Design and development of atypical multicopter with application of tricopter
Multicopter is a vertical takeoff and landing unmanned aerial vehicle (UAV). Due to technological advances, low cost flight controller is available for general public to design and develop their own multicopter. However, odd rotor configuration multicopters are less commonly seen due to their unbala...
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sg-ntu-dr.10356-639682023-03-04T18:25:04Z Design and development of atypical multicopter with application of tricopter Wong, Zhuo Wei Wong Chee How School of Mechanical and Aerospace Engineering DRNTU::Engineering::Mechanical engineering Multicopter is a vertical takeoff and landing unmanned aerial vehicle (UAV). Due to technological advances, low cost flight controller is available for general public to design and develop their own multicopter. However, odd rotor configuration multicopters are less commonly seen due to their unbalanced torque around the yaw axis. Thus, this project aims to explore the flight characteristic of a tricopter. The tricopter is built and tested for its flight stability. The control system in the flight controller is analyzed and parameters were adjusted to improve the flight performance of the tricopter. Autonomous flight navigation was carried out on the tricopter for potential military applications. Bachelor of Engineering (Mechanical Engineering) 2015-05-21T02:09:33Z 2015-05-21T02:09:33Z 2015 2015 Final Year Project (FYP) http://hdl.handle.net/10356/63968 en Nanyang Technological University 65 p. application/pdf |
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DRNTU::Engineering::Mechanical engineering Wong, Zhuo Wei Design and development of atypical multicopter with application of tricopter |
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Multicopter is a vertical takeoff and landing unmanned aerial vehicle (UAV). Due to technological advances, low cost flight controller is available for general public to design and develop their own multicopter. However, odd rotor configuration multicopters are less commonly seen due to their unbalanced torque around the yaw axis. Thus, this project aims to explore the flight characteristic of a tricopter. The tricopter is built and tested for its flight stability. The control system in the flight controller is analyzed and parameters were adjusted to improve the flight performance of the tricopter. Autonomous flight navigation was carried out on the tricopter for potential military applications. |
author2 |
Wong Chee How |
author_facet |
Wong Chee How Wong, Zhuo Wei |
format |
Final Year Project |
author |
Wong, Zhuo Wei |
author_sort |
Wong, Zhuo Wei |
title |
Design and development of atypical multicopter with application of tricopter |
title_short |
Design and development of atypical multicopter with application of tricopter |
title_full |
Design and development of atypical multicopter with application of tricopter |
title_fullStr |
Design and development of atypical multicopter with application of tricopter |
title_full_unstemmed |
Design and development of atypical multicopter with application of tricopter |
title_sort |
design and development of atypical multicopter with application of tricopter |
publishDate |
2015 |
url |
http://hdl.handle.net/10356/63968 |
_version_ |
1759854749008527360 |