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

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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,...

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Bibliographic Details
Main Author:	Wong, Seng Man
Format:	Monograph
Language:	English
Published:	Universiti Sains Malaysia 2018
Subjects:	T Technology TL1-4050 Motor vehicles. Aeronautics. Astronautics
Online Access:	http://eprints.usm.my/52534/ 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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