Acknowledgement
본 연구는 2020년도 정부(교육부)의 재원으로 한국연구재단의 기초연구사업의 지원을 받아 수행되었습니다(2020R1I1A3071793). 본 논문은 2021년도 정부(과학기술정보통신부)의 재원으로 한국연구재단의 지원을 받아 수행된 연구입니다(2021R1A5A1031868). 이 연구는 국방기술진흥연구소 핵심기술 연구개발과제 "중형헬기 진동저감을 위한 진동원(블레이드) 능동제어장치 SW 개발"(과제번호: 20-108-E00-018)의 지원으로 수행되었습니다.
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