Resultado final
The project coordinator submits an annual progress report to the European Commission, when it does not coincide with the EC mandatory periodic reporting, indicating the status of the project. The structure of this progress report will be the same as that of the periodic report. Task 5.1
Manufacturing design for advanced wingBased on the detailed design of the advanced wing from T26 all manufacturing related tooling design activities are performed This includes design of molds support structures attachment structures as well as data model generation for machining and printing processes
Validation of the integrated design toolchain for collaborative designValidation of the integrated design toolchain for collaborative design based on reengineering of FLEXOP 1 wing characteristics and design
Manufacturing advanced wing and fuselage finalizedThe results of the manufacturing of the advanced wing are finalized Special focus will be given to deviations through the production process versus the initial detail design of the advanced wing The report will include all major characteristic data of the manufactured wing eg mass CoGDue to the accident of the demonstrator several improvements are made to the overall avionics and structural layout of the aircraft The corresponding rebuild steps are described in this deliverable as well
Advanced wing integration and ground test completedBefore closure of the wing structure all relevant systems test equipment wiring sensors and actuators need to integrated and tested A detail description of the final wing buildup and internal layout will be documented as well as results from the initial testing of the integrated equipment Due to the fuselage rebuilt several additional tests are necessary to prove the flight worthiness of the aircraft what are also described in this deliverableThe DD actuator acceptance taxi tests and the GVT for the improved demonstrator under construction are described in this deliverable
"Flight Test Programme - Flight Test Phase #3"A detailed flight test programme is established defining the test objectives means of compliance requirements on specific test procedures to be followed The Flight test programme also specifies abnormal behaviour measures and quality gatesThe deliverable will describe the planned activities for Cochstedt Y23 program
Sensor concept advanced wing finalizedBased on the flight test programme and the formulated means of compliance a detailed sensor concept for the wings as well as for the overall demonstrator are established This includes also the requirements and interface definitions on borad of the demonstrator as well as in the ground control station and the data link equipment
Reference Model DefinitionBased on the expertise of partners a set of models with increasing fidelity will be set up, which provides a foundation for tools, interfaces and parameterization of models. The Flexible Aircraft Benchmark defined within D1.5 will also serve as a basis of the Scale-up (Task 4.1) where different candidate baseline configurations will be defined, and the Design Toolchain from Task 2.6 will be applied to these candidate configurations via the standardized interfaces.
Report on quantified design benefits, as compared with referenceThe report assesses the benefit gained with the developed design process on the scaleup aircraft model
Exploitation and Dissemination PlanExploitation goals of the consortium and the planning of the individual partners will be compiled in the Exploitation and Dissemination Plan. A preliminary version of the Exploitation and Dissemination Plan will be generated mid-project. The general objectives of the dissemination activities are: • to ensure maximum awareness and visibility of the achievements and results of the project particularly in influential aerospace bodies, • to make known new methodologies and standards that could be obtained as a part of the project results and to encourage their use to carry on this line of investigation, • to promote the use of the new technology developed and tested in the project, across companies and institutions who have an interest in flexible aircraft design. Task 5.3
Validation of data science based methods for modelling and controlThis report addresses the aspects of linear parametrized model approximation of dynamical systems in view of control design The modelfree or databased approaches and their application to the flight data specific objectives will be described within the deliverable In this work we are adopting bigdata techniques to analyze the vast data provided by the complex sensing and control system These methodologies are useful in mapping and revealing the underlying structure of the problem Data science technologies for optimal usage of these data are developed in FliPASED and recommendations for methods and useful sensor arrangements for future aerospace applications are described
Report on flight control system layoutReport describing the flight control architecture and structure. This control structure will address the complete integrated avionic process including aircraft shape, sensors and actuator locations and detailed control design. The aim of the report is more to detail the structure and tuning variables rather than the methodology employed to adjust them. This latter will serve as baseline for developments of WP2 activities
Scale-up design objectivesCaptures and describes the design objectives for the scaleup study
Scale-up aircraft re-design and control system lay-outControl system layout to be used in the scaleup aircraft model The parameters will be optimized within the MDO process
"Flight Test Programme – Flight Test Phase #1"A detailed flight test programme is established defining the test objectives, means of compliance, requirements on specific test procedures to be followed. The Flight test programme also specifies abnormal behaviour measures and quality gates.
Wing and demonstrator actuation and sensing conceptual design requirementsThe deliverable will capture the requirements related to the attainement of proposed project goals. To be able to demonstrate wing shape control the shape of the wing has to be estimated and proper actuators with the adequate flight control surfaces have to be placed on the aircraft. The rationale behind the conceptual design requirements will be documented in D1.1.
Standardization recommendations for data and model databases and toolsBased on the lessons learnt during the adaptation of tools in WP2 and their successful application to the demonstrator platform WP3 and to the scaleup task WP4 the recommendations for an iterative modelling framework will be established and formally defined in D17 Data from aircraft design scaleup simulation and flight test data will be assembled into a logical format with recommendations how to standardize the corresponding output analysis and design pairs respecting their interdependency
Data management planThe DMP will provide guidelines for the project partners with regard to all the datasets that will be generated within the project. The DMP will address the naming conventions, description of datasets, standards and metadata, and data sharing properties on a dataset by dataset basis. The DMP will be updated reflecting the current status of view on the data that will be produced, evolving during the lifespan of the project. Task 5.1
24 month Progress ReportThe project coordinator submits an annual progress report to the European Commission when it does not coincide with the EC mandatory periodic reporting indicating the status of the project The structure of this progress report will be the same as that of the periodic reportTask 51
Analytical redundancy methodsIn order to achieve the project goals with a reliable avionics architecture the already installed sensor and actuator settings will be used in a novel to define input and output blending, as well as novel sensor and actuator fusion to provide fault tolerance. In addition, the challenging and open problem of optimal sensor/actuator selections is investigated in relation to the novel movables design. The document will describe the proposed FDIR and sensor-actuator selection methods and their application to the demonstrator aircraft configuration
Final ReportThe project coordinator submits a final report to the European Commission covering the whole lifspan of the project while the 2nd periodic report which will be submitted at the same time will only cover the period M19M36 The structure of this progress report will be the same as that of the periodic report The report will be submitted after the closure of the project aligned with H2020 regulation
Demonstrator ground and flight test requirements definitionTo be able to demonstrate the proposed innovative ac design cycle the flight test will have to provide sufficiently rich information for both iterative refinement of tools and methods and proof about their performance According to the project objectives the ground and flight test requirements will be documented in D13 to be aligned with the remaining workpackages
"Flight Test Programme - Flight Test Phase #2"A detailed flight test programme is established defining the test objectives means of compliance requirements on specific test procedures to be followed The Flight test programme also specifies abnormal behaviour measures and quality gates
Requirements capture for a/c MDO designThe requirements for Integrated, Collaborative Design Tool Chain are developed first within D1.2, since that lays the foundation of the experimental and analytical research within the project. The aircraft sizing cycle has to fulfil various constraints, while optimizing fuel consumption and passenger comfort, to name a few. So their tradeoff and the required fidelity in the preliminary design stage are described in the deliverable, including the proposed way to incorporate novel steps within the MDO cycle - including control system parameters.
"Flight Test Report - Flight Test Phase #3"Based on the Flight Test programme for the specific flight test campaign the test conditions eg wheather aircraft configuration CoG weight will be documented as well as occurances or abnomalies during the conducted test flight Flight test data will decribed with respect to formats correction factors etcThe document will describe the two consecutive flight test campaigns of Y23 at DLR Cochstedt
Data Analytics for Model ValidationThe data from flight tests will serve as a baseline to validate structural dynamics aerodynamics controls and avionics instrumentation models Analysis tools with standard validation routines will be provided in Nastran and Matlab environment for structural dynamics and controls respectively These tools along with Python based data science software will be used within the project and the underlying theory along with interfaces of these tools will be documented in D16
"Flight Test Report - Flight Test Phase #2"Based on the Flight Test programme for the specific flight test campaign the test conditions eg wheather aircraft configuration CoG weight will be documented as well as occurances or abnomalies during the conducted test flight Flight test data will decribed with respect to formats correction factors etcThe deliverable will describe the flights conducted in the test campaigns during Y22
Information and interfaces definition for Collaborative Work ProcessThe interdisciplinary teams within the project will share models data and tools among them D14 formalizes these steps within the iteration loops and establishes a document to define their interdependency and their standard interfaces CAD NASTRAN Dymola MatlabSimulink embedded C code
"Flight Test Report - Flight Test Phase #1"Based on the Flight Test programme for the specific flight test campaign the test conditions eg wheather aircraft configuration CoG weight will be documented as well as occurances or abnomalies during the conducted test flight Flight test data will decribed with respect to formats correction factors etc
Aero-servo-structural design of the new advanced FliPASED wingThis report addresses the way to construct an Aeroservostructural design of the new advanced FliPASED wing
Report on tool adaptation for collaborative designThe report will consider at first the construction of parametrized structural model using CAD and FEM methods. Then, as a second step, the generation of reduced and parametric dynamical models, tailored to the analysis and the control design will be done. The purpose is to define an approach to bridge the gap between accurate and complex to accurate and simple models.
The project website will provide information on basic project information, partners, publications, links and contact information. Mathematical models of the demonstrator developed for aircraft design will be posted on the project website, together with ground and flight test data of various aircraft configurations, to provide a benchmark for the entire community. Project news will be posted on Linkedin. Task 5.1 and 5.2
Workshop / Final Exploitation and Dissemination ReportOrganization of an International Workshop on Interdisciplinary Design Principles for Flexible Wing Aircraft Technology to be held and open to worldwide experts in the area and EU graduate students Final Exploitation and Dissemination Report Exploitation goals of the consortium and the planning of the individual partners will be compiled in the Exploitation and Dissemination Plan A preliminary version of the Exploitation and Dissemination Plan will be generated midproject The general objectives of the dissemination activities are to ensure maximum awareness and visibility of the achievements and results of the project particularly in influential aerospace bodiesto make known new methodologies and standards that could be obtained as a part of the project results and to encourage their use to carry on this line of investigationto promote the use of the new technology developed and tested in the project across companies and institutions who have an interest in flexible aircraft designTask 53
The flight test data generated within the project will be published according to the standards of the Open Research Data Pilot The deliverable is tightly coupled with the flight test reports and feeds into the public dissemination workshop at the end of the project The initial release will be done at M39 but the data repository will be populated as we proceed with the ground and flight test campaigns and with the scaleup
Publicaciones
Autores:
Fernando Puelles
Publicado en:
2022
Editor:
TUM
Autores:
Lawan Nuri Sharif
Publicado en:
2022
Editor:
TUM
Autores:
Pedro Alexandre Tonet Fleig
Publicado en:
2021
Editor:
TUM
Autores:
Elias Simon Peter
Publicado en:
2023
Editor:
TUM
Autores:
Sebastian Lang
Publicado en:
2021
Editor:
TUM
Autores:
Guthörl Matthias Frank
Publicado en:
2021
Editor:
TUM
Autores:
Chang Xu
Publicado en:
2023
Editor:
TUM
Autores:
Mehdi Hammami
Publicado en:
2021
Editor:
TUM
Autores:
Olivia Aschermann
Publicado en:
2024
Editor:
TUM
Autores:
Joschua Gosda
Publicado en:
2022
Editor:
TUM
Autores:
SAI KIRAN EDIGA
Publicado en:
2023
Editor:
TUM
Autores:
Kenneth Yhen Hong Leow
Publicado en:
2022
Editor:
TUM
Autores:
Arturo Gutierrez Munoz
Publicado en:
2023
Editor:
TUM
Autores:
Yi Zhan
Publicado en:
2023
Editor:
TUM
Autores:
Yuchen Chou
Publicado en:
2024
Editor:
TUM
Autores:
Balázs Vidor Huszár
Publicado en:
2023
Editor:
Budapest Univesity Of Technology And Echonomics
Autores:
Chen Xiaohui
Publicado en:
2024
Editor:
TUM
Autores:
Bálint Patartics
Publicado en:
2022
Editor:
Budapest University of Technology and Economics
Autores:
Tamás Baár
Publicado en:
2023
Editor:
Budapest University of Technology and Economics
Autores:
German Nogues Armengol
Publicado en:
2022
Editor:
TUM
Autores:
Johanna Kärner
Publicado en:
2022
Editor:
TUM
Autores:
Bastian Scheufele
Publicado en:
2022
Editor:
TUM
Autores:
Mohamed El Hedi Letaief
Publicado en:
2024
Editor:
TUM
Autores:
Sebastian Lang
Publicado en:
2024
Editor:
TUM
Autores:
Zsombor Wermeser
Publicado en:
2022
Editor:
Budapest Univesity Of Technology And Echonomics
Autores:
Gribkov Aleksandr
Publicado en:
2023
Editor:
Budapest Univesity Of Technology And Echonomics
Autores:
Ákos László Radványi
Publicado en:
2022
Editor:
Budapest Univesity Of Technology And Echonomics
Autores:
Martin Löwenhauser
Publicado en:
2022
Editor:
TUM
Autores:
Marius Weber
Publicado en:
2022
Editor:
TUM
Autores:
Bastian Scheufele
Publicado en:
2022
Editor:
TUM
Autores:
Olga Balaska
Publicado en:
2023
Editor:
TUM
Autores:
Annina Metzner
Publicado en:
2022
Editor:
TUM
Autores:
Simon Schelle
Publicado en:
2022
Editor:
TUM
Autores:
Daniel Harlander
Publicado en:
2021
Editor:
TUM
Autores:
Victor Magalhaes
Publicado en:
2023
Editor:
TUM
Autores:
Milán Barczi
Publicado en:
2022
Editor:
Budapest Univesity Of Technology And Echonomics
Autores:
Marius Weber
Publicado en:
2022
Editor:
TUM
Autores:
Huang Ching-Ting
Publicado en:
2023
Editor:
TUM
Autores:
Marius Haag
Publicado en:
2021
Editor:
TUM
Autores:
Sergio Augustin Gallego
Publicado en:
2022
Editor:
TUM
Autores:
Bence Zsombor Hadlaczky, Noémi Friedman, Béla Takarics, Balint Vanek
Publicado en:
Proceedings of The 5th Annual Learning for Dynamics and Control Conference, Edición 211, 2023, Página(s) 1429-1440
Editor:
PMLR
Autores:
Thiemo M. Kier
Publicado en:
AIAA SCITECH 2023 Forum, 2023
Editor:
American Institute of Aeronautics and Astronautics, Inc.
DOI:
10.2514/6.2023-0177
Autores:
Özge Süelözgen
Publicado en:
AIAA SCITECH 2022 Forum, 2021
Editor:
American Institute of Aeronautics and Astronautics, Inc.
DOI:
10.2514/6.2022-0725
Autores:
Julius Bartasevicius, Sebastian J. Koeberle, Daniel Teubl, Christian Roessler, Mirko Hornung
Publicado en:
Proceedings of the 32nd Congress of the International Council of the Aeronautical Sciences (ICAS2021), Edición Biannual conference, 2021
Editor:
ICAS
Autores:
S. Olasz-Szabó, T. Baár, T.Luspay
Publicado en:
EURO GNC 2022, 2022
Editor:
CEAS
Autores:
Matthias Wustenhagen, Ozge Suelozgen, Lukas Ackermann, Julius Bartasevicius
Publicado en:
2021 IEEE Aerospace Conference (50100), 2021, Página(s) 1-18, ISBN 978-1-7281-7436-5
Editor:
IEEE
DOI:
10.1109/aero50100.2021.9438354
Autores:
Soal, Keith Ian and Nagy, Mihaly and Teubl, Daniel and Volkmar, Robin and Thiem, Carsten and Meddaikar, Muhammad Yasser and Vanek, B. and Govers, Yves and Böswald, Marc
Publicado en:
30th International Conference on Noise and Vibration Engineering, ISMA 2022, 2022
Editor:
ISMA
Autores:
Fanglin Yu; Julius Bartasevicius; Mirko Hornung
Publicado en:
ICAS PROCEEDINGS 33th Congress of the International Council of the Aeronautical Sciences, Edición Biannual conference, 2022
Editor:
International Council of the Aeronautical Sciences
DOI:
10.6084/m9.figshare.21656960
Autores:
Ábel OLGYAY, Béla TAKARICS, Bence KÖRÖSPARTI, János LELKES, Csaba HORVÁTH, Bálint VANEK
Publicado en:
The 18th International Conference on Fluid Flow Technologies, 2022
Editor:
CMFF
Autores:
Keith Soal, Robin Volkmar, Carsten Thiem, Julian Sinske, Yasser M. Meddaikar, Yves Govers, Marc Böswald, Daniel Teubl, Julius Bartasevicius, Mihaly Nagy and Balint Vanek
Publicado en:
AIAA SCITECH 2023 Forum, 2023
Editor:
American Institute of Aeronautics and Astronautics, Inc.
DOI:
10.2514/6.2023-0373
Autores:
Janos Bezsilla, Bela Takarics, Balint Vanek, Jian Guo
Publicado en:
IFAC MATHMOD 2022, 2022
Editor:
Vienna, Austria
DOI:
10.1016/j.ifacol.2022.09.102
Autores:
Özge Süelözgen
Publicado en:
AIAA SCITECH 2023 Forum, 2023
Editor:
American Institute of Aeronautics and Astronautics, Inc.
DOI:
10.2514/6.2023-0374
Autores:
Matthias Wustenhagen
Publicado en:
International Forum on Aeroelasticity and Structural Dynamics IFASD 2022, 2022
Editor:
Organization Committee of IFASD 2021
Autores:
Julius Bartasevicius, Mirko Hornung
Publicado en:
SFTE International Symposium 2023, 2023
Editor:
SFTE
Autores:
Özge Süelözgen, Gertjan Looye
Publicado en:
19th International Forum on Aeroelasticity and Structural Dynamics (IFASD 2022), 2022
Editor:
Organization Committee of IFASD 2021
Autores:
Julius Bartasevicius, Mirko Hornung
Publicado en:
AIAA SCITECH 2023 Forum, 2023
Editor:
American Institute of Aeronautics and Astronautics, Inc.
DOI:
10.2514/6.2023-0372
Autores:
Julius Bartasevicius, Pedro A. Fleig, Annina Metzner and Mirko Hornung
Publicado en:
AIAA SCITECH 2022 Forum, 2021
Editor:
American Institute of Aeronautics and Astronautics, Inc.
DOI:
10.2514/6.2022-1827
Autores:
Tamás Baár, Tamás Luspay
Publicado en:
2021 60th IEEE Conference on Decision and Control (CDC), 2022, ISBN 978-1-6654-3659-5
Editor:
IEEE
DOI:
10.1109/cdc45484.2021.9683413
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Matthias Wuestenhagen
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AIAA SCITECH 2022 Forum, 2021
Editor:
American Institute of Aeronautics and Astronautics, Inc.
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10.2514/6.2022-0440
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B Hadlaczky, N Friedman, B Takarics, B Vanek
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19th International Forum on Aeroelasticity and Structural Dynamics (IFASD 2022), 2022
Editor:
Organization Committee of IFASD 2021
Autores:
Matthias Wüstenhagen
Publicado en:
AIAA SCITECH 2023 Forum, 2023
Editor:
American Institute of Aeronautics and Astronautics, Inc.
DOI:
10.2514/6.2023-0371
Autores:
Thiemo Kier
Publicado en:
19th International Forum on Aeroelasticity and Structural Dynamics (IFASD 2022), 2022
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Organization Committee of IFASD 2021
Autores:
Béla Takarics, Bálint Patartics, Tamás Luspay, Balint Vanek, Charles Poussot-Vassal, Pierre Vuillemin and Matthias Wuestenhagen
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AIAA SCITECH 2023 Forum, 2023
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American Institute of Aeronautics and Astronautics, Inc.
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10.2514/6.2023-0175
Autores:
Yasser M. Meddaikar, Thiemo M. Kier, Julius Bartasevicius, Fanglin Yu, Balint Vanek, Abel Olgyay and Béla Takarics
Publicado en:
AIAA SCITECH 2023 Forum, 2023
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American Institute of Aeronautics and Astronautics, Inc.
DOI:
10.2514/6.2023-0176
Autores:
Balint Patartics, Yagiz Kumtepe, Bela Takarics, Balint Vanek
Publicado en:
IFAC-PapersOnLine, Edición 54/20, 2021, Página(s) 663-668, ISSN 2405-8963
Editor:
Elsevier
DOI:
10.1016/j.ifacol.2021.11.247
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Réka Dóra Mocsányi, Béla Takarics, Bálint Vanek
Publicado en:
IFAC-PapersOnLine, Edición 53/2, 2020, Página(s) 5725-5730, ISSN 2405-8963
Editor:
Elsievier
DOI:
10.1016/j.ifacol.2020.12.1600
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Peter Bauer, Lysandros Anastasopoulos, Franz-Michael Sendner, Mirko Hornung, Balint Vanek
Publicado en:
Journal of Intelligent & Robotic Systems, Edición 100/1, 2020, Página(s) 259-287, ISSN 0921-0296
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Kluwer Academic Publishers
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10.1007/s10846-020-01204-1
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Réka Dóra Mocsányi, Béla Takarics, Bálint Vanek
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IFAC-PapersOnLine, Edición 54/12, 2021, Página(s) 26-31, ISSN 2405-8963
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Elsevier
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10.1016/j.ifacol.2021.11.005
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Bálint Patartics, Bálint Vanek
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IFAC-PapersOnLine, Edición 55/6, 2022, Página(s) 603-610, ISSN 2405-8963
Editor:
Elsevier
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10.1016/j.ifacol.2022.07.194
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Balint Patartics, Gyorgy Liptak, Tamas Luspay, Peter Seiler, Bela Takarics, Balint Vanek
Publicado en:
IEEE Transactions on Control Systems Technology, 2021, Página(s) 1-15, ISSN 1063-6536
Editor:
Institute of Electrical and Electronics Engineers
DOI:
10.1109/tcst.2021.3066096
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Béla Takarics and Balint Vanek
Publicado en:
Asian Journal of Control, Edición Published six times a year, 2021, Página(s) 1-11, ISSN 1934-6093
Editor:
Wiley
DOI:
10.1002/asjc.2547
Autores:
Réka Dóra Mocsányi, Béla Takarics, Aditya Kotikalpudi, Bálint Vanek
Publicado en:
Fluids, Edición 5/2, 2020, Página(s) 47, ISSN 2311-5521
Editor:
MDPI
DOI:
10.3390/fluids5020047
Autores:
B Patartics, P Seiler, B Takarics, B Vanek
Publicado en:
IEEE Transactions on Control Systems Technology, Edición 31/1, 2022, Página(s) 155 - 165, ISSN 1063-6536
Editor:
Institute of Electrical and Electronics Engineers
DOI:
10.1109/tcst.2022.3173044
Autores:
B Patartics, P Seiler, J Carrasco, B Vanek
Publicado en:
IEEE Control Systems Letters, Edición 6, 2022, Página(s) 2605 - 2610, ISSN 2475-1456
Editor:
IEEE
DOI:
10.1109/lcsys.2022.3171707
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Tamás Baár, Tamás Luspay
Publicado en:
International Journal of Robust and Nonlinear Control, Edición 32/11, 2023, Página(s) 6086-6109, ISSN 1099-1239
Editor:
John Wiley & Sons Ltd
DOI:
10.1002/rnc.6141
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