NASA NTRS · 19940004741
Active flutter and gust response control
Abstract
After a short recall concerning the aeroelastic equations, active control law based on optimal stochastic control theory is synthesized for a wing flutter and gust response. Robustness of the control system due to structured and unstructured uncertainties is considered. Robustness recovery technique is applied to improve the stability margin.
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Oli, Muluneh. 1990-01-01. Active flutter and gust response control. https://ntrs.nasa.gov/citations/19940004741
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