Design and Experimental Validation of Gust Load Alleviation Based on H2-Optimal Blending of Inputs and Outputs

B Micheli, M Tang, F Stalla, C Hanke… - AIAA SciTech 2025 …, 2025 - arc.aiaa.org
The next generation of commercial aircraft might feature high-aspect-ratio wing
configurations to enhance efficiency and reduce emissions. However, these wings are more …

[PDF][PDF] Gust load alleviation wind tunnel tests of a folding wing tip configuration

L Marchetti, S Ricci, L Riccobene… - … on Aeroelasticity and …, 2024 - re.public.polimi.it
Increasing the aspect ratio is one way to improve aircraft aerodynamic efficiency. This
reduces the induced drag term but, at the same time, produces an increment of the wing …

Development of an Active Wingtip for Aeroelastic Control

F Toffol, S Ricci - Aerospace, 2023 - mdpi.com
This paper presents the design of an innovative wingtip device actively actuated to control
the aeroelastic loads, with a focus on the gust load alleviation. It summarizes the work …

Dual Loop PImPIn Control for an Aileron Positioning

A De Gaspari, P Mantegazza - IEEE Access, 2024 - ieeexplore.ieee.org
Aircraft control surfaces are subjected to uncertain design parameters and time–varying
external disturbances related to aerodynamic loads. This paper presents a control …

A Review of Counter Turbulence Strategies, With a Focus on Gust Load Alleviation Technology in Manned Aircraft

I Burgstaller, A Galffy - AIAA AVIATION FORUM AND ASCEND 2024, 2024 - arc.aiaa.org
Counter Turbulence Strategies have been researched since the 1960s to avoid aircraft
damage, passenger injuries and increase the aerodynamic efficiency of aircraft. This paper …

[PDF][PDF] Design of an Innovative Wing Tip for Aeroelastic Control: from Scratch to Flight Test

F Toffol, F Fonte, S Ricci - ICAS PROCEEDINGS, 2022 - re.public.polimi.it
This paper resumes the activities done in the framework of the Clean Sky 2 AIRGREEN2
project, where an Innovative Wing Tip (IWT) device was designed, built, and tested. The IWT …