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Automated control system for carrier rockets preparation and launching |
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IPC classes for russian patent Automated control system for carrier rockets preparation and launching (RU 2491599):
Radio-frequency identification system and elements for rolling mill / 2474859
System and method to be applied in the rolling device containing multiple bearing units; besides, each unit includes elements comprising guides (12, 18) and sets (20) of pads of rolling mill rolls. RFI system uses RFI marks on each of the variety of elements so that monitoring of characteristics or the whole bearing unit, or its individual elements, can be observed and/or performed. Readout device for RFI mark can be built into rolling mill (10) or can include portable devices. As per the first design version, scanning of RFI mark is performed both at the rolling mill, and at some remote point, to which is the bearing unit is supplied. Unique combination of load-carrying elements can be assembled, identified and subject to monitoring during subsequent rolling processes, thus allowing the operator of the rolling mill to perform the adjustment to improve the rolled product quality.
X-tree control method and device for its implementation / 2453683
Control method of X-tree consists in opening/closing of shutoff-control valves by supplying the working medium to mechanisms of actuators of underground cutout valve, side and master gate valves by means of control station. Control station includes pneumatic hydraulic system connected through monitoring sensors of station operation parameters to control unit of the station. As control unit there used is software-and-hardware system with local control panel containing a display with sensor control to enter commands in on-line mode and local keyboard.
Device for developing programmes, device for computer numerical control, programme generation method / 2438849
Inventions are referred to machine-building industry and may be used for controlling mechanical treatment of work pieces by using computer numerical control programme. The device for computerised numerical control of mechanical treatment includes device for generating programmes. The device ensures that programme is generated based on the data from the machined work piece shape and data on tolerable limits for shape data. The device contains a calculation unit of target mechanical treatment sizes, processing unit of shape data distortion and mechanical treatment programme generation unit. The tolerable limit data contain data on changed positions, relating to the method of moving graphical elements. The processing unit of shape data distortion is designed so that graphical elements positions can be set after their movement based on the above information on position change.
Method of configuring hollow spiral wheel machines and housings thereof / 2436143
Method of configuring components of hollow spiral wheels or housings thereof, in which values of input parameters are continuously checked for compatibility; mathematical parameters and basic configuration parameters are input; an operation is performed for configuration of profiles and other data which are specific for circular and spiral elements, the operation involving designing each front and rear edge using parts of geometric figures having a reference centre, and then joining them using parts of geometric figures, also having a reference centre, as a result of which sections of the body of the designed components are determined.
Automatic programming method and automatic programming device / 2333524
Invention refers to automatic programming devices used for automatic development of programs for numerically controlled machine tools. The machine working block corresponding to the cursor position on the editor display and to the model, consisting of the model of product and the model of workpiece displayed in the model display section, is displayed with highlighting and, during editing the created program, is strictly determined what cursor position on the editor display corresponds to which machine working block.
Automatic programming method and automatic programming device / 2331911
Invention refers to the technology of software development for the numerically controlled machine tool using automated design data such as product and bulging form. The data is chosen from the data base about the work piece describing the product's form and having the smallest diameter, for lathe machining around rotation axis by comparing data of the work piece model and the product model. Therefore the work piece model is located in such way that the central axis of each work piece correspond the centre of the rotation axis. The work piece model for lathe machining is created on the basis of chosen work piece data. The data about external diameter, internal diameter, length and tolerance value for machine working of the side end on basis of chosen work piece data are input in the corresponding data used for lathe programming as the work piece model for lathe machining.
Method of automatic programming and device of automatic programming / 2328033
Method of automatic programming includes the first processing that consists in definition of turning surface, which has the largest diameter in the product model, and determination of central rotational axis of defined turning surface as rotational axis of product model; the second processing that consists in displacement or turn of product model so that define axis of product model rotational axis corresponds to rotational axis of working model; and the third processing that consists in displacement of product model so that end surface of product model, which was displaced during the second processing, corresponds to initial point of program, which was preset in working model for automatic placement of product model for product model imposition on working model. Device contains the first unit of turning surface definition, the second and third units for displacement or turn of product model, the fourth unit for product model direction change.
Automatic programming method and automatic programming device / 2311672
Automatic programming method includes dividing mechanical processing area onto first processing area, where one end of template model is held for mechanical processing, and second processing area, where other end of template model is held for mechanical processing, and creation of program for controlling digital program control block on basis of mechanical processing area division by computing position which evenly divided volume of mechanical processing area towards lathe processing axis, as position of processing division which marks the boundary between first processing area and second processing area.
Cargo container for weapons module and container complex of rockets / 2491492
Container complex of missiles comprises container with launcher. Said container comprises stiff side and end walls, roof of two jointed panels and independent attachment panel. The main panel is rigidly jointed with the launcher while additional panel is equipped with a drive and arranged behind the main panel to turn about horizontal axis.
Mobile air defense system / 2487310
Mobile air defense system is installed inside a cargo container (1), which is prepared for transportation on a car chassis. Inside the container (1) there is a support (2) fixed on stands (3). On the support (2) there is a power boom (4) hingedly fixed with a power cylinder (5). Missile containers (6) are grouped by three into cassettes (7), which are crossed one above another with the help of a bearing frame (8). On the rear wall of the container (1) there is a lever (9), which is connected to the power cylinder (10). On the free end of the lever (9) there is a bracket (11) for a radar (12). The cover of the container (1) is divided into segments (14) and (15). To launch a missile, at first the lever (9) is turned with the roof and the radar (12) into vertical position, and then the boom is turned so that the boom (4), so that the frame (8) is vertically resting with the end against the container (1) floor.
Device for automatic drop and catch of cover of transporter-launcher container installed on missile launcher / 2484408
Invention relates to rocketry and is intended for removal of transporter-launcher container (TLC) covers on missile launchers (ML) before missile launch. The device is installed on ML and contains quick-release connection of cover with container butt, separable hinged joint of cover attachment to lower part of container butt, journals and catcher with shock-absorbers. Additional pair of journals on cover is located below cover's centre of gravity. The catcher is made as rotating frame with two pairs of grips (upper ones with hollows and lower ones) with spring-loaded latches. Rotating frame is equipped with stowing locks with spring-loaded tie-rods and slewing arms and simultaneously at both sides is spring-loaded by stoppers with damper hooks and is fixed with cover in dropped position. Axis of rotating frame and axis of cover hinged joint are positioned so that during simultaneous turn of rotating frame and cover the journals move into hollows of rotating frame grips. Shock-absorbers are provided with screw and ring springs. Screw springs interacts with rotating frame at initial part movement, ring springs - at final part.
Air system of turbopump plant of hydraulic torpedo launcher tube / 2483269
Air system of a turbopump plant of a hydraulic torpedo launcher tube comprises an air turbine, a compressed air cylinder, a cut-off valve and an air flow controller. The cylinder outlet is connected to the turbine by a pipeline via the cut-off valve and the air flow controller. The pipeline comprises two control stages, systems of air filling of the main cylinder, control of controller and cut-off valve operation with the help of a cutter. The system of cut-off valve control includes at least two cutters connected in parallel. In the air pipeline between the outlet from the cylinder and the controller there is a controlled switch installed for switching modes of operation of the turbopump plant. The switch of modes comprises limiters of air pipeline section - throttles, and by number of cutters - channels of their communication with the air pipeline.
Firearms and service projectile for firearms / 2482421
Weapon comprises a barrel, with a gas-port hole on a side wall, with a gas cylinder and a gas piston, where the barrel is made of two split parts, connected to each other with a threaded head, a bracket for fixation of barrel parts, a ratchet wrench with a fixator for screwing and unscrewing of barrel parts, a handle, a pusher, a pusher's stem, a "П"-shaped bracket for clamping of a service projectile, an electric current battery for creation of an ignition spark, a cock, a muffler. The muffler comprises a body, a sleeve tightly built into the barrel hole, a valve switch, a cylinder, which holds a piston, a stem and a return spring, an accumulator battery with an electric drive and an optical sight. The projectile for firearms is a cartridge, where a fire-resistant plastic bullet is placed, made with a figured slot and a lead hemisphere, electric contacts for ignition of powder and a mini rocket. The mini rocket comprises a body, which consists of a tail part with a chamber for powder and a pressure indicator, a starter casing, a perforated partition for fire transfer, and a front part with propellant.
Method for reducing gas-dynamic influence on ground of start position and launching station of starting missile jet stream at angles close to vertical angle and device for its implementation / 2481540
Device for reducing gas-dynamic influence on ground and launching station (LS) contains jet deflector in the form of additional jet propulsion engine (JPE) with elements of fixing, lifting and dropping, nozzle with cylindrical tip. Internal diameter and length of the tip depend upon diameter of critical nozzle, Mach number at nozzle shear, environmental pressure, gas total pressure in additional JPE. The device is connected to LS and by series of sequential pulses of jet stream it performs deflection of jet stream of starting missile from LS.
Mobile combat laser complex and method of increasing its combat efficiency / 2478179
Proposed complex comprises caterpillar-tracked fighting machine with combat laser there atop and, at least, one auxiliary machine with bogie landing carriage. Armored compartment of fighting machine accommodate fuel tank. Combat laser is mounted above armored compartment in vertical armored cylinder on rotary platform comprises liquid propellant rocket engine with turbo pump unit and combustion chamber arranged vertically to exhaust combustion products vertically upward, and, at least, one resonator arranged inclined to combustion chamber axis. Armored cylinder top part is closed by armored cap with hole made at its center to comply in shape in size with nozzle edge. Armored cylinder has holes to accommodate resonator lenses. Auxiliary machines make one refueller one oxidiser feeder. Every complex on the move comprises, at least, two machines: fighting vehicle with combat laser and refueller.
Mobile combat laser complex and method of increasing its combat efficiency / 2478178
Proposed complex comprises caterpillar-tracked fighting machine with combat laser there atop and, at least, one auxiliary machine with bogie landing carriage. Armored compartment of fighting machine accommodate fuel tank. Combat laser is mounted above armored compartment in vertical armored cylinder on rotary platform and comprises liquid propellant rocket engine with turbo pump unit and combustion chamber arranged vertically to exhaust combustion products vertically upward, and, at least, one resonator arranged inclined to combustion chamber axis. Armored cylinder top part is closed by armored cap with hole made at its center to comply in shape in size with nozzle edge. Armored cylinder has holes to accommodate resonator lenses. Auxiliary machine makes, at least, one refueller.
Device for lifting carrier rocket mounter and retaining it vertically at launch pad / 2477247
Invention relates to aerospace engineering and may be used in preparing carrier rockets for launching at highly-automated lunch pad. Proposed device comprises frame resting on starting structure, boom pivoted to frame and provided with boom drive hydraulic cylinder, hydraulic and electrical equipment. Frame is composed of a base secured with concrete starting structure and two triangular-box-section beams interconnected by crossbar. Bosses to secure boom drive hydraulic cylinder lower axle are welded in lengthwise beams while ears are made at top ends of said beams to secure boom rotational axles. Said boom is composed of lengthwise beams, tail beam and crosswise beams. Bosses to secure hydraulic cylinder top axle and bosses to secure boom to frame are welded in lengthwise beams. Carriage composed of frame and two bars is mounted at crosswise beams. Said bars are integrated into rigid frame structure to make carriage guides.
Mobile combat laser system, and method for improving combat effectiveness of that system / 2473039
Ground laser combat system includes combat vehicle with combat laser in upper part. Combat vehicle is made based on a tank containing caterpillar undercarriage, lower platform, and oxidiser and fuel tanks. Combat laser is installed above oxidiser and fuel tanks, and combat laser includes liquid-propellant rocket engine and resonator, which are installed mutually perpendicular. Auxiliary machines are made in the form of at least one oxidiser refueller and at least one fuel refueller. Method for improving combat effectiveness of the system consists in the fact that for each system there added to combat transport column on the move are at least three machines: combat machine with combat laser and at least one oxidiser refueller and one fuel refueller. Combat machine participates in fighting using combat laser till complete depletion of oxidiser and fuel; after that, oxidiser and fuel refuellers perform oxidiser and fuel filling, and combat plant is again involved in fighting.
Transport-launching module / 2245503
The transport-launching module has a sealed casing in the form of a cup with the front and rear covers with a seal. A rocket with a nose cone is installed inside the cup. The rocket nose cone partially projects from the cup, and in the assembled state of the transport-launching module serves at the same time as the front cover of the transport-launching module cover. The transport-launching module is provided with a changeable ring component, whose one end face is conjugate to the respective end face of the cup. Longitudinally positioned threaded members (for example, bolts) are passed through the changeable ring component, with the aid of them the changeable ring component is connected to the cup. BY means of longitudinally positioned break-off components made in the form, for example, of explosive bolts, as well as of radially positioned break-off components made, for example, in the form of explosive bolts the changeable ring component is fastened to the rocket nose cone. Inside the transport-launching module provision is made for an obturator, which is positioned in the bottom (tail) section of the rocket. The cup is made with an inner smooth cylindrical surface. Detachable means for creation of a behind-rocket volume of the preset value are installed on the rear cover with the id of brackets.
Guiding device for missile launching / 2246679
The guiding device has a launching tube, device for missile roll twist made in the form of lugs on the missile body engageable with the inner surface of the launching tube, and plate springs fastened in cantilever to the missile body generating line. A ring-shaped flange is installed on the rear end of the launching tube, it has a bore and grooves, in which the tops of the lugs are located with a stop at their end face surfaces, the lugs have sharpened edges turned relative to the missile longitudinal axis through the twist angle. The lugs are positioned in the center of the springs, and a ring with a stop at the end face surface of the lugs is installed in the bore.
Hand grenade launcher / 2247914
The engine body is made integral with the barrel, with centering outer ring bands. An annular shoulder is made on the inner side on the boundary of separation of the engine body and barrel. The pre-combustion chamber is made in the form of a thin-walled metal tube with an inner annular stop on the end face at the annular shoulder and gas conducting openings, and installed in the front bottom of the engine up to the stop against the annular shoulder. The tensioner is centered by a perforated diaphragm in the unconfined space of the grenade rear section and installed inside the pre-combustion chamber on the annular stop of the thin-walled tube. The tensioner represents a screw with a cylindrical head, on which gas conducting grooves are made in the same plane with the gas conducting openings. An additional powder charge is covered with a lattice. An adapter in the form of a short tube with a blind bottom that divides the adapter into two planes - one with a perforated surface and the other - with throttle openings and an initiator is installed between the pre-combustion chamber and the engine nozzle block, the igniter is fastened around them on the outer side.
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FIELD: electricity. SUBSTANCE: system contains four automated workstations for operators, a panel of software-hardware modules control subsystem, customer's movable panel, five control and communication devices; two communication devices with fibre-optic link for data transfer, two network switches, three distributors for primary power supply, remote control device for primary power supply, remote control device for primary power supply of the launcher, two distributors for secondary power supply (DSPS), two power supply units for actuating elements and systems, three uninterrupted power supply units for DSPS, eight launchers for actuating elements, nine units to define functional readiness, seven units to input/output of discrete data, power supply distributor for equipment of central timing system, time data processor, unit to input/output of analogue and discrete data, two devices for spark-proof input of analogue data, seven devices for spark-proof input of discrete data, device for spark-proof input of discrete sensors of motion contact, processor of discrete signals, two power supply units for pyroelements. EFFECT: in-line check of rocket lift-off commencement and synchronisation of a final launching phase. 7 cl, 37 dwg
The invention relates to complex products of automation and computing, it can be used for automation objects, important and dangerous conditions, mainly in the aerospace industry. Known automated redundant control system filling cryogenic upper stage (ARSUZ ISC) (patent RF №2216760 C2 IPC G05B 17/02 from 13.11.2001,) that contains system-wide communication line, the device operational data changes (WAID), the device initial exchange priorities (UNEP), the local device management (LUU), communication devices with fiber-optic communication line (USUALE), communication device with the object subsystem works with the components of the booster block (SPAN), communication devices with object - process equipment (USATO) filling and software components, the determination of the functional blocks readiness (BOFG), the start device of the Executive elements (USIA), local control panel, the block I / o discrete data control device startup actuators and communication with the Central system training flight (BWDI), station a freelance management (IEDs), blocks of watchdog timers (BST), a block adjustable input information (BRVI), blocks of variable frequency survey (BPCA), blocks determine the validity of vvdimagination information (BODAI), blocks adaptive input information (BAVI), BST consists of node encryption and status display controller LAN CPU (USIC), node time (SPM), the node of the adjustable delay signal failure (protective relays), IED consists of a control reserve center (URC), junction with system-wide communication line, node interfacing with the system bus, connected by a set of external and internal relations, LOU consists of a workstation operator (ARMO) and Central processing unit (CPU). However, the above system (1) has a number of disadvantages, not allowing its use as a universal automated control system preparation of a family of launch vehicles. The most important of them are as follows: is not provided by spectacle the onboard systems of the launch vehicle by placing them at the start of the pre-operational period; is not provided in full control of the circuit connection with the control objects (PH and ground technological equipment): no verify the correct resistance of the circuit element, determine the galvanic separation of the elements of the control object and their relations; - no provision of uninterrupted power supply for the work of the preparatory cycle, when the power supply is istemi is not from an uninterruptible power supply systems; - not exempt operators of the subsystems of the management from the collection and diagnostics fault "of his" equipment; - the structure of the highways network of exchange between the individual devices of the system does not exclude the presence of collisions while accessing shared communication line, which slows down the transmission of data; this is especially dangerous in the pre-launch period. The closest in technical essence of the present invention is the automated management system training boosters (RF patent No. 2450306 C1 IPC G05B 19/00 from 10.05.2012), which contains four workstations operators, two communication devices with fiber-optic transmission line information, about fifteen blocks determine the functional readiness, seven devices in communication with the object - process equipment, eleven devices running actuators, eight blocks of I / o discrete data, five devices, control and communications, remote control subsystem hardware and software, two network system switch, four devices in the allocation of primary power supply, remote control primary power remote command post, the remote control primary power supply one hundred is a Hilbert structure, four devices distribution secondary power supply for different models of the family of boosters, four device power supply control devices and systems booster, five software simulators, four uninterruptible power supply connected by a corresponding set of links. However, the above system (2) has the disadvantage of not allowing its use for the final stages of preparation and start-up after refueling, which are characterized by the synchronization of the interaction of the fixing unit to start with the movement of the device allocation unit detachable joints (PP SRS) and exact fixation of the fact of the starting PH. The existing practice of synchronization of the above processes through other systems inaccurate, cumbersome and difficult. The problem solved by this invention is to expand the functional capabilities of an automated training system boosters engaged in loading and drain (if necessary), allowing monitoring and control of synchronization of interaction equipment launch complex with the launch of LV. Because of the specific hazards of the work and components of rocket fuel (MCT) in order to avoid abnormal emergencies automated system should have a high probability of RA is the notes and high reliability of formation issued commands to the control object. This can be achieved by introducing redundancy in the structure of the devices composing the system. For the optimality of price and quality, you must observe the principle of reasonable redundancy. Therefore, a hardware-software system is involved in the formation of management teams, have a structure with dual redundancy, ensuring the principle of majority control "two of three", the electronics power supply and network connection duplicated by the method of "hot spare". The electric circuit connection of the automated management system preparation and launch vehicles (MES PH) PH and elements of the launch complex pass through a temporary emergency intrinsically and fire and explosion hazard zone with the composition of the gas mixture of hydrogen with air. Therefore, all communications circuits must pass through the device intrinsically safe input analog and discrete signals. The technical solution is that the automated management system preparation and launch vehicles (MES PH), containing four workstations operators (ARMO), remote control subsystem hardware and software (PPS APS), five devices, control and communications (MCU), the first UUS - external related systems at the remote command post (BCP), the second UUS with elements and systems RA is em-media, third UUS process of filling the first component of rocket fuel (MCT), the fourth UUS process of filling the second MCT, fifth UUS - process temperature (TST) and external ground systems, each with the appropriate MCU software simulators (PI), two communication devices with fiber-optic transmission line information (USUALE), two network switch (FCS), three devices distribution primary power supply (UCAP), the first UCAP equipment of the CPSU, the second UCAP equipment in the initial construction, the third UCAP equipment starting structures providing power systems and actuators boosters, as well as the power of the Executive elements of the technological equipment of the control object, the remote control of the primary power supply of the CPSU (WUPAP-BCP), the remote control primary power supply starting structures (WUPAP-SS), the two devices distribution secondary power supply (ORWAP) for equipment management and control of the first (1 St) and second (2 St) LV stages, two devices for thermal actuators and systems (USIS), three uninterruptible power supply (mbea) for relevant UCAP, eight devices is the Executive upucka elements (USE) technological equipment facility management - management subsystems dressing and temperature control, nine blocks determine the functional readiness (BOFG), seven blocks I / o discrete information (BWDI), with group input-output optical signals of the first USUALE connected with group input-output optical signals of the second USUALE, the first group of input-output MES PH of inputs and outputs related automated control system of technological processes of ground-based equipment (APCS), the first group entrance MES PH uninterruptible power systems (CGAP), the second group input MES PH from system ground-based measurements (NDA) connected respectively to the second, fourth and sixth group of the inputs-outputs of the first MCU, the first group whose input is connected to the first output of the first group UCAP, group inputs and outputs and the inputs of the first to fifth software simulators PI connected respectively to the tenth group inputs-outputs and the outputs of the respective UUS, the ninth group of input-output of the first MCU is connected to the first group the entrance-exit of the first FCS, the second to the sixth group of the inputs and outputs of which are connected respectively to the first group inputs-outputs of the first-fourth ARMO and PPS APS, the first group inputs of the first-fourth ARMO and PSK The APS are connected respectively with W the eye of the fifth and the first duty group outputs the first UCAP, the twenty-eighth group of input-output of the first FCS is connected to the first group input-output first USUALE, the first duty of the DC voltage of the first UCAP connected with the first inputs of WUPAP-PCO and the first USUALE, the second group of input-output UDUPA-BCP is connected to the second group input-output first USUALE, the first group of input-output UDUPA-BCP is connected to a second group of exit and entrance PPS APS, the first input-output of the first mbea connected to the first input-output UDUPA-PCO group inputs and outputs of the first-third of the crimes connected with the first group inputs-outputs corresponding UCAP, the second group of input-output of the first UCAP connected to the second group input-output UDUPA-PCO group the output of the first FCS is connected to the first group input UDUPA-BCP, the sixth group, the output of the first UCAP connected to the first input of the first group SCQ, the third group entrance MES PH from the external power supply from distribution Board power supply (SRP) is connected with the first group inputs of the first-third UCAP, the first inputs of the second USUALE and UDUPA-SS connected to the first output of the duty of the DC voltage of the second UCAP, the first group of input-output the second USUALE connected with the twenty-eighth group entrance-exit of the second FCS, the second group of input-output the second USUALE connected to the third group input-output UDUPA-SS, the first and second group inputs and outputs which are connected respectively with the second group inputs-outputs of the second and third UCAP, the first group input UDUPA-SS is connected to the first output of the second group SCQ, the first and second inputs-outputs UDUPA-SS are connected respectively to the first inputs-outputs of the second and third mbea, the first group to the second input of the FCS is connected to the eighth group to output a second UCAP, the first and second group the outputs of which are connected with the first group inputs respectively of the first and second ORWAP, third-seventh group outputs the second UCAP connected to the first group to the second inputs-fifth UUS, the first inputs of the seventh and eighth USE, the first and second group outputs the third UCAP connected with the first group inputs respectively of the first and second USES, the third output of the third group UCAP connected to the first group the inputs of the first and second USE, the fourth output of the third group UCAP connected with the first group the inputs of the third and fourth USE, the fifth group the output of the third UCAP connected to the first inputs of the fifth and sixth USE, the first and second group the inputs and outputs of the second SCQ connected with group inputs and outputs respectively of the first and second ORWAP, third and fourth group inputs and outputs the second FCS under the turned off to the first group inputs-outputs, respectively, the fifth and sixth USE, the fifth and sixth group of the inputs and outputs of the second SSC are connected with the first group inputs and outputs respectively of the first and second BOTH, seventh, tenth, thirteenth and sixteenth group of the inputs and outputs of the second FCS is connected to the ninth group inputs-outputs, respectively, of the second to fifth UUS, eighth and ninth group inputs and outputs of the second SSC are connected respectively to the first inputs-outputs of the third and fourth BOTH, eleventh and twelfth group inputs and outputs of the second SSC are connected respectively to the first group inputs-outputs of the fifth and sixth BIG, fourteenth and fifteenth group inputs and outputs of the second SCQ connected respectively with the first group inputs-outputs of the seventh and eighth BIG, seventeenth and eighteenth group inputs and outputs of the second SSC are connected respectively to the first group inputs-outputs of the first and second USES, nineteenth to twenty-fifth group the inputs and outputs of the second SSC are connected respectively with the first group inputs-outputs of the first-fourth USE, ninth BIG, seventh and eighth USIA, the third output of the first ORWAP connected to the first inputs of the first, third, fifth, seventh and ninth BIG, fourth and fifth outputs of the first ORWAP connected respectively with the first and second inputs of the second BWDI the sixth and the seventh is the second outputs of the first ORWAP connected respectively to first and second inputs of the fourth BWDI, the eighth and ninth outputs of the first ORWAP connected respectively with the first and second inputs of the sixth BWDI, the first and second outputs of the second ORWAP connected respectively to first and second inputs of the first BWDI, the third output of the second ORWAP connected with the first inputs of the second, fourth, sixth and eighth BIG, fourth and fifth outputs of the second ORWAP connected respectively to first and second inputs of the third BWDI, sixth and seventh outputs of the second ORWAP connected respectively with the first and second inputs of the fifth BWDI, eighth and ninth outputs the second ORWAP connected respectively to first and second inputs of the seventh BWDI, the first subset of inputs the fifth group of the input from the first poles of the Executive members of the object management subsystem control elements and systems of the booster is connected to the second input of the first group BOTH, the second-eighth subgroup of the inputs of the fifth group of the input from the first poles of the Executive members of the object management subsystem control elements and systems boosters through the second subgroup, the control subsystem filling the first component of rocket fuel (KRT) via the third and fourth sub-groups, the sub control filling of the second MCT through the fifth and sixth subgroups, engine temperature (TST) through the seventh and simou subgroups are connected to pairs accordingly, the second group the inputs of the second-eighth BIG and the second group the inputs of the first-seventh BWDI, the first and second subsets of the inputs of the sixth group of input from discrete sensors and signals dock object management subsystem control elements and systems of the booster is connected to the fourth group inputs respectively of the first and second BOTH, the first and second subset of outputs of the first group of the system output at the second pole of the Executive members of the object management subsystem control elements and systems booster connected to pairs of the first group inputs BOTH and the first group outputs USES respectively of the first and second BOFH and the first and second USES, the seventh group input from analog sensor object management subsystem control elements and systems of the booster is connected to the fifth input of the first group BOTH, the first and second subset of outputs of the second group of output MES PH on power systems, rocket management subsystem elements and systems booster connected to pairs, respectively, the second group outputs of the first and second USES and the third group the inputs of the first and second BOTH, the first and second subsets of the inputs of the ninth group of input channels codes system booster, podci themes of control elements and systems booster connected respectively with subsets of inputs of the second and the fourth group of inputs-outputs of the second UUS, third-sixth subgroups of the outputs of the first group of the system output at the second pole of the Executive members of the object management subsystem controls the filling of the first MCT via the third and fourth sub-groups, the sub control filling of the second MCT through the fifth and sixth subgroups are connected to pairs of the first group inputs BOTH and the first group outputs USE respectively third to sixth BIG and the first-fourth USE, third, and fifth subset of inputs of the sixth group of input from discrete sensors and signal coupling facility control subsystem controls the filling of the first MCT through a third subgroup, the subsystem control filling of the second MCT through fifth subgroup are connected with pairs - the first group inputs BWDI and third group inputs BOTH respectively the second and fourth BWDI and the third and fifth BOTH, fourth, and sixth subgroups of the inputs of the sixth group of input from discrete sensors and signal coupling facility control subsystem controls the filling of the first MCT through fourth sub-group, subsystem control filling of the second MCT through sixth sub-group is connected to the third group inputs respectively the fourth and sixth BIG, group outputs of the first-fifth BWDI connected with the second group inputs, respectively, of the second USES the first-fourth USE, the first group inputs and outputs of the first-third BWDI connected respectively to the third group input-output second UUS, to the first and third group the inputs-outputs of the third UUS, the first group inputs and outputs of the third and fourth BWDI connected respectively with the first and third group inputs-outputs of the fourth UUS, seventh and eighth sub-groups of outputs of the first group of the system output at the second pole of the Executive members of the object management subsystem thermostat connected to pairs of the first group inputs BOTH and the first group outputs USE respectively the seventh and eighth BIG and the fifth and sixth USE, seventh subset of the inputs of the sixth group input from discrete sensors and signals dock object management subsystem thermostat connected to the pair of first group entrance on BWDI and the third group entrance seventh BIG, the eighth subgroup of the inputs of the sixth group of input from discrete sensors and signals dock object management subsystem thermostat is connected to the third group of the eighth input BOTH, the third group of input-output system from ground-based automated control system of the rocket (NASA PH) is connected with a pair of third group entrance on BWDI and the fourth group entrance seventh BIG, robovie outputs of the sixth and seventh BWDI connected to the second group inputs, respectively, the fifth and sixth USE, the first group inputs and outputs of the sixth and seventh BWDI connected respectively with the first and third group inputs-outputs of the fifth UUS, the first and third group inputs ninth BOTH connected respectively to the first group the outputs of the seventh and eighth USE, MES PH added power distribution equipment system of universal time (SPM), the device processing time information (WAVE), mobile remote customer (TEP), the block I / o analog and discrete data (BWADE), two devices intrinsically safe input analog information (TID), seven devices intrinsically safe input discrete data (TID-D), the device is intrinsically safe input discrete sensors "pin up" (TID-KP), the block processing of discrete signals (BODS), two power device of paraelemental (UPA), the third group the input of the system is additionally connected to the input of the TL, the output of which is connected to the third group input WAVE, the eighth group of the output of the first UCAP connected to the first group log FP, group input-output of which is connected to the eleventh group input-output of the first MCU, the first and second subgroups of the outputs on the group display TCH and time intervals VI, VI, the first and second subsets of the inputs of the time interval VI and the start signal of the second is hruppovoho input-output MES PH from common timing system (CTS) are connected respectively with the first and second group outputs corresponding group of outputs and the first and second group inputs corresponding group inputs WAVE, the second group of input-output WAVE connected to the eighth group input-output of the first MCU, the first group of input-output WAVE connected with the third group the entrance-exit of the first USUALE, the sixth group output third UCAP connected with the first group inputs of the first and second UPPA, the first output of the first ORWAP connected to the first input of BWADE, the second output of the first ORWAP connected with the second input BWADE, the power input of the first TID and TID-D, the tenth release of the first ORWAP connected to the first input of BEDS, the eleventh release of the first ORWAP connected to the power input the sixth and seventh TID-D, the second TID, TID-KP and the second input RODS, the first group of input-output of the second MCU is connected to the first group input-output BWADE, the first subgroup of the fifth group of input MES PH is additionally connected to the second group input BWADE, the output of the first group TID And connected to the third group input BWADE, whose first group input is connected to group the output of the first TID-D, the first group output BWADE connected to the first input of the first group USES, the fourth group of the input BWADE connected to the output of the second group uiv And, the first sub-group of the sixth group of the input MES PH is additionally connected to the input of the first group TID-D, the seventh group entrance MES IS N from analog sensors the first stage of the launch vehicle is additionally connected to the second input of the first group TID, whose first group input is connected to the eighth group of the entrance MES PH from analog sensors PRS, the second output of the second ORWAP additionally connected to the supply input of the second uiv-D, the first group of the first input BWDI connected to the output of the second group TID-D, whose group input is additionally connected to a second subgroup of the sixth group of the input MES PH, the fourth sub-group of the sixth group of the input MES PH is additionally connected with the group entrance to the third uiv-D group whose output is connected to the first group to the third input of BWDI, the sixth subgroup of the sixth group of the input MES PH is additionally connected with the group entrance TID fourth-D group whose output is connected to the first group sign-fifth BWDI, the eighth subgroup of the sixth group of the input MES PH is additionally connected with group sign-fifth TID-D, group output of which is connected to the first group entrance seventh BWDI, the fifth group of input-output fifth UUS connected with group input-output BODS, the fourth group entrance MES PH from node signal forming the lift-off" (KP) is connected with the ninth group entrance ninth BIG and group sign-TID-KP group whose output is connected to the second group input BODS, the first subgroup the tenth group of input MES PH from the first power poles is Lupanov device challenge (EC) is connected to the eighth group of the entrance of the ninth BIG and the fourth group input BEDS, the first subset of the third group of output MES PH on the second pole of the solenoid valves of the device of the challenge (EC) is additionally connected to the first group out of the seventh USE, the first subgroup of the eleventh group of the input MES PH from discrete sensors and signals dock right column AS (PC WHEN device drain is connected to the second group by the entrance of the sixth TID-D and the sixth group entrance ninth BIG, the first subgroup of the twelfth group of input MES PH from the first poles of paraelemental PP (PE) is connected to the eighth group input BODS and to the second group to the entrance of the ninth BIG, the first sub-group of the fourth group of output MES PH on the second pole of paraelemental PP (PE) is connected with the output of the first group of UPA and eleventh group entrance ninth BIG, the first subgroup of the thirteenth group of the input MES PH from analog sensors EE-1 is connected to the second group to the input of the second uiv-And the second subgroup of the eleventh group of the input MES PH from discrete sensors and signal coupling devices exhaust UO-1 is connected with the first group entry to the sixth TID-D and the seventh group entrance ninth BIG, group sixth output TID-D is connected to the sixth group input BEDS, the fifth group output MES PH signal KP in the NORTH at the start connected with the fifth group vyhoda is BODS, the second subgroup of the tenth group of input MES PH from the first poles of the solenoid valves of the device allocation (EC) PP-2 is connected to the tenth group entrance ninth BIG and the seventh group input BEDS, the second subset of the third group of output MES PH on the second pole of the solenoid valves of the left column WHEN (LK AS for device removal (EC) PP-2 is additionally connected with the group out of the eighth USIA, the third subgroup of the eleventh group of the input MES PH from discrete sensors and signal coupling devices exhaust LK WHEN connected to the second group to the entrance of the seventh TID-D and the fourth group to the entrance of the ninth BIG the second subgroup of the twelfth group of input MES PH from the first poles of paraelemental PP (PE) is connected with the fifth group input BODS and twelfth group entrance ninth BIG, the second sub-group of the fourth group of output MES PH on the second pole of paraelemental (PE) PP-2 is connected to the output of the second group of UPA and thirteenth group entrance ninth BIG, the second subgroup of the thirteenth group of the input MES PH from analog sensors EE-2 is connected to the first input of the second group TID, the fourth subgroup of the eleventh group of the input MES PH from discrete sensors and signals dock PP-2 connected to the first group to the entrance of the seventh TID-D and paramproperty entrance ninth BIG, group output of the seventh TID-D is connected with the third group input BODS, the first, second, third and fourth group outputs RODS connected respectively to the first group the inputs of the first and second USE, the first and the second UPA, the second group of input-output BUDS connected with group inputs-outputs of the first and second UPPA, the second input of the third BWDI additionally connected to the power input of the third uiv-d, the second input of the fifth BWDI additionally connected to the power input of the fourth TID-D, the second input of the seventh BWDI additionally connected to the power input of the fifth TID-D, the sixth group input-output of the second MCU is connected to the first group input BEDS. The automated management system preparation and launch-vehicle processing unit time intervals (WAVE) contains patch panel, two power distribution unit (PDU), three conversion unit time intervals (BPVI), the Central processor of the data processing (PCOD), mnogonatsionalny power supply (energy policy College), machine input (ATS), the first and second subsets of the inputs of the third group of input are connected respectively with group inputs of the first and second PDUs, the first outputs are connected respectively to the first and second group inputs ABP, group output of which is connected with group input energy policy College, GRU is model output energy policy College connected to group input PCOD, first, second and third inputs and outputs which are connected respectively to the first inputs-outputs of the first, second and third BPVI, second inputs and outputs which are respectively connected to the fifth, fourth and third group inputs-outputs a patch panel, the first inputs of the first, second and third BPVI connected respectively with the third, fourth and second outputs of the first PDU, the second inputs of the first, second and third BPVI connected respectively to the second, fourth and third outputs of the second PDU, the first and second group outputs the patch panel are connected respectively with the first and second group outputs WAVE, the first and second group inputs the patch panel are connected respectively to the first and second group inputs WAVE, the first and second group the inputs-outputs of the patch panel are connected respectively with the first and second group inputs-outputs WAVE. The automated management system preparation and launch of LV mobile remote customer (FP) contains the control panel power supply (GSPE), two AC/DC (AD), control panel, two modules I / o discrete information (MWDI), two panel computer, the node backplane, the first and the second sub-group group input FP are connected respectively with the first and second g is Provimi inputs, GSPE, the first and second outputs which are connected to the inputs respectively of the first and second AD, the outputs of which are connected respectively with the first and second inputs of the node backplane, the output of which is connected to the first input of the control panel, the first output and second input of the control panel are connected respectively to the first input and the first output of the first MWDI, input-output of which is connected to the first input-output of the first panel of the computer, the second output and the third input of the control panel are connected respectively to the first input and the first output of the second MWDI, input-output of which is connected to the first input-output of the second panel computer, the third exit the control panel is connected to third inputs of the first and second MWDI and the first inputs of the first and second panel computers, second and third inputs and outputs of the first panel of the computer is connected to the first and second inputs-outputs of the first sub-group group input-output FP, second and third inputs and outputs of the second panel computer is connected to the first and second entrance-exit of the second sub-group group input-output fire protection. The automated management system preparation and launch-vehicle device intrinsically safe input discrete sensors "pin up" (TID-KP) contains m nodes intrinsically safe input, each of which status is it from the DC/DC Converter (D), the intrinsic safety barrier (B), item galvanic isolation power supply (EGREP), the output node of the unit potential (WU" 1"), the output node of ground potential (WU "0"), power input D all m nodes are connected with a power inlet TID-KP, the inputs of the i-th subgroup group sign-TID-KP is connected to the input BI of a node i, the output D node connected to the first input of EGREP, the output B is connected to the second input of EGREP, the first output EGREP connected to the input VU "1", a second output connected EGREP to sign-WU "0", the first outputs WU "1", the first outputs WU "0", and the combination of the second outputs WU "1" and " WU "0" in the nodes from 1 to m are connected with the corresponding subgroups of outputs from 1-1 to 1-m in the group output TID-KP. The automated management system preparation and launch-vehicle processing unit discrete information (BODS) contains two switch network (COP), three peripheral processor (PDP), three blocks normalization discrete sensors (BNDD), three signal control BFSU), three mnogonazionaljnyh power supply peripheral (energy policy College-P), the control unit control circuits (BCCU), patch panel input signals (cpws), two units of analysis temporal information (BAVI), site of the majority of elements (UME), three multi-wire bus line (M), first the input RODS connected with the first inputs of three energy policy College-P, three BNDD, three BF is, the outputs of the first-third the energy policy College-N are connected respectively to the tires of the first-third of the M1÷M3 in terms of nominal power, each of the tires of the first-third of roads are connected respectively with group inputs-outputs of the first-third BNDD, BFSU, PDP and with the first-third group inputs-outputs of the two BAVI, the inputs and outputs of the first-third PDP connected respectively to the first to third inputs-outputs of the first and second CS, fourth inputs and outputs which are connected respectively with tires subgroups of the first group of input-output BODS, a second input connected to RODS the second inputs of the first-third BNDD, group the inputs of the first-third BNDD connected respectively with the first third group outputs CPUs, group outputs of the first-third BFSU connected respectively to the first to third group inputs UME, the second group of input-output BCCU connected with the first line, the tenth group entrance CPUs connected to the sixth group output UME and to the first sub-group input group input BCCU, eleventh group entrance CPUs connected with the seventh group output UME and the second sub-group input group input BCCU, the second group output UME is connected to the fourth group output BODS, third group output UME is connected with the third group output BODS, the first group o is d UME is connected to the fifth group output BODS, the fourth group output UME is connected to a second group output BODS, the fifth group output UME is connected to the first group output BODS, the first subset of the inputs of the second group of input-output RODS connected with the first group entrance CPUs, the second group of inputs of the second group of input-output RODS connected to the second group input CPUs, the third group entrance CPUs connected to the eighth group input BEDS, the fourth group entrance CPUs connected to the seventh group input BEDS, the fifth group entrance CPUs connected with the sixth group input BODS, the sixth group entrance CPUs connected to the fifth group input BODS, the seventh group entrance CPUs connected with the fourth group input BODS, the eighth group entrance CPUs connected to the third group input BEDS, ninth group entrance CPUs is connected to a second group input BODS, the first group of the input RODS connected to the first inputs of the first and second BAVI, the outputs of which are respectively connected to the tires of the first and second subset of outputs of the second group of input-output BODS. The automated management system preparation and launch-vehicle device power paraelemental (UPPA) contains eight modules rectifier (MB), grouped in pairs in four power supply (INRM), eight electronic keys (RWE), bus lane the second subgroup of the first input UPPE connected with the first inputs of the first, the third, fifth and seventh MB, tyres second subgroup of the first input UPPE connected to the first inputs of the second, fourth, sixth and eighth MB, subgroup inputs of the first group of input-output connected to second inputs of the first-eighth MB, the first outputs of the first-eighth MB connected to the corresponding tire subgroup outputs of the first group of input-output UPPA, the first bus of the second group of input UPPE connected with the first inputs of the first, third, fifth and seventh RWE, the second bus of the second group of input UPPE connected to the first inputs of the second, fourth, sixth and eighth RWE, the third the tire of the second group of input UPPE connected with integration of third inputs of the first and second MB and the fifth bus bar of the first subset of outputs of the first group of output UPPA, the fourth bus of the second group of input UPPE connected to the Association of third inputs of the third and fourth MB and the sixth bus first subset of outputs of the first group of output UPPA, the fifth bus of the second group of input UPPE connected with integration of third inputs of the fifth and sixth MB and with the seventh bus first subset of outputs of the first group of output OPPA, sixth bus of the second group of input UPPE connected to the Association of third inputs of the seventh and eighth MB and eighth bus first subgroup outputs of the first group of output OPPA, p the pout bus bar of the first subset of outputs of the first group of output UPPE connected to the output of the second RWE, the second bus, the first subset of outputs of the first group of output UPPE connected to the output of the fourth RWE, the third bus of the first subset of outputs of the first group of output UPPE connected to the output of the sixth RWE, the fourth bus of the first subset of outputs of the first group of output UPPE connected to the output of the eighth RWE, the first bus of the second subset of outputs of the first group of output UPPE connected to the output of the first RWE, the second bus of the second subset of outputs of the first group of output UPPE connected to the output of the third RWE, the third bus of the second subset of outputs of the first group of output UPPE connected to the output of the fifth RWE, the fourth bus of the second subset of outputs of the first group output connected UPPE the output of the seventh RWE, the first outputs of the first and second MB connected with the second inputs of the first and second RWE, the first outputs of the third and fourth MB are connected to each other and to the second inputs of the third and fourth RWE, the first outputs of the fifth and sixth MB connected with the second inputs of the fifth and sixth RWE, the first outputs of the seventh and eighth MB are connected to each other and to the second inputs of the seventh and eighth RWE. The automated management system preparation and launch-vehicle conversion unit time intervals (BPVI) contains two AC/DC (D), mnogonatsionalny the source of the IR peripheral power (energy policy College-P), the control circuit voltage (SKN), OCXO (TSG), digital to analog voltage Converter (DAC), the microprocessor (MCP), the adapter code RS-485 (Ad 485), the adapter code RS-232 (Ad 232), the display element (EI), the switch code (CC), the first and second group inputs BPVI connected with the first group inputs respectively of the first and second PJSC, the outputs of which are connected to each other and to the first inputs of energy policy College and SKN, the first output energy policy College connected with the first inputs of the ITUC, Hell, 485, Hell, 232, EI, QC, DACS, the second output energy policy College connected to the first input TSG and the second input of the DAC, the output SKN is connected to a second input of the MCP, the first TSG connected to the fourth input of the MCP, the DAC output is connected to the second input of the TSG, the second output TSG connected to the third input of the DAC, the first output of the MCP is connected to a second input of EI, the second output of the MCP is connected to the second input QC, the first and second inputs and outputs MCP is connected with the first inputs-outputs, respectively Hell 485 and 232 Hell, the second input-output Ad 485 connected to the first input-output QC of the second input-output Ad 232 connected to the first input-output BPVI, the first bus input group input-output BPVI connected to the third input of the MCP, the second bus input group input-output BPVI connected with the third input QC, the first and second outputs QC are connected respectively to the first and second tire of the output signals of the group who turn out BPVI, the second and third inputs and outputs QC are connected respectively with the first and second tire of the input / output group input / output BPVI. Introduction to automated system control processing and launch rockets distributor equipment single time (SPM), device processing time information (WAVE), mobile remote Customer (TEP), block I / o analog and discrete data (BWADE), the seventh block I / o discrete information (BWDI), the two devices intrinsically safe input analog information (TID), seven devices intrinsically safe input discrete data (TID-D), the device intrinsically safe input discrete sensors "pin up" (TID-KP), the ninth BIG seventh and eighth USE, block processing of discrete signals (BODS), two power supply units of paraelemental (UPA) and corresponds to the collection of links, known and newly introduced, to connect the blocks and devices restrictive and distinctive part of the formula, allows you to fully determine the functional readiness of the communications system with control objects, to organize the program staff work to prepare and launch rockets, to coordinate the work related systems at the remote command post and at the starting position, to synchronize inter the step motion hardware device allocation (PP) and the fixing unit start the launch power of paraelemental-stoppers PP. The system will be clear from the drawings shown in figures 1-37: figure 1 shows the diagram of the automated management system preparation and launch vehicles (MES PH); figure 2 presents the scheme of the automated workplace of the operator (ARMO); figure 3 presents a diagram of the remote control subsystem hardware and software (PPS APS); figure 4 presents a diagram of the device control and communication (UUS); figure 5 presents a diagram of the Central processor of the composition UUS; figure 6 presents the scheme of a software simulator (PI); figure 7 presents a diagram of the device in the allocation of primary power (UCEP); on Fig presents a diagram of the distributor of power equipment single time (RP); figure 9 presents a diagram of the device processing time information (WAVE); figure 10 presents the scheme of the mobile remote customer (FP); figure 11 shows a diagram of the remote control device of the primary power supply at the remote command post (WUPAP-BCP); on Fig shows a diagram of the uninterruptible power supply (mbea); on Fig presents a diagram of a network system switch (FCS); on Fig shows a diagram of the communication device with hair is Onno-optical transmission line information (USUALE); on Fig shows a diagram of the remote control device of the primary power supply in the starting structure (WUPAP-SS); on Fig presents a diagram of the device distribution secondary power supply (ORWAP); on Fig presents a block circuit diagram for determining the functional readiness (BOTH); on Fig presents a diagram of the device for thermal actuators and systems booster (USIS); on Fig presents a diagram of the device running the Executive process equipment (USIA); on Fig presents the block diagram of I / o discrete information (BWDI); on Fig presents the block diagram of I / o discrete and analog information (BWADE); on Fig presents the block diagram of the normalization of the discrete data from BWADE, BWDI, BODS (BNDD); on Fig presents a block circuit diagram of the generation of control signals from BWADE, BWDI (BFSU); on Fig presents the scheme of the multi-channel analog-to-digital Converter from BWADE (MACP); on Fig presents the scheme of the majority element key (IEC); on Fig presents a diagram of the device intrinsically safe input analog information (TID); on Fig presents a diagram of the device intrinsically safe input discrete sensors "pin up" (TID-KP); on Fig presents the block diagram of the processing of discrete information (BODS); on Fig presents a diagram of the device's power paraelemental (UPPA); on Fig the circuit block analysis of time intervals from BODS (BAVI); on Fig the circuit node modes of composition BOTH (YPP); on Fig presents the scheme of the controlled voltage divider is included BOTH (UDN); on Fig the circuit conversion unit time information (BPVI) from WAVY; on Fig presents the scheme of the control unit of the control circuits from BWADE, BWDI (BCCU); on Fig presents a graph-scheme of the mode electropower PH and equipment UO; on Fig presents a graph-scheme of the final part of the launch of LV for MES PH. Automated control system for the processing and launch boosters (MES PH) (figure 1), containing four workstations operators (ARMO) 4-1 to 4-4, remote subsystems control hardware and software (PPS APS) 5, five devices, control and communications (MCU), the first UUS 3-1 - external related systems at the remote command post (BCP), the second UUS 3-2 - with elements and systems boosters, third UUS 3-3 - process of filling the first component of rocket fuel (MCT), the fourth UUS 3-4 - with technology the logical equipment refueling second MCT, fifth UUS 3-5 - process temperature (TST) and external ground systems, each with the appropriate MCU software simulators (PI) 11-1 to 11-5, two communication devices with fiber-optic transmission line information (USUALE) 8-1, 8-2, two network switch (FCS) 7-1, 7-2, three devices distribution primary power supply (UCAP), the first UCAP 6-1 equipment of the CPSU, the second UCAP 6-2 equipment in the initial construction, the third UCAP 6-3 equipment launch facilities providing power systems and actuators boosters, and the power of the Executive elements of the technological equipment of the control object, the remote control of the primary power supply of the CPSU (WUPAP-BCP) 9, the remote control primary power supply starting structures (WUPAP-SS) 13, two devices distribution secondary power supply (ORWAP) for equipment management and control of the first (1 St) and second (2 St) LV stages, two devices for thermal actuators and systems (USES) 18-1, 18-2, three uninterruptible power supply (mbea) 12-1 to 12-3 for relevant UCAP, eight devices running actuators (USIA) 19-1 ÷ 19-8 technological equipment facility management - management subsystems of supra the coy and temperature control, nine blocks determine the functional readiness (BIG) 15-1 to 15-9 Appendix, seven blocks I / o discrete information (BWDI) 17-1 to 17-7, with group input-output optical signals 4 first USUALE 8-1 is connected with group input-output optical signals 4 second USUALE 8-2, the first group of input-output MES PH 1 from the inputs and outputs of adjacent automated control system of technological processes of ground-based equipment (APCS), the first group entrance MES PH 2 uninterruptible power systems (CGAP), the second group input MES PH 3 from system ground measurements (NDA) connected respectively to the second 2, 4 fourth and sixth group 6 inputs-outputs of the first UUS 3-1, the first group 10 is connected to the first group output 3 of the first UCAP 6-1, group inputs and outputs 2 inputs and 1 of the first to fifth software simulators PI 11-1 to 11-5 are connected respectively to the tenth group inputs outputs 11 and 12 outputs corresponding UUS 3-1 to 3-5, the ninth group of input-output 9 of the first UUS 3-1 is connected to the first group entrance-exit 1 of the first FCS 7-1, the second to the sixth group inputs outputs 2-6 which are connected respectively to the first group inputs-2 outputs the first to fourth ARMO 4-1 to 4-4 and PPS APS 5, the first group inputs 1 of the first-fourth ARMO 4-1 to 4-4 and PPS APS 5 are connected to the respectively with the second-fifth 4÷7 and the first duty 11 group outputs the first UCAP 6-1, the twenty-eighth group input-output 29 of the first FCS 7-1 is connected to the first group input-output 2 first USUALE 8-1, the first duty of the DC voltage 12 first UCAP 6-1 is connected with the first inputs 1 UDUPA-BCP 9 and the first USUALE 8-1, the second group of input-output 6 UDUPA-BCP 9 is connected to the second group input-output 3 of the first USUALE 8-1, the first group of input-output 3 UDUPA-BCP 9 is connected to a second group entrance-exit 3 PPS APS 5, the first input-output 1 of the first mbea 12-1 is connected to the first input-output 5 UDUPA-BCP 9, group inputs-2 outputs of the first-third mbea 12-1 to 12-3 are connected with the first group inputs-outputs 2 relevant UCAP 6-1 to 6-3, the second group of input-output 13 of the first UCAP 6-1 is connected to the second group input-output 4 UDUPA-BCP 9, group output 30 of the first FCS 7-1 is connected to the first group input 2 UDUPA-BCP 9, the sixth group output 8 of the first UCAP 6-1 is connected to the first group to the input 28 of the first FCS 7-1, the third group input 5 MES PH from external power distribution Board power supply (SRP) is connected with the first group inputs 1 first-third UCAP 6-1 to 6-3, the first input 1 of the second USUALE 8-2 and UDUPA-SS 13 connected to the first output duty voltage DC 12 second UCAP 6-2, the first group of input-output 2 of the second USUALE 8-2 connection is from the twenty-eighth group input-output 29 of the second FCS 7-2, the second group of input-output 3 of the second USUALE 8-2 is connected to the third group input-output 9 UDUPA-SS 13, the first and second group inputs and outputs 3 and 4 which are connected respectively with the second group inputs-outputs 13 of the second and third UCAP 6-2, 6-3, the first group input 2 UDUPA-SS 13 is connected to the first group output 30 of the second FCS 7-2, the first and second inputs and outputs 6 and 7 UDUPA-SS 13 are connected respectively to the first inputs-outputs 1 12-2 second and third 12-3 mbea, the first group entry 28 second SCQ 7-2 is connected to the eighth group of the output 10 of the second UCAP 6-2, the first 3 and second 4 group outputs of which are connected with the first group inputs 13 respectively of the first 14-1 and the second 14-2 ORWAP, third-seventh group outputs 5-9 second UCAP 6-2 is connected to the first group inputs 10 of the second to fifth UUS 3-2 ÷ 3-5, the inputs 1 of the seventh 19-7 and eighth 19-8 USE, the first 3 and second 4 group outputs the third UCAP 6-3 is connected with the first group inputs 1, respectively, the first 18-1 and 18-2 of the second USIS, the third group exit 5 third UCAP 6-3 is connected to the first group inputs 1 of the first and second USE 19-1 and 19-2, the fourth group output 6 third UCAP 6-3 is connected with the first group inputs 1 third 19-3 and fourth 19-4 USE, the fifth group exit 7 third UCAP 6-3 is connected to the first input 1 of the fifth 19-5 and W is stage 19-6 USE, the first 1 and second 2 group inputs and outputs of the second FCS 7-2 connected with group inputs-12 outputs respectively of the first and second ORWAP 14-1 and 14-2, the third 3 and fourth 4 group inputs and outputs of the second FCS 7-2 is connected to the first group inputs-2 outputs, respectively, of the fifth 19-5 and sixth 19-6 USE, fifth 5th and sixth 6th group inputs and outputs of the second FCS 7-2 is connected with the first group inputs-2 outputs respectively of the first 15-1 and the second 15-2 BIG, 7 seventh, tenth, 10, 13 thirteenth and sixteenth group 16 inputs-outputs of the second SSK 7-2 is connected to the ninth group inputs-outputs 9 respectively of the second to fifth UUS 3-2 ÷ 3-5, 8 eighth and ninth group 9 inputs and outputs of the second FCS 7-2 are connected respectively with the first group inputs-2 outputs the third 15-3 and fourth 15-4 BIG, 11 eleventh and twelfth 12 group inputs and outputs of the second FCS 7-2 connected respectively to the first group inputs-outputs 2 fifth 15-5 and sixth 15-6 BIG, 14 fourteenth and fifteenth 15 group inputs and outputs of the second FCS 7-2 are connected respectively with the first group inputs-outputs 2 seventh 15-7 and eighth 15-8 BIG, seventeenth 17 and 18 eighteenth group inputs and outputs of the second FCS 7-2 connected respectively to the first group inputs-2 outputs the first 18-1 and 18-2 of the second USES, nineteenth to twenty-fifth 19-25 group the s inputs and outputs of the second FCS 7-2 are connected respectively with the first group inputs-2 outputs the first to fourth USE 19-1 to 19-4, ninth BIG 15-9 Appendix, seventh and eighth USE 19-7 and 19-8, the third output 3 of the first ORWAP 14-1 is connected to the first input 1 of the first 15-1, third 15-3, fifth 15-5, seventh 15-7 and ninth 15-9 Appendix BFG, 4 fourth and fifth 5 outputs the first ORWAP 14-1 are connected respectively with the first 1 and second 3 inputs of the second BWDI 17-2, 6 sixth and seventh 7 outputs the first ORWAP 14-1 are connected respectively to the first 1 and second 3 inputs the fourth BWDI 17-4, 8 eighth and ninth 9 outputs the first ORWAP connected respectively with the first 1 and second 3 inputs sixth BWDI 17-6, the first 1 and second 2 outputs the second ORWAP 14-2 are connected respectively to the first 1 and second 3 inputs of the first BWDI 17-1, the third output 3 second ORWAP 14-2 is connected to the first input 1 of the second 15-2, fourth 15-4, sixth 15-6 and eighth 15-8 BIG, 4 fourth and fifth 5 outputs the second ORWAP 14-2 are connected respectively to the first 1 and second 3 inputs of the third BWDI 17-3, 6 sixth and seventh 7 outputs the second ORWAP 14-2 are connected respectively with the first 1 and second 3 inputs fifth BWDI 17-5, 8 eighth and ninth 9 outputs the second ORWAP 14-2 are connected respectively to the first 1 and second 3 inputs seventh BWDI 17-7, 8-1 first subset of inputs of the fifth group of the input from the first poles of the Executive members of the object management subsystem control elements and systems of the booster is connected with the second group the second input 4 of the first 15-1 BIG, the second-eighth subgroup 8-2 ÷ 8-8 inputs of the fifth group of the input from the first poles of the Executive members of the object management subsystem control elements and systems boosters through the second subgroup 8-2, the control subsystem filling the first component of rocket fuel (MCT) through a third 8-3 and fourth 8-4 subgroups, subsystem control filling of the second MCT through fifth 8-5 and sixth 8-6 subgroups, engine temperature (TST) through the seventh 8-7 and eighth 8-8 subgroups are connected to pairs, respectively, the second group to the 4 inputs of the second-eighth BIG 15-2 ÷ 15-8 and the second group to the input 6 of the first-seventh BWDI 17-1 to 17-7, the first 10-1 and 10-2 second subset of inputs of the sixth group of input from discrete sensors and signals dock object management subsystem control elements and systems of the booster is connected to the fourth group inputs 6 respectively of the first 15-1 and the second 15-2 BOTH, the first 9-1 and 9-2 second subset of outputs of the first group of the system output at the second pole of the Executive members of the object management subsystem control elements and systems booster connected to pairs of the first group inputs 3 BFG and the first group outputs 4 USES respectively the first 15-1 and the second 15-2 BIG and the first 18-1 and 18-2 of the second USES, the seventh group input 11 from the Ana is ogowych sensors object management subsystem control elements and systems of the booster is connected with the fifth group of the entrance 7 of the first BIG 15-1, first 13-1 and the second 13-2 subgroup outputs of the second group of output MES PH on power systems, rocket management subsystem elements and systems booster connected to pairs, respectively, the second group outputs 5 of the first 18-1 and 18-2 of the second USIS and the third group inputs 5 of the first 15-1 and the second 15-2 BIG, first 14-1 and the second 14-2 subset of inputs of the ninth group of input channels codes systems booster subsystem control elements and systems booster connected respectively with subsets of inputs of the second 2 and 4 fourth group of inputs-outputs of the second UUS 3-2, third-sixth subgroups outputs 9-3 ÷ 9-6 first group of the system output at the second pole of the Executive members of the object management subsystem controls the filling of the first MCT through a third 9-3 and fourth 9-4 subgroups, subsystem control filling of the second MCT through fifth 9-5 and sixth 9-6 subgroups are connected to pairs of the first group inputs 3 BFG and the first group outputs 4 USE respectively third to sixth BIG 15-3 to 15-6 and the first-fourth 19-1 to 19-4 USE, third 10-3 and fifth 10-5 subset of inputs of the sixth group of input from discrete sensors and signal coupling facility control subsystem controls the filling of the first MCT through a third subgroup 10-3, the control subsystem filling the second the RT through fifth subgroup 10-5 connected with pairs - the first group inputs 4 BWDI and third group inputs 5 BOTH respectively 17-2 second and fourth 17-4, BWDI and third 15-3 and fifth 15-5 BIG, fourth 10-4 and sixth 10-6 subset of inputs of the sixth group of input from discrete sensors and signal coupling facility control subsystem controls the filling of the first MCT through the fourth subgroup 10-4, engine control filling of the second MCT through sixth subgroup 10-6 connected to the third group inputs 5, respectively, the fourth 15-4 and sixth 15-6 BIG, group outputs 5 of the first-fifth BWDI 17-1 to 17-5 connected with the second group 3 inputs, respectively, of the second USES 18-2, the first fourth USE 19-1 to 19-4, the first group inputs-2 outputs of the first-third BWDI 17-1 to 17-3 are connected respectively to the third group input-output 3 of the second UUS 3-2, the first 1 and third 3 group inputs-outputs of the third UUS 3-3, the first group inputs and outputs 2 17-4 third and fourth 17-5, BWDI connected respectively with the first 1 and third 3 group inputs-outputs of the fourth UUS 3-4, seventh 9-7 and eighth 9-8 subgroup outputs of the first group of the system output at the second pole of the Executive members of the object management subsystem thermostat connected to pairs of the first group inputs 3 BFG and the first group outputs 4 USE respectively sedimo what about 15-7 and eighth 15-8 BIG and fifth 19-5 and sixth 19-6 USE, seventh subgroup of inputs 10-7 sixth group of input from discrete sensors and signals dock object management subsystem thermostat connected to the pair of first group input 4 sixth BWDI 17-6 and the third group input 5 seventh BIG 15-7, eighth subgroup of inputs 10-8 sixth group of input from discrete sensors and signals dock object management subsystem thermostat is connected to the third group the input 5 of the eighth BIG 15-8, the third group of input-output system 6 from ground-based automated control system of the rocket (NASA PH) is connected with a pair of third group input 7 sixth BWDI 17-6 and the fourth group input 6 of the seventh BIG 15-7, group outputs 5 sixth 17-6 and seventh 17-7, BWDI connected to the second group 3 inputs, respectively, of the fifth 19-5 and sixth 19-6 USE, the first group inputs and outputs 2 sixth 17-6 and seventh 17-7, BWDI connected respectively with the first 1 and third 3 group inputs-outputs of the fifth UUS 3-5, the first 3 and the third group 5 inputs ninth BIG 15-9 Appendix are connected respectively to the first group outputs 4 USE 19-7 and USE 19-8, characterized in that the MES PH added power distribution equipment system of universal time (RP) 2, the device processing time information (WAVE) 1, mobile remote customer (TEP) 10, block BB is Yes / o analog and discrete data (BWADE) 16, two devices with intrinsically safe input analog information (TID) 20-1, 20-2, seven devices intrinsically safe input discrete data (TID-D) 21-1 to 21-7, the device is intrinsically safe input discrete sensors "pin up" (TID-KP) 24, the block processing of discrete signals (BODS) 23, two devices power paraelemental (UPPA) 22-1 and 22-2, the third group input system 5 is additionally connected to the input 1 RP 2, exit 2 which is connected to the third group input 7 WAVE 1, the eighth group output 10 of the first UCAP 6-1 is connected to the first group input 1 FP 10, group input-output 2 which is connected to the eleventh group input-output 13 of the first UUS 3-1, 4-1 first and second 4-2 subgroup outputs on the group display TCH and time intervals VI, VI, the first 4-3 and 4-4 second subset of inputs of the time interval VI and the start signal of the second group of input / output 4 MES PH from common timing system (CTS) are connected respectively with the first 5 and second 6 group outputs and with the first 1 and second 2 group inputs WAVE 1, the second group input-output 4 WAVE 1 is connected to the eighth group input-output 8 of the first UUS 3-1, the first group of input-output 3 WAVE 1 is connected with the third group entrance-exit 5 first USUALE 8-1, the sixth group exit 8 third UCAP 6-3 is connected with the first group inputs 1 PE is the first 22-1 and 22-2 of the second, UPPA, the first 1 out of the first ORWAP 14-1 connected to the first input 1 of BWADE 16, the second output 2 of the first ORWAP 14-1 is connected to the second input 3 of BWADE 16, power input 4 of the first TID-20-1 and TID-D 21-1, ten 10 the output of the first ORWAP 14-1 is connected to the first 1 input RODS 23, eleventh output 11 of the first ORWAP 14-1 is connected to the power input 4 of the sixth and seventh TID-D 21-6 and 21-7, second uiv-And 20-2, a power inlet 3 TID-KP 24 and the second input 3 of RODS 23, the first group 1 input-output of the second UUS 3-2 is connected to the first group input-output 2 BWADE 16, the first subgroup 8-1 fifth group of input MES PH is additionally connected to the second group input 6 BWADE 16, group output 1 of the first TID-connected to the third group input 7 BWADE 16, whose first group input 4 is connected with the group output 1 of the first TID-D 21-1, the first group output 5 BWADE 16 is connected to the first group input 3 of the first USES 18-1, the fourth group input 8 BWADE 16 is connected with the group output 1 second uiv-And 20-2, the first subgroup of the sixth group of the entrance 10-1 MES PH is additionally connected to group input 2 of the first TID-D 21-1, the seventh group input 11 MES PH from analog sensors the first stage of the launch vehicle is additionally connected to the second group input 3 of the first TID-20-1, whose first group input 2 is connected to the eighth group input 12 MES PH from analog Dutch the Cove BRS, the second output 2 second ORWAP 14-2 additionally connected to the power input 4 of the second uiv-D 21-2, the first group input 4 of the first BWDI 17-1 is connected to the group output 1 second uiv-D 21-2, whose group input 2 is additionally connected to a second subgroup of 10-2 sixth group input MES PH, the fourth subgroup 10-4 sixth group of input MES PH is additionally connected with group input 2 of the third uiv-D 21-3, whose group output 1 is connected to the first group to the input 4 of the third BWDI 17-3, sixth subgroup 10-6 sixth group of input MES PH is additionally connected with group input 2 fourth TID-D 21-4, whose group output 1 is connected to the first group input 4 fifth BWDI, eighth subgroup 10-8 sixth group of input MES PH is additionally connected with group input 2 fifth TID-D 21-5, group output 1 which is connected to the first group input 4 seventh BWDI 17-7, the fifth group of input-output 5 fifth UUS 3-5 connected with the group entrance-exit 2 RODS 23, the fourth group input 7 MES PH from node signal forming the lift-off" (KP) is connected with the ninth group input 11 of the ninth BIG 15-9 Appendix and group input 2 TID-KP 24, whose group output 1 is connected to the second group input 8 RODS 23, the first subgroup 15-1 tenth group of input MES PH from the first poles of the solenoid valves of the drainage devices (is) connected to the eighth group of the entrance 10 the ninth BIG 15-9 Appendix and the fourth group input 12 RODS 23, the first subgroup 16-1 third group of output MES PH on the second pole of the solenoid valves of the device of the challenge (EC) is additionally connected to the first group output 4 seventh USE 19-7, the first subgroup 17-1 eleventh group of input MES PH from discrete sensors and signals dock right column AS (PC WHEN device drain is connected to the second group input 3 sixth TID-D 21-6 and the sixth group input 8 ninth BIG 15-9 Appendix, the first subgroup 18-1 twelfth group of input MES PH from the first poles of paraelemental PP (PE) is connected to the eighth group input 16 RODS 23 and to the second group input 4 ninth BIG 15-9 Appendix, the first subgroup 19-1 fourth group of output MES PH on the second pole of paraelemental PP (PE) is connected with group 4 first UPPE 22-1 and the eleventh group of the entrance 13 of the ninth BIG 15-9 Appendix, the first subgroup 20-1 thirteenth group of input MES PH from analog sensors UO connected to the second group to the input 3 of the second uiv-And 20-2, the second subgroup 17-2 eleventh group of input MES PH from discrete sensors and signal coupling devices exhaust UO-1 is connected with the first group input 2 of the sixth TID-D 21-6 and the seventh group input 9 ninth BIG 15-9 Appendix, group output 1 of the sixth TID-D 21-6 connected to the sixth group input 14 RODS 23, the fifth group exit 21 MES THE N signal CP in the NORTH at the start connected with the fifth group exit 17 RODS 23, the second subgroup 15-2 tenth group of input MES PH from the first poles of the solenoid valves of the device allocation (EC) PP-2 is connected to the tenth group to the input 12 of the ninth BIG 15-9 Appendix to the seventh group input 15 RODS 23, the second subgroup 16-2 third group of output MES PH on the second pole of the solenoid valves of the left column WHEN (LK AS for device removal (EC) PP-2 is additionally connected with group 4 eighth USE 19-8, the third subgroup 17-3 eleventh group of input MES PH from discrete sensors and signal coupling devices exhaust LK WHEN connected to the second group to the input 3 of the seventh TID-D 21-7 and the fourth group to the input 6 of the ninth BIG 15-9 Appendix, the second subgroup 18-2 twelfth group of the entrance. MES PH from the first poles of paraelemental PP-2 (PE) is connected with the fifth group of the entrance 13 RODS 23 and the twelfth group of the entrance 14 of the ninth BIG 15-9 Appendix, the second subgroup 19-2 fourth group of output MES PH on the second pole of paraelemental (PE) PP-2 is connected to group the output 4 of the second UPA 22-2 and the thirteenth group of the entrance 15 of the ninth BIG 15-9 Appendix, the second subgroup 20-2 thirteenth group of input MES PH from analog sensors EE-2 is connected with the first group input 2 of the second uiv-And 20-2, the fourth subgroup 17-4 eleventh group of input MES PH from discrete sensors and signals dock UO-2 under Lucena to the first group input 2 seventh TID-D 21-7 and the fifth group the input 7 of the ninth BIG 15-9 Appendix, group output 1 of the seventh TID-D 21-7 connected with the third group input 11 of RODS 23, the first 4, second 6, third 9 and fourth 10 group outputs RODS 23 connected respectively to the first group to the input 3 of the first 19-7 and second 19-8 USE, first 22-1 and 22-2 of the second, UPPA, the second group of input-output 7 RODS 23 is connected with group inputs inputs 2 first 22-1 and 22-2 of the second, UPPA, the second input 3 of the third BWDI 17-3 additionally connected to the power input 4 of the third uiv-D 21-3, the second input 3 fifth BWDI 17-5 advanced connected to the power input 4 fourth TID-D 21-4, the second input 3 of the seventh, BWDI 17-7 additionally connected to the power input 4 fifth TID-D 21-5, the sixth group of input-output 6 of the second UUS 3-2 is connected to the first group entry 5 BEDS 23. The automated workplace of the operator ARMO 4 (figure 2) contains two network switch 25-1 and 25-2, three monitor 26-1 to 26-3, three system units 27-1 to 27-3, three universal keyboard 28-1 to 28-3, three manipulator "mouse" 29-1 to 29-3, two automatic standby 30-1 and 30-2, three switch USB ports 31-1 to 31-3. Remote control subsystem hardware and software PSK APS 5 (figure 3) contains three network switch 25-3 ÷ 25-5, three monitor 26-4 ÷ 26-6, three system unit 27-4 ÷ 27-6, three universal keyboard 28-4 ÷ 28-6, three of the mouse 29-4 ÷ 29-6, two automatic standby 30-3 and 30-4, three switch ports USB 31-4 ÷ 31-6, three is the network adapter from the USB outputs 32-1 to 32-3, the printer 33. Device control and communication UUS 3 (figure 4) contains two network switch 25-6 and 25-7, three tire M1, M2 and M3, the site collection fault 34-1, the CPU 35, mnogonatsionalny power supply (energy policy College) 37-1 and three multi-interface card (MIC) 36-1 to 36-3. The CPU 35 of the composition UUS (figure 5) contains two switch network 25-8 and 25-9, site collection fault 34-2, five energy policy College 37-2 ÷ 37-6, three processor for centralized data processing (PCOD) 38-1 to 38-3, device power management (UWEP) 39. Software simulator PI 11 (6) contains PCOD 38-4 and MICK 36-4. Device allocation of primary power UBAP (7) contains the machine input AVR 30-5, the mode switch control 40, two relays phase monitor 41-1 and 41-2, two network power switch battery 42-1 and 42-2, two electroconductor 43-1 and 43-2, two contact groups corresponding electroconduction 44-1 and 44-2, two sources of secondary power supplies power supplies 45-1 and 45-2, twenty individual machines 46-1 ÷ 46-20, two node failover 47-1 and 47-2. Power distribution equipment system of universal time (RP) (Fig) contains two individual machine 46-21 and 46-22, two emergency switch voltage 47-3 and 47-4, two voltage indicator 48-1 and 48-2, two monitoring devices 49-1 and 49-2. The mouth of austo processing time intervals (WAVE) 1 (Fig.9) contains patch panel 50, two power distribution unit (PDU) 51-1 and 51-2, three conversion unit time intervals (BPVI) 52-1 to 52-3, processor, Central processing (PCOD) 38-4, mnogonatsionalny power supply (energy policy College) 37-7, machine input (ATS) 30-5, first 7-1 and 7-2 second subgroup of group inputs input 7 WAVE 1 are connected respectively with group inputs 1 first 51-1 and the second 51-2 PDU, the first 2 outputs which are connected respectively to the first 1 and second 2 group inputs ABP 30-5, group output 3 which is connected with group input 1 energy policy College 37-7, group output 2 energy policy College 37-7 connected to group input 4 PCOD, the first 1, second 2 and third 3 inputs-outputs of which are connected respectively to the first inputs-2 outputs the first 52-1, second 52-2 and the third 52-3, BPVI, the second inputs-4 outputs which are respectively connected to the fifth 9, the fourth 8 and the third group 7 inputs-outputs a patch panel 50, the first input 1 of the first 52-1, second 52-2 and the third 52-3, BPVI connected respectively with the third 4 fourth 5 3 and the second outputs of the first PDU 51-1, the second inputs 3 first 52-1, second 52-2 and the third 52-3, BPVI connected respectively to the second 3, the fourth 5 and 4 third outputs of the second PDU, the first 1 and second 2 group outputs patch panel 50 are connected respectively with the first 5 and second 6 group outputs WAVE 1, the first 3 and the second group 4 inputs the patch panel 50 are connected respectively to the first 1 and second 2 group inputs WAVE 1, the first 5 and second 6 group input-output patch panel 50 are connected respectively with the first 3 and second 4 group inputs-outputs WAVE 1. Mobile remote customer (TEP) 10 (figure 10) contains the control panel power supply (GSPE) 53, two transducer 54-1 and 54-2 AC/DC (AD), the control panel 55, two modules I / o discrete information 56-1 and 56-2 (MWDI), two panel computer 57-1 and 57-2, the node backplane 58, the first 1-1 and 1-2 second subgroup of group input 1 FP 10 is connected respectively with the first 1 and second 2 group inputs GSPE 53, the first 3 and second 4 outputs which are connected to the inputs 1, respectively, the first 54-1 and the second 54-2 AD, 2 outputs which are connected respectively with the first 1 and second 2-input node backplane 58, exit 3 which is connected to the first input 1 of the control panel 55, the first 2 and the second input 3 of the control panel 55 are connected respectively to the first input 1 and the first output 2 first MWDI 56-1, input-output 3 which is connected to the first input-output 1 of the first panel computer 57-1, the second 4 and the third input 5 control panel 55 are connected respectively to the first input 1 and the first output 2 of the second MWDI 56-2, input-output 3 which is connected to the first input-output 1 of the second panel computer 57-2, the third output 6 control panel 55 is connected to third inputs of the 4 first is th 56-1 and the second 56-2, MWDI and the first input 4 of the first 57-1 and second 57-2 panel computers the second 2 and third 3 inputs-outputs of the first panel computer 57-1 connected to the first 1 and second 2 inputs-outputs of the first sub-group 2-1 group of input / output 2 FP 10, the second 2 and third 3 inputs-outputs of the second panel computer connected with the first 1 and second 2 inputs-outputs of the second subgroup 2-2 group of input / output 2 FP 10. Work RFP 10 in the preparation of PH to start is to present the operator RFP information direct and countdown on the screen panel computers 57-1 and 57-2. The operator FP is in the same room with the operator monitoring equipment preparation spacecraft SPACECRAFT customer. In case of receiving information from the head of works on preparation of PH on completion of training and not until this moment the voice information about the readiness of the SPACECRAFT, the operator cancels the RFP start. He clicks on the control panel 55 the CANCEL button START. The signal cancellation formulated by pressing the button, will be transferred to the outputs of the 2-1 and 2-2 in UUS 3-1, and from there to the ARMO 4-1. The Manager takes the decision to cancel the start. The remote control of the primary power supply at the remote command post of WUPAP-VK (11) contains three network switch 25-10 ÷ 25-12, three elements galvanic isolation power supply EGREP 58-1 to 58-3, site of the majority of elements of the VME 59-1, three interface the data relay module IRM 60-1 to 60-3, six modules I / o MW 66-1 to 66-6. The uninterruptible power supply mbea 12 (Fig) contains a node failover 47-3, the inverter 63, the storage unit 64, the rectifier 65, the monitoring unit 66, the filter 67. Network system switch SCQ 7 (Fig) contains two switch network 25-13 and 25-14, two multichannel power supply energy policy College 37-8 37-9 and, two circuit breakers AB 68-1 and 68-2. Communication device with fiber-optic transmission line information, POLPI 8 (Fig) contains five receivers and transmitters converters "copper-glass and glass-copper" 69-1 ÷ 69-5. The remote control of the primary power supply in the starting structure UDUPA-SS 13 (Fig) contains three network switch 25-15 ÷ 25-17, three elements galvanic isolation power supply EGREP 58-4 ÷ 58-6, three nodes majority of elements 59-2 ÷ 59-4, nine interface relay modules IRM 60-4 ÷ 60-12, nine modules I / o 61-7 ÷ 61-18. Device distribution secondary power supply ORWAP 14 (Fig) contains two switch network 25-18 and 25-19, three mnogonazionaljnyh power source peripheral energy policy College-P 74-1 to 74-3, electroconductor 43-3, time relay 70, three peripheral processor 71-1 to 71-3, three blocks of the Normalizer of discrete data BNDD 72-1 to 72-3, three signal control 73-1 to 73-3, node majority of elements 59-5, about inidcate power sources INRM 75-1 ÷ 75-11, three tire M1, M2, M3. Unit definition functional readiness BOTH 15 (Fig) contains bus line M1, mnogonatsionalny power supply peripheral energy policy College-P 74-14, processor peripheral 71-4, measuring the power of IIEP 76, four electronic key 77-1 ÷ 77-4, the signal control BFSU 73-4, two switch analog signal CAS 78-1 and 78-2, host modes URR 80, four transducer 81-1 to 81-4, multichannel analog-to-digital Converter MACP 62-1, a controlled voltage divider UDN 79. Device for thermal actuators and systems USES 18 (Fig) contains machine input AVR 30-3, the source of secondary power supplies power supplies 45-3, the module I / o MW 61-19, two power supply INRM 75-12 and 75-13, four electronic key 77-5 - 77-8. The device running the Executive elements of the technological equipment USE 19 (Fig) contains machine input AVR 30-4, the source of secondary power supplies power supplies 45-4, the module I / o EBM 61-20, power supply INRM 75-14, two electronic key 77-9 and 77-10. Block I / o discrete information, BWDI 17 (Fig) contains three mnogonazionaljnyh power supply peripheral energy policy College-P 74-5 ÷ 74-7, three processor peripheral 71-4 ÷ 71-6, three blocks normalization discrete d is tchikov BNDD 72-4 ÷ 72-6, three signal control BFSU 73-5 ÷ 73-7, site of the majority of elements of the VME 59-5, p majoritarian elements-keys IEC 83-1 to 83-R. Block I / o analog and digital information, BWADE 16 (Fig) contains three mnogonazionaljnyh power supply peripheral energy policy College-P 74-8 ÷ 74-10, three processor peripheral 71-7 ÷ 71-9, three blocks normalization discrete sensors BNDD 72-7 ÷ 72-9, three signal control BFSU 73-7 ÷ 73-9, three multi-channel analog-to-digital Converter MACP 82-2 ÷ 82-4, p majoritarian elements-keys IEC 83-R-1 ÷ 83-2P. The unit normalization of the discrete sensors BNDD 72 from BWDI, BWADE (Fig) contains 2k of inputs galvanic isolation WAGR 84-1 to 84-2k, electronic key nutrition 85, shaper test parcels 86, the node voltage OTP 87-1, microprocessor MCP 88-1, the item display 89-1, element galvanic isolation power supply EGREP 58-7. The signal control BFSU 73 from BWDI, BWADE (Fig) contains an element galvanic isolation power supply EGREP 58-8, the node voltage OTP 87-2, microprocessor MCP 88-2, the item display 89-2, the output node keys UVC 90, n output relays 91-1 to 91-n, the node of the feedback elements OS 93, delay element τ 92, n contact groups 94-1 to 94-n. Multi-channel analog-to-digital p is OBRAZOVATEL MACP 82 of the composition BOTH, BWADE (Fig) contains an element galvanic isolation power supply EGREP 58-9, node low voltage OTP 87-3, the microprocessor MCP 88-3, multiple-input analog-to-digital Converter 62-2, the display element EI 89-3. The majority element is the key IEC 83 from BWDI, BWADE (Fig) contains six normally open relay contacts 95-1 ÷ 95-6. The device is intrinsically safe input analog signals TID-20 (Fig) contains 2n stabilizing input nodes of intrinsic barriers BI 97, elements galvanic isolation normalized signal EGMS 98, nodes galvanic isolation power PRP 96, the output of the inverters 99. The device is intrinsically safe input discrete sensors "pin up" (TID-KP) 24 (Fig) contains m nodes intrinsically safe input, each of which consists of a DC/DC Converter (D) 96, barrier intrinsic safety (BI) 97, item galvanic isolation power supply (EGREP) 98, the output of the single node potential (WU "1") 100, the output node of ground potential (WU "0") 101, a power input 1 D 96 all m nodes connected to the power input 3 TID-KP 24, the inputs of the i-th subgroup 2-i group input 2 TID-KP 24 is connected to the input 1 97 BI of a node i, output 2 D 96 node connected to the first input 1 EGREP 98, output 2 BI 97 is connected to the second input 2 EGREP 98, the first 3 EGREP 98 is connected to the input 1 WU "1" 100, the second output 4 EGREP 98 is connected to the input 1 WU "0" 101, the first outputs 2 WU "1" 100, the first choice of the outputs 2 WU "0" 101, and the combination of the second outputs 3 WU "1" 100 and WU "0" 101 in units from 1 to m are connected with the corresponding subgroups of outputs from 1-1 to 1-m in group 1 TID-KP 24. The device is intrinsically safe input digital data integrity-D. 21 Fig) contains 2P intrinsic barriers BI 97, converters DC/DC DD 96, control units and galvanic decoupling UPR 98 and output relays BP 99. The processing unit discrete information (BODS) (Fig) contains two switch network (COP) 25-20 and 25-21, three peripheral processor (PDP) 71-11 ÷ 71-13, three blocks normalization discrete sensors (BNDD) 72-10 ÷ 72-12, three signal control BFSU) 73-11 ÷ 73-13, three mnogonazionaljnyh power supply peripheral (energy policy College-P) 74-11 ÷ 74-13, the control unit control circuits (BCCU) 103, a switching panel input signals (CPUs) 104, the two units of analysis temporal information (BAVI) 105-1 and 105-2, the node the majority of items (UME) 59-6, three multi-wire bus line (M) M1 ~ M3, the first input 1 of RODS connected to the first input 1 of the three energy policy College-P 74-11 ÷ 74-13, 2 - three BNDD 72-10 ÷ 72-12, 2 - three BFSU 73-11 ÷ 73-13, 2 outputs of the first-third the energy policy College-P 74-11 ÷ 74-13 connected respectively to bus routes M1 ~ M3 in terms of nominal power, each of the tyres in the first third of the M1÷M3 are connected respectively with group inputs-outputs 4 BNDD 72-10 ÷ 72-12, 3 - BFSU 73-11 ÷ 73-13, - PDP 71-11 ÷ 71-13 and with the first-third group inputs-outputs 2-4 two BAVI 105-1 and 105-2, the inputs and outputs 2 PDP 71-11 ÷ 71-13 connected respectively to the first to third inputs-outputs 1-3 COP 25-20 and 25-21, fourth inputs and 4 outputs which are connected respectively with tires 2-1 and 2-2 of the subgroups of the first group of input / output 2 BEDS, the second input 3 of RODS connected to the second inputs 3 BNDD 72-10 ÷ 72-12, group inputs 1 BND 72-10 ÷ 72-12 connected respectively with the first third group outputs 1-3 CPUs 104, group outputs 1 BFSU 73-11 ÷ 73-13 connected respectively to the first to third group inputs 1÷3 UME 59-6, the second group of input-output 2 BCCU 103 is connected to the line M1, the tenth group input 4 CPUs 104 is connected to the sixth group exit 9 UME 59-6 and to the first subset of inputs 1-1 group input 1 BCCU 103, the eleventh group input 5 CPUs 104 is connected with the seventh group output 10 UME 59-6 and a second subgroup of the inputs 1-2 group input 1 BCCU 103, the second group output 5 UME 59-6 connected to the fourth group output 10 BEDS, the third group output 6 UME 59-6 connected with the third group exit 9 BEDS, the first group output 4 UME 59-6 connected to the fifth group exit 17 BEDS, the fourth group exit 7 UME 59-6 is connected to a second group output 6 BEDS, the fifth group exit 8 UME 59-6 connected to the first group to exit 4 BEDS, the first subgroup in the W 7-1 second group of input / output 7 BUDS connected with the first group input 6 CPUs 104, the second group of inputs 7-3 second group of input / output 7 RODS connected to the second group input 7 CPUs 104, the third group input 8 CPUs 104 is connected to the eighth group of the entrance 16 BEDS, the fourth group input 9 CPUs 104 is connected to the seventh group input 15 BEDS, the fifth group input 10 CPUs 104 is connected with the sixth group of the entrance 14 BEDS, the sixth group input 11 CPUs 104 is connected to the fifth group input 13 BODS, the seventh group input 12 CPUs 104 is connected with the fourth group input 12 BEDS, the eighth group input 13 CPUs 104 is connected to the third group input 11 BEDS, ninth group input 14 CPUs 104 is connected to a second group input 8 BEDS, the first group input 5 BEDS connected to the first inputs 5 BAVI 105-1 and 105-2, outputs 1 are respectively connected to the tire first 7-2 and 7-4 second subgroup outputs of the second group of input / output 7 BEDS. The power of paraelemental (UPPA) (Fig) contains eight modules rectifier (MB) 113-1 to 113-8, grouped in pairs in four power supply (EPI) the EPI 46-21 ÷ INRM 46-24, eight electronic keys (RWE) 77-4 ÷ 77-11, tires first subgroup 1-1 of the first input 1 of UPPE connected with the first input 1 of the first 113-1, third 113-3, the fifth 113-5 and seventh 113-7 MB 113, tyres second subgroup 1-2 of the first input 1 of UPPE connected to the first input 1 of the second 113-2, the fourth 113-4, sixth 113-6 and is osimage 113-8 MB 113, subgroup inputs 2-1 first group of input / output 2 UPPE connected with the second inputs 2 MB 113-1 to 113-8, the first group outputs 3 MB 113-1 to 113-8 connected to the corresponding tire subgroup outputs 2-2 first group of input / output 2 UPPA, the first bus 3-1 second group of input 3 UPPE connected with the first input 1 of the first 77-4, third 77-6, fifth 77-8 and seventh 77-10 RWE 77, the second bus 3-2 second group of input 3 UPPE connected to the first input 1 of the second 77-5, fourth 77-7, sixth 77-9 and eighth 77-11 RWE 77, the third bus 3-3 the second group of input 3 UPPE connected with integration of third inputs 5 of the first 113-1 and the second 113-2 MB 113 and the fifth bus "1-" first subgroup 4-1 outputs the first group of output 4 UPPE, the fourth bus 3-4 second group of input 3 UPPE connected to the Association of third inputs 5 third 113-3 and fourth 113-4 MB 113 and the sixth bus "2-" the first subgroup outputs 4-1 first group of output 4 UPPE, the fifth bus 3-5 second group of input 3 UPPE connected with integration of third inputs 5 fifth 113-5 and sixth 113-6 MB 113 and with the seventh bus "3-" the first subgroup outputs 4-1 first group of output 4 UPPE, sixth bus 3-6 second group of input 3 UPPE connected to the Association of third inputs 5 seventh 113-7 and eighth 113-8 MB 113 and eighth bus "4-" the first subgroup outputs 4-1 first group of output 4 UPPE, the first bus "1+" first under the group's 4-1 outputs the first group of output 4 UPPE connected to the output 3 of the second RWE 77-5, the second bus "2+" first subgroup 4-1 outputs the first group of output 4 UPPE connected to the output 3 of the fourth RWE 77-7, the third bus "3+" of the first subgroup 4-1 outputs the first group of output 4 UPPE connected to the output 3 of the sixth RWE 77-9, the fourth bus "4+" of the first subset of outputs 4-1 first group of output 4 UPPE connected to the output 3 of the eighth RWE 77-11, the first bus 2n1 second subgroup outputs 4-2 first group of output 4 UPPE connected to the output 3 of the first RWE 77-4, the second bus 2n2 second subgroup outputs 4-2 first group of output 4 UPPE connected to the output 3 of the third RWE 77-6, the third bus 2n3 second subgroup outputs 4-2 first group of output 4 UPPE connected to the output 3 of the fifth RWE 77-8, the fourth bus 2n4 second subgroup outputs 4-2 first group of output 4 UPPE connected to the output 3 of the seventh RWE 77-10, the first 4 outputs the first 113-1 and the second 113-2 MB 113 are connected with the second input 2 of the first 77-4 and second 77-5 RWE 77, the first 4 outputs the third 113-3 and fourth 113-4 MB 113 are connected to each other and to the second input 2 of the third 77-6 and fourth 77-7 RWE 77, the first 4 outputs the fifth 113-5 and sixth 113-6 MB 113 are connected with the second input 2 of the fifth 77-8 and sixth 77-9 RWE 77, the first 4 outputs the seventh 113-7 and eighth 113-8 MB 113 are connected to each other and to the second input 2 of the seventh 77-10 and eighth 77-11 RWE 77. The unit of analysis of time intervals is AVI 105 from BODS (Fig) contains two majority element 83-R+1 and 83-R+2, delay element τ 92-2, three decoder LH 108-1 to 108-3, three trigger TG109-1 to 109-3, three register 110-1 to 110-3, three counter 111-1 to 111-3, konjunktur OR 112. Host modes URR 80 (Fig) contains nine relay contacts CR 95-7 ÷ 95-15 (labeled control). Managed the voltage divider UDI 79 of the composition BOTH (Fig) contains two electronic key 77-5 and 77-6, seven resistors 114-1-114-7. The conversion unit time intervals (BPVI) 52 (Fig) contains two AC/DC 54-3 and 54-4 (D), mnogonatsionalny power supply peripheral (energy policy College-P) 74-14, the control circuit voltage (SKN) 115, OCXO (TSG) 119, - analog voltage Converter (DAC) 120, the microprocessor (MCP) 88-4, the adapter code RS-485 (Ad 485) 116, the adapter code RS-232 (Ad 232) 117, a display element (EI) 89-4, the switch code (CC) 118, the first 1 and second 3 group inputs BPVI connected with the first group inputs 1, respectively, the first 54-3 and the second 54-4 surfactants, 2 outputs which are connected to each other and to the first inputs 1 energy policy College 74-14 and SKN 115, the first output 2 energy policy College 74-14 connected with the first inputs 1 MCP 88-4, Hell 485 116, Hell 232 117, EI 89-4, QC 118, DAC 120, the second output 3 energy policy College 74-14 connected to the first input 1 TSG 119 and the second input 2 of the DAC 120, output 2 SKN 115 is connected to the second input 2 of the MCP 88-4 the first output 2 TSG 119 connected to the fourth input 4 MCP 88-4, exit 3 DAC 120 is connected to a second I the house 4 TSG 119, the second output 3 TSG 119 is connected to the third input 4 DAC 120, the first 5 MCP 88-4 connected with the second input 2 EI 89-4, the second output 6 MCP 88-4 connected to the second input 3 QC 118, the first 7 and second 8 inputs-outputs MCP 88-4 connected with the first inputs-2 outputs respectively Hell 485 116 and Hell 232 117, the second input-output 3 Hell 485 116 connected to the first input-output 2 QC 118, the second input-output 3 Ad 232 117 connected to the first input-output 2 BPVI, the first bus input 4-1 group of input / output 4 BPVI connected to the third input 3 MCP 88-4, the second bus input 4-2 group of input / output 4 BPVI connected with the third input 8 QC 118, the first 4 and second 5 outputs QC 118 are connected respectively to the first 4-3 and 4-4 second bus output group input / output 4 BPVI, the second 6 and third 7 inputs-outputs QC 118 are connected respectively with the first 4-5 and 4-6 second tires of the input / output group input / output BPVI. Control block control circuits, BCCU 103 from BODS (Fig) contains a node low voltage OTP 87-5, element galvanic isolation power supply EGREP 58-9, the microprocessor MCP 88-5, the display element EI 89-6, twenty-four differential chain operating mode DC1 119-1 ÷ 119-24, twenty-four differential chain test mode DC2 120-1 ÷ 120-24, the output relay power GRP 121, node keys 122 of the criminal code. Graph-scheme of algorithm electropower PH, technologies the CSOs equipment refueling and temperature control, and equipment PP (Fig) contains the following notation of functional nodes and conditional vertices. 123 - start operation mode electropower; 124 - input voltage ~ 380/220 V AC; 125 - enable PPS APS, UCEP, UCEP, SSK, SSK, POLPI, POLPI, UDUPA-BCP, UDUPA-SS, UUS, ORWAP (YEP, YEP, YEP, YEP), ORWAP (IEP), BIG ÷ BIG, TID-1 and 2, TID-KP, USES 1 and 2 (IEP); 126 - resolution supervisor to conduct electropower received? 127 - PSK APS enter the count of the checked element ; 128 - measure using the appropriate BIG insulation resistance current IE RfromIE; 129 - value of 130 - record the deviation of the parameter from the norm in repair list and continue measuring down the address of the parameter with a positive result; 131 - measure the resistance of a circuit element 132 - value of 133 - measure mutual resistance between IEiand IEjin one cable 134 - value of 135 - go to the address of the next IE Schaie+1 → Schaie; 136 - number of scanned IE less than N? 137 - PSK APS to enter the counter number of scanned discrete sensors 138 - measure using the appropriate BIG insulation resistance current DD 139 - value of 140 to measure the mutual resistance between DDiand DDjin one cable 141 - value of 142 - go to the following address DD of Scadd+1 → Scadd; 143 - number of scanned DD is less than the set M? 144 - PSK APS to enter the counter number of scanned analog sensors 1ththe PH level 145 - measure using the appropriate BIG insulation resistance current YES 146 - value of 147 to measure the circuit resistance of the analog sensor 148 - value of 149 - measure mutual resistance between YESiand YESjin one cable 150 - value of 151 - go to the following address YES SCADA+1 → SCADA; 152 - YES number of scanned is less than the set R? 153 - PSK APS to enter in sketchiest check onboard systems 1 thand 2thLV stage 154 - to inspect the health information channels (IR) onboard computing systems (BS) through the exchange of test parcels between UUS and systems; 155 the results of health checks IR BS positive? 156 - go to the address of the next BS Scabs+1 → Scabs; 157 - number of scanned BS is less than the set S? 158 - read in BWADE the results of measuring the size and condition of analog sensors BRS, WA and WA of TID-20-1 and TID-20-2; 159 - forward characteristics deviation YES BRS, WA and WA repair sheet; 160 - visualization repair records. The end of the regime of electropower. Graph-scheme of algorithm the final part of the launch of LV for MES PH (Fig) contains the following notation for the functional units and conventional cages is. 161 - start mode. The initial state summed UO - "ready"; 162 - pressure pneumatic equipment served? 163 - open electroneurography (EC) right column cable-filling tower (PC THAN for the working pressure in newmexico management (PSU) for PP-1; 164 the delay τ1; 165 - open EC of the left column AS (LC THAN for the working pressure in PSU for PP-2; 166 - pressure on the equipment served? 167 - Troubleshooting malfunctions; 168 - open EC PC AS and LC THAN for pneumatic device venting PP-1 and PP-2; 169 - pressure actuators PP submitted? 170 - emergency stop; 171 - break signal resistor jumpers "KP" received? 172 - signal "CP" in the NORTH; 173 the delay τ2; 174 to set fire to the pyroelectric mechanism retraction actuator UO-1; 175 the delay τ3; 176 to set fire to the pyroelectric mechanism retraction actuator PP-2; 177 - close to EC for implementation of drainage compressed air from PSU; 178 - to carry out pressurization PSU nitrogen; 179 - end mode. Automated control system for the processing and launch rockets MES PH works as follows. When installing the PH to the starting position and the connection of communications PH MES PH technological systems refueling and thermostability the tion is a supply kit device allocation blocks connectors PP BRS PH. MES PH, besides connecting to a PH of communications and control, the same communications associated with technological equipment refueling and temperature control with set UO BRS PH, the control unit rise in PH (the lift-off" - "KP"), with adjacent systems: automated control system of technological processes of ground-based equipment (APCS), a system of guaranteed power supply spaceport (CGAP), a system of ground-based measurements (NDA), a unified time system (CTS), ground-based automated control system PH (NASA PH). First, there is a partial inclusion of equipment MES PH for the implementation of mode electropower communications components and systems PH and technological equipment refueling and temperature. While previously included WP2 and WAVE. When applying for group input 5 in MES input three-phase AC voltage ~ 380/220 V from the power distribution panel (SRP) energy systems of the spaceport, included the resident set of equipment necessary for conducting mode electropower. At the remote command center is activated PSC APS 5 UDUPA BCP 9, POLPI 8-1. UCAP 6-1 is in a state of "Readiness". In starting the construction of SS include UDUPA SS 13 and USUALE 8-2. UCAP 6-2 is in the state "Ready is here". Input voltage AC input 5 MES PH can be fed from two voltage sources. In the preparatory commissioning period at the entrance MES PH is energized from the two systems normal power supply SES. In this case, the equipment system works in conjunction with devices uninterruptible power supply mbea 12-1 to 12-3 are connected to the corresponding UCAP 6-1 to 6-3. Mode electropower with PH and technological equipment is standard. Input 5 MES PH serves voltage from the two networks uninterruptible power systems CHAP spaceport. In this work, the mbea is disconnected from ORWAP using the manual controls. When applying voltage to the input 5 of the system is sent to group inputs 1 UCAP 6-1 ÷ 6-3 (7). In each UCAP mains voltage from the first network input 1-1 arrives at the inputs 1 relay phase monitor RKF 41-1, node failover UAP 47-1, power switch battery PPB 42-1 their crimes and entry 3 source of secondary power supplies power supplies 45-1. The voltage from the second network input 1-2 arrives at the inputs 1 RKF 41-2, UAP 47-2, PPB 42-2 and input 3 input power supplies 45-2. With outputs 2 RKF 41-1 and 41-2 on the output bus state 13-2 generates signals 3 and 9 "Norm 380/220 B1" and "Normal 380/220 B2"indicating the presence of stresses in the norm in the seeming, with outputs 1 power supplies 45-1 and 45-2 are signals 4 and 7 "IWEP 1 on" and "power supplies 2 inclusive. With outputs 2 PPB 42-1 and 42-2 mains network I and network II is coming to the inputs 1 and 2 of the machine input AVR 30-5. The combined outputs 3 PPB 42-1 and 42-2 issue on output bus state 13-2 signal 8 "ABP connected." In addition, the combined outputs 2 power supplies 45-1 and 45-2 filed to the input of the mode switch control spring 40, which may be in a state of local control and remote control, manually installed its control. Depending on the control mode bus States generates signals 1 and 2 of "Local control" or "Remote control". The set of signals 1÷4, 7÷9 of the bus 13-2 each UCAP transmitted respectively in the group of input-output 4 UDUPA-VCP from UCAP 6-1 and group inputs and outputs 6-8 UDUPA-SS 13, respectively, of UCAP 6-2 and 6-3. With outputs 3 UAP 47-1 voltage networks I and II are sent to the input 3 of the contact groups 44-1 and 44-2 and inputs 1 individual machines 46-9 and 46-19 formed at the output 11 UCAP 6-1 duty AC voltage of 220 C. With outputs 1 and 2 power supplies 45-1 and 45-2, respectively, are combined circuit of the positive and negative poles received: from outputs 1 on input 2 electroconduction 43-1 and 43-2 and positive poles of a group of outputs 12 UCAP 6-1 and 6-2, from outputs 2 chrome the previously mentioned input 1 of the spring 40 and the negative poles of the group of outputs 12 UCAP 6-1 and 6-2. Formed on duty voltage DC = 24 Cent. Duty voltage ~ 220V output 11 UCAP 6-1 served on the inclusion PPS APS 5 input 1. Duty voltage = 24 V outputs 12 UCAP 6-1 and 6-2 includes inputs 1 UDUPA-BCP 9, POLPI 8-1 and 8-2, UDUPA-SS 13. The system is ready to turn on the equipment required for carrying out the mode of LV electrical tests. For holding mode electropower communications MES PH with process control objects for filling and temperature control, control of PH rise, set of equipment PP BRS PH and elements and systems PH must also resident equipment to include BOTH 15-1 to 15-9 Appendix, ORWAP 14-1 and INRM from 75-1, 75-2, 75-3, 75-11, ORWAP 14-2 and INRM 75-1 of its composition, TID-20-1 and 20-2, TID-KP 24, USES 18-1 and 18-2, INRM 75-13 in their composition. Checked the following elements and systems: discrete sensors PH, technological equipment and UO BRS and resistive jumper control unit rise in PH (KP); signals docking of compounds of elements of the object and the individual parts of the system; analog temperature sensors type thermistors RTD; analog potentiometric pressure sensors traffic in strn, BRS and sensors YES PP BRS; Executive elements IE type electroneurography EPA, EC and paraelemental PE; - multi-wire bus feed the systems PH; - bus serial code systems PH. Types of electropower carried out in MES PH: - measurement of insulation resistance; - resistance measurement circuit; the continuity test; - measure resistance between the different elements (galvanic separation). The principle of electropower - measuring resistors in the circuit for measuring BOTH (Fig). You must connect the two poles of the measured resistance. To measure the insulation resistance of the second pole is the body of the equipment for other electropower second pole of the scanned objects are used from the lists of elements. A comprehensive check of all links of scanned items is consistent resistance check all contacts of the object relative to the second pole. For example, for element IE is measured resistances R+1-1, R+2-1, R-2-1, which should be normally equal to R+2+1=R+1-1=RPC+Rie, R-2-1=0 (short circuit), where RPCthe resistance of the supply chain from MES PH to IE and IE to MES PH. The resistance Rieusually equal to several tens of Ohms. The scheme of measurements BOTH consists of measuring power supply IIEP 76, the control voltage divider UDN 79, host modes At The R 80, electronic keys 77-1 ÷ 77-4, transducers 81-1 to 81-4, multichannel analog-to-digital Converter 82-1. Driver control signals 73-4 and processor 71-4 manages the scheme of measurement and conversion processing for the issuance of its input-output 2 in the FCS 7-2. The first pole of the measured object is connected with the output switch analog signal CAS 78-1 to log in URR 80. The second pole of the inspected object connects to the scheme of measurement of the output Cam 78-2 input 10 YPP 80. The second pole of the measurement to check the insulation resistance Rfromconnected to the housing through the inlet 7 YPP 80. Input 16 BIG 15 is connected to the input 8 URR 80 for possible checks the resistance of the object relative to the other wires in the system, in addition to the corps. Besides carrying electropower relationship of the elements of the control objects and the elements themselves validated system PH. Part of the inspections, which consists in measuring insulation resistance screens lived communication systems, is carried out in a number of electropower elements. Advanced system checked algorithmically by analysing information from systems PH. To initiate the operation of systems and analysis of their information you must include in addition to the equipment electropower UUS 3-2 and USES 18-1 and 18-2. The power on these device is TBA served with already included UCAP 6-2. Commands to enable UUS 3-2, USES 18-1 and 18-2 are served with PPS APS 5 through UDUPA-BCP 9, POLPI 8-1, 8-2, UDUPA-SS 13 and through the FCS 7-1, POLPI 8-1, 8-2 (network TV), SSK 7-2 (UUS 3-2 and USES 18-1 and 18-2). With SSK 7-2, with its input-output 7, the command to enable UUS 3-2 input-output 9. With SSK 7-2, with its inputs-outputs 17 and 18, serves to activate respectively USES 18-1 and 18-2. On the same inputs-outputs examines the state of the included devices. They must be in the ready state. Otherwise, their state of unpreparedness is transmitted to PPS APS for making decisions about the restoration of the included devices. In UUSS (figure 4) exchange of information with the FCS 7-2 there are two bus network 9-1 and 9-2. The team with PPS APS 5 is fed to the inputs and outputs are 4 switches in the network 25-5 and 25-6 and thence to the inputs-outputs 3 inputs-outputs 5-1 and 5-2 CPU 35. Information from UUS in the Central processor (figure 5) to the inputs-outputs 5-1 and 5-2 are accepted on inputs-outputs 5 switches in the network 25-8 and 25-9 and passed from them to the processors 38-1 to 38-3 on inputs-outputs 6÷8. In USES (Fig) exchange of information with the FCS 7-2 is based on group input-output 2 on tires 2-1 and 2-2. In the module I / o 61-19 gathers information about the state of INRM 75-12 and 75-13 their outputs 4-1 to 4-4 and depending on the state of INRM 75-12 and 75-13 they can be served the team is connecting with the group of output 3 MW subgroups 3-3 and 3-4 on INRM 75-13. For electropower included only INRM 75-13. States INRM can be: 4-1 "Fault 1", the corresponding fault is included in the EPI 75 module rectifier MB 113-1; 4-2 - Readiness", which is formed by the presence of two signals "Ready" modules rectifier 113-1 and 113-2; 4-3 - Enabled after enabling both MB 113-1 and 113-2; 4-4 - "Fault 2"corresponding to the faults included in the EPI 56 module 113-2. This is shown in Fig for OPPA, where EPI is opened to its constituent MB. If you receive at least one signal "Fault 1" or "Alarm 2", then this is notified to the operator PPS APS, and next steps to continue or restore the performance of MB - takes the operator PPS APS. After you enable USES 18-1 and 18-2 output voltage power systems PH subgroups 12-1 and 12-2 group exit 12 MES PH is fed to the power equipment systems for the first and second stages PH (strn, strn) multi-wire bus power. UUS 3-2 receives information from systems and its analysis make sure of serviceability or malfunction of the system PH. Electrical test communications from analog sensors YES for PRS to the inputs 12 MES PH and YES sets UO-1 BRS PH and PP-2 BRS PH respectively to the inputs 20-1 and 20-2 MES PH produced using TID-20-1 and uiv-And 20-2. TID (Fig), comprising the her of 2n nodes, transformation and normalization, has the hardware capability to verify the integrity of the sensor circuits analog signals. When a defective condition of the circuit lines on the front panel two nodes, arranged structurally in a single module, glow with red light indicators, and the analog signal is out of range normalization and equal to the 11th Century For data YES characteristics of the circuit continuity is sufficient. The signals of the measurement results and verify the integrity of the circuits YES come in BWADE 16. In BWADE 16 (Fig) analog signals are in MACP 82-2 ÷ 82-4 and later in the processors 71-7 ÷ 71-9 through M1 ~ M3. From BWADE 16 information comes in UUS 3-2 and then through the FCS 7-2, POLPI 8-2, 8-1, SSK 7-1 she seems to be in PPS APS operator. Further regular modes refills and temperature PH and synchronization start not used BOTH 15-1 to 15-9 Appendix. In addition, for UCAP 6 not used mbea 12-1 to 12-3, for UUSS not used PI 11-1 to 11-5. Accordingly, in ORWAP 14-1 and 14-2 disabled INRM 75-3 each. In addition to the devices that are enabled for mode electropower UCAP 6-1 and 6-2, PPS APS 5, SSK 7-1 and 7-2, POLPI 8-1 and 8-2, UDUPA BCP 9, UDUPA SS 13, ORWAP 14-1 and 14-2, 3-2 MCU, BWADE 16, USES 18-1 and 18-2, TID-20-1, TID-KP 24-enabled device UUS 3-1, 3-3 to 3-5, ARMO 4-1 to 4-4, UCAP 6-3, fire protection 10, BWDI 17-1 to 17-7, USE 19-1 to 19-8, TID-D 21-1 to 21-5, TID And 20-2, UPPA 22-1 and 22-2. In ORWAP 1-1 and 14-2 includes all INRM except 75-3, in USES 18-1 and 18-2 included INRM 75-12 in each. Information on the status of discrete sensors DD and signal coupling SS for PH and technological equipment refueling and temperature STM, STM, TORT, TORT, TST is introduced into the system through subgroups 10-1 ÷ 10-8 group of 10 MES PH. It arrives respectively for group 2 inputs TID-D 21-1, TID-D 21-2, group inputs 4 BWDI 17-2 and group inputs 2 TID-D 21-3, group inputs 4 BWDI 17-4, group 2 inputs TID-D 21-4, group inputs 4 BWDI 17-6, group 2 inputs TID-D 21-5. In TID-D 21 (Fig) signals from DD and SS via terminals 2-1 to 2-R arrive at the inputs of the intrinsic barriers 97 discrete signals of the nodes 1÷R. the Nodes of intrinsic safety and normalization have also composed of a control unit and galvanic decoupling UPR 98, the DC/DC Converter DD 96, the output relay V.R. 103. The set of these nodes and their connections provide electrical isolation between the incoming signals and supply power in case of an emergency communications discrete signals from DD and SS provide safety equipment MES PH in the path of the discrete data. Process control equipment fueling and temperature control for 1thstage PH (strn) is non-explosive zone, therefore, the signals from the subgroups 10-3, 10-5 and 10-7 arrive at whodi relevant BWDI 17-2, 17-4, 17-6. In BWDI 17 (Fig) signals via terminals 4-1 to 4-k arrive at the inputs 1-1 ÷ 1-k normalizers discrete sensors 72-4 ÷ 72-6. Process control equipment fueling and temperature control second-stage PH (strn) is located in a hazardous area, therefore, the signals from the subgroups 10-4, 10-6 and 10-8 are received at the inputs TID-D, respectively 21-3 ÷ 21-5. With outputs 1 TID-D 21-3 ÷ 21-5 information supplied respectively to the inputs 4 BWDI 17-3, 17-5 and 17-7. In BWDI output TAR 72-4 ÷ 72-6 information via a bus line M1 ~ M3 is transmitted to the peripheral processors 71-4 ÷ 71-6. From the outputs of the processors in the group of input-output 2 processed in accordance with the algorithms computing the information is transmitted to the corresponding WUSS: inputs-outputs 2 BWADE 16, BWDI 17-1 - UUS 3-2, with inputs-outputs 2 BWDI 17-2 and 17-3 - UUS 3-3, with inputs-outputs 2 BWDI 17-4 and 17-5 - UUS 3-4, inputs-outputs 2 BWDI 17-6 and 17-7 - UUS 3-5. From input-output 9 UUS 3-2 ÷ 3-5 information through the FCS 7-2 and 7-1, passing USUALE 8-2 and 8-1, distributed in the FCS 7-1 in the appropriate ARMO: from UUS 3-2 - ARMO 4-1, from UUS 3-3 - ARMO 4-2, from UUS 3-4 - ARMO 4-3, from UUS 3-5 - ARMO 4-4. If for any channels available information about the fault DD or SS, it is translated in PPS APS 5 to diagnose the problem. Information from analog sensors YES is entered in the system in the filling mode, termostatico the project through the group entrance 11 MES PH. She arrives at the group entrance 3 uiv-And 20-1. In uiv (Fig) information received via the inputs 3-1 to 3-n to the inputs of intrinsic barriers BI 97 analog signals into corresponding node intrinsically safe Normalizer analog information INAI. INAI comprises in addition to the input stabilizing barrier intrinsic safety 97 element galvanic isolation power supply EGREP 98, the output Converter is the Normalizer of Pnorm 99 and the node of the power conversion DC/DC DD 96. The set of these elements in the node INAI and their relationships provide galvanic isolation of the incoming information and the supplied power. Outputs of INAI 1-n+1 ÷ 1-2n normalized in the range 0-10V and explosion signals, providing safety equipment MES PH in the path of the analog information, proceed to the appropriate bus group input 4 BWADE 16. Input 4 BWADE (Fig) signals arrive at the inputs 1-1 ... 1-m modules multi-channel analog-to-digital Converter MACP 82-2 ÷ 82-4. MACP 82 (Fig) contains an element multichannel ADC 62-2, the inputs of which 1-1 ÷ 1-m receives input information from output TID-20, scheme 87-3 undervoltage element galvanic isolation power supply EGREP 58-9, the microprocessor MCP 88-3, the display element EI 89-3. Input 2 in MACP powered, input-output organizatsia communication with the processor. Service entrance-exit 4 in the preparatory period contains the information in the PCs 88-3. Received from MACP 62-2 input signal "Ready", ITUC 88-3 produces the output 2 in MACP 62-2 command "Read". Command codes with output 4 MACP 62-2 is fed to the input 3 MCP 8-3. With input-output 3 MACP 82-2 ÷ 82-4, respectively, via a bus line M1 ~ M3 information in a digital code is supplied to the inputs-outputs 4 peripheral processors 71-7 ÷ 71-9 in BWADE 16. With inputs-outputs 2 and 3 of the processor through the input-output 2 BWADE 16 information comes in UUS 3-2, and then through the FCS 7-2, 7-1, POLPI 8-2, 8-1 in ARMO 4-1. Issuing control commands for components and systems PH is from BWADE 16, USES 18-1, BWDI 17-1, USES 18-2 control UUS 3-2. The control commands for the subsystem charging of the first MCT is organized using BWDI 17-2 and 17-3, USE 19-1 and 19-2 running from UUS 3-3. The control commands for the subsystem charging of the second MCT is organized using BWDI 17-4 and 17-5, USE 19-3 and 19-4 running from UUS 3-4. The control commands for the subsystem temperature is organized using BWDI 17-6 and 17-7, USE 19-5 and 19-6 running UUS 3-5. Issuing single commands set ARMO, for subsystem control elements and systems PH - ARMO 4-1, for subsystem control filling of the first MCT - ARMO 4-2, for subsystem control filling of the second MCT - ARMO 4-3, p is sistemy control temperature control with ARMO 4-4. With ARMO commands via the FCS 7-1, POLPI 8-1, 8-2, SSK 7-2 transferred to the appropriate MCU. If running any mode, with the arm in UUS issued only to run mode, and the control commands are generated by the programs in UUS. Of UUS in BWADE 16, BWDI 17 team come on group inputs-outputs 1 and 3 and proceed to group the inputs and outputs 2 BWADE, BWDI. In BWADE, BWDI the CPU 71 via a bus line M1 ~ M3 are transmitted in blocks forming control signals, BFSU 73. BFSU 73 (Fig) contains an element galvanic isolation power supply EGREP 58-8, circuit undervoltage SF 87-2, microprocessor MCP 88-2, the display element EI 89-2, the node 90 of the output keys UVC output relays 91-1 to 91-n, item 92 delay, the node 93 items feedback contact group 94-1 to 94-n output relay with fuse and diode. Group output 1-1 to 1-n of the contact groups contains two outputs: direct 1-1-1 to 1-1-n and 1-2-1 feedback ÷ 1-2-n. The outputs of the contact groups arrive at a majority of the contact elements 83 (Fig), which majorityof team of three BFSU 73. After the power is in BFSU 73 input 2 and obtain the input-output 3 command to issue MCP 88-2 issues a group of commands (control signals) from its instruction register their outputs 3-1 to 3-n input to the output node keys UVC 90. The command "You shall AMB" output 2 MCP 88-2 gates UVC 90 and transmits appropriate signals to output relay 91. When triggered, the set of contacts 94 of relay 91 signals from outputs of feedback 1-2-1 ... 1-2-n with a delay τ in the delay elements 92 are recorded in the register feedback OEWG 93 and later in MCP 88-2 on inputs 4-1 to 4-n on the command input 5 MCP 88-2. MES PH interacts with the outside adjacent systems as a remote command post of the CPSU and the starting position in the starting structure of the SS. On BCP interaction with the automated control system of technological processes of surface equipment control system (APCS) is carried out by a group inputs-outputs 1 MES PH, uninterruptible power systems (SGAP) 2, system ground-based measurements (NDA) 3, single time SITTING - group inputs outputs 4 MES PH. These systems are connected respectively to the second, fourth, sixth and eighth (through WAVE 1) group inputs-outputs UUS 3-1 (figure 4). These inputs and outputs are connected respectively to the first, second, third and fourth inputs-outputs of the three multi-interface card (MIC) 36-1 to 36-3. Signals from external devices accepted these MICK and they form a team for APCS BUT group inputs and outputs 6 MICK 36-1 to 36-3 via a bus line M1 ~ M3 exchange information with the Central processor 35. Information from external connecting devices to the CPSU passed ARMO 4-1, where included in algori the m interaction with adjacent systems. On the starting position in the starting structure SS MES PH receives data from ground-based automated control system of the NASA PH on group input-output 6, issues a command group exit 7 BWDI 15-7. Output 17 RODS 23 in the region of information transmitted by the contacts of output relays, and with a subset of input 8-3 information from the NASA PH via IEC 62-n+1 enters the TAR 53-7 ÷ 53-9 and forth via a bus line M1 ~ M3 processors 29-8 ÷ 29-10. Systems MES PH PH interacts after power-on transducers systems from USES 18-1 and 18-2 and receives data through the first and second subgroups 14-1 and 14-2. Information systems PH goes on group inputs-outputs 2 and 4 UUS 3-2. In UUS 3-2 information systems PH goes to MICK 36-1 to 36-3 and forth via a bus line M1 ~ M3 processor 35. The synchronization mode start PH requires interaction MES PH system with a single time SITTING. MES PH communicates with taking BCP with WAVY, and information on the early start PH issues in the NORTH to the starting position (from SS) using RODS 23. The inclusion of WAVE is carried out in advance, even before the mode electropower communications MES PH with PH, technological equipment refueling and temperature control and set UO BRS. The inclusion WAVE is feeding him voltages from the two AC networks group is new to the input 1 through individual machines 46-21 and 46-22 of the composition distributor WP2 (Fig). WP2 is included in the manual mode for a few days before the start of the regular work MES PH. First of WAVE takes from SITTING on three independent channels of serial interface subgroups 4-3 group of input / output 4 in MES PH code current time and date (VI NORTH). After completion of the MES PH for normal refueling and temperature PH WAVE provides information exchange with the control unit and communication UUS 3-1 responsible in the system for communication with adjacent systems. WAVE provides reception of UUS 3-1 in the group entrance-exit 4: code estimated time of start (WI); commands stop/resume count. WAVE provides transmission in UUS 3-1 informational messages with a periodicity of τ containing; code current time (WI); code countdown time or flight time (WI); code of estimated or actual start time (WI); ID successfully adopted team (if you receive one during the preceding time interval τ); - information about the state of each channel WAVE (good condition/malfunction, the power from each of the two independent AC sources, the presence of signals docking hardware CTS). With the direct exchange of information with the NORTH group input-output 4 system WAVE is well coordinated transmission in the NORTH in the subgroup output 4-2 information about countdown time or flight time (VI) and in the subgroup output 4-1 information about the estimated or actual start time (VI) for subsequent display on wall displays in NORTH America. At the start of the PH in the first place will know MES PH signal "KP", WAVE receives from UUS 3-1 command shutdown countdown STOP. This team WAVE passes in the NORTH VI is not a countdown, and flight time. Also in the NORTH is passed to the actual starting time. WAVE after SOWING input 4-4 signal START provides: - translation UI with an estimated start time to the actual time; - translation UI with a countdown on the direct flight time. The reference flight time starts from zero. WAVE (Fig.9) includes: three conversion unit time information, BPVI 52-1 to 52-3; the Central processor of the data processing PCOD 38-4; two power distribution unit PDU 51-1 and 51-2; - patch panel 50. The basis WAVE are three BPVI 52-1 to 52-3. BPVI (Fig) is implemented in the microcontroller 86-4, which carries out the processing of temporal information, communication from the NORTH and parts MES, diagnosis integral part of BPVI, communication channels WAVE, the presence of signals dock. In case of failure of channels SOWING forming VI, OCXO TSG 119 from BPVI provides the necessary accuracy of the time information. An element digital-to-analogue Converter DAC 120 call is employed to stabilize the frequency of TSH 119. Duplicate converters AC/DC 54-3 and 54-4, together with peripheral mnogopoliarnym source of supply energy policy College-P 74-14 and control circuit voltage SKN 115 provide a reliable supply of components BPVI and control its availability. The interaction of MES PH from the NORTH after receiving the signal "CP" from the node control start group input 7 system is the development of the STOP signal for WAVE and develop information for SOWING of early separation the PH of the starting table. The signal "CP" from the entrance 7 MES PH goes on group input 2 in TID-KP 24, where it is normalized and becomes intrinsically safe. The group output 1 TID-KP 24 signal KP enters RODS 23 on the second group input 8. In BODS 23 (Fig) through patch panel input signals CPUs 104 is transmitted through three channels 1, 2, 3 in BNDD 72-10 ÷ 72-12 in the form of sub-signals. From BNDD 72-10 ÷ 72-12 through M1 ~ M3 and via processors 71-11 ÷ 71-13 information is transmitted in BFSU 73-11 ÷ 73-13 and then majorities in the majority of relevant elements of the VME 59-6. Group output 4 UME 59-6 the fifth group exit 17 BODS 23 information about the beginning of the separation the PH of the starting table in the fifth group exit 21 MES PH is passed to the NORTH. The interaction of MES PH with elements of the set PP SRS occurs from the moment of installation of the PH to the starting position to the last phase of the start and unstressed is Toda communications from PH with a kit UO PH BRS. Set UO BRS PH at the beginning of the interaction with MES PH should be in state "Ready to work". Job readiness is a state of the set in which it is ready to support work on the preparation of the PH to start. When translated set status to "Ready to work" should be checking the technical condition and health PP BRS PH, power, and compressed gases, control of the initial position of its component parts, operation verification. The initial state set (designated position UO) is characterized by the following: - arrows UO allocated, the allocation mechanisms (MO) abstracted discrete sensors DD PP-1 and PP-2 are partially included (sensors, responsible for the allocation of EE); - pressure compressed air and nitrogen on technological equipment PP - pneumomia management PSU is not issued; - power supply with electrical kit removed (not connected power supply USE 19-7 and 19-8, as well as in UPPE 22-1 and 22-2). When the PH at the start, is supplied thereto PP-1 and PP-2. Summed up the state of MA is characterized by the following: - arrows UO and MO summed up, tracking systems UO connected to respective BRS; - arrows UO fixed lock; - peraclean (PE) drive MO closed; - pressure compressed gases and the supply of pneumatic equipment (ON) is adopted; discrete sensors DD PP-1 and PP-2, responsible for supply PP included. After joining UO to BRS on PH, gaskets and connecting communications to the PRS checks the integrity of the circuits described already in the mode electropower communications PH and technological equipment. Next steps MES PH with elements of the set UO BRS PH is represented on a graph-scheme of the final part of the launch of LV for MES PH (Fig). In accordance with the sequence diagram pre-start preparation PH to start shortly before the start is supplied compressed air to pneumatic equipment (ON) set PP SRS. This is fixed by the state part of the discrete sensors DD left and right columns AS (PC THAN and THAN LK). In addition, constantly monitored signals dock pneumatic equipment tested in mode electropower. The analysis of the status signals, DD, SS, filed under group inputs 17-1 and 17-2 MES PH from PC THAN and THAN LK. The signals are sent to group inputs TID-D 21-6 and TID-D 21-7, respectively. Reception of signals at the device intrinsically safe input required since the hardware kit PP SRS is located in fire zone because of the atmosphere of hydrogen and air. After passing the TID-D 21-6 and 21-7 information with their group outputs enters RODS 23 group inputs 14 and 11, respectively the military. In BODS signals are accepted for group inputs 10 and 13 CPUs 104, and a group of outputs 1-3 CPUs they are distributed in the channel BNDD 72-10 ÷ 72-12 group inputs 1. With outputs 4 BNDD 72-10 ÷ 72-12 through M1 ~ M3 reported to group inputs 1 processor peripheral 71-11 ÷ 71-13. From the outputs of the processor information through the network switches 25-20 and 25-21 with a group of input / output 2 BEDS 23 is transmitted to the MCU 3-5. In the UUS information majorities and through the FCS 7-2, POLPI 8-2, 8-1, SSK 7-1 goes in ARMO 4-4. In UUS a signal is generated PRESSURE ON SUBMITTED (ON - equipment). The generated signal is transmitted to the ARMO and displayed on the monitor. Further according to the algorithm in UUS 3-5 is formed team of the opening of the electrovalves EC in PSU located on the PC THAN and THAN LK. Compressed air is supplied to PDU and receiving the working pressure is fixed at the actuation of the respective DD PC THAN and THAN LK. With the appropriate DD PC and WHEN Luke WHEN signals are issued in RODS 23 and later in UUS 3-5 and ARMO 4-4. On the monitor ARMO 4-4 shows the signal PRESSURE ON ON SUBMITTED. In the absence of a signal PRESSURE ON ON SUBMITTED are searching and Troubleshooting. To this end, the monitor PPS APS 5 must be inferred values DD PC and WHEN Luke AS promptly stored in the peripheral processors 71-11 ÷ 71-13 RODS 23. To this end, the team from UUS 3-5 transmitted to RODS 23 input-output 2 via the switches in the network 25-20 and 25-21 recorded in the processor 71-11 ÷ 71-13. Processor via M1 ~ M3 team opening required EC is transmitted in BFSU 73-11 ÷ 73-13. After activation of the required output relays i to their contacts management KU 94-i in three channels corresponding to BFSU 73-11 ÷ 73-13 they are in UME 59-6, where the majority of the contact elements, combined in a node of a majority of elements UME 59-6. Majorityowned commands from group outputs 7 and 8 of the VME through the appropriate group outputs 6 and 4 come in USE 19-8 and 19-7, where group outputs 4 outputs are routed through 16-2 and 16-1 on EK LK WHEN and PC AS well. After opening the command is required EC compressed air from PSU is supplied to the pneumatic device venting. In the presence of compressed air in the pneumatic trigger the appropriate DD - alerters pressure - give signals about the appropriate operating pressures in pneumatic circuits. The signals from these DD group inputs 17-1 and 17-2 come through uiv-D 21-6 and 21-7 in BAGS, arrive in UUS 3-5. In UUS 3-5 on the amount of any TLD is of the three detectors of pressure in pneumatic circuits from each PSU signals are formed and transferred to the ARMO 4-4 PRESSURE ON the ACTUATOR UO FILED. In the further presence of signals with these DD monitored. In the case of the disappearance of the signal from any PSU (will not be available at least two signals of the three), the program of preparation PH to start must be stopped. After all the preparatory work, ensure readiness for the interaction of MES PH with elements of UO BRS PH on the final phase start PH pre-filled and is in the standby mode, further actions with PP BRS, uncoupling BRS and outlet UO BRS. The last phase start PH starts with obtaining the MES PH signal group input 7 from the host signal (UIF) the lift-off". The formation of this signal is available in TID-KP 24, where analyzed separately line condition and the condition of the sensor KP - sets of resistive bridges. UIF "KP" contains two sets of resistive bridges - three jumpers in each kit for PP-1 and PP-2. The signal KP is formed at break of at least two jumpers in each set. All options signal "CP" output TID-KP 24 presented in the table. 1
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0 | 1 | 0 | 1 | × | × | 1 | 1 | |||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
8 | × | × | 0 | 1 | 0 | 1 | 0 | 1 | × | × | 0 | 1 | 1 | 1 | ||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
9 | × | × | 0 | 1 | 0 | 1 | × | × | 0 | 1 | 0 | 1 | 1 | 1 |
In the process of starting PH after receiving the signal "CP" MES PH is required to form after a pause τ1the team at undermining cutter for UO-1.
The formation of teams of undermining the cutter is in the unit of analysis time is i.i.d. intervals BAVI 105.
To undermine cutter for UO-1 command generates BAVI 105-1, and UO-2 - BAVI 105-2.
Interaction equipment MES PH to undermine paraelemental PE PP-1 and PP-2 is as follows.
After receiving the signal KP in TID-KP 24 there based on the analysis of path conditions of the first and second sets of FDS "KP" (see table 1) produced signals that the group output 1 TID-KP are input 8 in BEDS 23. In BODS signals fed to the input 14 CPUs 104, and then allocated to outputs 1÷3 and sent to BNDD 72-10 ÷ 72-12. The received information from outputs 4 BNDD through a bus M1 ~ M3 recorded in the peripheral processors 71-11 ÷ 71-13. The processor starts implemented control algorithm elements set UO PH BRS.
With a group of inputs-outputs 1 processors via M1 ~ M3 information about the time delay for issuing commands undermine PE PP-1 and PP-2 is recorded in BAVI 105-1 and 105-2. In BAVI (Fig) information on the group inputs 2-4 transmitted to the decoders binary code 108-1 to 108-3. In BAVI 108-1 entered delay time τ1for PP-1, and in BAVI 108-2 - delay time τ2for PP-2.
With outputs 1 accident 108-1 to 108-3 signal start timing to generate commands to undermine PE translates triggers 109-1 to 109-3 in the enabled state ("1" in the output). Output triggers strobilus registers delay time 111-1 to 111-3 on input 1. The following soo is the incarnation - code time delay is recorded with inputs BAVI 2÷4 strobirovaniya registers 110-1 to 110-3. Codes from registers 110 correspond to the latency counters 111-1 to 111-3. Decrement the read (decrease by one) counters from τ (τ1for BAVI 105-1, τ2for BAVI 105-2) to 0 is the timestamp from the output element OR 112. Simultaneously with the outputs of the elements OR 112 operates regular reset registers 110-1 to 110-3 input 4. This is done to prevent the formation of false signals recording in the counters 111 to register 110. The signals at the output of the element OR 112 appear or formed and majorityowned signal on the majority element 83-2P+2 or input 5 BAVI.
The time signal (time stamps) in MES PH can be transferred in BAVI in two ways depending on the actual load of the internal communications in the system.
In the first case, the time signal is transmitted from WAVE 1 group entrance-exit 4 in UUS 3-1 at the group entrance-exit 8. Further, the signal from the MCU 3-3 group entrance-exit 9 is transmitted in the FCS 7-1 on group input / output 1. Further, the signal group output input SSK 7-1 29 is fed to group the input-output 2 USUALE 8-1 and through group input-output 4 is transmitted to the group of input-output 4 USUALE 8-2, then through the group entrance-exit 2 through 29 input-output SCQ-2 group input-output SCQ 7 7-2 before what is in UUS 3-5 through group input-output 9. From UUS 3-5 group entrance-exit 5 information is transmitted in the group entrance-exit 2 in RODS 23. In BODS 23 information through the network switches 25-20 and 25-21 recorded in the processor 71-11 ÷ 71-13 and then through M1 ~ M3 and group inputs 2-4 BAVI 105 through outputs 2 LH 108-1 to 108-3 and me 83-2P-2 is fed to the input 1 of the OR element 112.
Backup path, which bypasses UUS 3-1, at this time may be overloaded communication with adjacent systems, includes the transmission of WAVE 1 input output 3 input-output 5 USUALE 8-1. Next, from USUALE 8-1 on group input-output 4 information is transmitted in USOLE 8-2 on the corresponding input-output 4. From USUALE 8-2 on group input-output 2 information comes in UUS 8-2, and group entrance-exit 7 is passed to the MCU 3-2 input-output 9. From UUS 3-2 input-output 6 information time signal arrives at the input 5 in RODS 23, and (Fig) is sent by the input 5 in BAVI 105-1 and 105-2. In BAVI 105 (Fig) signal input 5 is fed to the input 2 of the OR element 112.
After conversion, the required number of time stamps for delays τ1in BAVI 105-1 and τ2in BAVI 105-2 trigger counters 111-1 to 111-3 and majoritively signal with the majority element 82-2P+1 goes to output 1 BAVI 105 and through a delay element EZ 92-2 resets to "0" triggers 109-1 to 109-3. Output 1 BAVI in the subgroup 7-2 output for BAVI 105-1 and subgroup 7-4 DL is BAVI 105-2 through group input-output 7 BEDS arrives at UPPA 22-1 (output 7-2) and OPPA 22-2 (output 7-4) subgroup of inputs 2-1.
In UPPE 22 (Fig) there are sources of power INRM 46-21 ÷ 46-24. Each EPI 46 consists of a pair of rectifier modules MB. MB 113-1 and 113-2 form INRM 46-21, MB 113-3 and 113-4 - INRM 46-22, MB 113-5 and 113-6 - INRM 46-23, MB 113-7 and 113-8 - INRM 46-24. Each EPI 46 its output 4 is connected to the inputs of two pairs of electronic switches RWE 77. Outputs RWE 77-4, 77-6, 77-8, 77-10 form a subgroup 4-2 group 4, UPPA supplied to the second pole PE. From UPPA 22-1 subgroup 4-2 output 4 UPPE connected to the output 19-1 MES PH corresponding to the second pole PE PP-1; from WPA 22-2 this sub-group is connected to the output 19-2 MES PH corresponding to the second pole PE PP-2.
Outputs RWE 77-5, 77-7, 77-9, 77-11, together with the inputs-outputs 4 INRM 46-21 ÷ 46-24 connected at BOTH 15-9 Appendix and used in the mode electropower.
The first pole PE PP-1 and PP-2, respectively, of the input 18-1 and 18-2 are connected with 16 and 13 inputs RODS 23. In BODS inputs from the first poles of the PE connected to 8 and 11 inputs CPUs. The 4 outputs of the first poles PE PP-1 CPUs connected with the first subset of inputs 1-1, BCCU 103, and outputs the first 5 poles PE is connected to a second subset of the inputs 1-2 BCCU 103. In addition, passing the inputs of a majority node majority of elements 59-6, organized on the output contacts BFSU 73-11 ÷ 73-13, upon actuation commands to undermine PE, they form a chain in UME 59-6 with 6 outputs for PE PP-1 and 5 for PE PP-2, providing undermining PE from the EP 46 in UPPE 22-1 and 22-2.
BCCU 103 performs the function of the operational integrity of the control circuits during periods of normal operation. Due to its importance to the operation of undermining PE is a need to control the integrity of the tract, including PE.
BCCU (Fig) contains the set of elements of the differential circuits DC2 120-1 ÷ 120-24 to verify the integrity of the control circuits outside of the mode of interaction with elements of UO PH BRS.
The integrity of the control circuit in this case is checked by wrapping small currents.
Voltage wrapping small currents and served with output 3 item galvanic isolation power supply EGREP 58-9. Flowing currents control are node keys 122 of the criminal code, the elements of which have the relay characteristic, restoring to the normal value small currents. From the output 122 of the criminal code signals the integrity of the controlled circuits are recorded in the microprocessor MCP 88-5. In operation, when the signals on the actuation element, in this case, PE, another group working differential circuits DC 119 serves as a load running IE. The signals from the outputs of the DC 119-1 ÷ 119-24 recorded in the PCs 88-5.
Further, after blowing PE for PP-1 and PP-2 MES PH interacts with elements of the set UO BRS on measuring circuits analog sensors - YES PP-1 and PP-2 - transformers primary angular movements of POP for the determining the angles of rotation of the shafts PP-1 and PP-2 and the rotation angles of the RAM mechanism allotment PP-1 and PP-2.
In a system for converting and normalizing the analog signals from PUP located in temporary emergency fire zone PVOS permanent control a working state of the measuring circuits and provide the type of protection "intrinsically safe electrical circuit level ib" are used transducers with a universal input - nodes INI is located in the device intrinsically safe analog input uiv-And 20-2. Each node INAI accepts the analog signal from PUP located in PVOS, converts it into a linearized, fully insulated signal in the safe area.
Next, the normalized signals from outputs of INAI arrive at the inputs MACP three channels 82-2 ÷ 82-4, located in BWADE 16 (Fig).
In MACP 82 is analog-to-digital conversion of the signals in digital form are transmitted through M1 ~ M3 processor peripherals 71-7 ÷ 71-9. After that, the signals are sent from BWADE in UUS 3-2, where are averaged values from different channels.
In the interaction of MES PH with elements of the set UO the PRS signal circuits from discrete sensors DD is monitoring the status of the limit switches PP to determine the position of the arrows PP-1 and PP-2 and the control contacts of the switches pressure switch SD to control the availability of compressed gases in newmexico control the La element EK in PCSB, LK THAN. Signals from DD PC THAN, THAN LK, UO-1, UO-2, located in PVOS, proceed to the inputs 17-1 to 17-4 system in TID-D 21-6 and 21-7. In TID-D are elements intrinsic barriers, performing normalization of signals discrete sensors and convert them into fully isolated signals in a safe area. Outputs TID-D 21-6 and 21-7 connected respectively to the inputs 14 and 11 RODS 23. In BOGS (Fig) discrete signals going to the marshalling in CPUs arrive at the inputs of the three channels BNDD 72-10 ÷ 72-12. After BND through M1 ~ M3 information is written to the peripheral processors 71-11 ÷ 71-13. Then, through the switches in the network 25-20 and 25-21 information is recorded in UUS 3-5 and analyzed to assess the accuracy of passing algorithm of interaction of the system with elements of UO PH BRS.
At the end of the start up mode provides drainage of compressed air from PSU and charging for security PSU nitrogen. With this purpose, control the operation of the relevant EC and control their execution state DD PC THAN and THAN LK.
The inventive automatic control system preparation and launch of LV can be implemented in the following form.
Personal computers for ARMO (figure 2) and PPS APS (figure 3) in the configuration:
- the system unit 27 consists of:
- Intel Core 2 DUO E8600 3.33/1333/6M/LGA775;
- case GHI 252 V2U with power supply 300 watt, USB/F, white;
module memory is DDR 2 2Gb;
as the rigid disk at least 320 Gb 7200;
- DVD-RW;
- MV type MSI RT-s;
- video card GigaByte GV-210 OS 512 Mb;
network card D-Link DGE 530T;
external devices:
keyboard 28 USB;
arm 29 "mouse" USB;
software Windows XP Prifessional Russian (oem);
monitor 26 30" TFT kit with HDMI cable-HDMI;
- the switch port 31 USB - KVM switch-type Aten CS-1764;
- network adapter from the USB output 32 - Trendnet TU2-ETG USB 2.0 k Gigabit Ethernet;
- printer 33 network type HP 5200 n;
switch 25 Ethernet type FGSW-2620;
machine 30 load transfer switch for backup power supply type ARS AR.
Device control and communication 3 (figure 4), the CPU (figure 5) and a software simulator (6) are implemented in the following form:
- Ethernet switches, 25-6 and 25-7 type at-8524;
node 34-1 collection of fault - 6051 ADAM;
- multi-interface card 36-1 to 36-4 - CPCI-3544;
- mnogonatsionalnyi power supply 37-1 to 37-5 - Power module CPCI 250 w - P AC/DC;
processors 38-1 to 38-4 - CPC-502 (RS);
device power management 39 IPM-8002.
Device allocation of primary power supply 6 (7) and WP2 (Fig) implemented in the following form:
switch 40 control modes switch CN-014 ULH company Shneider Electric and buttons MP1-20G and MP1-20R ABB;
relay 41-1 and 41-2 control phase - ELM-08 firm Meander;
switches 42-1 and 42-2 power battery ebbm - CN-014 ULH is Irma Shneider Electric;
- electroconductor 43-1 and 43-2 with contact groups 44-1 and 44-2 - A-30-2280 ABB;
source 45-1 and 45-2 of the secondary power - DNR 240 PS 24-01 firms XP-POWER;
individual machines 46-1 ÷ 46-22 phase in the range of 6 A, 10 a, 16 a and 25 A - type D according to category No. 06579, 06581, 06583 and 06585 Legrand;
- automatic activation of reserve 30-5 - ARS AR firm ARS;
- node failover 47-1 and 47-4 - CS-003 ALH Shneider Electric company;
indication of voltage 48-1 and 48-2 - "indicator light green No. 18321 Legrand;
control voltmeters 49-1 and 49-2 VLT-16061 firm Merlin Gerin.
The device processing time information WAVE 1 (Fig.9) is implemented in the following way:
- patch panel 50 has a constructive implementation TSUI firm "IRV", implemented on the contact Wago;
- power distribution units 51-1 and 51-2 TSUI commutes voltage networks 1 and 2 are implemented on the contact Wago and contain the fuses construct Wago in the form of terminals with fuse, catalogue No. 282-122;
blocks conversion time intervals, BPVI 52-1 and 52-2 (see Fig);
- mnogonatsionalny power supply energy policy College 37-7 type AT-PWR 3004;
the Central processor of the data processing 38-4 ramek-011-600;
machine input AVR 30-5 type ARS AR.
Mobile remote customer FP 10 (figure 10) is implemented in the following form:
- panel control the Oia power supply 53 is a complete design, contains a set of controls and display: ON/OFF switches for networks 1.2 type KIH-014 ULH Shneider Electric company; indicators network type "indicator light green" 18321 Legrand; fuses in the construction Wago in the form of terminals with fuse 1A, catalogue No. 282-122;
- converters AC/DC 54-1 and 54-2 type S-100 companies Mean Well;
- unifying the node 58 on the Schottky diodes type KD 269+EU;
control panel 55 includes buttons of PKN 1923 and indicators type indicator light green" 18321 Legrand has a constructive implementation RS company "SKB Orion";
modules I / o discrete information 56-1 and 56-2 type 6052 ADAM Advantech;
panel computers 57-1 and 57-2 AFL-FOBA-N270/R/16-R10 company AFOLUX.
Remote control unit primary power supply UDUPA-BCP 9 (11) and UDUPA-SS 13 (Fig) implemented in the following form:
- network switches 25-10 ÷ 25-12 and 25-15 ÷ 25-17 - ADAM-6521 Advantech;
modules I / o MW 61-1 ÷ 61-18 - ADAM 6050 Advantech;
- interface modules relay IRM 60-1 ÷ 60-12 49.31.7.024.0050 firm Finder;
element galvanic isolation power supply EGREP 58-1 ÷ 58-6 - DC/DC Converter SD-15B-24;
hosts the majority of the elements of the VME 59-1 to 59-4 collected on the relay contacts of the composition of the IRM 60.
Devices 12-1 to 12-3 uninterrupted power supply (Fig) is taken as the purchase of equipment; type APC Smart-UPS RT 20 kvA firm ARS./p>
Network system switch 7 (Fig) is implemented in the following form:
- network switches 25-13 and 25-14 - type at-8550 SP;
- mnogonatsionalnyi sources of supply energy policy College 37-8 37-9 and type at-PWR 3004;
- automatically switches 68-1 and 68-2 contain the fuse will automatically shut down relay-indicator from the device UVZ RP-RS company "Orion".
In communication fiber-optic transmission line information, POLPI 8-1, 8-2 (Fig) receiver-transmitters signals optic lines, which converts optical signals into signals of copper wire transmission lines and back, are implemented on the output stages of modules MW ADAM-6521 UDUPA-SS and UDUPA-BCP and cascades of FCS switches at-8550 SP.
Device distribution secondary power supply ORWAP 9 (Fig) implemented in the following form:
- network switches 25-18 and 25-19 type EDS-G308;
- electroconductor 43-3 - type 15984;
- time relay 70 - type ACTt 15419;
- power supply 74-1 to 74-3 in the products UP-RS company "Orion";
processors 71-1 to 71-3 in block MP-RS company "Orion";
- BND 72 (Fig), BFSU 73 (Fig);
- power supply 75-1 ÷ 75-11 presented on Fig within OPPA as consisting each of two modules rectifier 113 MB.
Unit definition functional readiness 15 (Fig) is implemented as follows:/p>
- mnogonatsionalny power supply energy policy College 74-4 - Power module CPCI 250 w - P AC/DC;
processor 71-4 CPC-20302 of Fastwel, parallel bus line M1 Compact PCI;
the signal control BFSU 73-4 see Fig;
measuring the power of IIEP 76 has a nominal output voltage of 27±is 0.135 In, input voltage ~ 220 Century uses of the source - product firms XP and Lambda (Nemic Lambda Ltd);
keys 77-1 ÷ 77-4 it contacts output relay BFSU 73-4;
switches analog signals CAS 78-1 and 78-2 are implemented on the relay contacts, relay type FTR-B4CA4.5Z Fujitsu Components, inc. All. The register, which is part of the switch is implemented on the chip CRT, the decoder on the chip CRID;
measuring converters 81-1 to 81-4 implemented on the chip PG204 by BURR-BROWN;
- multi-channel analog-to-digital Converter 62-1 containing nodes:
site management and control - microprocessor MB90F591GPE Fujitsu;
the digital - to-analog Converter - on-a-chip AD5542AR of Analog Devises;
- operational amplifiers - on-a-chip OP2177AD of Analog Devises;
- analog-to-digital Converter - on-a-chip AD7894 of Analog Devises;
- site digital selection feedback - on-a-chip PGA206 by BURR-BROWN;
switch analog signals implemented on the chip ADG408BR by BURR-BROWN;
- managed the voltage divider UDN 79 (Fig);
node modes URR 80 - see Fig.
Device for thermal actuators and systems USES 18 (Fig) and the unit start element USIA 19 (Fig) implemented in the following form:
- automatic activation of reserve 30-3 switch backup power type ARS AR;
the source of secondary power supplies power supplies 45 DNR 240 PS 24-01 firms XP-Power;
keys 77 on the contacts of the output relay module I / o 61-19;
module I / o 61-19 - two modules ADAM 6051;
the power supply 75 is presented on Fig within OPPA.
Block I / o discrete and analog information, BWADE 16 (Fig) and block I / o discrete information, BWDI 17 (Fig) implemented in the following form:
processors 71-4 ÷ 71-9 - ALS 20302 of Fastwel, bus line M1 ~ M3 Compact PCI;
- mnogonatsionalnyi sources of supply energy policy College 74-5 ÷ 74-10 in the composition of the UE device 37 WITH RS company "Orion";
- blocks the normalization of discrete sensors BNDD 72-4 ÷ 72-9 (Fig);
- blocks forming control signals, BFSU 73-4 ÷ 73-9 (Fig);
modules multichannel ADC 82-2 ÷ 82-4 (Fig);
- majoritarian elements-83 keys on the contacts of the output relay is BFSU 73-4 ÷ 73-9 (Fig).
The unit normalization of the discrete sensors BNDD 72 (Fig), the signal control BFSU 73 (Fig)module multichannel analog-to-digital conversion is the user MACP 82 (Fig) and the control unit control circuit 103 (Fig) have common nodes and specific nodes, characteristic for each module.
Shared nodes are implemented as follows.
Scheme 87 lowering the voltage on the power module P26TG2405E2:1M firm Peak Electronics and controller hot standby TPS2491DGS company Texas Instruments.
The elements 58 of the galvanic separation of the optocoupler LTV-827 firms Lite-on, the resistors in the performance: CHIP resistor J1206, CHIP resistor J2010, CHIP resistor F1206, CHIP resistor F1206, the Zener diode TL431 IPK company Texas Instruments, fuse SMD075-2, the capacitors in the performance: CHIP capacitor ceramic X7R-50 TO 1206, CHIP tantalum capacitor.
The microprocessor 88 is implemented on the microcontroller MB90F591GPF Fujitsu.
Indication elements 89 are implemented using a set of: light-emitting diodes 551-0201 and 551-0401 company Dialight, CHIP resistors J1206, buffer register 74HC245D.
BNDD 72 (Fig) in addition to the common node has nodes implemented as follows:
elements of the input 84-1 to 84-2k-1 for external signals - protective diodes SM6T-30 company Vishay;
elements test 84-2 ÷ 84-2k for test code - optocoupler LTV-827 firms Lite-on;
element 86 of the former test code - optocoupler LTV-827 firms Lite-on;
node 85 memory power-up - on-a-chip TM;
BFSU 73 (Fig) in addition to the common node has nodes implemented as follows:
node 90 of the output key - on circuits 133 TM;
relay - 91-1 to 91-n - bistable relay FTR-B4C IN 4.5Z Fujitsu Takamisawa;
node 93 feedback - photo-coupler LTV-827 firms Lite-on, the resistors in the performance of the CHIP resistor J2512;
- contact nodes 94-1 to 94-n, including the relay contacts of relay 91, fuse type FSMD 185-2 of the Poly-Switch, diode 50SQ 0806 company International Rectiver;
element 92 delay - on-a-chip AG.
MACP 82 (Fig) in addition to the common node has a node multichannel ADC 62-2 on-chip analog-to-digital Converter AD640AR of Analog Devices and a multiplexer on the chip ADG527AKR Analog Devices.
The device is intrinsically safe input analog information TID-20 (Fig) implemented on intrinsically safe transducers D1072 S/B series D1000 GM International.
The device is intrinsically safe input "pin up" TID-KP 24 (Fig) implemented on intrinsically safe repeater position sensor 100 with transistor input D1033 D/B and repeaters of the contact sensor 101 with relay output D1032 Q/B. Both elements of the family D1000 GM International.
The device is intrinsically safe input discrete information TID-D 21 (Fig) implemented on intrinsically safe repeater contact state sensors D1032 Q/B series D1000 GM International.
Block processing of discrete signals BODS 23 (Fig) is implemented in the following form:
- Ethernet switches, 25-20 and 25-21 type EDS-G308;
processors peripheral 71-11 ÷ 71-13 type CDS 20302 of Fastwel;
- bus line M1 ~ M3 Compact PCI;
- mnogonatsionalnyi sources of supply energy policy College 74-11 ÷ 74-13 type Power module CPCI 250 w - R AC/DC;
- BND 72-10 ÷ 72-12 (see Fig);
- BFSU 73-11 ÷ 73-13 (see Fig);
- BCCU 103 (see Fig);
- BAVI 105-1 and 105-2 (see Fig);
node majority of elements UME 59-6 implemented as a group the majority of items-keys IEC 83 (see Fig);
switching fee of input signals CPUs 104 built on the Wago terminals.
The device undermining of paraelemental UPPE 22 (Fig) is implemented in the following way:
- INRM 75-12 ÷ 75-15 consist each of two modules rectifier 113 MB; MB specialized development and production company SCAN SCAN 3.211.041 - SCAN 3.211.048-08;
- electronic keys RWE 77-4 ÷ 77-11 built on the contacts of the output relay is BFSU 73-11 ÷ 73-13 from RODS 23.
Power supply INRM 46 of the composition Fig is composed of modules rectifier 113. The rectifier modules specialized collection SCAN 3.211.041 ÷ SCAN 3.211.048-08, the company "CJSC SCAN".
The unit of analysis temporal information BAVI 105 (Fig) from RODS 23 is implemented in the following form:
- majoritarian elements-83 keys-2P+2 and 83-2P+1 (see Fig) on the contacts of the output relay is BFSU 73-11 ÷ 73-13 from BOGS;
- delay element 73 92-2 built on the chip 533 AHP;
- decoders accident 108-1 to 108-3 built on the chip KID;
triggers Tg 109-1 to 109-3 - on the chip TM;
the registers RG 110-1 to 110-3 - chip IR;
counter - MF 111-1 to 111-3 - chip IE;
Host modes URR 80 (Fig) of BOTH 15 implemented on the relay contacts 95-7 ÷ 95-15 D2A 050000 company COSMO ELECTRONICS CORPORATION.
Managed the voltage divider UDN 79 (Fig) of BOTH 15 consists of resistors 114-1 ÷ 114-7. Keys 77-2 and 77-3 is the output relay driver 73-4 control signals.
The conversion unit time intervals, BPVI 52 (Fig) from WAVE 1 is implemented in the following form:
- OCXO TSG 119 on the element chip GC-TC-54A-1 (ADCS TU);
- analog Converter DAC 120 on the chip PA (EAR 431320.160-01 TU);
- MCP 88-4 consists of programmable logic matrix PLA EPM 7256 SQC208 Altera and microcontroller A89c51ED2 Atmel;
- converters AC/DC AD 54-3 and 54-4 type S-100 companies Mean Well;
- adapters RS-485 116 and RS-232 117 built on the element MAH AE PI firm MAXIM.
Control block control circuits, BCCU 103 (Fig) from RODS 23 in addition to the common parts (see notes to BNDD, BFSU, MMACP) contains two groups of differential circuits DC2 and DC1. The elements in each group is connected in series optocoupler, resistor, diode, Zener diode. Type optocoupler LTV-827 firms Lite-On, CAY16-101JA, a resistor, CHIP, 1 kω F1206, 3.3 kω J2010, the Zener diode DL 4744 And firm DCCOM, diode LL4148 f is RMI Vishay.
The proposed automated control system preparation and launch of launch vehicles has a number of advantages in comparison with known systems. The introduction of MES PH extends the functionality of automated control systems preparation of LV, so once the work on the preparation of the PH to start (filling with propellant components and temperature control starting position) to operatively control the fact the beginning of the ascent of the rocket from the launch site and synchronize the final phase of the launch.
Additional functions allow you to:
- to interact with the hardware synchronization and single time measuring range and launch complexes;
- be responsible for issuing commands to undermine ProCredit mechanisms allotment communications kit device allocation blocks detachable joints (PP BRS);
- to control the position (PP SRS).
MES PH provides explosion - and fire-circuits the input data in the rational volume defined by the hardware configuration of the control objects.
In MES PH implemented optimal redundancy structure devices (majoritarian structure) and the links between devices in the system to ensure a high probability of failure-free operation and high reliability issue commands to the objects of the Council is to be placed.
Sources of information
1. RF patent № RU 2216760, C2 IPC G05B 17/02, 13.11.2001,
2. RF patent № RU 2450306, C1 IPC G05B 19/00, dated 21.04.2011, (prototype).
3. Digital and analog integrated circuits:
Reference S. Jakubowski, LI, Nisselson, V. Kuleshov, etc. Ed. by S. Jakubowski - M.: Radio and communication, 1990.
4. ProSoft www.prosoft.ru. A brief catalog of products ProSoft 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-electronicsGmbH DC to 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 series D1000 for control systems of technological processes in explosive environment. www.gmintemational.ru.
21. ABB www.abb.com. Product catalog.
22. ARS www.apc.com. Product catalog.
23. Finder wwwfincler.com. Product catalog.
1. Automated control system for the processing and launch boosters (MES PH), containing four workstations operators (ARMO), remote control subsystem hardware and software (PPS APS), five devices, control and communications (MCU), the first MCU with external related systems at the remote command post (BCP), the second MCU with elements and systems boosters, third UUS process of filling the first component of rocket fuel (MCT), the fourth UUS process of filling the second MCT, fifth UUS process temperature (TST) and external ground systems, each with the appropriate MCU software simulators (PI), two communication devices with fiber-optic transmission line information (USUALE), two network switch (FCS), three devices distribution primary power supply (UCAP), the first UCAP equipment of the CPSU, the second UCAP equipment in the initial construction, the third UCAP equipment launch facilities providing power systems and actuators boosters, as well as the power of the Executive elements of the technological equipment of the control object, the remote control of the primary power supply of the CPSU(WUPAP-BCP), the remote control primary power supply starting structures (WUPAP-SS), the two devices distribution secondary power supply (ORWAP) for equipment management and control of the first (1 St) and second (2 St) LV stages, two devices for thermal actuators and systems (USIS), three uninterruptible power supply (mbea) for relevant UCAP, eight devices running actuators (USIA) technological equipment facility management - management subsystems dressing and temperature control, nine blocks determine the functional readiness (BOFG), seven blocks I / o discrete information (BWDI)when this group the input-output optical signals of the first USUALE connected with group input-output optical signals of the second USUALE, the first group of input-output MES PH of inputs and outputs related automated control system of technological processes of ground-based equipment (APCS), the first group entrance MES PH uninterruptible power systems (CGAP), the second group input MES PH from system ground-based measurements (NDA) are connected respectively to the second, fourth and sixth group of the inputs-outputs of the first MCU, the first group whose input is connected to the first output of the first group UCAP, GRU movie the inputs and outputs and the inputs of the first to fifth software simulators PI connected respectively to the tenth group inputs-outputs and the outputs of the respective UUS, the ninth group of input-output of the first MCU is connected to the first group the entrance-exit of the first FCS, the second to the sixth group of the inputs and outputs of which are connected respectively to the first group inputs-outputs of the first-fourth ARMO and PPS APS, the first group inputs of the first-fourth ARMO and PPS APS are connected respectively with the second-fifth and the first duty group outputs the first UCAP, the twenty-eighth group of input-output of the first FCS is connected to the first group input-output first USUALE, the first duty of the DC voltage of the first UCAP connected with the first inputs of WUPAP-PCO and the first USUALE, the second group of input-output UDUPA-BCP is connected to the second group input-output first USUALE, the first group of input-output UDUPA-BCP is connected to a second group of exit and entrance PPS APS, the first input-output of the first mbea connected to the first input-output UDUPA-PCO group inputs and outputs of the first-third of the crimes connected with the first group inputs-outputs corresponding UCAP, the second group of input-output of the first UCAP connected to the second group input-output UDUPA-PCO group the output of the first FCS is connected to the first group input UDUPA-BCP, the sixth group, the output of the first UCAP connected to the first input of the first group SCQ, the third group entrance MES IS N from the external power supply from distribution Board power supply (SRP) is connected with the first group inputs of the first-third UCAP, the first inputs of the second USUALE and UDUPA-SS connected to the first output of the duty of the DC voltage of the second UCAP, the first group of input-output of the second USUALE connected with the twenty-eighth group entrance-exit of the second FCS, the second group of input-output of the second USUALE connected to the third group input-output UDUPA-SS, the first and second group inputs and outputs which are connected respectively with the second group inputs-outputs of the second and third UCAP, the first group input UDUPA-SS is connected to the first output of the second group SCQ, the first and second inputs-outputs UDUPA-SS connected respectively to the first inputs-outputs of the second and third mbea, the first group to the second input of the FCS is connected to the eighth group to output a second UCAP, the first and second group the outputs of which are connected with the first group inputs respectively of the first and second ORWAP, third-seventh group outputs the second UCAP connected to the first group the inputs of the second to fifth UUS, the first inputs of the seventh and eighth USE, the first and second group outputs the third UCAP connected with the first group inputs respectively of the first and second USES, the third output of the third group UCAP connected to the first group the inputs of the first and second USE, the fourth group the output of the third UCAP connection is with the first group the inputs of the third and fourth USE, the fifth group the output of the third UCAP connected to the first inputs of the fifth and sixth USE, the first and second group the inputs and outputs of the second SCQ connected with group inputs and outputs respectively of the first and second ORWAP, third and fourth group the inputs and outputs of the second FCS is connected to the first group inputs-outputs, respectively, the fifth and sixth USE, fifth and sixth group of the inputs and outputs of the second SSC are connected with the first group inputs and outputs respectively of the first and second BOTH, seventh, tenth, thirteenth and sixteenth group of the inputs and outputs of the second FCS is connected to the ninth group inputs-outputs respectively second-fifth UUS, eighth and ninth group inputs and outputs of the second SSC are connected respectively to the first inputs-outputs of the third and fourth BOTH, eleventh and twelfth group inputs and outputs of the second SSC are connected respectively to the first group inputs-outputs of the fifth and sixth BIG, fourteenth and fifteenth group inputs and outputs of the second SSC are connected respectively with the first group inputs-outputs of the seventh and eighth BIG, seventeenth and eighteenth group inputs and outputs of the second SSC are connected respectively to the first group inputs-outputs of the first and second USES, nineteenth to twenty-fifth group inputs and outputs second When It is connected respectively with the first group inputs-outputs of the first-fourth USE, ninth BIG, seventh and eighth USIA, the third output of the first ORWAP connected to the first inputs of the first, third, fifth, seventh and ninth BIG, fourth and fifth outputs of the first ORWAP connected respectively with the first and second inputs of the second BWDI, sixth and seventh outputs of the first ORWAP connected respectively to first and second inputs of the fourth BWDI, eighth and ninth outputs of the first ORWAP connected respectively with the first and second inputs of the sixth BWDI, the first and second outputs of the second ORWAP connected respectively to first and second inputs of the first BWDI, the third output of the second ORWAP connected with the first inputs of the second the fourth, sixth and eighth BIG, fourth and fifth outputs of the second ORWAP connected respectively to first and second inputs of the third BWDI, sixth and seventh outputs of the second ORWAP connected respectively with the first and second inputs of the fifth BWDI, eighth and ninth outputs the second ORWAP connected respectively to first and second inputs of the seventh BWDI, the first subset of the inputs of the fifth group of the input from the first poles of the Executive members of the object management subsystem control elements and systems of the booster is connected to the second input of the first group BOTH, the second-eighth subgroup of the inputs of the fifth group of the input from the first pole ispolnitel the x elements control object, subsystem control elements and systems boosters through the second subgroup, the control subsystem filling the first component of rocket fuel (KRT) via the third and fourth sub-groups, the sub control filling of the second MCT through the fifth and sixth subgroups, engine temperature (TST) through the seventh and eighth sub-groups are connected to pairs, respectively, the second group the inputs of the second-eighth BIG and the second group the inputs of the first-seventh BWDI, the first and second subsets of the inputs of the sixth group of input from discrete sensors and signals dock object management subsystem control elements and systems of the booster is connected to the fourth group inputs respectively the first and second BOTH, the first and second subset of outputs of the first group of the system output at the second pole of the Executive members of the object management subsystem control elements and systems booster connected to pairs of the first group inputs BOTH and the first group outputs USES respectively of the first and second BOFH and the first and second USES, the seventh group input from analog sensor object management subsystem control elements and systems of the booster is connected to the fifth input of the first group BOTH, the first and second subset of outputs of the second is hruppovoho output MES PH on power systems, rocket management subsystem elements and missile systems a carrier connected to pairs, respectively, the second group outputs of the first and second USES and the third group the inputs of the first and second BOTH, the first and second subsets of the inputs of the ninth group of input channels codes systems booster subsystem control elements and systems booster connected respectively with subsets of inputs of the second and fourth group of inputs-outputs of the second UUS, third-sixth subgroups of the outputs of the first group of the system output at the second pole of the Executive members of the object management subsystem controls the filling of the first MCT via the third and fourth sub-groups, the sub control filling of the second MCT through the fifth and sixth subgroups are connected to pairs of the first group inputs BOTH and the first group outputs USE respectively third to sixth BIG and the first-fourth USE, third, and fifth subset of inputs of the sixth group of input from discrete sensors and signal coupling facility control subsystem controls the filling of the first MCT through a third subgroup, the subsystem control filling of the second MCT through fifth subgroup are connected with pairs of the first group inputs BWDI and third group inputs BOTH respectively the second and fourth BWDI and the third and fifth BOTH, fourth, and sixth subgroups of the inputs of the sixth group of input from discrete sensors and signals dock object management subsystem management zapravka is th first MCT through the fourth subgroup, subsystem control filling of the second MCT through sixth sub-group is connected to the third group inputs respectively the fourth and sixth BIG, group outputs of the first-fifth BWDI connected with the second group inputs, respectively, of the second USES, the first-fourth USE, the first group inputs and outputs of the first-third BWDI connected respectively to the third group input-output second UUS, to the first and third group the inputs-outputs of the third UUS, the first group inputs and outputs of the third and fourth BWDI connected respectively with the first and third group inputs-outputs of the fourth UUS, seventh and eighth sub-groups of outputs of the first group of output system to the second pole of the Executive members of the object management subsystem thermostat connected to pairs of the first group inputs BOTH and the first group outputs USE respectively the seventh and eighth BIG and the fifth and sixth USE, seventh subset of the inputs of the sixth group of input from discrete sensors and signals dock object management subsystem thermostat connected to the pair of first group entrance on BWDI and the third group entrance seventh BIG, the eighth subgroup of the inputs of the sixth group of input from discrete sensors and signals dock object management subsystem Ter is astationary connected to the third group of the eighth input BOTH, the third group of input-output system from ground-based automated control system of the rocket (NASA PH) is connected with a pair of third group entrance on BWDI and the fourth group entrance seventh BIG, group outputs of the sixth and seventh BWDI connected to the second group inputs respectively the fifth and sixth USE, the first group inputs and outputs of the sixth and seventh BWDI connected respectively with the first and third group inputs-outputs of the fifth UUS, the first and third group inputs ninth BOTH connected respectively to the first group the outputs of the seventh and eighth USE, characterized in that the MES PH added power distribution equipment system of universal time (SPM), the device processing time information (WAVE), mobile remote customer (TEP), the block I / o analog and discrete data (BWADE), two devices intrinsically safe input analog information (TID), seven devices intrinsically safe input discrete data (TID-D), the device is intrinsically safe input discrete sensors "pin up" (TID-KP), the block processing of discrete signals (BODS), two power device of paraelemental (UPA), the third group the input of the system is additionally connected to the input RP, the output of which is connected to the third group input WAVE, Wasim the th group the output of the first UCAP connected to the first group log FP, group input-output of which is connected to the eleventh group input-output of the first MCU, the first and second subgroups of the outputs on the group display TCH and time intervals VI, VI, the first and second subsets of the inputs of the time interval VI and the start signal of the second group of input-output MES PH from common timing system (CTS) are connected respectively with the first and second group outputs corresponding group of outputs and the first and second group inputs corresponding group of entries WAVE, the second group of input-output WAVE connected to the eighth group input-output of the first MCU, the first group input-output WAVE connected with the third group the entrance-exit of the first USUALE, the sixth group output third UCAP connected with the first group inputs of the first and second UPPA, the first output of the first ORWAP connected to the first input of BWADE, the second output of the first ORWAP connected with the second input BWADE, the power input of the first TID and TID-D, the tenth release of the first ORWAP connected to the first input of BEDS, the eleventh release of the first ORWAP connected to the power input of the sixth and seventh TID-D, the second TID, TID-KP and the second input RODS, the first group input-output of the second MCU is connected to the first group input-output BWADE, the first subgroup of the fifth group of input MES PH to omnitele is connected to the second group input BWADE, group the output of the first TID-connected to the third group input BWADE, whose first group input is connected to group the output of the first TID-D, the first group output BWADE connected to the first input of the first group USES, the fourth group of the input BWADE connected to the output of the second group TID, the first sub-group of the sixth group of the input MES PH is additionally connected to the input of the first group TID-D, the seventh group entrance MES PH from analog sensors the first stage of the launch vehicle is additionally connected to the second input of the first group TID, whose first group input is connected to the eighth group of the entrance MES PH from analog sensors PRS, the second output of the second ORWAP additionally connected to the supply input of the second uiv-D, the first group of the first input BWDI connected to the output of the second group TID-D, whose group input is additionally connected to a second subgroup of the sixth group of the input MES PH, the fourth sub-group of the sixth group of the input MES PH is additionally connected with the group entrance to the third uiv-D group whose output is connected to the first group to the third input of BWDI, the sixth subgroup of the sixth group of the input MES PH is additionally connected with group input fourth TID-D, group whose output is connected to the first group the input of the fifth BWDI, eighth subgroups of the sixth group of the input MES PH is additionally connected with group sign-fifth TID-D, group the output of which is connected to the first group entrance seventh BWDI, the fifth group of input-output fifth UUS connected with group input-output BODS, the fourth group entrance MES PH from node signal forming the lift-off" (KP) is connected with the ninth group entrance ninth BIG and group sign-TID-KP group whose output is connected to the second group input BODS, the first subgroup of the tenth group of input MES PH from the first poles of the solenoid valves of the device of the challenge (EC) is connected to the eighth group of the entrance of the ninth BIG and the fourth group input BODS, the first subset of the third group output MES PH on the second pole of the solenoid valves of the device of the challenge (EC) is additionally connected to the first group to exit the seventh USES, the first subgroup of the eleventh group of the input MES PH from discrete sensors and signals dock right column AS (PC WHEN device drain is connected to the second group by the entrance of the sixth TID-D and the sixth group entrance ninth BIG, the first subgroup of the twelfth group of input MES PH from the first poles of paraelemental PP (PE) is connected to the eighth group input BODS and to the second group to the entrance of the ninth BIG, the first sub-group of the fourth group of output MES PH on the second pole of paraelemental PP (PE) is connected with the group vyhoda the first UPA and eleventh group entrance ninth BIG, the first subgroup of the thirteenth group of the input MES PH from analog sensors EE-1 is connected to the second group to the input of the second uiv-And the second subgroup of the eleventh group of the input MES PH from discrete sensors and signal coupling devices exhaust UO-1 is connected with the first group entry to the sixth TID-D and the seventh group entrance ninth BIG, group sixth output TID-D is connected to the sixth group input BEDS, the fifth group output MES PH signal CP in the NORTH at the start connected with the fifth group output BODS, the second subset of the tenth group of input MES PH from the first poles of the solenoid valves device removal (EC) PP-2 is connected to the tenth group entrance ninth BIG and the seventh group input BEDS, the second subset of the third group of output MES PH on the second pole of the solenoid valves of the left column WHEN (LK AS for device removal (EC) PP-2 is additionally connected with the group out of the eighth USIA, the third subgroup of the eleventh group of the input MES PH from discrete sensors and signal coupling devices exhaust LK WHEN connected to the second group to the entrance of the seventh TID-D and the fourth group to the entrance of the ninth BIG, the second subgroup of the twelfth group of input MES PH from the first pole paraelemental PP (PE) is connected with the fifth group input BODS and twelfth GRU is Polym entrance ninth BIG, the second sub-group of the fourth group of output MES PH on the second pole of paraelemental (PE) PP-2 is connected to the output of the second group of UPA and thirteenth group entrance ninth BIG, the second subgroup of the thirteenth group of the input MES PH from analog sensors EE-2 is connected to the first input of the second group TID, the fourth subgroup of the eleventh group of the input MES PH from discrete sensors and signals dock PP-2 is connected to the first group to the entrance of the seventh TID-D and the fifth group to the entrance of the ninth BIG, group seventh output TID-D is connected with the third group input BEDS, the first, second, third and fourth group outputs RODS connected respectively to the first group the inputs of the first and second USE, the first and the second UPA, the second group of input-output BUDS connected with group inputs-outputs of the first and second UPPA, the second input of the third BWDI additionally connected to the power input of the third uiv-d, the second input of the fifth BWDI additionally connected to the power input of the fourth TID-D, the second input of the seventh BWDI additionally connected to the power input of the fifth TID-D, the sixth group of input-output of the second MCU is connected to the first group input BODS.
2. Automated control system preparation and launch-vehicle according to claim 1, characterized in that the device processing time is i.i.d. intervals (WAVE) contains patch panel, two power distribution unit (PDU), three conversion unit time intervals (BPVI), the Central processor of the data processing (PCOD), mnogonatsionalny power supply (energy policy College), machine input (ATS), the first and second subsets of the inputs of the third group of input are connected respectively with group inputs of the first and second PDUs, the first outputs are connected respectively to the first and second group inputs ABP, group output of which is connected with group input energy policy College, group output energy policy College connected to group input PCOD, the first, second and third inputs and outputs which are connected respectively with the first inputs-outputs of the first, second and third BPVI, second inputs and outputs which are respectively connected to the fifth, fourth and third group inputs-outputs a patch panel, the first inputs of the first, second and third BPVI connected respectively with the third, fourth and second outputs of the first PDU, the second inputs of the first, second and third BPVI connected respectively to the second, fourth and third outputs of the second PDU, the first and second group outputs the patch panel are connected respectively with the first and second group outputs WAVE, the first and second group inputs the patch panel are connected respectively to the first and the second grupowy the inputs of WAVE, the first and second group the inputs-outputs of the patch panel are connected respectively with the first and second group inputs-outputs WAVE.
3. Automated control system preparation and launch-vehicle according to claim 1, characterized in that the mobile remote customer (FP) contains the control panel power supply (GSPE), two AC/DC (HAD), control panel, two modules I / o discrete information (MWDI), two panel computer, the node backplane, the first and the second sub-group group input FP are connected respectively with the first and second group inputs GSPE, the first and second outputs which are connected to the inputs respectively of the first and second surfactants, the outputs of which are connected respectively with the first and second inputs of the node backplane whose output is connected to the first input of the control panel, the first output and second input of the control panel are connected respectively to the first input and the first output of the first MWDI, input-output of which is connected to the first input-output of the first panel of the computer, the second output and the third input of the control panel are connected respectively to the first input and the first output of the second MWDI, input-output of which is connected to the first input-output of the second panel computer, the third output control panel is connected to third inputs of the first and the showing of MWDI and the first inputs of the first and second panel computers the second and third inputs and outputs of the first panel of the computer is connected to the first and second inputs-outputs of the first sub-group group input-output FP, second and third inputs and outputs of the second panel computer is connected to the first and second entrance-exit of the second sub-group group input-output fire protection.
4. Automated control system preparation and launch-vehicle according to claim 1, characterized in that the device is intrinsically safe input discrete sensors "pin up" (TID-KP) contains m nodes intrinsically safe input, each of which consists of a DC/DC Converter (D), intrinsic safety barrier (B), item galvanic isolation power supply (EGREP), the output node of the unit potential (WU "1"), the output node of ground potential (WU "0"), power input D all m nodes are connected with a power inlet TID-KP, the inputs i-th subgroup group sign-TID-KP is connected to the input BI of a node i, the output D node connected to the first input of EGREP, the output B is connected to the second input of EGREP, the first output EGREP connected to the input VU "1", the second output EGREP connected to the input of WU "0", the first outputs WU "1", the first outputs WU "0", and the combination of the second outputs WU "1" and " WU "0" in the nodes from 1 to m are connected with the corresponding subgroups of outputs from 1-1 to 1-m in group output TID-KP.
5. Automated control system of preparation and uscom PH according to claim 1, characterized in that the processing unit discrete information (BODS) contains two switch network (COP), three peripheral processor (PDP), three blocks normalization discrete sensors (BNDD), three signal control BFSU), three mnogonazionaljnyh power supply peripheral (energy policy College-P), the control unit control circuits (BCCU), patch panel input signals (cpws), two units of analysis temporal information (BAVI), site of the majority of elements (UME), three multi-wire bus line (M), the first input is connected to RODS the first inputs of three energy policy College-P, three BNDD, three BFSU, the outputs of the first-third the energy policy College-N are connected respectively to the tires of the first-third of the highways M1÷M3 in terms of nominal power, each of the tires of the first-third of roads are connected respectively with group inputs-outputs of the first-third BNDD, BFSU, PDP and with the first-third group inputs-outputs of the two BAVI, the inputs and outputs of the first-third PDP connected respectively to the first to third inputs-outputs of the first and second CS, fourth inputs and outputs which are connected respectively with tires subgroups of the first group of input-output BODS, the second input RODS connected to the second inputs of the first-third BNDD, group the inputs of the first-third BNDD connected respectively with the first third group outputs the PVA, group outputs of the first-third BFSU connected respectively to the first to third group inputs UME, the second group of input-output BCCU connected with the first line, the tenth group entrance CPUs connected to the sixth group output UME and to the first sub-group input group input BCCU, eleventh group entrance CPUs connected with the seventh group output UME and the second sub-group input group input BCCU, the second group output UME is connected to the fourth group output BODS, the third group output UME is connected with the third group output BODS, the first group output UME is connected to the fifth group output BODS, the fourth group output UME is connected to a second group output BODS, the fifth group output UME is connected to the first group output BODS, the first subset of the inputs of the second group of input-output RODS connected with the first group entrance CPUs, the second group of inputs of the second group of input-output RODS connected to the second group input CPUs, the third group entrance CPUs connected to the eighth group input BEDS, the fourth group entrance CPUs connected to the seventh group input BEDS, the fifth group entrance CPUs connected with the sixth group input BODS, the sixth group entrance CPUs connected to the fifth group input BODS, the seventh group entrance CPUs connected with evertym group input BEDS, the eighth group entrance CPUs connected to the third group input BEDS, ninth group entrance CPUs is connected to a second group input BODS, the first group of the input RODS connected to the first inputs of the first and second BAVI, the outputs of which are respectively connected to the tires of the first and second subgroups of the outputs of the second group of input-output BODS.
6. Automated control system preparation and launch-vehicle according to claim 1, characterized in that the device power paraelemental (UPPA) contains eight modules rectifier (MB), grouped in pairs in four power supply (INRM), eight electronic keys (RWE), the tires of the first subgroup of the first input UPPE connected with the first inputs of the first, third, fifth and seventh MB, tyres second subgroup of the first input UPPE connected to the first inputs of the second, fourth, sixth and eighth MB, subgroup inputs of the first group of input-output connected to second inputs of the first-eighth MB first group outputs of the first-eighth MB connected to the corresponding tire subgroup outputs of the first group of input-output UPPA, the first bus of the second group of input UPPE connected with the first inputs of the first, third, fifth and seventh RWE, the second bus of the second group of input UPPE connected to the first inputs of the second, fourth, sixth and eighth RWE, the third W is on the second group of input UPPE connected with integration of third inputs of the first and second MB and the fifth bus bar of the first subset of outputs of the first group of output OPPA, the fourth bus of the second group of input UPPE connected to the Association of third inputs of the third and fourth MB and the sixth bus first subset of outputs of the first group of output UPPA, the fifth bus of the second group of input UPPE connected with integration of third inputs of the fifth and sixth MB and with the seventh bus first subset of outputs of the first group of output OPPA, sixth bus of the second group of input UPPE connected to the Association of third inputs of the seventh and eighth MB and eighth bus first subset of outputs of the first group of output UPPA, the first bus of the first subset of outputs of the first group of output UPPE connected to the output of the second RWE, the second bus, the first subgroup outputs of the first group of output UPPE connected to the output of the fourth RWE, the third bus of the first subset of outputs of the first group of output UPPE connected to the output of the sixth RWE, the fourth bus of the first subset of outputs of the first group of output UPPE connected to the output of the eighth RWE, the first bus of the second subset of outputs of the first group of output UPPE connected to the output of the first RWE, the second bus of the second subset of outputs of the first group of output UPPE connected to the output of the third RWE, the third bus of the second subset of outputs of the first group of output UPPE connected to the output of the fifth RWE, the fourth bus of the second subset of outputs Pervov the group of output UPPE connected to the output of the seventh RWE, the first outputs of the first and second MB connected with the second inputs of the first and second RWE, the first outputs of the third and fourth MB are connected to each other and to the second inputs of the third and fourth RWE, the first outputs of the fifth and sixth MB connected with the second inputs of the fifth and sixth RWE, the first outputs of the seventh and eighth MB are connected to each other and to the second inputs of the seventh and eighth RWE.
7. Automated control system preparation and launch-vehicle according to claim 1, characterized in that the conversion unit time intervals (BPVI) contains two AC/DC (AD), mnogonatsionalny power supply peripheral (energy policy College-P), the control circuit voltage (SKN), OCXO (TSG), digital to analog voltage Converter (DAC), the microprocessor (MCP), the adapter code RS-485 (Ad 485), the adapter code RS-232 (Ad 232), the display element (EI), the switch code (CC), the first and the second group inputs BPVI connected with the first group inputs respectively of the first and second AD, the outputs of which are connected to each other and to the first inputs of energy policy College and SKN, the first output energy policy College connected with the first inputs of the ITUC, Hell, 485, 232 Hell, EI, QC, DACS, the second output energy policy College connected to the first input TSG and the second input of the DAC, the output SKN is connected to a second input of the MCP, the first TSG connected to the fourth input of the MCP, the output of the DAC is Yong with a second input TSG, the second output TSG connected to the third input of the DAC, the first output of the MCP is connected to a second input of EI, the second output of the MCP is connected to the second input QC, the first and second inputs and outputs MCP is connected with the first inputs-outputs, respectively Hell 485 and 232 Hell, the second input-output Ad 485 connected to the first input-output QC of the second input-output Ad 232 connected to the first input-output BPVI, the first bus input group input-output BPVI connected to the third input of the MCP, the second bus input group input-output BPVI connected with the third entrance QC, the first and second outputs QC connected respectively to the first and second bus output group input / output BPVI, second and third inputs and outputs QC are connected respectively with the first and second tire of the input / output group input / output BPVI.
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