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Thrust Vectoring Control of a Novel Tilt-Rotor UAV Based on Backstepping Sliding Model Method
In this paper, a control method of a novel tilt-rotor UAV with a blended wing body layout is studied. The novel UAV is capable of vertical take-off and landing and has strong stealth capabilities that can be applied to carrier-borne reconnaissance aircraft. However, the high aspect ratio of blended...
| Autores principales: | , , |
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| Formato: | Online Artículo Texto |
| Lenguaje: | English |
| Publicado: |
MDPI
2023
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| Materias: | |
| Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9864851/ https://www.ncbi.nlm.nih.gov/pubmed/36679369 http://dx.doi.org/10.3390/s23020574 |