Adaptive Attitude Control of a Satellite by Considering Magnetorquer Faults
In this paper, an adaptive fault-tolerant control based on modified nonsingular fast terminal sliding mode control is developed for attitude tracking of a satellite with three magnetorquers and one reaction wheel. The proposed approach is designed to be robust in the presence of actuator faults, ext...
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| Asıl Yazarlar: | , , , , |
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| Materyal Türü: | Artigo |
| Dil: | Persa |
| Baskı/Yayın Bilgisi: |
Iranian Space Research Institute
2024-08-01
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| Seri Bilgileri: | علوم، فناوری و کاربردهای فضایی |
| Konular: | |
| Online Erişim: | https://journal.isrc.ac.ir/article_195056_b496a6280ebc01b66284957ec45d72b6.pdf |
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