Active flutter suppression, which is a part of the group of flight vehicle technologies known as
active controls, is an important contributor to the effective solution of aeroelastic instability …

Aeroelasticity is still dynamic, challenging, and a key part of cutting-edge airplane
technology. Emerging trends, as well as challenges and needs in the eld of airplane …

Aircraft structure design is a complex industrial process that requires multidisciplinary
analyzes and considerations in fields as diverse as aerodynamics, structure, materials and …

The series Advances in Industrial Control aims to report and encourage technology transfer
in control engineering. The rapid development of control technology impacts all areas of the …

AEROSERVOELASTICITY study considers the interaction between aerodynamic, inertial,
structural, actuation, and control systemdynamics. 1 Flightcontrollersareusuallydesignedforarigi …

The most common approach to flight flutter testing is to track estimated modal damping ratios
of an aircraft over a number of fight conditions. However, the risk is inevitable when this …

P= plant model Pnom= nominal plant model Prob= robust plant model Ptrue= true plant
model q= dynamic pressure Win= weighting matrix on input uncertainty D …

Uncertainties denote the operators which describe data error, numerical error and model
error in the mathematical methods. The study of aeroelasticity with uncertainty embedded in …

An approach for computing worst-case flutter margins has been formulated in a robust
stability framework. Uncertainty operators are included with a linear model to describe …

This paper describes a novel time-delayed control scheme for suppressing the body-
freedom flutter of a flexible flying-wing drone and verifies its robustness. The simple …