Proceedings of the Korean Society for Noise and Vibration Engineering Conference (한국소음진동공학회:학술대회논문집)
- 2004.05a
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- Pages.452-456
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- 2004
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- 1598-2548(pISSN)
Gust Response Analysis and Alleviation Method for Aircraft Wing
항공기 날개 돌풍 응답해석 및 완화기법
Abstract
A study on gust loads alleviation using aircraft control surface was performed. Aeroservoelastic model including control surface controller was formulated and validated by comparing the results of continuous turbulence response analysis with those of MSC/NASTRAN. Optimal control with output feedback was adopted for designing the control surface controller, and the effects of gust loads alleviation was validated by performing the numerical simulation for the controller designed.
Keywords