Výsledky vyhledávání - "Giovanni MEDICI"

Akademický článek

REVLANSYS: Mission and GNC Design of Terminal Entry and Landing Missions for Advanced Re-Entry Vehicles

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

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Advanced European Re-Entry System Based on Inflatable Heat Shields EFESTO project overview: system and mission design and technology roadmap

Autor: Federico Trovarelli, Giuseppe Guidotti, Giovanni Medici, Thorn Schleutker, Burkard Esser, Ingrid Monika Dietlein, Giovanni Gambacciani, GIUSEPPE GOVERNALE, Jean-Luc Verant, Yann Dauvois, Ysolde Prevereaud

Publikováno v: HAL
D2. IAF space transportation solutions and innovations symposium
72ND INTERNATIONAL ASTRONAUTICAL CONGRESS (IAC 2021)
72ND INTERNATIONAL ASTRONAUTICAL CONGRESS (IAC 2021), Oct 2021, Dubaï, United Arab Emirates. pp.IAC-21-D2.3.1 (x66011)

International audience; European Union H2020 EFESTO project is coordinated by DEIMOS Space with the end goals of improving the European TRL of Inflatable Heat Shields for re-entry vehicles from 3 to 4/5 and pave the way to In-Orbit Demonstration that

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::606db1c0f1236c1f26e01a8c1d8243d3
https://elib.dlr.de/145410/

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Development and validation of on‐board systems control laws

Autor: Sabrina Corpino, Nicole Viola, Giovanni Medici, Marco Fioriti

Publikováno v: Aircraft Engineering and Aerospace Technology. 84:151-161

PurposeThe purpose of this paper is to describe the tool and procedure developed in order to design the control laws of several UAV (Unmanned Aerial Vehicle) sub‐systems. The authors designed and developed the logics governing: landing gear, nose w

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b9b415ce076a4d85f788fc8a83dc8f95
https://doi.org/10.1108/00022661211222003

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Turbojet Steady State and Transient Analytical Model Development and Validation

Autor: Sabrina Corpino, A. Sbuttoni, Sergio Chiesa, M. Balbo, Giovanni Medici

This paper describes the modeling and validation procedure of a single spool Turbojet engine. This work was conducted during the collaboration between Politecnico di Torino and Alenia Aermacchi. The aim of such research is to investigate the performa

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::aefd384d5a2787393ce718951a37f7c6
http://hdl.handle.net/11583/2458641

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