Zobrazeno 1 - 1
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pro vyhledávání: '"Klebes R. Arias"'
Publikováno v:
2012 IEEE Aerospace Conference.
In a one-unit (1U) CubeSat satellite, the attitude determination and control system restricts its allocated mass to be in the range of 150–200 g, and to operate with at most 1 W. Under such tight constraints, effective attitude control system desig
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::21dc8486b7b8c94786810af478e52e3f
https://doi.org/10.1109/aero.2012.6187239
https://doi.org/10.1109/aero.2012.6187239
