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.
Active flutter and gust response control
1990-01-01
Conference paper
No indication
English
Flutter and gust response analysis of flexible aircraft with active control
Tema Archive | 1976
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