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FLiPASED SIGNED

FLIGHT PHASE ADAPTIVE AERO-SERVO-ELASTIC AIRCRAFT DESIGN METHODS

Total Cost €

EC-Contrib. €

Partnership

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FLiPASED project word cloud

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

50 instrumentation lower improvement aeroelastic dimension mode accurate separately aerodynamics cycle tightly validated simulation weight goals affordable avionics of fuel aircraft detection safe collaborative servo 10 coupling source synthesis reconfiguration optimized becomes optimization flight designs tool gust entire disciplines aero chain enhanced coupled toolchains flipased wing multidisciplinary adaptive life elastic standardized efficiency experimental tools amplitude fault consideration context accuracy 20 complete opens structural joint certification flexible active shared integration advantage models platform former performance exploited feasible peak interfaces aeroelasticity discipline

Project "FLiPASED" 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]
Total cost	3˙846˙245 €
EC max contribution	3˙846˙245 € (100%)
Programme	1. H2020-EU.3.4. (SOCIETAL CHALLENGES - Smart, Green And Integrated Transport)
Code Call	H2020-MG-2018-TwoStages
Funding Scheme	RIA
Starting year	2019
Duration (year-month-day)	from 2019-09-01 to 2022-12-31

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	1˙066˙875.00
2	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˙235˙375.00
3	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	941˙495.00
4	OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES Organization address address: CHEMIN DE LA HUNIERE city: PALAISEAU postcode: 91120 website: www.onera.fr contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	FR (PALAISEAU)	participant	602˙500.00

Map

Project objective

Flight Phase Adaptive Aero-Servo-Elastic Aircraft Design Methods (FliPASED) opens a complete new dimension for the integrated aircraft design. Coupling between aeroelasticity, gust response, flight control methods, instrumentation and certification aspects is not exploited in current aircraft design. A common set of models, coupled with joint requirements enable a multidisciplinary-optimized design for the entire aircraft, leading to more optimized overall performance. The concept of exploiting coupling between disciplines will take advantage of tools developed by the partners in former projects. The main objectives of the proposal aim at tightly coupled multi-objective optimization of advanced, active controlled wing designs through the integration of a collaborative design tool chain. More than 10% fuel efficiency improvement, and 20% reduction in peak amplitude of the gust response, as well as a 50% reduction of number of distinct models used during the development and certification process are set as project goals. Through the integration of all discipline tools from aerodynamics, structural design, aeroelastic simulation and control design in one integrated tool chain an active, condition optimized wing design becomes feasible, enabling enhanced performance at lower weight and cost. The project will raise the efficiency of a currently separately existing development toolchains, by advanced multidisciplinary and collaborative capabilities for whole aircraft along its life cycle. It will develop methods and tools for very accurate flexible-mode modelling and flexible aircraft control synthesis, in the context of reliable implementation of the avionics system, taking into consideration the fault detection and reconfiguration. The accuracy of developed tools and methods will be validated on a safe and affordable experimental platform, and results will be shared along with design requirements and standardized interfaces in an open source approach.

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The information about "FLIPASED" are provided by the European Opendata Portal: CORDIS opendata.