The present invention relates to an attitude control device by preventing a wing folding phenomenon of a plane-shaped drone and, more specifically, relates to a device which comprises a light source, a double arrangement optical cable to control bending in one direction, an optical detection unit, and a wing control drive device, wherein the wing folding phenomenon uses bending optical loss characteristics of an optical fiber.
본 발명품은 비행기 형태 드론의 날개 꺾임 현상을 예방하여 자세를 제어하는 장치에 관한 것으로서, 날개 꺾임 현상은 광섬유의 구부림 광손실 특성을 이용하는 장치이며, 장치는 광원, 한 방향 굽힘을 제어하는 2중 배치의 광케이블, 광검출부 및 날개 제어 구동 장치로 구성되어 있는 장치에 관한 것이다.
An Attitude Control Device of Drone using Bending Loss of Fiber
광섬유 구부림 손실을 이용한 드론의 자세 제어 장치
31.01.2019
Patent
Elektronische Ressource
Koreanisch
IPC: | B64C AEROPLANES , Flugzeuge / G01J Messen der Intensität, der Geschwindigkeit, der spektralen Zusammensetzung, der Polarisation, der Phase oder der Pulscharakteristik von infrarotem, sichtbarem oder ultraviolettem Licht , MEASUREMENT OF INTENSITY, VELOCITY, SPECTRAL CONTENT, POLARISATION, PHASE OR PULSE CHARACTERISTICS OF INFRA-RED, VISIBLE OR ULTRA-VIOLET LIGHT / G02B Optische Elemente, Systeme oder Geräte , OPTICAL ELEMENTS, SYSTEMS, OR APPARATUS |
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