Zobrazeno 1 - 10
of 27
pro vyhledávání: '"Federica Angeletti"'
Autor:
Maurizio Parisse, Federica Angeletti
Publikováno v:
Aerospace, Vol 11, Iss 9, p 694 (2024)
Thermally induced vibrations usually affect spacecraft equipped with light and slender appendages such as booms, antennas or solar panels. This phenomenon occurs when a thermal shock, resulting from the sudden cooling and warming phases at the entran
Externí odkaz:
https://doaj.org/article/7f24af18fc064f2d905b25ba0a64e269
Publikováno v:
Applied Sciences, Vol 13, Iss 17, p 9715 (2023)
Piezoelectric actuators and sensors can be incorporated into aerospace structures to suppress unwanted flexible oscillations. These devices need to interact with various passive structures, including innovative materials such as thermoplastic composi
Externí odkaz:
https://doaj.org/article/c33fc0a68ae24acb96c56ab35d54bad9
Publikováno v:
Sensors, Vol 23, Iss 17, p 7515 (2023)
The diagnostics of environmentally induced damages in composite structures plays a critical role for ensuring the operational safety of space platforms. Recently, spacecraft have been equipped with lightweight and very large substructures, such as an
Externí odkaz:
https://doaj.org/article/4fe8464fedfc4511b9b90a6ce63a48b8
Publikováno v:
Sensors, Vol 23, Iss 1, p 368 (2022)
Most modern Earth and Universe observation spacecraft are now equipped with large lightweight and flexible structures, such as antennas, telescopes, and extendable elements. The trend of hosting more complex and bigger appendages, essential for high-
Externí odkaz:
https://doaj.org/article/6959983d2a214b0e9b86c77fcaba515a
Autor:
Alice Pellegrino, Maria Giulia Pancalli, Andrea Gianfermo, Paolo Marzioli, Federico Curianò, Federica Angeletti, Fabrizio Piergentili, Fabio Santoni
Publikováno v:
Remote Sensing, Vol 13, Iss 12, p 2399 (2021)
This paper presents the HORUS mission, aimed at multispectral and multiangle (nadir and off-nadir) planetary optical observation, using Commercial Off-The-Shelf (COTS) instruments on-board a 6-Unit CubeSat. The collected data are characterized by a s
Externí odkaz:
https://doaj.org/article/cbc9e1b906544d4db3d8681f989e0ac6
Publikováno v:
Acta Astronautica. 199:401-411
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e995bd25d08a257a986c0842c380a38f
https://doi.org/10.1016/j.actaastro.2022.07.024
https://doi.org/10.1016/j.actaastro.2022.07.024
Publikováno v:
Acta Astronautica. 198:445-453
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7ccbb491b6207cd72f73bec8f5707b5d
https://doi.org/10.1016/j.actaastro.2022.05.016
https://doi.org/10.1016/j.actaastro.2022.05.016
Publikováno v:
Sensors; Volume 23; Issue 1; Pages: 368
Most modern Earth and Universe observation spacecraft are now equipped with large lightweight and flexible structures, such as antennas, telescopes, and extendable elements. The trend of hosting more complex and bigger appendages, essential for high-
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3e021836e96a201baf3000b2d8f3083e
https://hdl.handle.net/11573/1664071
https://hdl.handle.net/11573/1664071
Publikováno v:
Acta Astronautica. 187:416-428
The standard approach of controlling in-orbit large flexible structures only by adopting actuators and sensors located at platform level is currently being challenged by new missions’ stringent requirements in terms of demanding guidance profiles a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::56e19850d1ea349d94239ec86d512ebe
https://doi.org/10.1016/j.actaastro.2021.04.007
https://doi.org/10.1016/j.actaastro.2021.04.007
Publikováno v:
Aerotecnica Missili & Spazio. 100:147-160
Fault Detection and Isolation (FDI) techniques have captured extensive interest and attention in modern autonomous systems; in particular, they are of foremost importance in space applications, due to their scientific relevance, cost and current inab
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4085645619e2bce5058567297fc769b8
https://doi.org/10.1007/s42496-021-00080-8
https://doi.org/10.1007/s42496-021-00080-8