Redesign, analysis, fabrication and testing of light weight fuselage, boom and empennage for solar UAV : part 1
In recent years, a lot of research efforts have been put into Unmanned Aerial Vehicle (UAV) due to its ability to perform a wide variety of missions which include surveillance and recon, search and rescue operations, transport operations and other special operations deemed too dangerous or unsuitabl...
Saved in:
Main Author: | Yap, Kelvin Bing Hui |
---|---|
Other Authors: | School of Mechanical and Aerospace Engineering |
Format: | Final Year Project |
Language: | English |
Published: |
2014
|
Subjects: | |
Online Access: | http://hdl.handle.net/10356/60441 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Nanyang Technological University |
Language: | English |
Similar Items
-
Redesign, analysis, fabrication and testing of light weight fuselage, boom and empennage for solar UAV : Part 3
by: Tan, Thomas Peng Ngee
Published: (2015) -
Redesign, analysis, fabrication and testing of light weight wing for solar UAV : part 2
by: Oh, Ying Qun
Published: (2014) -
Redesign, analysis, fabrication and testing of light weight wing with solar panels as wing skin for solar UAV : part 1
by: Koh, Hui Wei
Published: (2014) -
Development and fabrication of solar powered UAV : Part 1
by: Pang, Xue Wen
Published: (2015) -
Development and fabrication of solar powered UAV : Part 2
by: Cheng, Shi Wee
Published: (2015)