Design And Development Of A Fixed-Wing Vertical Take-Off And Landing Unmanned Aerial Vehicle

Design And Development Of A Fixed-Wing Vertical Take-Off And Landing Unmanned Aerial Vehicle

The interest in building hybrid Unmanned Aerial Vehicles (UAVs) are increasing intensively due to its capability to perform Vertical Take-Off and Landing (VTOL), in addition to the forward flight mode. With the capability, the hybrid UAVs are highly on demand in various industries such as military,...

Полное описание

Библиографические подробности
Главный автор:	Wong, Seng Man
Формат:	Monograph
Язык:	English
Опубликовано:	Universiti Sains Malaysia 2018
Предметы:	T Technology TL1-4050 Motor vehicles. Aeronautics. Astronautics
Online-ссылка:	http://eprints.usm.my/52534/1/Design%20And%20Development%20Of%20A%20Fixed-Wing%20Vertical%20Take-Off%20And%20Landing%20Unmanned%20Aerial%20Vehicle_Lester%20Wong%20Seng%20Man__A2_2018_MJMS.pdf

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