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FLEXOP SIGNED

Flutter Free FLight Envelope eXpansion for ecOnomical Performance improvement

Total Cost €

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EC-Contrib. €

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Partnership

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Project "FLEXOP" data sheet

The following table provides information about the project.

Coordinator
MAGYAR TUDOMANYOS AKADEMIA SZAMITASTECHNIKAI ES AUTOMATIZALASI KUTATOINTEZET 

Organization address
address: KENDE UTCA 13-17
city: BUDAPEST
postcode: 1111
website: www.sztaki.hu

contact info
title: n.a.
name: n.a.
surname: n.a.
function: n.a.
email: n.a.
telephone: n.a.
fax: n.a.

 Coordinator Country Hungary [HU]
 Project website https://flexop.eu
 Total cost 6˙692˙164 €
 EC max contribution 6˙692˙163 € (100%)
 Programme 1. H2020-EU.3.4. (SOCIETAL CHALLENGES - Smart, Green And Integrated Transport)
 Code Call H2020-MG-2014_TwoStages
 Funding Scheme RIA
 Starting year 2015
 Duration (year-month-day) from 2015-06-01   to  2019-11-30

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    MAGYAR TUDOMANYOS AKADEMIA SZAMITASTECHNIKAI ES AUTOMATIZALASI KUTATOINTEZET HU (BUDAPEST) coordinator 980˙801.00
2    FISCHER ADVANCED COMPOSITE COMPONENTS AG*FACC AG AT (RIED IM INNKREIS) participant 1˙177˙444.00
3    TECHNISCHE UNIVERSITAET MUENCHEN DE (MUENCHEN) participant 1˙129˙835.00
4    AIRBUS DEFENCE AND SPACE GMBH DE (TAUFKIRCHEN) participant 895˙563.00
5    DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV DE (KOELN) participant 735˙453.00
6    UNIVERSITY OF BRISTOL UK (BRISTOL) participant 643˙468.00
7    INASCO HELLAS ETAIREIA EFARMOSMENON AERODIASTIMIKON EPISTIMON EE EL (GLYFADA ATHINA) participant 528˙532.00
8    AIRBUS GROUP LIMITED UK (LONDON) participant 282˙150.00
9    TECHNISCHE UNIVERSITEIT DELFT NL (DELFT) participant 223˙378.00
10    RHEINISCH-WESTFAELISCHE TECHNISCHE HOCHSCHULE AACHEN DE (AACHEN) participant 95˙535.00

Map

 Project objective

The FLEXOP project is about developing multidisciplinary aircraft design capabilities for Europe that will increase competitiveness with emerging markets -particularly in terms of aircraft development costs. A closer coupling of wing aeroelasticity and flight control systems in the design process opens new opportunities to explore previously unviable designs. Common methods and tools across the disciplines also provide a way to rapidly adapt existing designs into derivative aircraft, at a reduced technological risk (e.g. using control to solve a flutter problem discovered during development). The goal will be achieved by: (a) improving efficiency of currently existing wing, by increased span at no excess structural weight, while establishing modifications by aeroelastic tailoring to carry the redesigned derivative wing; (b) developing methods and tools for very accurate flutter modeling and flutter control synthesis, to enable improved flutter management during development, certification, and operation, enabling to fly with the stretched wing at same airspeed as the baseline aircraft; (c) validating the accuracy of developed tools and methods on an affordable experimental platform, followed by a scale-up study, demonstrating the interdisciplinary development cycle. Manufacturers will gain cost efficient methods, tools and demonstrators for enhancing aircraft performance by integrated development of flutter control and aeroelastic tailoring. These inter-disciplinary capabilities will improve the design cycle and the Verification& Validation process of both derivative and new aircraft. Better control of development and certification costs can be achieved if these capabilities are used to address problems early in the design process. Flight test data will be posted on the project website to provide a benchmark for the EU aerospace community. The project’s results will serve as a preliminary outlining of certification standards for future EU flexible transport aircraft.

 Deliverables

List of deliverables.
Workshop / Final Exploitation and Dissemination Report Documents, reports 2020-02-27 15:43:47
Release of the flight test results and models of the a/c for the community Documents, reports 2020-02-27 15:43:44
Report on aeroelastic tailoring methods Documents, reports 2019-04-05 09:41:35
Project Homepage, social media site Websites, patent fillings, videos etc. 2019-04-05 09:41:35
Report on robust analysis techniques for flexible aircraft and flutter Documents, reports 2019-04-05 09:41:35
Report on LFT/LPV modelling and order reduction techniques Documents, reports 2019-05-31 12:16:08
Report on flexible aircraft control techniques Documents, reports 2019-05-31 12:15:56

Take a look to the deliverables list in detail:  detailed list of FLEXOP deliverables.

 Publications

year authors and title journal last update
List of publications.
2019 Süelözgen, Özge and Wüstenhagen, Matthias
Operational Modal Analysis For Simulated Flight Flutter Test Of An Unconventional Aircraft
published pages: , ISSN: , DOI:
International Forum on Aeroelasticity and Structural Dynamics IFASD 2019 2020-01-29
2019 Andrea Iannelli, Peter Seiler, Andrés Marcos
Worst-Case Disturbances for Time-Varying Systems with Application to Flexible Aircraft
published pages: 1261-1271, ISSN: 0731-5090, DOI: 10.2514/1.g004023
Journal of Guidance, Control, and Dynamics 42/6 2020-01-30
2019 Andrea Iannelli, Andrés Marcos, Rocco Bombardieri, Rauno Cavallaro
Linear Fractional Transformation co-modeling of high-order aeroelastic systems for robust flutter analysis
published pages: , ISSN: 0947-3580, DOI: 10.1016/j.ejcon.2019.12.002
European Journal of Control Published online: 12 Dec. 2019 2020-01-30
2019 Andrea Iannelli
Advanced Linear and Nonlinear Analysis of Aircraft Flutter
published pages: , ISSN: , DOI:
PhD thesis March 2019 2020-01-30
2019 Iannelli, A. , Lowenberg, M., & Marcos, A.
An extension of the structured singular value to nonlinear systems with application to robust flutter analysis
published pages: , ISSN: , DOI:
5th CEAS Conference on Guidance, Navigation & Control, Milan, Italy, 3/04/19 2020-01-30
2019 Sérgio Waitman, Andrés Marcos
Active flutter suppression: non-structured and structured H∞ design
published pages: 146-151, ISSN: 2405-8963, DOI: 10.1016/j.ifacol.2019.11.184
IFAC-PapersOnLine 52/12 2020-01-30
2019 Andrea Iannelli, Peter Seiler, Andrés Marcos
Region of attraction analysis with Integral Quadratic Constraints
published pages: 108543, ISSN: 0005-1098, DOI: 10.1016/j.automatica.2019.108543
Automatica 109 2020-01-30
2019 Sérgio Waitman, Andrés Marcos
H∞ Control Design for Active Flutter Suppression of Flexible-Wing Unmanned Aerial Vehicle Demonstrator
published pages: 1-17, ISSN: 1533-3884, DOI: 10.2514/1.g004618
Journal of Guidance, Control, and Dynamics Online: 20 Dec. 2019 2020-01-30
2019 Manuel Pusch, Daniel Ossmann, Tamás Luspay
Structured Control Design for a Highly Flexible Flutter Demonstrator
published pages: 27, ISSN: 2226-4310, DOI: 10.3390/aerospace6030027
Aerospace 6/3 2019-11-26
2017 Stefan Vocks
Design of System Architecture for Active Flutter Suppression
published pages: , ISSN: , DOI:
2019-05-24
2017 István Gőzse, Tamás Péni, Tamás Luspay, Alexandros Soumelidis
On the correspondence of hyperbolic geometry and system analysis
published pages: 9285-9290, ISSN: 2405-8963, DOI: 10.1016/j.ifacol.2017.08.917
IFAC-PapersOnLine 50/1 2019-05-27
2018 Patartics Bálint, Péni Tamás, Vanek Bálint
FLEXIBILIS SZÁRNYÚ REPÜLŐGÉP AKTÍV FLATTERSZABÁLYOZÁSA (Hungarian)
published pages: , ISSN: 1789-770X, DOI:
Repüléstudományi Közlemények 2019-05-27
2018 Andrea Iannelli, Andrés Marcos, Mark Lowenberg
Aeroelastic modeling and stability analysis: A robust approach to the flutter problem
published pages: 342-364, ISSN: 1049-8923, DOI: 10.1002/rnc.3878
International Journal of Robust and Nonlinear Control 28/1 2019-05-27
2017 Iannelli, Marcos, Lowenberg
Nonlinear flutter analysis with uncertainties based on Describing Function and Structured Singular Value with an IQC validation
published pages: , ISSN: , DOI: 10.13009/EUCASS2017-90
Proceedings of the 7th European Conference for Aeronautics and Space Sciences (EUCASS 2017)  2019-05-27
2018 Andrea Iannelli, Andrés Marcos, Mark Lowenberg
Study of Flexible Aircraft Body Freedom Flutter with Robustness Tools
published pages: 1083-1094, ISSN: 0731-5090, DOI: 10.2514/1.G003165
Journal of Guidance, Control, and Dynamics 41/5 2019-05-27
2017 Gy. Lipták, T. Luspay, T. Péni, B. Takarics, B. Vanek
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.
published pages: 6344-6349, ISSN: 2405-8963, DOI: 10.1016/j.ifacol.2017.08.1015
IFAC-PapersOnLine 50/1 2019-05-27
2017 Andrea Iannelli, Pedro Simplício, Diego Navarro-Tapia, Andrés Marcos
LFT Modeling and μ Analysis of the Aircraft Landing Benchmark
published pages: 3965-3970, ISSN: 2405-8963, DOI: 10.1016/j.ifacol.2017.08.766
IFAC-PapersOnLine 50/1 2019-05-27
2018 Tamás Luspay, Tamás Péni, István Gőzse, Zoltán Szabó, Bálint Vanek
Model reduction for LPV systems based on approximate modal decomposition
published pages: 891-909, ISSN: 0029-5981, DOI: 10.1002/nme.5692
International Journal for Numerical Methods in Engineering 113/6 2019-05-27
2016 Luspay, T.; Peni, T.; Gozse, I.; Szabo, Z.; Vanek, B.
Model reduction for LPV systems based on approximate modal decomposition
published pages: , ISSN: , DOI:
3 2019-05-27
2017 Andrea Iannelli, Andrés Marcos, Mark Lowenberg
Limit cycle oscillation amplitude tailoring based on describing functions and μ analysis
published pages: 101-119, ISSN: , DOI: 10.1007/978-3-319-65283-2_6
2019-05-27
2018 Andrea Iannelli, Andres Marcos, Mark Lowenberg
Nonlinear Robust Approaches to Study Stability and Postcritical Behavior of an Aeroelastic Plant
published pages: 1-14, ISSN: 1063-6536, DOI: 10.1109/TCST.2017.2779110
IEEE Transactions on Control Systems Technology 2019-05-27
2018 Iannelli, Marcos, Lowenberg
Estimating the region of attraction of uncertain systems with invariant sets
published pages: , ISSN: , DOI:
9th IFAC Symposium on Robust Control Design, ROCOND\'18 2019-05-27
2017 Rozov, V.; Hermanutz, A.; Breitsamter, C.; Hornung, M
Aeroelastic Analysis of a Flutter Demonstrator with a very Flexible High-Aspect-Ratio Swept Wing
published pages: , ISSN: , DOI:
International Forum on Aeroelasticity and Structural Dynamics [IFASD], 2017 28 June 2017 2019-05-24
2017 B. Patartics, T. Luspay, T. Péni, B. Takarics, B. Vanek, T. Kier
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.
published pages: 8163-8168, ISSN: 2405-8963, DOI: 10.1016/j.ifacol.2017.08.1263
IFAC-PapersOnLine 50/1 2019-05-27
2017 Simon Schulz
Aeroelastic control law design using different synthesis methods (Master thesis)
published pages: , ISSN: , DOI:
2019-05-27
2017 Iannelli, Marcos, Lowenberg
Limit cycle oscillation amplitude tailoring based on describing functions and μ analysis
published pages: , ISSN: , DOI:
4th CEAS Specialist Conference on Guidance, Navigation & Control 2019-05-27
2016 Alexander Böhm
Retrospective Cost Adaptive Control of a flexible Aircraft
published pages: , ISSN: , DOI:
Master Thesis 2019-05-24
2016 T. Luspay, T. Peni, I. Gozse, Z. Szabo, B. Vanek
Model reduction for LPV systems based on approximate modal decomposition
published pages: , ISSN: , DOI:
arXiv online repository of scientific papers 2019-05-24
2016 A. Iannelli, A. Marcos, M. Lowenberg
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
published pages: 409-414, ISSN: 2405-8963, DOI: 10.1016/j.ifacol.2016.09.070
IFAC-PapersOnLine 49/17 2019-05-24
2016 Daniel Stein
Condensation of Large 3D FEM Models and Integration in dAEDalus for Fast Dynamic Aeroelastic Analysis
published pages: , ISSN: , DOI:
Master Thesis 2019-05-24

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