“…Their implementation would enable to increase the flutter speed, enhance the aeroelastic response by attenuating excessive vibrations, and convert the unstable limit cycle oscillation (LCO), in which case the flutter boundary is catastrophic, into a stable LCO, in which case the flutter boundary is benign. One of the limitations of the performance of the active control consists of the presence of unavoidable time-delays in controller and actuators (Palkovics et al, 1992;Ramesh and Narayanan, 2001;. These delays can be detrimental in the sense of deteriorating the control performance, and even of precipitating the occurrence of the instability of the aeroelastic system.…”