Design, Manufacturing, and Flight Testing of an Experimental Flying Wing UAV

This paper presents the design, manufacturing, and flight testing of an electric-powered experimental flying wing unmanned aerial vehicle (UAV). The design process starts with defining the performance requirements including the stall speed, maximal speed, cruise altitude, absolute ceiling, and turn...

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Autors principals: Pei-Hsiang Chung, Der-Ming Ma, Jaw-Kuen Shiau
Format: Article
Idioma:English
Publicat: MDPI AG 2019-07-01
Col·lecció:Applied Sciences
Matèries:
Accés en línia:https://www.mdpi.com/2076-3417/9/15/3043