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http://dx.doi.org/10.5139/JKSAS.2004.32.8.109

Design of Control System for Gust Load Alleviation using Control Surface  

Lee, Sang-Wook (한국항공우주연구원 기체구조그룹)
Kim, Tae-Uk (한국항공우주연구원 기체구조그룹)
Hwang, In-Hee (한국항공우주연구원 기체구조그룹)
Ha, Chul-Keun (울산대학교 수송시스템공학부)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.32, no.8, 2004 , pp. 109-117 More about this Journal
Abstract
A study on gust load alleviation using aircraft control surface was performed. Aeroservoelastic model including control surface controller was formulated and validated by comparing the results of continuous gust 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 load alleviation was validated by performing the numerical simulation for the controller designed.
Keywords
Gust Load Alleviation; Aeroservoelastic Model; Continuous Gust; Optimal Control; Output Feedback;
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