Zobrazeno 1 - 10
of 109
pro vyhledávání: '"Leonardo Reyneri"'
Publikováno v:
Aerospace, Vol 10, Iss 12, p 1009 (2023)
Current CubeSats usually exhibit a low structural mass efficiency and a low internal volume for their payloads. The present work aims to propose an advanced structural architecture for CubeSats that addresses the issues of low structural mass efficie
Externí odkaz:
https://doaj.org/article/5997504ad4a448bda5b3878493d4bcad
Publikováno v:
International Journal of Aerospace Engineering, Vol 2019 (2019)
In recent years, the development market for low-cost nanosatellites has grown considerably. It has been made possible due to the availability of low-cost launch vectors and the use of “commercial off-the-shelf components” (COTS). The satellite de
Externí odkaz:
https://doaj.org/article/bb3dfab09419442a90863f5aaae57e58
Autor:
Rehan Mahmood, Qamar ul Islam, Muhammad Rizwan Anjum, Hassan Ali, Muhammad Rizwan Mughal, Leonardo Reyneri
Publikováno v:
IEEE Journal on Miniaturization for Air and Space Systems. 2:105-111
CubeSats have become increasingly important in the last two decades and are playing a very important role in the space industry, especially with Earth-oriented nanosatellites. Earth-oriented nanosatellites require more precise attitude control when t
Publikováno v:
International Journal of Satellite Communications and Networking. 37:588-600
The ever-decreasing size of the small satellites with more demanding payloads has opened new research areas to investigate innovative onboard data-handling solutions. This paper presents the use of optical intra-satellite communication using discrete
An attitude control system (ACS) is one of the critical subsystems of any spacecraft and typically is in charge of de-tumbling, controlling, and orienting the satellite after initial deployment and during the satellite operations. The magnetorquer is
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8d398dcadee0a744dd2206ccde628f56
https://aaltodoc.aalto.fi/handle/123456789/40444
https://aaltodoc.aalto.fi/handle/123456789/40444
Publikováno v:
IEEE Access, Vol 8, Pp 146196-146207 (2020)
In space thermal environment, satellites are exposed to multiple heat sources which can deteriorate structural and equipment integrity over long periods of time. Normally radiators are used to release heat, but due to space and weight constraints, it
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::70bbaef8a0e0bad390b937af6339bec5
https://aaltodoc.aalto.fi/handle/123456789/46627
https://aaltodoc.aalto.fi/handle/123456789/46627
Publikováno v:
Aircraft Engineering and Aerospace Technology. 90:379-389
Purpose This paper aims to present an innovative system able to establish an inter-satellite communication crosslink and to determine the mutual physical positioning for CubeSats belonging to a swarm. Design/methodology/approach Through a system invo
Autor:
Alejandro Serrano-Cases, Antonio Martínez-Álvarez, Leonardo Reyneri, Yolanda Morilla, Sergio Cuenca-Asensi
Publikováno v:
idUS. Depósito de Investigación de la Universidad de Sevilla
instname
Electronics
Volume 8
Issue 6
RUA. Repositorio Institucional de la Universidad de Alicante
Universidad de Alicante (UA)
Electronics, Vol 8, Iss 6, p 653 (2019)
Digital.CSIC. Repositorio Institucional del CSIC
instname
Electronics
Volume 8
Issue 6
RUA. Repositorio Institucional de la Universidad de Alicante
Universidad de Alicante (UA)
Electronics, Vol 8, Iss 6, p 653 (2019)
Digital.CSIC. Repositorio Institucional del CSIC
A high-level C++ hardening library is designed for the protection of critical software against the harmful effects of radiation environments that can damage systems. A mathematical and empirical model to predict system behavior in the presence of rad
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e7c3ecf118ad977d76c380007d8f21f1
Publikováno v:
Aerospace
Volume 7
Issue 2
Aerospace, Vol 7, Iss 2, p 17 (2020)
Volume 7
Issue 2
Aerospace, Vol 7, Iss 2, p 17 (2020)
CubeSats usually adopt aluminum alloys for primary structures, and a number of studies exist on Carbon Fiber Reinforced Plastic (CFRP) primary structures. The internal volume of a spacecraft is usually occupied by battery arrays, reducing the volume