Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Chesi, Simone"'
Autor:
Chesi, Simone, Romano, Marcello
Patent A method of simulating 3-degrees of freedom spacecraft rotational dynamics is provided that includes attaching a payload, using a spherical air bearing, to an inner gimbal of a 3-axis gimbal, where the 3-axis gimbal includes an outer gimbal, a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::af69e8a2a28da6d0983df86b75e5cf35
https://hdl.handle.net/10945/65070
https://hdl.handle.net/10945/65070
Autor:
Leung, Lawrence, Beukelaers, Vincent, Chesi, Simone, Yoon, Hyosang, Walker, Daniel, Egbert, Joshua
Publikováno v:
AIAA/USU Conference on Small Satellites
The Attitude Determination and Control System (ADCS) is considered one of the most critical subsystems of a spacecraft, and must be carefully calibrated and monitored to ensure mission success. Many emerging small satellite missions feature large con
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______1459::7c5855455b38098d4839d4a13013c9d0
https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=4239&context=smallsat
https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=4239&context=smallsat
Autor:
Mero, Bena, Quillien, Kevin A., McRobb, Malcolm, Chesi, Simone, Marshall, Ross, Gow, Alasdair, Clark, Craig, Anciaux, M., Cardoen, P., De Keyser, J., Demoulin, Ph., Fussen, D., Pieroux, D., Ranvier, S.
Publikováno v:
Small Satellite Conference
PICASSO is a highly ambitious 3U CubeSat science mission with the objective of studying ozone distribution in the stratosphere, characterizing the air temperature profile up to the mesosphere, and measuring the electron density and temperature in the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______1459::043fdfb4e722549df61a21075e20c34d
https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=3179&context=smallsat
https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=3179&context=smallsat
This paper presents the design and development of a nanosatellite-scale spacecraft three-axis simulator (“Cu- beSat Three-Axis Simulator,” or “CubeTAS”), the purpose of which is to enable experimental testing of Attitude Determination and Con
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______2778::032edef9895458aeedbc9fe74982e518
https://hdl.handle.net/10945/50871
https://hdl.handle.net/10945/50871
Autor:
Chesi, Simone
Publikováno v:
Chesi, Simone. (2015). ATTITUDE CONTROL OF NANOSATELLITES USING SHIFTING MASSES. UC Santa Cruz: Applied Mathematics and Statistics. Retrieved from: http://www.escholarship.org/uc/item/61r1d1sm
Since the development of the CubeSat standard, the number of nanosatellites developed by universities, federal agencies and commercial companies has greatly increased as well as their mission complexity. This thesis focuses on the development of atti
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od_______325::c052505310dd32188766e0ab8e31c434
http://www.escholarship.org/uc/item/61r1d1sm
http://www.escholarship.org/uc/item/61r1d1sm
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