6, 16-9, 16-10 are not turned on . Then the power to the IE does not come from these devices. From the outputs of feedbacks 1-2-1 ... 1-2-n, information can be read and written in the MCP 81-2 in the RGOS at the inputs 4-1 ÷ 4-n. Thus, the mode of removal from the object is more complete than the "dry refueling", can check the performance of the automated control system of the launch vehicle.

ACS RN interacts with external adjacent systems both at the remote command post of the CPSU and at the starting position in the starting structure of the SS.

At the CPSU, interaction with the automated process control system of ground equipment (ACS TP NO) is carried out by group inputs and outputs, from the guaranteed power supply system (CGEP), ground-based measurement system (SED), single-time system SEV - by group inputs. These systems are connected, respectively, to the second, fourth, sixth and eighth group inputs-outputs of the UUS 1-1 (figure 4). These inputs and outputs are connected respectively with the first, second, third and fourth inputs and outputs of three multi-channel interface cards (MICs) 27-1 ÷ 27-3. Signals from external devices are received by these MICs, and they also form commands for industrial control systems NO, group inputs and outputs 5 MICs 27-1 ÷ 27-3 through the bus lines exchange information with the central processor 26. Information from external adjacent devices to the VKP is transmitted to ARMO 2-1, where it is included in the general algorithm of interaction with adjacent systems.

At the starting position in the SS start-up structure, the automated control system for automated control systems of missiles receives information from the ground-based automated control system of the control system of the NASU PH for group input-output 8, issues a command for group output 7 of the BVVDI 15-7. Information from the system for measuring the parameters of the technological object SIP TO via group input 14 is fed to group input 2 of the control system 1-5 and then through the MIC 27-1 ÷ 27-3 and bus lines M1 ÷ M3 to the central processor 26. From the BVVDI output to SEV information it is transmitted by the contacts of the output relays, and from the input subgroup 8-3, information from the NASU RN through IEC 62-n + 1 goes to the NDC 53-7 ÷ 53-9 and then through the bus lines M1 ÷ M3 to the processors 29-8 ÷ 29-10 .

With the LV systems, the M2 model of the ASUP RN interacts after supplying power to the system converters from the ultrasonic sensors 14-1 and 14-2 and receives information through the first and second subgroups 13-1 and 13-2. Information from the LV systems arrives at the group inputs-outputs 2 and 4 of the DCS 1-2. In UUS 1-2 information from the LV systems goes to the MIC 27-1 ÷ 27-3 and then through the bus lines M1 ÷ M3 to the processor 26.

The inventive automated control system for the preparation of launch vehicles can be implemented in the following form.

Personal computer for ARMO (figure 2) and remote control PSK APS (figure 3) in the configuration:

- system unit 19 comprising:

- Core 2 DUO E8600 3.33 / 1333 / 6M / LGA775 processor

- housing GHI 252V2U with power supply 300 W, USB / F, white

- memory module not less than DDR 2 2Gb

- a hard disk of at least 320 Gb 7200

- DVD RW

- MV type MSI P45T-C51

- video card GigaByte GV-210 OS 512 Mb

- network card type D-Link DGE 530T

- external devices

- keyboard 20 USB

- manipulator 21 "mouse" USB

- software Windows XP Prifessional Russian (oem)

- 18 30 "TFT monitor complete with HDMI-HDMI cable

- USB 23 port switch - Aten CS 1764 type KVM switch

- network adapter from USB 24 output - Trendnet TU2-ETG USB 2.0 k Gigabit Ethernet

- printer 36 network type HP 5200 n

- Ethernet switch 17 network type FGSW-2620

- automatic transfer switch 22 - backup power switch type ARS AR7723.

The control and communication device 1 (Fig. 4) and a central processor 26 (Fig. 5) and a software simulator (Fig. 6) are implemented as follows:

- Ethernet switches 17-5 and 17-6 type AT-8524

- Fault Collection Node 25-1 - ADAM 6051

- multi-channel interface cards 27-1 ÷ 27-4 - CPCI-3544

- multi-nominal power supplies 28-1 ÷ 28-5 - Power Modul CPCI 250 w - P AC / DC

- processors 29-1 ÷ 29-4 - SRS-502 (RSZ.037.542)

- power management device 30 IPM-8002

The primary power distribution device 4 (Fig.7) is implemented as follows:

- switch 31 control modes - switch K1N-014 ULH from Shneider Electric and buttons MP1-20G and MP1-20R from ABB

- relay 32-1 and 32-2 phase control - EL11M-08 company Meander

- Switches 33-1 and 33-2 of battery power supply UBEP - K1N-014 ULH from Shneider Electric

- electrical contactors 34-1 and 34-2 with contact groups 35-1 and 35-2 - A110-30-2280 of ABB

- sources 37-1 and 37-2 of secondary power supply - DNR 240 PS 24-01 from XP-POWER

- individual machines 38-1 ÷ 38-20 single-phase in assortment of 6 A, 10 A, 16 A and 25 A - type D, respectively, categories No. 06579, 06581, 06583 and 06585 from Legrand

- automatic transfer switch 22-5 - АРС АР7723 of company АРС

- emergency switching units 39-1 and 39-2 - K1C-003 ALH from Shneider Electric.

Devices 5-1 ÷ 5-4 uninterrupted power supply (Fig. 8) are taken as purchased equipment; APC type Smart-UPS RT 20 kvA from APC.

Network system switch 6 (Fig.9) is implemented as follows:

- network switches 17-16 ÷ 17-19 - type AT-8550 SP

- multi-nominal power supplies MIEP 28-7 and 28-8 - type AT-PWR 3004

- circuit breakers 45-1 and 45-2 contain a fuse that automatically turns off a relay indicator from the composition of the UVZ RP12-S RS5.289.455 device of the Orion company.

Remote control devices for primary power supply UDUPEP-VKP 7 (Fig. 10) and UDUPEP-SS 11 (Fig. 11) are implemented in the following form:

- network switches 17-9 ÷ 17-14 - ADAM-6521 from Advantech

- I / O modules MVV 49-1 ÷ 49-18 - ADAM 6050 from Advantech

- interface modules of the IRM relay 48-1 ÷ 48-12 49.31.7.024.0050 of the company Finder

- galvanic isolation element of power supply EGREP 46-1 ÷ 46-6 - DC / DC converter SD-15B-24

- nodes of the majority elements of VME 47-1 ÷ 47-4 are assembled on the relay contacts from the IRM 48.

In the communication devices of the fiber-optic information transmission line USVOLPI 8-1, 8-2 (Fig. 12), the optical signal transceivers that convert optical signals to signals of copper wire transmission lines and vice versa are implemented on the output stages of the ADAM-6521 MVV modules UDUPEP-SS and UDUPEP-VKP and on cascades of SSK AT-8550 SP switches.

The distribution devices of the secondary power supply URVEP 9 (Fig.13) are implemented in the following form:

- network switches 17-20 and 17-21 type EDS-G308

- electric contactor 34-3 - type 15984

- timer 51 - type ACTt 15419

- power supplies 63-1 ÷ 63-3 as part of the device UP37-S RS5.009.648 of the company "Orion"

- processors 52-1 ÷ 52-3 as part of the MP1-S PC3.037.810 block of the Orion company

- blocks NDD (Fig.24) and FSU (Fig.25)

- power supplies 56-1 ÷ 56-10 (Fig.21).

The functional readiness determination unit 12 (Fig. 14) is implemented as follows:

- multi-nominal power supply MIEP 28-9 - Power Modul CPCI 250 w - P AC / DC

- Fastwel processor 29-4 CPC-20302, Ml parallel bus of Compact PCI type

- shaper control signals FSU 54-4 - see Fig.25

- measuring power supply source IIEP 57 - has an output voltage rating of 27 ± 0.135 V, input voltage ~ 220 V. Variants of using the source are products of XP and Lambda (Nemic Lambda Ltd)

- keys 58-1 ÷ 58-4 - these are the contacts of the output relays FSU 54-4

- KAS 59-1 and 59-2 analog signal switches are implemented on relay contacts, relay type FTR-B4CA4.5Z from Fujitsu Components, inc. All. The register included in the switch is implemented on the KR1554TM8 microcircuits, the decoder is implemented on the KR1554ID7 microcircuits

- measuring transducers 64-1 ÷ 64-4 are implemented on PG204 microcircuits from BURR-BROWN

- multichannel analog-to-digital Converter 65-1, containing nodes:

- control and monitoring unit - based on Fujitsu microprocessor MB90F591GPE

- digital-to-analog converter - on the AD5542AR chip from Analog Devises

- operational amplifiers - on the OP2177AD chip from Analog Devises

- analog-to-digital converter - on an AD7894 chip from Analog Devises

- digital feedback selection node - on a BURR-BROWN chip PGA206

- analog signal switch is implemented on the ADG408BR chip from BURR-BROWN

- controlled voltage divider UDN 60 (Fig.23)

- node operating modes OAI 61 - see Fig.22

The device for powering the actuating elements and systems of the ultrasonic ultrasonic sensors 14 (Fig. 15) and the actuator for actuating the actuating elements of the ultrasonic sensors 16 (Fig. 16) are implemented as follows:

- automatic transfer switch 22-3 - backup power switch type ARS AR7723

- secondary power supply source IVEP 37-7 DNR 240 PS 24-01 from XP-Power

- keys 58-5 ÷ 58-8 on the contacts of the output relays of the input-output module 49-19

- I / O module 49-19 - on two ADAM 6051 modules

- power supplies 56-11 and 56-12.

A communication device with an object - technological equipment USOTO 13 (Fig.17) and the input-output unit of discrete information BVVDI (Fig.18) are implemented in the following form:

- processors 29-5 ÷ 29-10 - СРС 20302 of Fastwel company, bus lines M1 ÷ M3 of type Compact PCI

- multi-nominal power supplies MIEP 63-4 ÷ 64-9 as part of the unit UP 37-S RS5.009.648 of the company "Orion"

- normalizers of discrete data NDD 53-4 ÷ 53-9 (Fig.24)

- shapers control signals FSU 54-5 ÷ 54-10 (Fig.25)

- multi-channel ADC 65-2 ÷ 65-4 (Fig.26)

- intrinsic safety barriers of discrete signals BIDS 66-1 ÷ 66-k (Fig. 20) on the repeater elements of the state of contact sensors D1032 Q / B from GM International

- intrinsically safe analog information normalizers INAI 67-1 ÷ 67-m on the elements D1072 D / B of GM International (Fig.19)

- majority key elements 62-5 on the contacts of the output relays FSU 54-5 ÷ 54-7 (Fig.27).

The power source of the IEP 56 (Fig.21) incorporates modules 73-1 and 74-2. Modules rectifier specialized family SCAN 3.211.041 ÷ SCAN 3.211.048-08, company "CJSC SCAN".

Conjunctors 74-1 and 74-2 are implemented by mounting the contacts of the output relays from the rectifier modules. Type of relay - solid state PVT 312 or PS 7122 AL-2 manufactured by NEC.

The node operating modes OAF 61 (Fig.22) from the BOFG 12 is implemented on the relay contacts 75-1 ÷ 75-9 D2A 050000 of the company COSMO ELECTRONICS CORPORATION.

The controlled voltage divider UDN 60 (Fig.23) from the BOFG 12 consists of resistors 76-1 ÷ 76-5, 76-7 and the shunt divider 76-6 included in it. Keys 58-11 and 58-12 are the contacts of the output relay of the shaper 54-4 control signals.

The NDD discrete data normalizer 53 (Fig. 24), the FSU control signal generator 54 (Fig. 25) and the multi-channel analog-to-digital converter MACP (Fig. 26) have common nodes and specific nodes specific to each module.

Common nodes are implemented as follows.

The undervoltage circuit 80 is based on the P26TG2405E2: 1M power supply module from Peak Electronics and the Texas Instruments TPS2491DGS hot standby controller.

Elements 46-7 ÷ 46-9 of galvanic isolation on the Lite-on LTV-827 optocoupler, resistors in the performance: ChIP resistor J1206, ChIP resistor J2010, ChIP resistor F1206, ChIP resistor F1206, on the TL431 IPK zener diode from Texas Instruments, SMD075-2 fuse, capacitors: Chip capacitor ceramic X7R-50 K1206, Chip capacitor tantalum.

Microprocessors 80-1 ÷ 80-3 are implemented on a Fujitsu microcontroller MB90F591GPF.

Display elements 82-1 ÷ 82-3 are implemented using a set of: light-emitting diodes 551-0201 and 551-0401 from Dialight, chip resistors J1206, buffer register 74HC245D.

FSU 54 (Fig.25) in addition to common nodes has nodes implemented as follows:

- node 84 output keys - on chips 133 TM5;

- relays 85-1 ÷ 85-n - on bistable relays FTR-B4C В 4.5Z manufactured by Fujitsu Takamisawa;

- feedback node 87 — on Lite-on LTV-827 optocouplers, resistors in the performance of the J2512 chip resistor;

- contact nodes 88-1 ÷ 88-n, including the contacts of the control relay from relay 85, fuse 89 type FSMD 185-2 from Poly-Switch, diode 90 50SQ 0806 from International Rectiver;

- element 86 delay - on the chip 533AG3.

NDD 53 (Fig.24) in addition to common nodes has nodes implemented as follows:

- input elements 77-1 ÷ 77-2k-1 - for external signals - protective diodes SM6T-30 manufactured by Vishay;

- test elements 77-2 ÷ 77-2k for the test code - optocoupler LTV-827 from Lite-on;

- element 79 of the shaper of the test code - optocoupler LTV-827 company Lite-on;

- node 78 memory power supply - on a chip 133TM5.

MADC 65 (Fig. 26), in addition to common nodes, has a multi-channel ADC 91-2 assembly on an AD640AR analog-to-digital converter chip by Analog Devices and an ADG527AKR multiplexer on Analog Devices chip.

The proposed automated control system for the preparation of launch vehicles has several advantages over known systems; the introduction of the system allows it to be used to control the preparation of four models of launch vehicles of different classes instead of four separate control systems for the preparation of models BM, M2, M3, M4, which gives a significant gain in the amount of equipment.

ACS RN provides remote control of reconfiguration of the included equipment for the corresponding models of the carrier rocket family and automated electrical check of the working condition of communication circuits with control objects and related systems:

- control of docking signals for communication cables with control objects;

- insulation resistance control (for circuits: power supply, actuator control, analog and discrete sensors) relative to the housing;

- resistance control of communication circuits (for circuits: control of actuating elements, analog sensors);

- control of insulation resistance of communication circuits with the objects of control among themselves;

- control of signal transmission (for information transmission channels via a serial interface - LV systems and related systems).

ACS RN by providing power supply to control the actuating elements and the RN system allows not to expend power resources of the onboard equipment.

ACS RN provides for the input of data in explosion and fireproof circuits in a rational volume, determined by the configuration of the equipment of the control objects.

The automated control system for automated control systems of the RN implements optimal redundancy of the device structure (majorized structure) and connections between system devices to ensure a high probability of failure-free operation and high reliability of issuing commands to control objects.

Information sources

1. RF patent No. RU 2084011 C1, IPC G05B 9/03, 12/22/1995.

2. RF patent No. RU 2216760, C2 IPC G05B 17/02, dated 13.11.2001 (prototype).

3. Digital and analog integrated circuits: Reference S.V. Yakubovsky, L. I. Nisselson, V. I. Kuleshova and others. Ed. S.V. Yakubovsky - M .: Radio and communications, 1990.

4. Prosoft www.prosoft.ru. A brief catalog of Prosoft products 2007/2008.

5. COSMO ELECTRONICS CORPORATION, www.cosmoic.com. Product Catalog.

6. BURR-BROWN CORPORATION, www.dodeca.ru. Product Catalog.

7. Lite-on www.liteonit.eu/ru. Product Catalog.

8. Shneider Electric, www.shneider.com. Product Catalog.

9. Texas Instruments, www.ti.com. Product Catalog.

10. FUJITSU, www.fujtsu.com. Product Catalog.

11. Analog Devices, Inc, www.analog.com.ru. Product Catalog.

12. Yageo Corporation, www.yageo.com. Product Catalog.

13. Dialight Corporation, www.dialight.com. Product Catalog.

14. Vishay, www.vishay.com. Product Catalog.

15. International Rectifier, www.inf.com/indexnsw.html. Product Catalog.

16. Fujitsu-Takamisawa, www.tacy.co.jp/english/index.html.

17. Peak-electronics GmbH DC DC Converter, www.peak-electronics.de. Product Catalog.

18. Aimtec / AC-DC Converter / DC-DC Converters / Modular Power Supplies, www.amitec.com. Product Catalog.

19. DCCOM, www.dccom.ro/index1024htm. Product Catalog.

20. GM. International Technology for safety. Intrinsically safe interfaces of the D1000 series for process control systems in hazardous industries, www.gminternational.ru.

21. ABB, www.abb.com. Product Catalog.

22. APC, www.apc.com. Product Catalog.

23. Fincler, www.fincler.com. Product Catalog.

Claims (11)

1. Automated control system for the preparation of launch vehicles (ASUP RN), containing automated workstations of operators (ARMO), communication devices with a fiber-optic transmission line of information (USVOLPI), blocks for determining functional readiness (BOFG), communication devices with an object - technological equipment (USO), actuator triggering devices (USE), discrete information input-output blocks (BVVDI), while the inputs and outputs of the optical signals of the first FIRM are connected to the inputs and outputs of the optical Ignalov of the second USVOLPI, the first-fourth, sixth, tenth and fourteenth subgroups of the fifth group of inputs of the automated control system of the launch vehicle from the first poles of the executive elements of the control object, the subsystem for controlling the elements and systems of the launch vehicle through the first-fourth subgroups, the control subsystem for filling the first rocket fuel component (CRT ) through the sixth subgroup, the control subsystems for refueling the second SRT through the tenth subgroup, the thermostat subsystems (TST) through the fourteenth subgroup are connected to pairs - the second groups the first inputs of the corresponding BOFGs and the second group inputs of the first-seventh USO, the fifth, seventh-ninth, eleventh-thirteenth and fifteenth subgroups of the fifth group of inputs of the automated control system of the control system from the first poles of the actuating elements of the control object, the fueling control subsystem of the first SRT through the fifth, seventh and eighth subgroups, control subsystems for refueling the second SRT through the ninth, eleventh and twelfth subgroups, thermostat subsystems through the thirteenth and fifteenth subgroups are connected to the second group inputs of the corresponding BOFGs, the first group inputs of the second, sixth and tenth ultrasound detectors are connected to the first group outputs of the fifth to seventh USO, the fifth to fifteenth subgroups of the first group of ACS of the PH to the second poles of the actuating elements, the control subsystem for filling the first SRT through the fifth to eighth subgroups , subsystems for controlling the refueling of the second SRT through the ninth to twelfth subgroups, the subsystems of the TST through the thirteenth to fifteenth subgroups are connected respectively to the first group outputs Dams of the first to eleventh ultrasonic radiation sensors, the first to fourth, sixth, tenth and fourteenth subgroups of the sixth group of ACS LV inputs from discrete sensors of the control object, the subsystem for controlling elements and systems of the launch vehicle through the first to fourth subgroups, the control subsystem for refueling the first SRT through the sixth subgroup, the fuel supply control subsystems of the second SRT through the tenth subgroup, the TST subsystems through the fourteenth subgroup are connected to the first group inputs, respectively, of the first to seventh USO, the third input groups The first, third and fourth USOs are connected, respectively, with the first or third subgroups of the seventh group of inputs of the automated control system of the PH from analog sensors, characterized in that five control and communication devices (CCS) are additionally introduced into the automatic control system of the control gear, the first CCC with external adjacent remote systems command point (VKP), the second control room — with the elements and systems of launch vehicles, the third control room — with the process equipment for refueling the first SRT, the fourth control room — with the process equipment for refueling the second SRT, the fifth control room — with the technological equipment TST ore and external terrestrial systems, a remote control subsystem for hardware and software (PSK APS), two network system switches (SSK), four primary power distribution devices (URPEP), the first URPEP - VKP equipment, the second UREP - equipment in the starting structure, control equipment for the distribution of secondary power supply and UUS, the third URPEP - equipment of the launch facility, providing power to the systems and actuators of the launch vehicles, the fourth UREP - start equipment weapons providing power to the executive elements of the technological equipment of the control object - fueling control and temperature control subsystems, VKP primary energy remote control device (UDUPEP-VKP), primary power remote control remote control device (UDUPEP-SS), four secondary power distribution devices (URVEP) for various models of the carrier rocket family, the first URVEP for the base model (BM) of the launch vehicle, the second URVEP for the complementary equipment of the second model of the launch vehicle (DM2), the third URVEP for the additional equipment of the third model of the launch vehicle (DM3), the fourth URVEP for the additional equipment of the fourth model of the launch vehicle (DM4), four power supply devices for actuating elements and systems (UZIES), five software simulators for the corresponding DCS, four uninterruptible power supply devices (UBEP) for the corresponding UREP, the first group input-output of the automated control system of the launch vehicle from the inputs and outputs of the adjacent automated control system of technolo processes of ground equipment (ACS TP NO), the first group input of the automated process control system of the spacecraft from the guaranteed power supply system (SEC) of the cosmodrome, the second group input of the automatic control system of the spacecraft from the ground measurement system (SNI), the third group input of the automatic control system of the spacecraft from the single time system (SEV) are connected respectively, to the second, fourth, sixth and eighth group inputs and outputs of the first CCS, the first group input of which is connected to the first group output of the first UREP, the group inputs and outputs of the first to fifth software simulators are connected to to the nineth group input-outputs of the corresponding CID, the group inputs of the first to fifth software simulators are connected to the group outputs of the corresponding CID, the ninth group input-output of the first CID is connected to the first group input-output of the first CCK, the second to sixth group input-outputs of which are connected respectively to group inputs-outputs of the first-fourth ARMO and to the first group input-output of the PSK APS panel, group inputs of the first-fourth ARMO, the first SSK and PSK APS panel are connected respectively to the second the fifth and ninth group outputs of the first URPEP, the thirty-ninth group input-output of the first SSK is connected to the first group input-output of the first UVOLPI, the output of the first URPEP is connected to the first inputs of UDUPEP-VKP and the first UVOLPI, the third group input-output of UDUPEP-VKP is connected to the second group input-output of the first FIRM, the first group input-output of the UDUPEP-VKP is connected to the second group input-output of the PSK APS console, the first output of the first UBEP is connected to the second input of the UDUPEP-VKP, the first group input-output of the first UBEP with dinen with the first group input-output of the first URPEP, whose second group input-output is connected to the second group input-output of UDUPEP-VKP, the group output of the first SSK is connected to the first group input of UDUPEP-VKP, the first inputs of the second UVOLPI and UDUPEP-SS are connected to the output of the second URPEP, the first group input-output of the second USVOLPI is connected to the thirty-ninth group input-output of the second SSK, the second group input-output of the second UVOLPI is connected to the fourth group input-output of UDUPEP-SS, the first-third group inputs-output which are connected respectively to the second group inputs-outputs of the second-fourth UREPP, the first group input and the second-fourth inputs of the UDUPEP-SS are connected respectively to the first group output of the second SSK and to the first outputs of the second-fourth UBEP, the first group input of the second SSK is connected to the tenth group output of the second UREPP, the first to fourth group outputs of which are connected to the first group inputs of the first to fourth UREP, respectively, the fifth to eighth group outputs of the second UREP are connected to the first and group inputs, respectively, of the second-fifth UUSP, the first-fourth group outputs of the third UREP are connected to the first group inputs of the first-fourth UZIES, the first group output of the fourth URES is connected to the first group inputs of the first-fourth UZIE of the technological equipment of the fueling subsystem of the first SRT, the second the group output of the fourth UREP is connected to the first group inputs of the fifth to eighth ultrasonic ultrasonic sensors of the technological equipment of the fueling subsystem of the second SRT, t the third group output of the fourth UREP is connected to the first group inputs of the ninth to eleventh ultrasonic measuring devices of the technological equipment of the TST subsystem, the first group inputs and outputs of the second and fourth UBEP are connected to the first group inputs and outputs, respectively. the second-fourth UREP, the first-fourth group inputs-outputs of the second SSK are connected to the first group inputs-outputs, respectively, of the first-fourth UREP, the eighth to eleventh group inputs-outputs of the second SSK are connected to the first group inputs-outputs, respectively, of the first-fourth BOPG, twelfth the group input-output of the second SSK is connected to the ninth group input-output of the second CCS, the thirteenth to sixteenth group inputs and outputs of the second SSK are connected to the first group inputs and outputs, respectively about the eighth BFG, the seventeenth group input-output of the second SSK is connected to the ninth group input-output of the third CCS, the eighteenth to twenty-first group inputs and outputs of the second SSK are connected to the first group inputs and outputs of the ninth to twelfth BFG, twenty-second group input the output of the second SSK is connected to the ninth group input-output of the fourth CCS, the twenty third to twenty fifth group inputs and outputs of the second SSK are connected to the first group inputs and outputs of the thirteenth to fifteen, respectively FG, the twenty-sixth group input-output of the second SSK is connected to the ninth group input-output of the fifth CCS, the twenty-seventh-thirtieth group inputs-outputs of the second SSK are connected to the first inputs-outputs, respectively, of the first-fourth UZIES, thirty first-thirty-fourth group inputs- the outputs of the second SSK are connected to the first group inputs and outputs, respectively, of the first to fourth ultrasonic detectors, thirty-fifth to thirty-eighth group inputs and outputs of the second SSK are connected to the first group inputs and outputs, respectively of the eighth UZIE, the fifth-seventh group inputs-outputs of the second SSK are connected to the first group inputs-outputs of the ninth-eleventh ultrasound, respectively, the first and second outputs of the first URVEP are connected respectively to the first and second inputs of the first USO, the third output of the first URVEP is connected to the first the inputs of the first, fifth, ninth and thirteenth BOFG, the fourth and fifth outputs of the first URVEP connected respectively to the first and second inputs of the first BVVDI, the sixth and seventh outputs of the first URVEP connected respectively to the first and second inputs of the fourth air-conditioning device, the eighth and ninth outputs of the first URVEP are connected respectively to the first and second inputs of the seventh air-conditioning device, the first and second outputs of the second URVEP are connected respectively to the first and second inputs of the second USVO, the third output of the second URVEP is connected to the first inputs of the second, sixth , tenth and fourteenth BOFG, the fourth and fifth outputs of the second URVEP connected respectively to the first and second inputs of the fifth USO, the sixth and seventh outputs of the second URVEP connected respectively to the first and second the sixth USRO, the eighth and ninth outputs of the second URVEP are connected respectively to the first and second inputs of the seventh USO, the first and second outputs of the third URVEP are connected respectively to the first and second inputs of the third USO, the third output of the third URVEP is connected to the first inputs of the third, seventh, eleventh and the fifteenth BOFG, the fourth and fifth outputs of the third URVEP connected respectively to the first and second inputs of the second BVVDI, the sixth and seventh outputs of the third URVEP connected respectively to the first and second inputs and the fifth BVVDI, the eighth and ninth outputs of the third URVEP are connected respectively to the first and second inputs of the eighth BVVDI, the first and second outputs of the fourth URVEP are connected respectively to the first and second inputs of the fourth USO, the third output of the fourth URVEP is connected to the first inputs of the fourth, eighth, and twelfth BOFG , the fourth and fifth outputs of the fourth URVEP are connected respectively to the first and second inputs of the third BVVDI, the sixth and seventh outputs of the fourth URVEP are connected respectively to the first and second inputs of the sixth BVVDI, the first, third, fifth and seventh group inputs and outputs of the second CID are connected to the first group inputs and outputs of the first-fourth CID, respectively, the second, fourth, sixth and eighth group inputs and outputs of the second CID are connected to the first and fourth subgroups of the fourth groups of inputs and outputs of the automated control system for control systems with serial codes of the systems of the first to fourth models of the carrier rocket family, the first group outputs of the first to fourth ultrasonic sensors are connected to the first group inputs of the corresponding BOFGs and correspondingly with the first and fourth subgroups of the second poles of the actuating elements of the first group control system of the automated control system for the launch vehicle in the subsystem for controlling the elements and systems of the launch vehicle, the second group inputs and outputs of the first and fourth UZIES are connected to pairs - the fourth group inputs of the corresponding BOFGs and to the corresponding first to fourth subgroups the third group input-output of the automated control system for the power supply of the systems of the first to fourth models of the carrier rocket family, the first group inputs of the first to seventh USO are additionally connected s with third group inputs of the first, fourth, sixth, tenth, and fourteenth BOFGs respectively, the second group inputs of the first and fourth UZIES are connected to the first group outputs of the corresponding USOFs, the third group inputs of the first, third, and fourth USOFs are additionally connected to the fifth group inputs of the corresponding BOFGs, the first, third, fifth and seventh group inputs and outputs of the third CID are connected to the first group inputs and outputs of the first BVVDI, fifth USOTO, second and third BVVDI, first e group inputs of the fifth to fifteenth BOFG are additionally connected respectively to the first group outputs of the first to eleventh ultrasound, the first group outputs of the first to eighth BVVDI are connected to the first group inputs of the first, third to fifth, seventh to ninth and eleventh ultrasound, the first group inputs of the first the eighth BVVDI are connected, respectively, with pairs - the fifth, seventh, ninth, eleventh-thirteenth and fifteenth subgroups of the sixth group input of the automated control system of control systems from discrete sensors and third group inputs of the fifth, seventh-ninth, eleventh-thirteenth and fifteenth BOFGs respectively, the second group inputs of the fifth, seventh-ninth, eleventh-thirteenth and fifteenth BOFGs are additionally connected to the second group inputs of the first to eighth BVVDI, the first, third, fifth and seventh the group inputs and outputs of the fourth CID are connected respectively to the first group inputs and outputs of the fourth BVVDI, the sixth USO, the fifth and sixth BVVDI, the first-third and fifth group inputs-outputs of the fifth UUS are connected respectively to the first group input-output of the seventh BVVDI, the eighth group input of the automated process control system of the technological object (SIPTO), the first group inputs and outputs of the seventh USVO and the eighth of the BVVD, the second group input-output of the automatic control system of the vehicle from the ground-based automated control system the launch vehicle (NASU RN) is connected to the second group input-output of the seventh BVVDI and the fourth group input of the thirteenth BOFG, the third group output of the ASUP RN to the single time system (SEV) at the launch ozitsii connected to the second output of the group of the seventh to fifth and BVVDI multicast entry thirteenth BOFG. 2. The automated control system for the preparation of launch vehicles according to claim 1, characterized in that the control panel of the hardware and software control subsystem (PSK APS) contains three monitors, three system units, three universal keyboards, three mouse pads, three network switches , two automatic transfer switches, three USB port switches, three network adapters from the USB output and a printer, the first and second power supply networks of the first group input of the PSK APS console are connected respectively to the first and second inputs of two automatic transfer switches, exit q the first machine is connected to the first input of the first network switch, to the first inputs of the first and third system units, the first and third monitors, the first and third USB port switches, the output of the second machine is connected to the first inputs of the second and third network switches, printer, second monitor, system unit and port switch, the first and second buses of the first group I / O of the APS PSK console are respectively connected to the first inputs and outputs of the first and second switches, the first inputs and outputs of the first to third systems volume units are connected to the first inputs and outputs of the first to third monitors respectively, the second inputs and outputs of the first to third system units are connected to the first inputs and outputs of the first to third network adapters, the third to fifth inputs and outputs of the first to third system units are connected respectively to each other with a friend and with the corresponding first inputs and outputs of the first to third port switches, the second inputs and outputs of the first to third network adapters are connected respectively to the first and third buses of the second group the odes of the PSK APS remote control, the second inputs and outputs of the first and second network switches are connected to the sixth and seventh inputs and outputs of the first system unit, the third inputs and outputs of the first and second network switches are connected to the six and seventh inputs and outputs of the second system unit , the fourth inputs and outputs of the first and second network switches are connected respectively to the sixth and seventh inputs and outputs of the third system unit, the fifth inputs and outputs of the first and second network switches are connected respectively To the first and second inputs and outputs of the third network switch, the third input-output of which is connected to the printer input-output, the first and third universal keyboards are connected to the second inputs and outputs of the first and third port switches, the first and third mouse switches are connected with third inputs and outputs, respectively, of the first to third port switches. 3. The automated control system for the preparation of launch vehicles according to claim 1, characterized in that the control and communication device of the CCS contains two network switches, three bus lines, a fault collection unit, a central processor, a multi-nominal power supply (MIEP) and three multi-channel interface cards (MIC), the first, third, fifth, and seventh group inputs / outputs of the CCS have two buses of the local area network, the first of which are connected respectively to the seventh, sixth, fifth, and fourth inputs and outputs of the first network switch, the second buses of these inputs and outputs are connected respectively to the seventh, sixth, fifth and fourth inputs and outputs of the second network switch, the input-output of the fault collection node is connected to the first inputs and outputs of the first and second network switches, the first inputs of the first and second switches the networks are connected to the second bus of the first group input of the master control unit, the first bus of the first group input of the master control unit is connected to the MIEP input, both buses, the first and second, are connected to the corresponding buses of the first group input of the central the processor, the first group inputs of the first and second switches of the network are connected to the group output of the MIEP, which is also connected by a bus of one of the output ratings to the input of the fault collection unit, the second group input-output of the UUS, as well as the fourth, sixth and eighth inputs and outputs, consists of their three subgroups of inputs and outputs connected respectively to the first group inputs and outputs of the first to third MICs, three subgroups of inputs and outputs of the fourth group input-output of the DCS are connected to the second group inputs and outputs of the first to third MIC, three subgroups of inputs and outputs of the sixth group input-output of the MCS are connected respectively to the third group inputs and outputs of the first to third MICs, three subgroups of the inputs and outputs of the eighth group input-output of the CMC are connected respectively to the fourth group inputs and outputs of the first to third MIC, the first to third subgroups of the second group input / output and the corresponding subgroups of the second group input of the central processor are connected via bus I / O lines to the fifth group inputs / outputs the first-third MIC, the first and second buses of the third group input-output of the central processor are connected respectively to the second inputs and outputs of the first and second network switches, the third inputs and outputs of which are connected respectively to the first and second buses of the ninth group input-output of the CCS, the first and the second input / output bus of the tenth group input / output of the UCS is connected to the first group input / output of the central processor, the first group output of the central processor is connected to the first group output of the UCS, the first the outputs of the first and third MICs and the second MIEP output are connected to the corresponding buses of the first group input of the fault collection unit. 4. The automated control system for the preparation of launch vehicles according to claim 1, characterized in that the primary power distribution device (URPEP) contains a reserve input machine (ATS), a control mode switch, two phase monitoring relays, two network switches, two electrical contactors, two contact groups of the corresponding electric contactors, two sources of secondary power supply (IWEP), twenty individual automatic machines, two nodes of emergency switching, the first network bus power supply of the first group input RPEP is connected to the first inputs of the first phase control relay, the first failover unit, the first network switch and the input of the first power supply, the second mains supply bus of the first group input UREPP is connected to the first inputs of the second phase control relay, the second failover node, the second network switch and to the input of the second IWEP, the input bus of the first group input-output UREP is connected to the second inputs of the first and second nodes of the emergency switching, the output bus of the first group input-output UREPP connected to the output of the ATS, the first and second inputs of which are connected respectively to the first outputs of the first and second network switches, the second outputs of which are combined and connected to the bus "ATS connected" subgroup of the status outputs of the second group input-output UREP, the outputs of the first and second monitoring relays phases are connected respectively to the “Norma 380/220 V1” and “Norma 380/220 В2” buses of the subgroup of state outputs of the second group input of the UREP, the first output of the first IVEP is connected to the bus “IVEP1 turned on” of the subgroup of state outputs the second group input-output UREPP and combined with the first output of the second IVEP, which is also connected to the bus "IVEP2 included" subgroups of the state outputs of the second group input-output UREPP, the combined outputs of the first and second IVEP connected to the second inputs of the first and second electrical contactors and to the bus the positive pole of the output URPEP standby DC voltage, the second outputs of the first and second IVEP are combined and connected to the first input of the switch control modes and to the negative pole bus of the first output and URPEP standby DC voltage, the input bus command of the second group input-output URPEP connected to the second input of the switch control modes, the second and third outputs of which are connected respectively to the buses "Remote control" and "Local control" subgroup of outputs of the status of the second group input-output UREPP, the first output of the control mode switch is connected to the first inputs of the first and second electrical contactors, the outputs of which are galvanically connected to the second inputs of the respective contact groups, the output of the first emergency switching unit is connected to the first input of the first contact group and to the input of the ninth individual machine, the output of the second emergency switching unit is connected to the input of the second contact group and to the input of the nineteenth individual automatic device, the outputs of the ninth and nineteenth individual automatic devices are connected to the first and the second busbars of the ninth group output of the standby AC voltage, the first outputs of the first and second contact groups are connected respectively to the buses “220 V1 on” and “220 V2 on” are subgroups of the state outputs of the second group input-output UREP, the second outputs of the first and second contact groups are respectively connected to the inputs of the groups of individual machines of the first group of the first-eighth, tenth machines and the second group of the eleventh and eighteenth, of the twentieth automatic machines, the outputs of the first-eighth and tenth individual machines are connected to the first buses of the first-eighth and tenth group outputs of the UREP, respectively, the outputs of the individual machines of the eleventh on the eighteenth and twentieth are connected to the second buses of the first to eighth and tenth group outputs of the UREP, respectively. 5. The automated control system for the preparation of launch vehicles according to claim 1, characterized in that the network system switch (SSK) contains four network switches, two multichannel power supplies (MIEP), two circuit breakers, the first buses of the first to twenty-fourth group inputs SSK outputs are connected to the corresponding inputs and outputs of the first network switch, the first buses of the twenty-fifth to thirty-eighth group I / Os are connected to the corresponding first to fourteenth inputs and outputs of the second network switch, the second buses of the first to twenty-fourth group input-output SSK are connected to the corresponding inputs and outputs of the third network switch, the second buses of the twenty-fifth to thirty-eighth group input-output SSK are connected to the corresponding first to fourteenth inputs-outputs of the fourth network switch, twenty the fifth inputs and outputs of the first and second network switches are connected and connected to the first bus of the thirty-ninth SSK input-output, the twenty fifth inputs and outputs of the third and fourth network switches combined and connected to the second bus of the thirty-ninth input-output CCK, the first bus of the first group input CCK is connected to the input of the first circuit breaker, the second bus of the first group input CCK is connected to the input of the second circuit breaker, the first output of the first circuit breaker is connected to the inputs of the first and second MIEP, the first output of the second circuit breaker is connected to the second inputs of the first to fourth switches of the network, the output of the first MIEP is connected to the first inputs of the first and second about the network switches and with the bus “MIEP 1 on” of the first group output of the SSK, the output of the second MIEP is connected to the first inputs of the third and fourth switches of the network and to the bus “MIEP 2 turned on” of the first group output of the SSK, the second outputs of the first and second circuit breakers are connected respectively with tires “Feeder 1 on” and “Feeder 2 on”. 6. The automated control system for the preparation of launch vehicles according to claim 1, characterized in that the remote control device for primary power supply at a remote command post (UDUPEP-VKP) contains three network switches, three elements of galvanic isolation of power supply (EGREP), a majority element node ( VME), three interface relay modules (IRM), six input-output modules (MVV), the first input of the UDUPEP-VKP is connected to the inputs of the first and third EGREP, the output of the first EGREP is connected to the inputs of the first and second MVV and the first network utensil, the output of the second EGREP is connected to the inputs of the third and fourth MVV and the second switch of the network, the output of the third EGREP is connected to the inputs of the fifth and sixth MVV and the third switch of the network, the first group input of UDUPEP-VKP is connected to the group inputs of the first, third, and fifth MVV, the inputs and outputs of which are connected to the fourth inputs and outputs of the first to third switches of the network, three subgroups of the first group input and output of the UDUPEP-VKP are connected to the fifth inputs and outputs of the first to third switches, respectively networks, a subgroup of inputs of the second group input-output UDUPEP-VKP is connected to the first subgroups of the inputs of the second, fourth and sixth MVV, a subgroup of outputs of the VME is connected to the buses of the subgroup of the outputs of the second group input-output of the UDUPEP-VKP, the first and third group inputs of the VME are connected respectively to the second group outputs of the first-third IRM, group inputs and the first group outputs of the first-third IRM are connected respectively to group outputs and second subgroups of the group input of the second, fourth and net MVV, the inputs and outputs of the second, fourth and sixth MVV are connected to the third inputs and outputs of the first to third network switches, the second input of the UDUPEP-VKP is connected to the second input and output of the first network switch, the first inputs and outputs of the first to third network switches are connected respectively, to the first to third subgroups of inputs and outputs of the third group input-output UDUPEP-VKP. 7. The automated control system for the preparation of launch vehicles according to claim 1, characterized in that the remote control device for primary power supply in the launch facility (UDUPEP-SS) contains three network switches, three elements of galvanic isolation of power supply (EGREP), three nodes of majority elements ( VME), nine interface relay modules (IRM), twelve input-output modules (MVV), the first input of the UDUPEP-SS is connected to the inputs of the EGREP, the output of the first EGREP is connected to the inputs of the first network switch and the first and fourth BB, the output of the second EDGE is connected to the inputs of the second network switch and the fifth to eighth MVV, the output of the third EDGE is connected to the inputs of the third network switch and the ninth to twelfth MV, the first group input of UDUPEP-SS is connected to the group inputs of the first, fifth, and ninth MVV, the outputs which are connected to the fifth input-output, respectively, of the first-third network switches, the second-fourth inputs of the UDUPEP-SS are connected respectively to the ninth, eighth and seventh inputs-outputs of the first network switch, a subgroup of inputs of the first group the new input-output UDUPEP-SS is connected to the first subgroup of inputs of the second, sixth and tenth MVV, the group of outputs of the first VME is connected to the subgroup of the outputs of the first group input-output of the UDUPEP-SS, the subgroup of inputs of the second group input-output of the UDUPEP-SS is connected to the first subgroups the inputs of the third, seventh and eleventh MVV, the group of outputs of the second VME is connected to a subgroup of the outputs of the second group input-output UDUPEP-SS, the subgroup of inputs of the third group input-output of the UDUPEP-SS is connected to the first subgroups of inputs even of the eighth, eighth and twelfth MVV, the group of outputs of the third VME is connected to a subgroup of the outputs of the third group input-output UDUPEP-SS, the first to third group inputs of the first VME are connected respectively to the second group outputs of the first, seventh and fourth IRM, the first to third group inputs of the second VMEs are connected respectively to the second group outputs of the fifth, second, and eighth IRMs, the first and third group inputs of the third VME are connected respectively to the second group outputs of the third, sixth, and ninth IRMs, the inputs and first group outputs of the first-third IRM are connected respectively to group outputs and second subgroups of inputs of the second-fourth MVV, respectively, group inputs and first group outputs of the fourth-sixth IRM are connected respectively to group outputs and to second subgroups of inputs of the sixth-eighth MVV, group inputs and first group outputs of the seventh-ninth IRM are connected respectively to group outputs and second subgroups of inputs of the tenth to twelfth MVV, respectively, the inputs are the outputs of the second-fourth MVV are connected respectively to the fourth, third and second inputs-outputs of the first network switch, the inputs and outputs of the sixth-eighth MVV are connected respectively to the fourth, third and second inputs-outputs of the second network switch, the inputs and outputs of the tenth-twelfth MVV are connected respectively, to the fourth, third and second inputs and outputs of the third network switch, the first inputs and outputs of the first to third network switches are connected respectively to the first and third subgroups of the fourth group input yes output UDUPEP-SS. 8. The automated control system for the preparation of launch vehicles according to claim 1, characterized in that the secondary power distribution device (URVEP) (Fig. 13) contains two network switches, three multi-nominal low-voltage power sources (MIEP-N), an electric contactor, a time relay , three peripheral processors, three discrete data normalizers (NDI), three control signal conditioners (FSU), the majority element node (VME), ten power sources (IED), three bus lines M1, M2, M3, the first subgroup The first input of the URVEP is connected to the first inputs of the time relay, the electric contactor and the tenth IED, the second subgroup of the group input of the URVEP is connected to the second inputs of the time relay, the electric contactor and the tenth IEP, the first and second outputs of the time relay are connected respectively to the third and fourth inputs of the electric contactor, whose first output connected to the first inputs of the first to ninth IEP, the second output of the electrical contactor is connected to the second inputs of the first to ninth IEP, the outputs of the first to third MIEP-N are connected respectively to the first to third To the main lines, the first line is connected to the group inputs and outputs of the first peripheral processor, NDD, FSU and to the first input of the processor, the second line is connected to the group inputs and outputs of the second peripheral processor, NDD, FSU and to the first input of the second processor, the third line is connected to group inputs and outputs of the third peripheral processor, NDD, FSU and with the first input of the third processor, the first inputs and outputs of the first and third peripheral processors are connected respectively to the second and fourth inputs moves of the first network switch, the second inputs and outputs of the first to third peripheral processors are connected respectively to the second and fourth inputs and outputs of the second network switch, the inputs of both network switches and the first and third MIEP-N are connected to the output of the tenth IED, the group output of the tenth IED is connected to the tenth subgroup of group inputs of the first to third NDI, the group inputs of the first to ninth IEP are connected respectively to the first to ninth subgroups of the output of VMEs, the group outputs of the first to ninth IED are connected respectively to the first to ninth subgroups of the group inputs of the first to third NDI, the group outputs of the first to third FSD are connected respectively to the first to third group inputs of the VME, the outputs of the first to ninth IED are connected respectively to the first to ninth outputs of the UREC, the first inputs and outputs of the first and second network switches connected respectively to the first and second subgroups of input-output URVEP. 9. The automated control system for the preparation of launch vehicles according to claim 1, characterized in that the device for powering the executive elements and systems (UZIES) contains an automatic transfer switch (ATS), a secondary power supply (IWEP), an input-output module (MVV), two power supply source (IED), four electronic keys, the first subgroup of the first group input of the UZIES is connected to the first inputs of the ATS, the first and second IES, the second subgroup of the first group input of the UZIES is connected to the second inputs of the ATS, the first and second IES, the output of the ATS is it is single with the input of the IEDC, whose output is connected to the inputs of the MVE and the first to fourth electronic keys, the four outputs of the group output states of the first IED are connected to the corresponding first to fourth inputs of the group input of the MVE, the outputs of the positive and negative voltage poles of the first IED are multiplied and connected with multi-wire buses, respectively to the first group output and the second group input of the UZIES, the first and second inputs of the group input of the first IED are connected respectively to the outputs of the first and second electronic x keys, the inputs of which are connected respectively to the first and second outputs of the MVV group output, all four outputs of the group output states of the second IED are connected respectively to the fifth to eighth inputs of the MVV group input, the outputs of the positive and negative voltage poles of the second IED are multiplied and the multi-wire buses are connected respectively to a subgroup of outputs and a subgroup of inputs of the second group input-output of the UZIES, the first and second inputs of the group input of the second IED are connected respectively to the outputs of the third fourth electronic switches whose inputs are connected respectively to the outputs of the third and fourth output MBB group, group MBB input-output connected to a second input-output of the group UZIES. 10. The automated control system for the preparation of launch vehicles according to claim 1, characterized in that the communication device with the object - technological equipment (USOTO) contains three multi-nominal low-voltage power supplies (MIEP-N), three peripheral processors, three bus lines M1 ÷ M3, three discrete data normalizers (NDI), three control signal conditioners (FSU), three multichannel analog-to-digital converters (MASP), k discrete signal intrinsic safety barriers (BIDS), p major key elements (ME) K), m intrinsically safe analog information normalizers (INAI), the first input of the USOTO is connected to the first inputs of the first-third MIEP-N, the first-third NDD, the first-third FSD and the first-third MACP, three subgroups of the first group input-output of the USOT are connected respectively, to the pairs - the first and second inputs-outputs of the first to third peripheral processors, the second input of the USO is connected to the second inputs of the first to third NDI, the first inputs of k BIDS and the first inputs of m INAI, the outputs of the first and third MIEP-N are connected to the corresponding other highways М1 ÷ М3, the group inputs and outputs of the processors and their first inputs are connected respectively to the first or third bus lines, the first NDD, FSU and MATsP group inputs and outputs are connected to the first bus line, the second NDD, FSU and MACP group inputs and outputs connected to the second bus line, the third NDD, FSU and MatsP group inputs and outputs are connected to the third bus line, the inputs from the first to the k-th first group input USO are connected to the inputs of the corresponding first - k-th BIDS, the outputs of which are connected are inputs to the corresponding inputs of the group input of the first to third NDD, the inputs from the first to the pth second group input of the USOTO are connected to the fourth inputs of the corresponding first to the pth IEC, the outputs of which are connected to the corresponding outputs of the group output of the USOTO, the outputs from the first to p- nth first-third FSU are connected to the first-third inputs of the corresponding IEC so that any n-th output of the first-third FSU is connected respectively to the first-third inputs of the n-th IEC, inputs from the first to the mth third group input s with inputs, respectively, of the first - m-th INAI, each output of which is connected to the corresponding inputs of the first-third MACP. 11. The automated control system for the preparation of launch vehicles (ASUP RN) according to claim 1, characterized in that the functional readiness determination unit (BOFG) comprises a bus line, a multi-rated power supply (MIEP), a processor, a measuring power supply (IIEP), four electronic keys, a shaper of control signals (FSU), two switches, analog signals (CAS), a node of operating modes (URR), four measuring transducers, a multi-channel analog-to-digital converter (MAC), a controlled divider l voltage (UDN), the first input of the BOFG is connected to the inputs of the IIEP and MIEP, the first and second outputs of the IIEP are connected respectively to the first input of the UDN and the first input of the first electronic key, the output of which is connected to the eighth input of the UDN, the second input of the first electronic key is connected to the first single output of the first group output of the FSU, the MIEP group output is connected to the M1 bus line, the processor group input-output and its first input are connected via the bus line to the group FSO and MACP input-outputs and their second inputs, the first the processor input-output is connected to the BOFG input-output, the first to fifth group BOFG inputs are connected respectively to the first to fifth subgroups of the inputs of the second group input of the first and second CAS, the first group outputs of which are connected respectively to the first and second subgroups of the outputs of the first group output of the FSU, the outputs of the first and second UAN are connected respectively to the first and third inputs of the URR, the first to fifth outputs of which are connected respectively to the third to seventh inputs of the UDN, the second input of the URR is connected to the bus of the BOFG case , the first group input of the URR is connected to the sixth group input of the BFG, the second group input of the URR is connected to the third subgroup of the outputs of the first group output of the FSU, the first group input of the UDN is connected to the fourth subgroup of the outputs of the first group output of the FSU, the first output of the UDN is connected to the second input of the fourth measuring transducer the output of which is connected to the fourth single input of the first group input of the MACC, the first input of the fourth measuring transducer is connected to the eighth single output of the first group FSU output, the third input of the fourth measuring transducer is connected to the third inputs of the first to third measuring transducers, the first input of the second electronic key and the second output of the UDN, the first input of the first measuring transducer is connected to the fifth single output of the first group output of the FSU, the output of the first measuring transducer is connected to the third single input of the first group input of the MACP, the third output of the UDN is combined with the output of the second electronic key and connected to the second input of the first measuring transducer, the first input of the second measuring transducer is connected to the sixth single output of the first group output of the FSU, the second inputs of the second to fourth electronic keys are connected respectively to the second and fourth single outputs of the first group output of the FSU, the first input of the third electronic key is connected to the fourth output of the UDN, the fifth output of which is combined with the output of the third electronic key and is connected to the second input of the second measuring transducer, the output of which is connected inen with the second single input of the second group input of the MACC, the first input of the third measuring transducer is connected to the seventh single output of the first group output of the FSU, the output of the third measuring transducer is connected to the first single input of the first group MACC, the second input of the third measuring transducer is connected to the seventh output of the UDN, sixth the output and the second input of the UDN are connected respectively to the first input and output of the fourth electronic key.

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