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FRPC RDC

Ramenskoye Design Company
The conducting Russian developer of the integrated complexes, systems and devices of the onboard radio-electronic equipment

Integrated Navigating Systems: IIB, BINS-1, ISS-1, SBKV-95, SBKV-2B, SBKV-85, IG

Integrated inertial navigation system
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Photo Description
The integrated navigating systems are intended for the various purposes including for measurement of making vectors of linear acceleration, maintenance of definition and delivery of pilotazhno-navigating parameters and intended for complexes of prompting, management of rockets of various classes, etc.

The list of made navigating systems


IIB Inertial measuring unit

The IIB inertial measuring unit is designed for measurement of liner acceleration vector and angular rates components in coordinates system connected with the product.
It is used for control systems of maneuvering flight vehicles, in integrated navigation systems and complexes of aircraft and helicopters, naval and surface transport facilities.

BINS-1 Strapdown inertial navigation system

The system provides the determination and output of flight/navigation parameters and it is designed for guidance and control systems of drones.

ISS-1 Inertial - sattelite system

The system is developed on base of inertial gyro platform and service electronics.

INS-2000 Inertial navigation system

The system provides definition and delivery of pilotazhno-navigating parameters and is intended for new and modernized helicopters and planes.

NS BKV-95 Navigation attitude and heading referense system

It is designed for civil aircraft and helicopters.

IGS-90 Inertial geodesyc system

The system is designed for the determination of location during the solution of task of engineering geodesy and geophysics as well as it can be used as a survey controller for determination of geodetic parameters of mobile launchers.

SBKV-2V Strapdown attitude and heading referense system

It is designed for the application either as main or as stand-by sensor for modern and updating military aircraft and helicopters.

SBKV-85 Strapdown attitude and heading referense system

The system provides the determination and output of flight parameters and it is designed for modern and updating civil aircraft.

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Integrated inertial navigation system
IIB, BINS-1, ISS-1, SBKV-95, SBKV-2B, SBKV-85, IG
Information display tools
IKSH-1М, MFI-10-5, MFI-10-6, Multifunction control panels
Gyros
TVG-3-1, GVK-16, GVK-17, MG-4, GVK-6-1, GVK-10, GVK-18
Accelerometers
ATs-1, A-15, A-16, A-17, AES-1
Ground unified complex of flieght missions planning
Ground unified complex of flieght missions planning and afterflight analyses
Magnetic heading measurement channels
KIMK-1, KMK-1, DFDM-3, PSM-2
Magnetometers
МА-2, МА-3, МА-4М, МА-5
Calibration tools
LBU-K, NPS-2M
Equipment for low-temperature diffusion welding
SDVU-100 (SDVU-50), low-temperature diffusion welding
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El: 77-6097 from 14 February 2002. Publishes since February, 3, 1997.