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Stefano Carletta, Paolo Teofilatto and M. Salim Farissi
Attitude determination represents a fundamental task for spacecraft. Achieving this task on small satellites, and nanosatellites in particular, is further challenging, because the limited power and computational resources available on-board, together wit...
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M. Salim Farissi, Stefano Carletta, Augusto Nascetti and Paolo Teofilatto
The subject of this work is the implementation and experimental testing of a purely magnetic attitude control strategy, which can provide stabilization after the deployment and pointing of the spacecraft without any attitude information. In particular, t...
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