Explore the words cloud of the FLiPASED project. It provides you a very rough idea of what is the project "FLiPASED" about.
The following table provides information about the project.
MAGYAR TUDOMANYOS AKADEMIA SZAMITASTECHNIKAI ES AUTOMATIZALASI KUTATOINTEZET
|Coordinator Country||Hungary [HU]|
|Total cost||3˙846˙245 €|
|EC max contribution||3˙846˙245 € (100%)|
1. H2020-EU.3.4. (SOCIETAL CHALLENGES - Smart, Green And Integrated Transport)
|Duration (year-month-day)||from 2019-09-01 to 2022-12-31|
Take a look of project's partnership.
|1||MAGYAR TUDOMANYOS AKADEMIA SZAMITASTECHNIKAI ES AUTOMATIZALASI KUTATOINTEZET||HU (BUDAPEST)||coordinator||1˙066˙875.00|
|2||TECHNISCHE UNIVERSITAET MUENCHEN||DE (MUENCHEN)||participant||1˙235˙375.00|
|3||DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV||DE (KOELN)||participant||941˙495.00|
|4||OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES||FR (PALAISEAU)||participant||602˙500.00|
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.