Flutter Free FLight Envelope eXpansion for ecOnomical Performance improvement

Resultado final

The project requires a public and an internal restricted homepage to share the work within the consortium and to promote them toward the general public Various social media site like linkedin twitter and Facebook will be set up to reach different groups

Report on LFT/LPV modelling and order reduction techniques

A general overview of the LFT/LPV modelling and order reduction techniques that are applicable for the flexible aircraft problems.

Report on robust analysis techniques for flexible aircraft and flutter
Report on flexible aircraft control techniques
Report on aeroelastic tailoring methods

The review of the approaches to design aeroelastically tailored wings taken by the consortium

Release of the flight test results and models of the a/c for the community

In accordance with the open research data initiative, flight test results and models of the demonstrator are released to the community. The models and data are documented in this report.

Workshop / Final Exploitation and Dissemination Report

The results of the project are presented in an international Workshop. The conclusions and summary of this event and the responses from various stakeholders are described in this report.

Publicaciones

Design of a flying demonstrator wing for manoeuvre load alleviation with cruise shape constraint

Autores: Jurij Sodja, Noud Werter, Roeland De Breuker
Publicado en: 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018, ISBN 978-1-62410-532-6
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-2153

Aeroelastic Stability Analysis of the FLEXOP Demonstrator using the Continuous Time Unsteady Vortex Lattice Method

Autores: Simon Binder, Andreas Wildschek, Roeland De Breuker
Publicado en: 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018, ISBN 978-1-62410-532-6
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-0950

Designing an UAV Propulsion System for Dedicated Acceleration and Deceleration Requirements

Autores: Franz-Michael Sendner, Philipp Stahl, Christian Rößler, Mirko Hornung
Publicado en: 17th AIAA Aviation Technology, Integration, and Operations Conference, 2017, ISBN 978-1-62410-508-1
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2017-4105

Mission and Aircraft Design of FLEXOP Unmanned Flying Demonstrator to Test Flutter Suppression within Visual Line of Sight

Autores: Philipp Stahl, Franz-Michael Sendner, Andreas Hermanutz, Christian Rößler, Mirko Hornung
Publicado en: 17th AIAA Aviation Technology, Integration, and Operations Conference, 2017, ISBN 978-1-62410-508-1
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2017-3766

Aeroelastic Analysis of a Flutter Demonstrator with a very Flexible High-Aspect-Ratio Swept Wing

Autores: Rozov, V.; Hermanutz, A.; Breitsamter, C.; Hornung, M
Publicado en: International Forum on Aeroelasticity and Structural Dynamics [IFASD], 2017, Edición 28 June 2017, 2017
Editor: International Forum on Aeroelasticity and Structural Dynamics

Flight control oriented bottom-up nonlinear modeling of aeroelastic vehicles

Autores: Bela Takarics, Balint Vanek, Aditya Kotikalpudi, Peter Seiler
Publicado en: 2018 IEEE Aerospace Conference, 2018, Página(s) 1-10, ISBN 978-1-5386-2014-4
Editor: IEEE
DOI: 10.1109/AERO.2018.8396537

Tensor product type polytopic LPV modeling of aeroelastic aircraft

Autores: Bela Takarics, Alexandra Szollosi, Balint Vanek
Publicado en: 2018 IEEE Aerospace Conference, 2018, Página(s) 1-10, ISBN 978-1-5386-2014-4
Editor: IEEE
DOI: 10.1109/AERO.2018.8396538

Control oriented reduced order modeling of a flexible winged aircraft

Autores: Tamas Luspay, Tamas Peni, Balint Vanek
Publicado en: 2018 IEEE Aerospace Conference, 2018, Página(s) 1-9, ISBN 978-1-5386-2014-4
Editor: IEEE
DOI: 10.1109/AERO.2018.8396496

Nonlinear flutter analysis with uncertainties based on Describing Function and Structured Singular Value with an IQC validation

Autores: Iannelli, Marcos, Lowenberg
Publicado en: Proceedings of the 7th European Conference for Aeronautics and Space Sciences (EUCASS 2017) , 2017
Editor: -
DOI: 10.13009/EUCASS2017-90

Nonlinear stability and post-critical analysis of an uncertain plant with describing functions and integral quadratic constraints

Autores: Andrea Iannelli, Andres Marcos, Mark Lowenberg
Publicado en: 2017 IEEE 56th Annual Conference on Decision and Control (CDC), Edición 18/1/2018, 2017, Página(s) 1828-1833, ISBN 9781-509028740
Editor: IEEE
DOI: 10.1109/CDC.2017.8263913

Model order reduction of LPV systems based on parameter varying modal decomposition

Autores: Istvan Gozse, Tamas Luspay, Tamas Peni, Zoltan Szabo, Balint Vanek
Publicado en: 2016 IEEE 55th Conference on Decision and Control (CDC), 2016, Página(s) 7459-7464, ISBN 978-1-5090-1837-6
Editor: IEEE
DOI: 10.1109/CDC.2016.7799421

Modeling and robust Body Freedom Flutter Analysis of flexible aircraft configurations

Autores: Andrea Iannelli, Andres Marcos, Mark Lowenberg
Publicado en: 2016 IEEE Conference on Control Applications (CCA), 2016, Página(s) 243-248, ISBN 978-1-5090-0755-4
Editor: IEEE
DOI: 10.1109/CCA.2016.7587843

Aircraft Design and Testing of FLEXOP Unmanned Flying Demonstrator to Test Load Alleviation and Flutter Suppression of High Aspect Ratio Flexible Wings

Autores: Christian Roessler, Philipp Stahl, Franz Sendner, Andreas Hermanutz, Sebastian Koeberle, Julius Bartasevicius, Vladyslav Rozov, Christian Breitsamter, Mirko Hornung, Yasser M. Meddaikar, Johannes Dillinger, Jurij Sodja, Roeland De Breuker, Christos Koimtzoglou, Dimitrios Kotinis, Panagiotis Georgopoulos
Publicado en: AIAA Scitech 2019 Forum, Edición na, 2019, Página(s) na, ISBN 978-1-62410-578-4
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2019-1813

FLEXOP – Application of aeroelastic tailoring to a flying demonstrator wing

Autores: Muhammad Yasser Meddaikar, Johannes Dillinger, Jurij Sodja, Roeland De Breuker
Publicado en: DLRK 2018 – Deutscher Luft- und Raumfahrtkongress, Edición 04.-06. Sep. 2018, 2018, Página(s) na
Editor: Deutscher Luft- und Raumfahrtkongress

Design of an Electric Actuated Airbrake for Dynamic Airspeed Control of an Unmanned Aeroelastic Research UAV

Autores: Franz-Michael Sendner, Philipp Stahl, Christian Rössler, Mirko Hornung
Publicado en: 2018 Aviation Technology, Integration, and Operations Conference, Edición na, 2018, Página(s) na, ISBN 978-1-62410-556-2
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-3194

Baseline Flight Control System Design for an Unmanned Flutter Demonstrator

Autores: Daniel Ossmann, Tamas Luspay, Balint Vanek
Publicado en: 2019 IEEE Aerospace Conference, Edición yearly, 2019, Página(s) 1-10, ISBN 978-1-5386-6854-2
Editor: IEEE
DOI: 10.1109/aero.2019.8741853

Aeroservoelastic Modeling and Analysis of a Highly Flexible Flutter Demonstrator

Autores: Matthias Wuestenhagen, Thiemo Kier, Yasser M. Meddaikar, Manuel Pusch, Daniel Ossmann, Andreas Hermanutz
Publicado en: 2018 Atmospheric Flight Mechanics Conference, Edición na, 2018, Página(s) na, ISBN 978-1-62410-557-9
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-3150

Aircraft Aeroservoelastic Modelling of the FLEXOP Unmanned Flying Demonstrator

Autores: Yasser M. Meddaikar, Johannes Dillinger, Thomas Klimmek, Wolf Krueger, Matthias Wuestenhagen, Thiemo M. Kier, Andreas Hermanutz, Mirko Hornung, Vladyslav Rozov, Christian Breitsamter, James Alderman, Bela Takarics, Balint Vanek
Publicado en: AIAA Scitech 2019 Forum, Edición yearly, 2019, Página(s) na, ISBN 978-1-62410-578-4
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2019-1815

Advanced Aeroelastic Robust Stability Analysis with Structural Uncertainties

Autores: Süelözgen, Özge
Publicado en: EuroGNC 2019 5th CEAS Conference on Guidance, Navigation & Control, 2019
Editor: The Council of European Aerospace Societies

Operational Modal Analysis For Simulated Flight Flutter Test Of An Unconventional Aircraft

Autores: Süelözgen, Özge and Wüstenhagen, Matthias
Publicado en: International Forum on Aeroelasticity and Structural Dynamics IFASD 2019, 2019
Editor: International Forum on Aeroelasticity and Structural Dynamics

Algorithms for the estimation of the region of attraction with positively invariant sets

Autores: Andrea Iannelli, Andres Marcos, Mark Lowenberg
Publicado en: 2018 7th International Conference on Systems and Control (ICSC), Edición Aug. 2018, 2018, Página(s) 93-98, ISBN 978-1-5386-8537-2
Editor: IEEE
DOI: 10.1109/icosc.2018.8587774

Estimating the Region of Attraction of Uncertain Systems with Integral Quadratic Constraints

Autores: Andrea Iannelli, Peter Seiler, Andres Marcos
Publicado en: 2018 IEEE Conference on Decision and Control (CDC), 2018, Página(s) 3922-3927, ISBN 978-1-5386-1395-5
Editor: IEEE
DOI: 10.1109/cdc.2018.8619669

An equilibrium-independent region of attraction formulation for systems with uncertainty-dependent equilibria

Autores: Andrea Iannelli, Andres Marcos, Peter Seiler
Publicado en: 2018 IEEE Conference on Decision and Control (CDC), 2018, Página(s) 725-730, ISBN 978-1-5386-1395-5
Editor: IEEE
DOI: 10.1109/cdc.2018.8619153

Flight control design for a highly flexible flutter demonstrator

Autores: Tamás Luspay, Daniel Ossmann, Matthias Wuestenhagen, Dániel Teubl, Tamás Baár, Manuel Pusch, Thiemo M. Kier, Sergio Waitman, Andrea Ianelli, Andres Marcos, Balint Vanek, Mark H. Lowenberg
Publicado en: AIAA Scitech 2019 Forum, 2019, ISBN 978-1-62410-578-4
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2019-1817

An extension of the structured singular value to nonlinear systems with application to robust flutter analysis

Autores: Iannelli, A. , Lowenberg, M., & Marcos, A.
Publicado en: 5th CEAS Conference on Guidance, Navigation & Control, Milan, Italy, 3/04/19, 2019
Editor: EURO GNC

A symbolic LFT approach for robust flutter analysis of high-order models

Autores: Andrea Iannelli, Andres Marcos, Rocco Bombardieri, Rauno Cavallaro
Publicado en: 2019 18th European Control Conference (ECC), 2019, Página(s) 961-967, ISBN 978-3-907144-00-8
Editor: IEEE
DOI: 10.23919/ecc.2019.8796122

Active Flutter Mitigation Testing on the FLEXOP Demonstrator Aircraft

Autores: Béla Takarics, Bálint Patartics, Tamás Luspay, Balint Vanek, Christian Roessler, Julius Bartasevicius, Sebastian J. Koeberle, Mirko Hornung, Daniel Teubl, Manuel Pusch, Matthias Wustenhagen, Thiemo M. Kier, Gertjan Looye, Péter Bauer, Yasser M. Meddaikar, Sergio Waitman, Andres Marcos
Publicado en: AIAA Scitech 2020 Forum, 2020, ISBN 978-1-62410-595-1
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2020-1970

Design of System Architecture for Active Flutter Suppression

Autores: Stefan Vocks
Publicado en: 2017
Editor: Uni Stuttgart

Aeroelastic control law design using different synthesis methods (Master thesis)

Autores: Simon Schulz
Publicado en: 2017
Editor: University of Stuttgart

Retrospective Cost Adaptive Control of a flexible Aircraft

Autores: Alexander Böhm
Publicado en: Master Thesis, 2016
Editor: Technische Universität München

Condensation of Large 3D FEM Models and Integration in dAEDalus for Fast Dynamic Aeroelastic Analysis

Autores: Daniel Stein
Publicado en: Master Thesis, 2016
Editor: University of Stuttgart

Advanced Linear and Nonlinear Analysis of Aircraft Flutter

Autores: Andrea Iannelli
Publicado en: PhD thesis, Edición March 2019, 2019
Editor: University of Bristol

LPV model reduction methods for aeroelastic structures * *The research leading to these results is part of the FLEXOP project. This project has received funding from the European Unions Horizon 2020 research and innovation programme under grant agreement No 636307.

Autores: Gy. Lipták, T. Luspay, T. Péni, B. Takarics, B. Vanek
Publicado en: IFAC-PapersOnLine, Edición 50/1, 2017, Página(s) 6344-6349, ISSN 2405-8963
Editor: IFAC
DOI: 10.1016/j.ifacol.2017.08.1015

Parameter varying flutter suppression control for the BAH jet transport wing * *The research leading to these results is part of the FLEXOP project. This project has received funding from the Horizon 2020 research and innovation programme of the European Union under grant agreement No 636307.

Autores: B. Patartics, T. Luspay, T. Péni, B. Takarics, B. Vanek, T. Kier
Publicado en: IFAC-PapersOnLine, Edición 50/1, 2017, Página(s) 8163-8168, ISSN 2405-8963
Editor: IFAC
DOI: 10.1016/j.ifacol.2017.08.1263

On the correspondence of hyperbolic geometry and system analysis

Autores: István Gőzse, Tamás Péni, Tamás Luspay, Alexandros Soumelidis
Publicado en: IFAC-PapersOnLine, Edición 50/1, 2017, Página(s) 9285-9290, ISSN 2405-8963
Editor: IFAC
DOI: 10.1016/j.ifacol.2017.08.917

Model reduction for LPV systems based on approximate modal decomposition

Autores: Tamás Luspay, Tamás Péni, István Gőzse, Zoltán Szabó, Bálint Vanek
Publicado en: International Journal for Numerical Methods in Engineering, Edición 113/6, 2018, Página(s) 891-909, ISSN 0029-5981
Editor: John Wiley & Sons Inc.
DOI: 10.1002/nme.5692

LFT Modeling and μ Analysis of the Aircraft Landing Benchmark

Autores: Andrea Iannelli, Pedro Simplício, Diego Navarro-Tapia, Andrés Marcos
Publicado en: IFAC-PapersOnLine, Edición 50/1, 2017, Página(s) 3965-3970, ISSN 2405-8963
Editor: IFAC
DOI: 10.1016/j.ifacol.2017.08.766

Estimating the region of attraction of uncertain systems with invariant sets

Autores: A. Iannelli, A. Marcos, M. Lowenberg
Publicado en: IFAC-PapersOnLine, Edición 51/25, 2018, Página(s) 246-251, ISSN 2405-8963
Editor: International Federation of Automatic Control
DOI: 10.1016/j.ifacol.2018.11.113

Study of Flexible Aircraft Body Freedom Flutter with Robustness Tools

Autores: Andrea Iannelli, Andrés Marcos, Mark Lowenberg
Publicado en: Journal of Guidance, Control, and Dynamics, Edición 41/5, 2018, Página(s) 1083-1094, ISSN 0731-5090
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/1.G003165

Aeroelastic modeling and stability analysis: A robust approach to the flutter problem

Autores: Andrea Iannelli, Andrés Marcos, Mark Lowenberg
Publicado en: International Journal of Robust and Nonlinear Control, Edición 28/1, 2018, Página(s) 342-364, ISSN 1049-8923
Editor: John Wiley & Sons Inc.
DOI: 10.1002/rnc.3878

Nonlinear Robust Approaches to Study Stability and Postcritical Behavior of an Aeroelastic Plant

Autores: Andrea Iannelli, Andres Marcos, Mark Lowenberg
Publicado en: IEEE Transactions on Control Systems Technology, Edición 27/2, 2018, Página(s) 1-14, ISSN 1063-6536
Editor: Institute of Electrical and Electronics Engineers
DOI: 10.1109/TCST.2017.2779110

FLEXIBILIS SZÁRNYÚ REPÜLŐGÉP AKTÍV FLATTER SZABÁLYOZÁSA (Hungarian)

Autores: Patartics Bálint, Péni Tamás, Vanek Bálint
Publicado en: Repüléstudományi Közlemények, 2018, ISSN 1789-770X
Editor: Nemzeti Közszolgálati Egyetem Katonai Repülő Intézet

Comparison of Aeroelastic Modeling and Robust Flutter Analysis of a Typical Section**This work has received funding from the European Union’s Horizon 2020 research and innovation programme under grant agreement No 636307, project FLEXOP

Autores: A. Iannelli, A. Marcos, M. Lowenberg
Publicado en: IFAC-PapersOnLine, Edición 49/17, 2016, Página(s) 409-414, ISSN 2405-8963
Editor: 20th IFAC Symposium on Automatic Control in AerospaceACA 2016
DOI: 10.1016/j.ifacol.2016.09.070

Structured Control Design for a Highly Flexible Flutter Demonstrator

Autores: Manuel Pusch, Daniel Ossmann, Tamás Luspay
Publicado en: Aerospace, Edición 6/3, 2019, Página(s) 27, ISSN 2226-4310
Editor: MDPI
DOI: 10.3390/aerospace6030027

Robust estimations of the Region of Attraction using invariant sets

Autores: Andrea Iannelli, Andrés Marcos, Mark Lowenberg
Publicado en: Journal of the Franklin Institute, Edición 356/8, 2019, Página(s) 4622-4647, ISSN 0016-0032
Editor: Pergamon Press Ltd.
DOI: 10.1016/j.jfranklin.2019.02.013

Worst-Case Disturbances for Time-Varying Systems with Application to Flexible Aircraft

Autores: Andrea Iannelli, Peter Seiler, Andrés Marcos
Publicado en: Journal of Guidance, Control, and Dynamics, Edición 42/6, 2019, Página(s) 1261-1271, ISSN 0731-5090
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/1.g004023

Region of attraction analysis with Integral Quadratic Constraints

Autores: Andrea Iannelli, Peter Seiler, Andrés Marcos
Publicado en: Automatica, Edición 109, 2019, Página(s) 108543, ISSN 0005-1098
Editor: Pergamon Press Ltd.
DOI: 10.1016/j.automatica.2019.108543

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

Autores: Sérgio Waitman, Andrés Marcos
Publicado en: Journal of Guidance, Control, and Dynamics, Edición Online: 20 Dec. 2019, 2019, Página(s) 1-17, ISSN 1533-3884
Editor: American Institute of Aeronautics & Astronautics
DOI: 10.2514/1.g004618

Linear Fractional Transformation co-modeling of high-order aeroelastic systems for robust flutter analysis

Autores: Andrea Iannelli, Andrés Marcos, Rocco Bombardieri, Rauno Cavallaro
Publicado en: European Journal of Control, Edición Published online: 12 Dec. 2019, 2019, ISSN 0947-3580
Editor: Lavoisier
DOI: 10.1016/j.ejcon.2019.12.002

Active flutter suppression: non-structured and structured H∞ design

Autores: Sérgio Waitman, Andrés Marcos
Publicado en: IFAC-PapersOnLine, Edición 52/12, 2019, Página(s) 146-151, ISSN 2405-8963
Editor: International Federation of Automatic Control
DOI: 10.1016/j.ifacol.2019.11.184

Limit cycle oscillation amplitude tailoring based on describing functions and μ analysis

Autores: Andrea Iannelli, Andrés Marcos, Mark Lowenberg
Publicado en: 4th CEAS Specialist Conference on Guidance, Navigation and Control (EuroGNC 2017), Edición Published online: 15 Dec. 2017, 2017, Página(s) 101-119, ISBN 978-3-319-65282-5
Editor: Springer International Publishing
DOI: 10.1007/978-3-319-65283-2_6

Model reduction for LPV systems based on approximate modal decomposition

Autores: T. Luspay, T. Peni, I. Gozse, Z. Szabo, B. Vanek
Publicado en: arXiv online repository of scientific papers, 2016
Editor: Cornell University Library

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