E. Oland, Alexander Aas, Tor Marius Steihaug, S. V. Mathisen, Frank R. Vedal
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引用次数: 1
Abstract
In this paper we present a design methodology for attitude determination and control systems for picosatellites. It is based on the ECSS documentations and shows through a practical example how the ECSS standard can be applied to a picosatellite project.
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