Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Giacomo Curzi"'
Publikováno v:
Aerospace, Vol 7, Iss 9, p 133 (2020)
Constellations of satellites are being proposed in large numbers; most of them are expected to be in orbit within the next decade. They will provide communication to unserved and underserved communities, enable global monitoring of Earth and enhance
Externí odkaz:
https://doaj.org/article/f990f4d83efa412d9b976e2bea7c9c23
Publikováno v:
Aerospace, Vol 7, Iss 3, p 31 (2020)
To enable a reliable verification of attitude determination and control systems for nanosatellites, the environment of low Earth orbits with almost disturbance-free rotational dynamics must be simulated. This work describes the design solutions adopt
Externí odkaz:
https://doaj.org/article/ab756921e600417ab8570941bef08964
Publikováno v:
International Journal of Aerospace Engineering, Vol 2018 (2018)
We propose a simple and relatively inexpensive method for determining the center of gravity (CoG) of a small spacecraft. This method, which can be ascribed to the class of suspension techniques, is based on dual-axis inclinometer readings. By perform
Externí odkaz:
https://doaj.org/article/c1c343d6ebdc4fed9cbe231f138a465d
Publikováno v:
Journal of Spacecraft and Rockets. 59:1125-1134
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ecc355c8b6ce29861bb3994a60a49a69
https://doi.org/10.2514/1.a35234
https://doi.org/10.2514/1.a35234
Publikováno v:
CEAS Space Journal. 14:197-204
As space traffic increases, Space Situational Awareness (SSA) is becoming fundamental for safe spaceflight operations. Cost-driven missions based on small satellite platforms would benefit from the availability of alternative tools providing prelimin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a7c245d00a0f0897aedc1d21ff409d2f
https://doi.org/10.1007/s12567-021-00375-3
https://doi.org/10.1007/s12567-021-00375-3
Autor:
Giacomo Curzi, Dario Modenini
A novel approach is developed for analytic orbit propagation based on asymptotic expansion with respect to a small perturbative acceleration. The method improves upon existing first order asymptotic expansions by leveraging on linear systems and aver
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2d296cfc49b62baca6db4d680e10f5a3
This work describes the development of a three degrees of freedom CubeSat attitude simulator testbed. To enable a reliable verification of attitude determination and control systems for nanosatellites, the environment of low Earth orbits with an almo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______4094::5caa2367c9481fc5e29cfaf1204c2de9
http://hdl.handle.net/11585/733310
http://hdl.handle.net/11585/733310
Publikováno v:
Aerospace, Vol 7, Iss 3, p 31 (2020)
Aerospace
Volume 7
Issue 3
Aerospace
Volume 7
Issue 3
To enable a reliable verification of attitude determination and control systems for nanosatellites, the environment of low Earth orbits with almost disturbance-free rotational dynamics must be simulated. This work describes the design solutions adopt
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a02ce1259c494dc049b3c2087aa74767
https://www.mdpi.com/2226-4310/7/3/31
https://www.mdpi.com/2226-4310/7/3/31
Publikováno v:
Aerospace, Vol 7, Iss 133, p 133 (2020)
Constellations of satellites are being proposed in large numbers; most of them are expected to be in orbit within the next decade. They will provide communication to unserved and underserved communities, enable global monitoring of Earth and enhance
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::507254ea2da31680be6a5495eb4db1ee
http://hdl.handle.net/11585/774007
http://hdl.handle.net/11585/774007
Publikováno v:
International Journal of Aerospace Engineering, Vol 2018 (2018)
We propose a simple and relatively inexpensive method for determining the center of gravity (CoG) of a small spacecraft. This method, which can be ascribed to the class of suspension techniques, is based on dual-axis inclinometer readings. By perform
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8b78e154e0877e25abdafb965c240758
http://hdl.handle.net/11585/679145
http://hdl.handle.net/11585/679145