지원사업
학술연구/단체지원/교육 등 연구자 활동을 지속하도록 DBpia가 지원하고 있어요.
커뮤니티
연구자들이 자신의 연구와 전문성을 널리 알리고, 새로운 협력의 기회를 만들 수 있는 네트워킹 공간이에요.
논문 기본 정보
- 자료유형
- 학술대회자료
- 저자정보
- 발행연도
- 2011.10
- 수록면
- 1,083 - 1,086 (4page)
이용수
초록· 키워드
오류제보하기
The final goal of this study is to develop a small and low altitude solar powered UAV. In the first step, the main design parameters were considered and the dynamic modeling was carried out. For the small size and low altitude operation, the design parameters were derived from the literature study. The fundamental aerodynamics of the selected airfoil was investigated. The energy consumption for mission profile and level flight are estimated according to the various altitudes. The flight motion equation by Lagrange-Euler was derived.
목차
Abstract
1. INTRODUCTION
2. OPERATION CONCEPT & DESIGN CONSIDERATION
3. ESTIMATION OF ENERGYCONSUMPTION
4. FLIGHT MOTION EQUATION
5. CONCLUSION
ACKNOWLEDGEMENT
REFERENCES
참고문헌 (0)
참고문헌 신청이 논문의 저자 정보
최근 본 자료
댓글(0)
0
UCI(KEPA) : I410-ECN-0101-2014-569-000914197