Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Cristina Recupero"'
Autor:
Antonio RUSSO, Alina IONITA, Fernando PINA CABALLERO, Giovanni MEDICI, Cristina RECUPERO, Gabriele DE ZAIACOMO, Murray KERR, Celia YABAR VALLES
Publikováno v:
INCAS Bulletin, Vol 10, Iss 2, Pp 75-90 (2018)
The ESA REVLANSYS study aims to develop key technologies in the field of Mission Engineering and GNC for autonomous re-entry vehicles, and to derive coherent mission, system and GNC requirements for the specific terminal entry and landing phases. As
Externí odkaz:
https://doaj.org/article/b68e5ac52c4943429e8826847bfb6fd7
Launcher reusability is the most effective way of reducing access to space costs, but remains a great technical challenge for the European aerospace industry. One of the challenges lies in the recovery GNC strategy and algorithms, in particular those
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e10e4c770cb5c1fccc644f0338ba04e5
https://zenodo.org/record/6205683
https://zenodo.org/record/6205683
Publikováno v:
CEAS Space Journal
Autor:
Josep Boada-Bauxell, Cristina Recupero, Murray Kerr, Vicente Fernández, Javier Montaño, Laurent Dalbies, Paulo Rosa
Publikováno v:
IFAC-PapersOnLine. 48:1006-1011
The RECONFIGURE Functional Engineering Simulator (FES) is a simulation software tool based on the MATLAB°/Simulink° modeling & simulation environment, specifically designed to support the industrial verification and benchmarking of the Fault Detect
Publikováno v:
2016 3rd Conference on Control and Fault-Tolerant Systems (SysTol).
This paper presents an overview of the preliminary results and contributions of the European Union 7th Framework Program (FP7) project RECONFIGURE (REconfiguration of CONtrol in Flight for Integral Global Upset REcovery). The RECONFIGURE project ran
Publikováno v:
2016 3rd Conference on Control and Fault-Tolerant Systems (SysTol).
This paper describes the maturation and in-flight testing of a recently developed fault detection (FD) system for a model scale unmanned aerial vehicle (UAV). The FD system design methodology is based on H techniques and exploits an LFT description o