메뉴 건너뛰기
소속 기관 / 학교 인증
인증하면 논문, 학술자료 등을  무료로 열람할 수 있어요.
한국대학교, 누리자동차, 시립도서관 등 나의 기관을 확인해보세요
(국내 대학 90% 이상 구독 중)
고객센터 ENG
주제분류

논문 기본 정보

저자정보
(금오공과대학교) (금오공과대학교)
저널정보
제어로봇시스템학회 제어로봇시스템학회 논문지 제어로봇시스템학회 논문지 제25권 제6호
오류 신고하기

피인용 0

검색

    초록·키워드

    One of the major disadvantages of the unmanned aircraft such as a drone is that it has finite capacity of the battery and it is almost impossible to change the battery during the flight. In order to overcome the drawback, this research proposes a novel airdrop operation with dual unmanned aircraft. The suggested dual unmanned aircraft is composed of a carrier octo-copter and a mission quad-copter. The carrier octo-copter with large payload carries the mission quad-copter and flies with its energy source. After fully consuming the energy, the carrier octo-copter drops the mission quad-copter in the air. Then, the mission quad-copter starts to operate its designated mission with its own energy source. To enable the airdrop operation, a foldable structure of the mission quad-copter was developed. Intensive experiments to verify this airdrop flight mechanism were carried out with autonomous flight-back to the destination. The position and altitude data during experiments were acquired using the GPS and barometer in the quad-copter flight control unit. Synthesizing the information from the experiments, it is confirmed that the suggested idea can be a promising alternative to enlarge the flight distance and duration of the unmanned aircraft.

    최근 본 자료 전체보기

      UCI(KEPA) : I410-ECN-0101-2019-003-000760445