This paper develops a sliding mode fault tolerant control scheme based on a Linear
Parameter Varying (LPV) system representation of the plant. The scheme includes a control …

The structural stiffness of a cable-struts structure is dependent on its feasible pre-stresses.
The search for the pre-stresses is an inverse problem, and classical approaches for this …

In this work a simple adaptive flutter suppression system is designed in order to increase the
operative speed range of a wing-aileron aeroelastic plant. The equivalent beam finite …

The suppression of aeroelastic vibrations due to flutter using a trailing edge flap is analyzed
to increase the speed operability range of wings. The aeroelastic model of a 3DOF airfoil in …

The occurrence of shimmy vibration in aircraft nose landing gear can cause an increase of
fatigue stress on the nose landing gear mechanical elements that can eventually lead to …

A linear parameter varying sliding mode fault reconstruction scheme is proposed. Compared
with other conventional sliding mode observer designs, the estimate emerges quite naturally …

This paper presents an extension of the simple adaptive control (SAC) deal with input
saturation for the attitude control of the unmanned aerial vehicle (UAV). A new SAC structure …

A piloted simulator evaluation is an important step for making a Fault-Tolerant Flight Control
(FTFC) system more practical and reliable. Especially, in the case of an adaptive technique …

This paper considers the problem of flying a UAV along a given trajectory at speeds close to
the speed of sound and above. A novel pitch channel control system is presented using the …

This study presents a transformer-based approach for fault-tolerant control in fixed-wing
Unmanned Aerial Vehicles (UAVs), designed to adapt in real time to dynamic changes …