Acknowledgement
본 연구는 국방과학연구소의 지원으로 차세대 고속 복합형 무인 회전익기 특화연구실에서 수행되었습니다. 본 논문의 일부는 한국항공우주학회 2021년도 춘계학술대회에서 발표되었습니다.
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