Series 2 PR-200 Mode Penal
The 2 PR-200 is intended for remote control of operation modes of the Series 2 SAU-10-02 automatic control system, mode activation signaling of the Series 2 SAU-10-02 automatic control system, and control of the display system in various modes of flight. The PR-200 panel is mounted in the pilot's cabin in the right board in a place convenient for the pilot.

PS-188-01 Selector panel
The PS-188-01 Selector panel is intended for inputting initial data in the Series 2 SAU-10-01 and the series 2 SVS-2C-2 for implementing control algorithms. The panel is mounted in the pilot's cabin in the right instrument board.

Series 2 PK-33
The Series 2 PK-33 monitoring panel is intended for carrieng out operational-kind preparation works of the PNK - 10PU - 02 altitude and heading reference complex. The monitoring panel is mounted in the aft - of - cockpit compartment of the airplane in a place convenient for the pilot.

KBI-140-01Data multiplexing unit
The KBI-140-01is part of the PNK-10PU-02 and intended for generating on-time commands for airplane's signaling system, and multiplexing signals on indication instruments in various control modes. The unit is mounted on its place using the St-10-02 shock-proof rack. In the KBI-140-01unit the following operations are carried out: generation of integrated limiting values of the angle of attack, vertical acceleration, and multiplexing data in various flight modes.

KBP-87-02 power supply circuits switching unit
The KBP-87-02 power supply circuits switching unit is intended for remote control of power supply of the PNK-10PU-02 altitude and heading reference complex, conversion of 3-phase 115V/400Hz into 3-phase 36V, and implementing power supply testing.
emote control of switching elements is carried out using on/off lines common for the entire PNK-10PU-02, as well as using individual lines for each system.

BKTS TV signals multiplexing unit
The BKTS is part of the SUV-P and intended for receiving TV signals, converting, multiplexing, and outputting those signals to the MFI. BKTS is a combination unit providing multiplexing output TV signals to channels desired, converting those signals into a numerical code, processing of video images in a digital format, and outputting to the MFI indicator device via a digital communication line. Besides, the units provide a required number of on-board interface channels. The modules are housed in a separate monoblock providing the conversion of supply network voltages, and interconnected by a common system bus. For providing outputting TV information from 14 TV analog transducers to 6 digital TV displays, a switching circuit is implemented in the BKTS, which ensures any TV transducer being connected with any number of TV displays. To provide compatibility of TV analog transducers with digital TV displays, four TV DAC channels are provided in the BKTS (two BKTS outputs backup two of the four TV DAC channels).

The following operation modes are available in the BKTS:
Test;
Scanning;
Magnification;
Correction.

KSOP-2 software debugging set
The KSOP-2 is intended for use on programmer's work stations.

MCP-4-42 CPU unit
The MCP-4-42 CPU unit is untended for fulfillment of mathematical and logical processing within various modification BCVM-486s. The unit is assembled using a 12-layer through-hole-plating PCB. The PCB has 8 layers with signal conductors, a power layer, and 3layers of circuit ground. The power layer and ground layers are wired in the form of a grid. The MCP-4-42 CPU is powered with DC voltage. Status ready time is no more 2sec (including computer and software initialization and testing).

PS-188-01 Selector panel
The PS-188-01 Selector panel is intended for inputting initial data in the Series 2 SAU-10-01 and the series 2 SVS-2C-2 for implementing control algorithms. The panel is mounted in the pilot's cabin in the right instrument board.

BCVM-486-6 on-board digital computer
The BCVM-486-6 is part of the SUV-VE system installed on the Su-30MKK aircraft. The BCVM is a combination of units ensuring the computing performance required. The units are housed in a separate monoblock providing conversion of supply network voltages, and interconnected by a common system bus. The availability of one of the two supply voltages (DC or AC) provides functioning of the BCVM. To prevent a supply failure separate terminals are provided which ensure connection with independent power supply with a diode isolation. The BCVM-486-6 is intended to operate as part of on-board avionics and for solution of applied tasks in a real time mode.

BPKTS-01 TV signals conversion and multiplex unit
The BPKTS-01intended for receiving TV signals from BREO transducers of object 30MKI, and for conversion, multiplex, and outputting those signals to display processors, an aviation head up display set (KAI), and logging means. The BPKTS-01is intended to work as part of the electro-optical navigation complex of object 30 MKI. The unit comprises standard on-board and software set, and transmits and receives code and TV signals. The BCVM-486-1 is a on-board digital computer containing REPROM memory, and intended to work as part of the OEPrNK product (the electro-optical navigation-attack complex of the Su-30MKI aircraft).

Baguette-53-15
Baguette is a new generation of on-board computers based on a super-fast processor. In the Baguette-53-15 an idea is implemented of developing a versatile computing complex which after being modernized and software changed can be used both on aircraft, automotive, railway, and sea transportation. The Baguette-53-15 modifications are used as part of the PNK-37DM altitude and heading reference complex of the Ka-31RLD airborne early radar warning helicopter.

TV signal transformation unit BPTS-1
The TV signal transformation unit BPTS-1 is intended for image generation on on-board displays of the Mi-24VM helicopter.

US-43 interface
The US-43 interface is part of on-board equipment of the Mi-24VM upgraded battlefield helicopter. The interface is intended for conversion of analog and digital data generated by sensors, and transmitting those data to on-board equipment of the helicopter.

EDSU-200 fly-by-wire control system
The EDSU-200 fly-by-wire control system is a digital-analog remote control system for the BE-200 amphibian airplane. Two operational modes are available: basic digital and standby analog(at a failure of the basic digital part). In the standby mode the EDSU-200 provides acceptable level of controllability and stability characteristics at a manual control and manual trimming in the longitudinal channel. Power to the EDSU-200 is supplied by two independent 27V DC power units which work in buffer with electrical storage batteries, and two independent 3-phase supply unit 115/200V 400Hz. The hydraulic system is fed by three independent hydraulics. The system meets the demands of ENLGC-3 and AP-25.

UM-1 power amplifier
The UM-1 microassembly (power amplifier) is used on the USK-10V, US-43 products etc.

PZA-2 digital-to-analog converter
The PZA-2 digital-to-analog converter is used on the USK-10V, US-43 products etc.

"Narcissus-M" unified display system
The "Narcissus-M" unified display system is intended for display of the information provided by on-board systems, complexes, sensors. The information is displayed on two displays - ILS-31 (on the windscreen) and IPV-1(direct vision) which are installed in the pilot's cabin. The remaining units are mounted on the RM-10 mounting frame in the instrument section. Both displays are monochrome type with green illumination. On the displays letters, numbers, and graphics can be displayed. The "Narcissus-M" display system is used on the Su-27 aircraft.

DS-83 "Gorizont" gimballess electronic compass
The DS-83 "Gorizont" is a gimballess electronic compass with automatic system of magnetic deviation compensation. The DS-83 "Gorizont" consists of the control & indication block and the sensor block.

The DS-83 compass provides
- automated magnetic deviation write off (calibration ) within one full circulation cycle;
- storage of declination parameters and calibration coefficients in non-volatile memory;
- direct connection with an external navigation system via a serial interface according with the NMEA-0183International Standard;
- calculation of the magnetic course in the range of 800 north latitude to 800 south latitude;

The DS-83 compass calculates the following values:
Magnetic course
True course
Deviation from the fixed course
Angle of heel
Angle of trim