과제정보
본 논문은 한국항공우주연구원(과제명: 차동 브레이크 고정익 무인기의 지상활주 및 자동이착륙 기술 개발)의 연구비 지원(과제번호: 20CAUV-B155368-02)을 받아 진행된 연구임.
참고문헌
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