Product name

FQMS(Fuel Quantity Measurement System)(KUH)

Model name

KUH, LCH, LAH, Next corps unmanned system

Description

- Fuel quantity measurement of fuel tank and remaining travel distance display
- NVIS, Dimming and fuel shortage alarm

Product name

ISI(Integrated Standby Instrument) (KUH)

Model name

KUH

Description

- Position information, Air-Data
- Display output equipment
- Display of flying information on flight position, altitude, speed, etc.

Product name

ISPU (Integrated Signal Processing Unit(KUH)

Model name

KUH

Description

Transmission of high-speed signal processed engine torque value of Gear Box to FADEC and DAU

Product name

Chip Processing Unit (CPU)(LAH)

Model name

Chip Processing Unit (LAH)

Description

- Detection and removal of chip that occurs in aircraft mission
- Process of Chip signals including FDR, HUMS, and DAU

Product name

LGCU (Landing Gear Control Unit) (KT-1)

Model name

KT-1

Description

- Installation in KT-1 aircrafts
- Lock & unlock command control for landing gear

Product name

Anti-ice control unit (LCH, LAH )

Model name

LCH, LAH

Description

Independent aircraft unit designed to control temperature of aircraft installation parts (windshield, engine air inlet)

Product name

FCC/FCS (unmanned system)

Model name

unmanned system

Description

- Flight control computer & system
- Position control and flight control operation controller
- Navigation Computer
- INU integrated system

Product name

ISI localization first in Korea

Model name

KF-X

Description

- FLCCETS is the equipment of providing functional and other kinds of test settings in the way of controlling and measuring analog and discrete in & out signals of FLCC UUT in real time. It offers a test setting in interaction with driver simulator, simulation computer, and Real-Actuator.
- RIUETS is the equipment of providing functional and other kinds of test settings for RIU (Remote Interface Unit). As a functional test, it simulates input & output signals and many different error situations for the development and diagnosis of RIU

Product name

AC/DC EMB (KUH)

Model name

KUH

Description

- Power distribution box
- Power supply to the internal system of aircraft, monitoring, and overload block
- Redundancy application for emergency

Product name

EMB 1/2 (LAH)

Model name

LAH

Description

- Power distribution control unit
- Power distributor for Surion using AC generator and other DC generator systems

Product name

EMU (KF-X)

Model name

KF-X

Description

- Power distribution and power monitoring for electric system of aircraft
- Built-in auto protection against electrical short
- Operation of degrade mode for blocking power and automatically creating electrical detour in case of input power (generator) abnormality
- Collection of power information on input & output of electric system transmission to MFD; record of the information more than 2 hours
- Built-in BIT for self-diagnosis of failure

Product name

ESU (APU Engine controller) (KUH)

Model name

KUH

Description

- Fuel quantity control for engine speed control
- Engine status monitoring and status display

Product name

PMU(power monitoring unit)(next corps unmanned system)

Model name

Next corps unmanned system

Description

- This equipment receives power from power generator & ground power unit (GPU) and next corps unmanned system, and battery, and then distributes the power to built-in aircraft devices.
- Equipment for monitoring power status

Product name

MEMS Inertial Navigation System (INS)

Model name

INS

Description

- HRG (Hemispheric Resonator Gyro) based
- Ultra-precision inertial navigation system
- Sensor raw data filtering technology
- Location & position estimation algorithm technology
- Integrated algorithm design technology
- Safe vessel sailing, planning, monitoring

Product name

Position and Azimuth angle measurement system (AHRS, Altitude & Heading Reference System)

Description

- Position & heading information output sensor
- Calculation of aircraft position with the use of MEMS IMU (Inertial Measurement Unit)
- Application of sensor error calibration algorithm to Roll, Pitch, and Yaw

Product name

Position and Azimuth angle measurement system (GPS/AHRS)

Description

- Complete GPS-Aided AHRS Solution
- Accuracy(deg) : < 1deg(Heading), < 0.2(Att)
- Interaction with ADC(Air Data Computer)

Product name

UAV cable & wiring

Description

- Optimal design for VTOL and smart unmanned system
- Compliance with MIL-W-5088 and use of CATIA V5 E3D