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Autor:
Oktaf Agni Dhewa, Fatchul Arifin, Ardy Seto Priyambodo, Anggun Winursito, Yasir Mohd. Mustafa
Publikováno v:
International Islamic University Malaysia Engineering Journal, Vol 25, Iss 2 (2024)
The stability of an Unmanned Aerial Vehicle (UAV) attitude is crucial in aviation to mitigate the risk of accidents and ensure mission success. This study aims to optimize and adaptively control the flight attitude stability of a flying wing-type UAV
Externí odkaz:
https://doaj.org/article/79a72f08e21f456298ddd7782646053b