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...

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Bibliografski detalji

Glavni autori:	Hye-Eun Yoo, Chang-Oh Kim, Sung-Hoon Mok, Jisoo Yu, Keeyoung Choi
Format:	Artigo
Jezik:	Inglês
Izdano:	MDPI AG 2026-02-01
Serija:	Aerospace
Teme:	attitude determination and control system automatic code generation CubeSat FlatSat verification flight software model-based design
Online pristup:	https://www.mdpi.com/2226-4310/13/2/189
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