항공우주시스템공학회지 (Journal of Aerospace System Engineering)
- 제2권1호
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- Pages.1-6
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- 2008
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- 1976-6300(pISSN)
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- 2508-7150(eISSN)
6자유도를 고려한 회전익 항공기 착륙장치의 동특성 해석
Dynamic Characteristics Analysis of Landing Gear that Consider 6-Degree of Freedom of Helicopter
초록
In this paper, full body modeling and analysis of nose and main landing gear's characteristics of a helicopter are performed using the dynamics analysis program ADAMS. Also, when land limiting about helicopter body's degree-of-freedom, compared the characteristics. In the case of helicopter, because there are a lot of dangerous missions under flight condition that is disadvantageous than fixed wing airplane, need more detailed research for a helicopter.