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
- 112 - 116 (5page)
이용수
초록· 키워드
오류제보하기
The effect of damage on the flight dynamic characteristics was studied. Partial right wing loss was considered for aircraft’s damage. To construct a 6-DOF model for the damaged asymmetric aircraft, a wing body UAV was designed and wind tunnel test for each damaged configuration was performed to identify the aerodynamic coefficient change. The mass, C.G. and MOI were also measured for each damaged configuration. The movement of longitudinal/lateral-directional flight mode poles was examined to evaluate the change of the flight dynamic characteristics. The result of this study shall be applied to the research on the controller design which can overcome the aerodynamic change from damage.
목차
Abstract
1. INTRODUCTION
2. 6-DOF MODELLING OF DAMAGED A/C
3. DAMAGE EFFECTS ANALYSIS
4. CONCLUSION
REFERENCES
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UCI(KEPA) : I410-ECN-0101-2014-569-000912173