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Your search keyword '"Alimenti, F."' showing total 251 results
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251 results on '"Alimenti, F."'

1. Wireless Harmonic Transponder Based on Piezo-Varactor Direct Phase Modulation

Author

Simoncini, G., Cicioni, G., Salvati, R., Palazzi, V., Schiavolini, G., Orecchini, G., Alimenti, F., Mezzanotte, P., Roselli, L., Angrisani, Leopoldo, Series Editor, Arteaga, Marco, Series Editor, Panigrahi, Bijaya Ketan, Series Editor, Chakraborty, Samarjit, Series Editor, Chen, Jiming, Series Editor, Chen, Shanben, Series Editor, Chen, Tan Kay, Series Editor, Dillmann, Rüdiger, Series Editor, Duan, Haibin, Series Editor, Ferrari, Gianluigi, Series Editor, Ferre, Manuel, Series Editor, Hirche, Sandra, Series Editor, Jabbari, Faryar, Series Editor, Jia, Limin, Series Editor, Kacprzyk, Janusz, Series Editor, Khamis, Alaa, Series Editor, Kroeger, Torsten, Series Editor, Li, Yong, Series Editor, Liang, Qilian, Series Editor, Martín, Ferran, Series Editor, Ming, Tan Cher, Series Editor, Minker, Wolfgang, Series Editor, Misra, Pradeep, Series Editor, Möller, Sebastian, Series Editor, Mukhopadhyay, Subhas, Series Editor, Ning, Cun-Zheng, Series Editor, Nishida, Toyoaki, Series Editor, Oneto, Luca, Series Editor, Pascucci, Federica, Series Editor, Qin, Yong, Series Editor, Seng, Gan Woon, Series Editor, Speidel, Joachim, Series Editor, Veiga, Germano, Series Editor, Wu, Haitao, Series Editor, Zamboni, Walter, Series Editor, Zhang, Junjie James, Series Editor, Cocorullo, Giuseppe, editor, Crupi, Felice, editor, and Limiti, Ernesto, editor

Published
2023
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5. Low-Noise Ku-band Receiver Frontend with Switchable SIW filters for Cubesat Applications

Author

Orecchini, G., primary, Schiavolini, G., additional, Mezzanotte, P., additional, Pauletto, S., additional, Loppi, A., additional, Beltramello, A., additional, Dogo, F., additional, Mania, D., additional, Palazzi, V., additional, Simoncini, G., additional, Roselli, L., additional, Gregorio, A., additional, Fragiacomo, M., additional, and Alimenti, F., additional

Published
2022
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14. A Ka-band Transceiver for Cubesat Satellites: Feasibility Study and Prototype Development

Author

Cuttin, A., Alimenti, F., Coromina, F., De Fazio, E., Dogo, F., Fragiacomo, M., Gervasoni, P., Gotti, G., Gregorio, A., Mezzanotte, P., Pagana, E., Palazzi, V., Pelusi, F., Pergolesi, F., Petrini, P., Roselli, L., Vincenti Gatti, R., European Microwave Association, Cuttin, A., Alimenti, F., Coromina, F., De Fazio, E., Dogo, F., Fragiacomo, M., Gervasoni, P., Gotti, G., Gregorio, A., Mezzanotte, P., Pagana, E., Palazzi, V., Pelusi, F., Petrini, P., Roselli, L., and Gatti, R. Vincenti

Subjects
Earth observation, satellite systems, Computer Networks and Communications, Computer science, 0211 other engineering and technologies, satellite system, 02 engineering and technology, satellite communications, Ka-band, nano-satellites, cubesat, satellite systems, satellite communication, 0202 electrical engineering, electronic engineering, information engineering, CubeSat, Ka band, satellite communications, Instrumentation, 021101 geological & geomatics engineering, Transponder, Radiation, business.industry, Electrical engineering, nano-satellite, nano-satellites, 020206 networking & telecommunications, Ka-band, Computer Networks and Communication, visual_art, Electronic component, visual_art.visual_art_medium, Communications satellite, Satellite, Transceiver, business, cubesat
Abstract

This paper describes the feasibility study of a Ka-band transceiver specifically designed for small satellite and CubeSat operations. The transponder is conceived to ensure up to 100 Mbit s-1 data rate with a target power consumption of 20W and an overall volume of 1.5U, not including the antenna. To keep the cost as low as possible, commercial, off-the-shelf electronic components are used whenever possible. Exploiting a data communication interface like the one proposed, the small satellites market could be opened to new applications such as remote sensing, Earth observation and commercial telecommunications.

Published
2018

19. A Ka-Band Transceiver for CubeSat Satellites: Feasibility Study and Prototype Development

Author

Cuttin, A., primary, Alimenti, F., additional, Coromina, F., additional, De Fazio, E., additional, Dogo, F., additional, Fragiacomo, M., additional, Gervasoni, P., additional, Gotti, G., additional, Gregorio, A., additional, Mezzanotte, P., additional, Pagana, E., additional, Palazzi, V., additional, Pelusi, F., additional, Petrini, P., additional, Roselli, L., additional, and Gatti, R. Vincenti, additional

Published
2018
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20. Europe and the future for WPT COST action IC1301 team

Author

Carvalho,NB, Georgiadis,A, Costanzo,A, Stevens,N, Kracek,J, Luís Manuel Pessoa, Roselli,L, Dualibe,F, Schreurs,D, Mutlu,S, Rogier,H, Visser,H, Takacs,A, Rocca,P, Dimitriou,A, Michalski,J, Raida,Z, Tedjini,S, Joseph,W, Duroc,Y, Sahalos,JN, Bletsas,A, Samaras,T, Nikoletseas,S, Raptis,TP, Boaventura,A, Collado,A, Trevisan,R, Minnaert,B, Svanda,M, Pereira,M, Mongiardo,M, Popov,G, Pan,N, Aubert,H, Viani,F, Siachalou,S, Kant,P, Vera,GA, Polycarpou,AC, Cruz,P, Mastri,F, Mazanek,M, Santos,H, Alimenti,F, Garcia Vazquez,H, Pollin,S, Poli,L, Belo,D, Masotti,D, Machac,J, Vítor Grade Tavares, Mezzanotte,P, Ndungidi,P, Oliveri,G, Fernandes,R, Salgado,H, Moeyaert,V, Massa,A, Goncalves,R, Pinho,P, Monti,G, Tarricone,L, Dionigi,M, Russer,P, and Russer,J

Subjects
IBCN
Published
2017

27. No Battery Required

Author

Kim, S, Mariotti, C, Alimenti, F, Mezzanotte, P, Georgiadis, A, Collado, A, Roselli, L, and Tentzeris, MM

Published
2013

31. The telescope and the double Fabry-Pérot interferometer for the ADAHELI solar space mission

Author

Greco, V, Cavallini, F, Berrilli, F, Velli, M, Roselli, L, Bigazzi, A, Moretti, Pf, Romoli, M, Orsini, S, Sabatini, P, Carbone, V, Consolini, G, Di Mauro MP, Ermolli, I, Pietropaolo, Ermanno, Romano, P, Ventura, P, Valdettaro, L, White, Sm, Zuccarello, F, Cauzzi, G, Giammaria, F, Reardon, K, Briguglio, R, Landi, S, Vecchio, A, Lepreti, F, Sorriso Valvo, L, Contarino, L, Guglielmino, S, De Pontieu, B, Cardini, D, Chieffi, A, Milillo, A, Mura, A, De Angelis, E, Mangano, V, Selci, S, Criscuoli, S, Giorgi, F, Alimenti, F, Palazzari, V, Biferale, L, Cantarano, S, Del Moro, D, Egidi, A, Penza, V, Piazzesi, R, Stangalini, M, Vantaggiato, M, Viticchiè, B, Casolino, M, De Santis, C, and Sparvoli, R.

Subjects
Astronomy, Orbital mechanics, law.invention, Telescope, Heliophysics, Optics, Settore FIS/05 - Astronomia e Astrofisica, Fabry-Perot, Space optics, Telescopes, Electronic, Optical and Magnetic Materials, Condensed Matter Physics, Computer Science Applications1707 Computer Vision and Pattern Recognition, Applied Mathematics, Electrical and Electronic Engineering, law, Electronic, Fabry-Perot interferometer, Astronomical interferometer, Optical and Magnetic Materials, Physics, Gregorian telescope, Spacecraft, solar space mission, business.industry, Astrophysics::Instrumentation and Methods for Astrophysics, telescopes, Interferometry, Physics::Space Physics, Satellite, Astrophysics::Earth and Planetary Astrophysics, business
Abstract

ADvanced Astronomy for HELIophysics (ADAHELI) is a Small Mission to study the structure and fast dynamics of the low solar atmosphere, performing Visible-NIR monochromatic and broad-band observations. The mission will achieve millimeter full disk observations as well. The ADAHELI Team has succesfully completed, in December 2008, the Phase A study awarded by the Italian Space Agency (ASI). The Interferometer for SOlar Dynamics (ISODY), on board the ADAHELI satellite, comprises a Gregorian telescope and its focal plane suite. The advanced design focal plane suite uses fast CMOS cameras for investigating photospheric and chromospheric fast dynamics and structure. ISODY is equipped with a pioneering focal plane suite composed of a spectral channel, based upon a tandem of Fabry-Perot interferometers operating in the visible-NIR spectral region, a broad band channel for high resolution imaging, and a correlation tracker used as an image stabilization system. ADAHELI's mission profile has been tailored to limit the spacecraft's radial velocity in the Sunward direction, to not exceed ±4 km/s, during 95% of the yearly orbit, to allow a continuous use of the on-board interferometer.

Published
2010
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