한국소음진동공학회:학술대회논문집 (Proceedings of the Korean Society for Noise and Vibration Engineering Conference)
- 한국소음진동공학회 2009년도 춘계학술대회 논문집
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- Pages.593-598
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- 2009
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- 1598-2548(pISSN)
스마트 무인기 4자유도 지상시험치구 구조진동해석
Structural Vibration Analysis of Smart UAV 4-Degree of Freedom Ground Test System
초록
In this study we present results for the design of ground test system for 4 degree of freedom(DOF) control test is one of the smart UAV ground test. This system is equipped with real smart UAV and Z direction DOF and 3 direction rotation DOF, Ensuring safe operation of the Smart UAV is a top priority. To this end, it is required to do structure analysis and test verification to confirm the design margin and safety. Based on the analysis, the ground test system has been redesigned to meet the structural conditions.
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