Proceedings of the Korean Society for Noise and Vibration Engineering Conference (한국소음진동공학회:학술대회논문집)

  • 2004.05a
  • /
  • Pages.452-456
  • /
  • 2004
  • /
  • 1598-2548(pISSN)
The Korean Society for Noise and Vibration Engineering (한국소음진동공학회)
권호 표지

Gust Response Analysis and Alleviation Method for Aircraft Wing

항공기 날개 돌풍 응답해석 및 완화기법

  • 이상욱 (한국항공우주연구원 기체구조그룹) ;
  • 김태욱 (한국항공우주연구원 기체구조그룹) ;
  • 황인희 (한국항공우주연구원 기체구조그룹) ;
  • 하철근 (울산대학교 수성시스템공학부)
  • Published : 2004.05.01
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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