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Attitude determination and control for centrifugal tether deployment on the ESTCube-1 nanosatellite; pp. 242–249

This paper presents the design, development, and pre-launch characterization of the ESTCube-1 Attitude Determination and Control System (ADCS). The design driver for the ADCS has been the mission requirement to spin up the satellite to 360 deg à sâ1 with controlled orientation of the spin axis and t...

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Principais autores: Andris Slavinskis, Erik Kulu, Jaan Viru, Robert Valner, Hendrik Ehrpais, Tõnis Uiboupin, Markus Järve, Endel Soolo, Jouni Envall, Tobias Scheffler, Indrek Sünter, Henri Kuuste, Urmas Kvell, Jaanus Kalde, Kaspars Laizans, Erik Ilbis, Tõnis Eenmäe, Riho Vendt, Kaupo Voormansik, Ilmar Ansko, Viljo Allik, Silver Lätt, Mart Noorma
פורמט: Artigo
שפה:Inglês
יצא לאור: Estonian Academy Publishers 2014-05-01
סדרה:Proceedings of the Estonian Academy of Sciences
נושאים:
attitude determination
attitude control
subsystem design
electric solar wind sail
sun sensor
nanosatellite
cubesat
estcube-1.
גישה מקוונת:https://kirj.ee/public/proceedings_pdf/2014/issue_2S/Proc-2014-2S-242-249.pdf
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