Robust optimal attitude control for hexarotors with disturbances, uncertainties, and delays
Abstract A robust optimal attitude controller for hexarotor helicopters is proposed. Compared to the previous research studies on hexarotors, the current study takes account of the influences of non‐linear and coupling dynamics, structured and unstructured uncertainties, external time‐varying distur...
Kaydedildi:
| Asıl Yazarlar: | , |
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| Materyal Türü: | Artigo |
| Dil: | Inglês |
| Baskı/Yayın Bilgisi: |
Wiley
2023-03-01
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| Seri Bilgileri: | IET Cyber-Physical Systems |
| Konular: | |
| Online Erişim: | https://doi.org/10.1049/cps2.12041 |
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