An Efficient Design-to-Verification Framework for CubeSat ADCS: Application to INHA RoSAT
CubeSats are increasingly adopted for space missions due to their low cost and short development cycles. However, their attitude determination and control systems (ADCS) often suffer from limited verification environments and constrained hardware configurations. This study addresses the development...
Αποθηκεύτηκε σε:
| Κύριοι συγγραφείς: | , , , , |
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| Μορφή: | Artigo |
| Γλώσσα: | Inglês |
| Έκδοση: |
MDPI AG
2026-02-01
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| Σειρά: | Aerospace |
| Θέματα: | |
| Διαθέσιμο Online: | https://www.mdpi.com/2226-4310/13/2/189 |
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