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
2019-01-31
Patent
Electronic Resource
Korean
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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