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Autor:
Muhammad Fikri Al-Fattah Isrinanto, Ony Arifianto, Willy Wahyanto, Marco Wijaya, Ghifari Hanif Mustofa, Fahmi Abdillah Sambodo
Publikováno v:
THE 8TH INTERNATIONAL SEMINAR ON AEROSPACE SCIENCE AND TECHNOLOGY – ISAST 2020.
Dual system hybrid VTOL UAV is one type of UAV that can take-off and landing using their rotary-wing system and cruise with their fixed-wing system. In this type of UAV, there is two propulsion system, the first one is a propulsion system for vertica
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::64b935deba1e803ea5b55d5bda80861e
https://doi.org/10.1063/5.0060064
https://doi.org/10.1063/5.0060064
