Flight mechanical analysis of a solar-powered high-altitude platform

YJ Hasan, MS Roeser, M Hepperle, S Niemann… - CEAS Aeronautical …, 2023 - Springer
Abstract The German Aerospace Center (DLR) is currently developing an unmanned
experimental solar-powered fixed-wing high-altitude platform designed to be stationed in the …

Structured control design for a highly flexible flutter demonstrator

M Pusch, D Ossmann, T Luspay - Aerospace, 2019 - mdpi.com
The model-based flight control system design for a highly flexible flutter demonstrator,
developed in the European FLEXOP project, is presented. The flight control system includes …

Control Design for Active Flutter Suppression of Flexible-Wing Unmanned Aerial Vehicle Demonstrator

S Waitman, A Marcos - Journal of Guidance, Control, and Dynamics, 2020 - arc.aiaa.org
Flutter is an aeroelastic phenomenon affecting flexible structures in a fluid flow and may lead
to unstable oscillations and to critical structural damage. This paper concerns the design of a …

[PDF][PDF] Blending of inputs and outputs for modal control of aeroelastic systems

M Pusch - 2020 - elib.dlr.de
The present thesis is the result of my work at the Institute of System Dynamics and Control at
the German Aerospace Center (DLR) in Oberpfaffenhofen, Germany. My thanks go to Prof …

Application of structured robust synthesis for flexible aircraft flutter suppression

B Patartics, G Lipták, T Luspay, P Seiler… - … on Control Systems …, 2021 - ieeexplore.ieee.org
This article presents a method for structured robust control design for systems with a mixture
of parametric and dynamic uncertainty. The proposed method alternates between an …

Fault-Tolerant control for a high altitude long endurance aircraft

C Weiser, D Ossmann - IFAC-PapersOnLine, 2022 - Elsevier
Abstract High Altitude Long Endurance (HALE) aircraft consist of extremely light-weight
structures in combination with a high wingspan and high aspect ratio. The combination of …

[PDF][PDF] Flight testing of 65kg t-flex subscale demonstrator

J Bartasevicius, SJ Koeberle, D Teubl… - 32nd Congress of …, 2021 - mediatum.ub.tum.de
FLEXOP is a project within the European Union's Horizon 2020 framework which develops
methods for aeroelastic wing tailoring and active flutter suppression. The developed …

Synthesis of a multiple-model adaptive gust load alleviation controller for a flexible flutter demonstrator

M Wuestenhagen - AIAA Scitech 2022 Forum, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-0440. vid Today's advanced
aircraft designs with respect to new materials and high aspect ratio wings demand for …

Model Predictive Gust Load Alleviation Control for Flexible Aircraft

M Schumann, M Wüstenhagen, M Pusch… - AIAA SCITECH 2025 …, 2025 - arc.aiaa.org
Flexible aircraft are particularly sensitive to wind disturbances. To prevent this drawback and
enable highly fuel-efficient aircraft design, the reduction of gust loads is an inevitable step to …

Wing shape estimation with Extended Kalman filtering and KalmanNet neural network of a flexible wing aircraft

BZ Hadlaczky, N Friedman… - … for Dynamics and …, 2023 - proceedings.mlr.press
The dynamic behaviour, stability, and the effects of the aerodynamic drag of a large-
wingspan aircraft are mainly influenced by the structural flexibility and shape of the wings …