Risultati finali
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
Pubblicazioni
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Fernando Puelles
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2022
Editore:
TUM
Autori:
Lawan Nuri Sharif
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2022
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TUM
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Pedro Alexandre Tonet Fleig
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2021
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TUM
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Elias Simon Peter
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2023
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TUM
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Sebastian Lang
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2021
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TUM
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Guthörl Matthias Frank
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2021
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TUM
Autori:
Chang Xu
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2023
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TUM
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Mehdi Hammami
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2021
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TUM
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Olivia Aschermann
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2024
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TUM
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Joschua Gosda
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2022
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TUM
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SAI KIRAN EDIGA
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2023
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TUM
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Kenneth Yhen Hong Leow
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2022
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TUM
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Arturo Gutierrez Munoz
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2023
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TUM
Autori:
Yi Zhan
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2023
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TUM
Autori:
Yuchen Chou
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2024
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TUM
Autori:
Balázs Vidor Huszár
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2023
Editore:
Budapest Univesity Of Technology And Echonomics
Autori:
Chen Xiaohui
Pubblicato in:
2024
Editore:
TUM
Autori:
Bálint Patartics
Pubblicato in:
2022
Editore:
Budapest University of Technology and Economics
Autori:
Tamás Baár
Pubblicato in:
2023
Editore:
Budapest University of Technology and Economics
Autori:
German Nogues Armengol
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2022
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TUM
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Johanna Kärner
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2022
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TUM
Autori:
Bastian Scheufele
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2022
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TUM
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Mohamed El Hedi Letaief
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2024
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TUM
Autori:
Sebastian Lang
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2024
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TUM
Autori:
Zsombor Wermeser
Pubblicato in:
2022
Editore:
Budapest Univesity Of Technology And Echonomics
Autori:
Gribkov Aleksandr
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2023
Editore:
Budapest Univesity Of Technology And Echonomics
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Ákos László Radványi
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2022
Editore:
Budapest Univesity Of Technology And Echonomics
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Martin Löwenhauser
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2022
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TUM
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Marius Weber
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2022
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TUM
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Bastian Scheufele
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2022
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TUM
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Olga Balaska
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2023
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TUM
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2022
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TUM
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Daniel Harlander
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Victor Magalhaes
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2023
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TUM
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Milán Barczi
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2022
Editore:
Budapest Univesity Of Technology And Echonomics
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Marius Weber
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2022
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TUM
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Huang Ching-Ting
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2023
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TUM
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Marius Haag
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2021
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TUM
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Sergio Augustin Gallego
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2022
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TUM
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Bence Zsombor Hadlaczky, Noémi Friedman, Béla Takarics, Balint Vanek
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