Increasing efficiency is at the core of next generation aircraft development. Aerodynamics
can be improved by high aspect ratio wings, but as these wings are more susceptible to …

The main objective of the present work is to find an approximate analytical solution for the
nonlinear differential equation of the vibro-impact oscillator under the influence of the …

In this paper, we propose a control approach for the robust stabilization of linear time-
invariant (LTI) systems with non-negligible sensor and actuator dynamics subject to time …

In this work, the effect of vibro-impact nonlinear, forced, and damped oscillator on the
dynamics of the electromagnetic actuation (EA) near primary resonance is studied. The vibro …

This paper presents a systematic methodology to evaluate the feasibility of suppressing
airplane flutter instabilities through the actively controlled closed-loop actuation of control …

Active gust load alleviation is a promising technique to reduce the structural weight of
flexible transport aircraft wings with high aspect ratio, ensuring lower fuel consumption and …

In this work, new static output feedback (SOF) controller synthesis conditions for the
stabilization of linear systems are proposed. The cases of uncertain linear time-invariant …

Alleviating gust and maneuver induced loads acting on the wing of a transport aircraft allows
to reduce structural weight, which in turn improves fuel economy and environmental …

Active control in aeroelasticity has gained more interest recently. It is investigated if a
nonlinear actuator model leads to better performance prediction of the aeroservoelastic …