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,...
Saved in:
Main Author: | Wong, Seng Man |
---|---|
Format: | Monograph |
Language: | English |
Published: |
Universiti Sains Malaysia
2018
|
Subjects: | |
Online Access: | 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 http://eprints.usm.my/52534/ |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Development of unmanned aerial vehicle – Part 1
by: Sidek, Shahrul Na'im, et al.
Published: (2011) -
Development of unmanned aerial vehicle – Part 2
by: Sidek, Shahrul Na'im, et al.
Published: (2011) -
Affordable unmanned aerial vehicle aircraft for surveillance
by: Sidek, Shahrul Na'im, et al.
Published: (2010) -
Slope Mapping using Unmanned Aerial Vehicle (UAV)
by: Muhammad Farhan, Zolkepli, et al.
Published: (2021) -
Energy efficient path-planning for unmanned aerial vehicle
by: Debnath, Sanjoy Kumar
Published: (2022)