영풍전자주식회사

FOR AIR

INU (Inertial Navigation Unit) URANUS-I

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INU (Inertial Navigation Unit) URANUS-I

Completed developing an integrated navigation system for UAM and small unmanned aerial vehicles, which provides precise guidance and control performance.

APPLICATION

Night Intruder-600 Vertical Take off & Landing Small Certified UAV KC-100

Overview

Inertial Navigation Unit

Provide essential flight data, including azimuth, speed, and position, necessary for automated flight and aircraft control to the flight control computer(FLCC) or users, utilizing data from an internal 3-axis MEMS IMU, GNSS receiver, and pneumatic sensors.
Ensure the reliability of navigation data with Built-In-Tests(BITs) for each situation, including IPBIT, CBIT, and IBIT.

FEATURES

Suitable for manned or unmanned aircraft with compatible sensors that meet the system requirements.

High Accuracy
Provide precise flight data 01
Integrated
Navigation System
Equipped with satellite and inertial navigation solution 02
High Reliability
Improve data reliability through BIT 03
High Accurate Heading
Provide high accurate heading data using GNSS dual antenna solution 04

Configuration

ROBUST ∙ RELIABLE ∙ OPTIMIZED

Integration between satellite and inertial navigation
and technology of Dual Heading and Dead Reckoning
offer a precise navigation solution.

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For more information, please download the product brochure.

BROCHURE

NAVIGATION

INU (Inertial Navigation Unit) URANUS-I

APPLICATION

Inertial Navigation Unit

FEATURES

ROBUST ∙ RELIABLE ∙ OPTIMIZED

DOWNLOAD