한국항공우주연구원

Flight Control Valve

Technique for controlling a flow of desired fluid and its amount

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Multistage Control Method of Flow Control Valve using DC Motor

Technique for controlling a flow rate by setting individual limit values to the stages of DC motor that rotates at an intended

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Apparatus and Method for Playing Video in Real Time

3D video of aircraft using aircraft information transmitted via communication link in flight tests of unmanned aerial vehicle

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High Performance Tilt Rotor Aircraft in which a Nacelle Tilt Angle and a Flaperon Angle Mechanically Interwork with Each Other

A nacelle and a flaperon mechanically and systematically connected by a power transmission mechanism such as a linkage system in a tilt rotor

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Restricted Zone Intrusion System for UAV

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Composite Material Z-Pinning

Inserting pins in a thickness direction of a composite material laminated structure to prevent separation and to strengthen connection

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Power Supply System having an Emergency Power Supply Cutoff Function

Technology to cut off the power supply using the uninterruptible power supply device even in the case of emergency

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Three Dimensional Rigid Ball Driving System

New concept of next generation actuator that can control the orientation in a three-axis direction with a single actuator

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Localization Method of Multiple Jammers

A device and method capable of localizing multiple jammers using a time difference of signal arrival (TDOA)

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Determining Driving Lane

Navigation device and road lane recognition method using steering wheel model

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Determining Road Lane

Autonomous vehicle assistance device that uses carrier-based differential GPS information from road lane recognition, electronic map, and steering model

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