Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Anton Bahu"'
Publikováno v:
Aerospace, Vol 9, Iss 4, p 223 (2022)
Dynamic spacecraft simulators are becoming a widespread tool to enable effective on-ground verification of the attitude determination and control subsystem (ADCS). In such facilities, the on-orbit rotational dynamics shall be simulated, thereby requi
Externí odkaz:
https://doaj.org/article/794d30a323404f99bb1ae1f37409a42b
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
Autor:
Anton Bahu, Dario Modenini
Publikováno v:
CEAS Space Journal. 13:543-554
A novel approach to the three-axis attitude control of a magnetically actuated spacecraft is proposed, based on hybrid systems theory. Due to the actuators type, the system model is instantaneously underactuated and time-varying, so that low pointing
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d4c36985111c88acee7f93c2553b3cbf
https://doi.org/10.1007/s12567-020-00340-6
https://doi.org/10.1007/s12567-020-00340-6
Publikováno v:
IFAC-PapersOnLine. 54:38-42
Due to their low size, mass, development cost and time, nanosatellites have become an increasingly popular tool at universities for providing students with hands-on experience in aerospace education. Among spacecraft subsystems, the attitude determin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2d6ba1f7cbe7e3a5144a504fd3da06d5
https://doi.org/10.1016/j.ifacol.2021.11.007
https://doi.org/10.1016/j.ifacol.2021.11.007
Autor:
Anton Bahu, Dario Modenini
Publikováno v:
CEAS Space Journal. 12:597-611
This paper describes the automatic balancing and inertia identification system for three degrees of freedom CubeSat attitude simulator testbed. For a reliable verification of the attitude determination and control subsystem, the on-orbit environment
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0a8608f8c9533cce3d3cebefbb02c762
https://doi.org/10.1007/s12567-020-00309-5
https://doi.org/10.1007/s12567-020-00309-5
Dynamic spacecraft simulators are becoming a widespread tool to enable effective on-ground verification of the attitude determination and control subsystem (ADCS). In such facilities, the on-orbit rotational dynamics shall be simulated, thereby requi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2add1625e4e43c8bc5be0f74a3a2e68f
http://hdl.handle.net/11585/887409
http://hdl.handle.net/11585/887409
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