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FLEXOP SIGNED

Flutter Free FLight Envelope eXpansion for ecOnomical Performance improvement

Total Cost €

EC-Contrib. €

Partnership

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Outcomes and
results

FLEXOP project word cloud

Explore the words cloud of the FLEXOP project. It provides you a very rough idea of what is the project "FLEXOP" about.

preliminary weight excess unviable certification benchmark efficient synthesis transport efficiency baseline validation tailoring experimental carry flight followed technological risk aeroelasticity airspeed data adapt gain verification standards establishing multidisciplinary flexop accuracy aeroelastic website outlining inter disciplines modifications interdisciplinary redesigned operation modeling aerospace coupling disciplinary cycle stretched serve manufacturers discovered designs platform markets validating posted fly affordable explore opens performance aircraft accurate demonstrating closer derivative competitiveness flexible tools structural wing span previously community demonstrators flutter

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 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.	HU (BUDAPEST)	coordinator	980˙801.00
2	FISCHER ADVANCED COMPOSITE COMPONENTS AGFACC AG FISCHER ADVANCED COMPOSITE COMPONENTS AGFACC AG Organization address address: FISCHERSTRASSE city: RIED IM INNKREIS postcode: 4910 website: www.facc.co.at contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	AT (RIED IM INNKREIS)	participant	1˙177˙444.00
3	TECHNISCHE UNIVERSITAET MUENCHEN TECHNISCHE UNIVERSITAET MUENCHEN Organization address address: Arcisstrasse 21 city: MUENCHEN postcode: 80333 website: www.tu-muenchen.de contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	DE (MUENCHEN)	participant	1˙129˙835.00
4	AIRBUS DEFENCE AND SPACE GMBH AIRBUS DEFENCE AND SPACE GMBH Organization address address: WILLY-MESSERSCHMITT-STRASSE 1 city: TAUFKIRCHEN postcode: 82024 website: www.airbus-group.com contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	DE (TAUFKIRCHEN)	participant	895˙563.00
5	DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV Organization address address: Linder Hoehe city: KOELN postcode: 51147 website: www.dlr.de contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	DE (KOELN)	participant	735˙453.00
6	UNIVERSITY OF BRISTOL UNIVERSITY OF BRISTOL Organization address address: BEACON HOUSE QUEENS ROAD city: BRISTOL postcode: BS8 1QU website: www.bristol.ac.uk contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	UK (BRISTOL)	participant	643˙468.00
7	INASCO HELLAS ETAIREIA EFARMOSMENON AERODIASTIMIKON EPISTIMON EE INASCO HELLAS ETAIREIA EFARMOSMENON AERODIASTIMIKON EPISTIMON EE Organization address address: NAPOLEONTOS ZERVA 18 city: GLYFADA ATHINA postcode: 16675 website: www.inasco.com contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	EL (GLYFADA ATHINA)	participant	528˙532.00
8	AIRBUS GROUP LIMITED AIRBUS GROUP LIMITED Organization address address: WELLINGTON HOUSE 125 130 STRAND city: LONDON postcode: WC2R 0AP website: n.a. contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	UK (LONDON)	participant	282˙150.00
9	TECHNISCHE UNIVERSITEIT DELFT TECHNISCHE UNIVERSITEIT DELFT Organization address address: STEVINWEG 1 city: DELFT postcode: 2628 CN website: www.tudelft.nl contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	NL (DELFT)	participant	223˙378.00
10	RHEINISCH-WESTFAELISCHE TECHNISCHE HOCHSCHULE AACHEN RHEINISCH-WESTFAELISCHE TECHNISCHE HOCHSCHULE AACHEN Organization address address: TEMPLERGRABEN 55 city: AACHEN postcode: 52062 website: www.rwth-aachen.de contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	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

List of publications.
year	authors and title	journal	last update
2019	SÃ¼elÃ¶zgen, Ã–zge and WÃ¼stenhagen, 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, AndrÃ©s 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, AndrÃ©s 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	SÃ©rgio Waitman, AndrÃ©s Marcos Active flutter suppression: non-structured and structured Hâˆž 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, AndrÃ©s 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	SÃ©rgio Waitman, AndrÃ©s Marcos Hâˆž 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, TamÃ¡s 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	IstvÃ¡n GÅ‘zse, TamÃ¡s PÃ©ni, TamÃ¡s 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 BÃ¡lint, PÃ©ni TamÃ¡s, Vanek BÃ¡lint FLEXIBILIS SZÃRNYÃš REPÃœLÅGÃ‰P AKTÃV FLATTERSZABÃLYOZÃSA (Hungarian) published pages: , ISSN: 1789-770X, DOI:	RepÃ¼lÃ©studomÃ¡nyi KÃ¶zlemÃ©nyek	2019-05-27
2018	Andrea Iannelli, AndrÃ©s 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)Â	2019-05-27
2018	Andrea Iannelli, AndrÃ©s 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. LiptÃ¡k, T. Luspay, T. PÃ©ni, 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 SimplÃcio, Diego Navarro-Tapia, AndrÃ©s Marcos LFT Modeling and Î¼ 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	TamÃ¡s Luspay, TamÃ¡s PÃ©ni, IstvÃ¡n GÅ‘zse, ZoltÃ¡n SzabÃ³, BÃ¡lint 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, AndrÃ©s Marcos, Mark Lowenberg Limit cycle oscillation amplitude tailoring based on describing functions and Î¼ 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. PÃ©ni, 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 Î¼ analysis published pages: , ISSN: , DOI:	4th CEAS Specialist Conference on Guidance, Navigation & Control	2019-05-27
2016	Alexander BÃ¶hm 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 Unionâ€™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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