Fabrication and real time testing of a tilt-rotor tricopter

In recent years, there has been an increasing interest in the development of lightweight and small sized unmanned aerial vehicles as technology continues to disrupt industries worldwide. Non-conventional platforms, such as tricopters, are also gaining popularity due to their superior manoeuvrability...

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Main Author: Brian, Kenny
Other Authors: Erdal Kayacan
Format: Final Year Project
Language:English
Published: 2017
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Online Access:http://hdl.handle.net/10356/71489
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-714892023-03-04T18:51:24Z Fabrication and real time testing of a tilt-rotor tricopter Brian, Kenny Erdal Kayacan School of Mechanical and Aerospace Engineering DRNTU::Engineering::Mechanical engineering In recent years, there has been an increasing interest in the development of lightweight and small sized unmanned aerial vehicles as technology continues to disrupt industries worldwide. Non-conventional platforms, such as tricopters, are also gaining popularity due to their superior manoeuvrability and higher cruising speeds. In this project, various manufacturing techniques are used to produce a tilt-rotor tricopter that is small and lightweight. Two tricopter prototypes are manufactured using different techniques. One was 3D printed using ABSplus as its filament. Assembly and fabrication challenges lead to several design modifications to the second prototype, which is 3D printed and reinforced with carbon fibre prepregs, increasing the structure’s stiffness and strength. The final prototype weighs 14% lighter and is 25 % smaller in size than the original platform. It will eventually be used to perform various control experiments in a motion capture laboratory. Models of the tricopter are created using Solidworks in order to test closed loop control algorithms in a simulated environment. Upon successful simulation of the control algorithm, the tricopter is tested in real-time. The structure proved to be robust and lighter while demonstrating satisfactory response to trajectory commands. Based on the test results, it is concluded that carbon fibre reinforcements may not be an ideal technique to be used in conjunction with rapid prototyping. In addition, smaller tricopter designs can be achieved with the use of lighter batteries, which reduces the overall weight and, in turn, the size of propellers used as well. Recommendations for future development of the tricopter are explored further in the report. Bachelor of Engineering (Mechanical Engineering) 2017-05-17T04:01:21Z 2017-05-17T04:01:21Z 2017 Final Year Project (FYP) http://hdl.handle.net/10356/71489 en Nanyang Technological University 77 p. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering::Mechanical engineering
spellingShingle DRNTU::Engineering::Mechanical engineering
Brian, Kenny
Fabrication and real time testing of a tilt-rotor tricopter
description In recent years, there has been an increasing interest in the development of lightweight and small sized unmanned aerial vehicles as technology continues to disrupt industries worldwide. Non-conventional platforms, such as tricopters, are also gaining popularity due to their superior manoeuvrability and higher cruising speeds. In this project, various manufacturing techniques are used to produce a tilt-rotor tricopter that is small and lightweight. Two tricopter prototypes are manufactured using different techniques. One was 3D printed using ABSplus as its filament. Assembly and fabrication challenges lead to several design modifications to the second prototype, which is 3D printed and reinforced with carbon fibre prepregs, increasing the structure’s stiffness and strength. The final prototype weighs 14% lighter and is 25 % smaller in size than the original platform. It will eventually be used to perform various control experiments in a motion capture laboratory. Models of the tricopter are created using Solidworks in order to test closed loop control algorithms in a simulated environment. Upon successful simulation of the control algorithm, the tricopter is tested in real-time. The structure proved to be robust and lighter while demonstrating satisfactory response to trajectory commands. Based on the test results, it is concluded that carbon fibre reinforcements may not be an ideal technique to be used in conjunction with rapid prototyping. In addition, smaller tricopter designs can be achieved with the use of lighter batteries, which reduces the overall weight and, in turn, the size of propellers used as well. Recommendations for future development of the tricopter are explored further in the report.
author2 Erdal Kayacan
author_facet Erdal Kayacan
Brian, Kenny
format Final Year Project
author Brian, Kenny
author_sort Brian, Kenny
title Fabrication and real time testing of a tilt-rotor tricopter
title_short Fabrication and real time testing of a tilt-rotor tricopter
title_full Fabrication and real time testing of a tilt-rotor tricopter
title_fullStr Fabrication and real time testing of a tilt-rotor tricopter
title_full_unstemmed Fabrication and real time testing of a tilt-rotor tricopter
title_sort fabrication and real time testing of a tilt-rotor tricopter
publishDate 2017
url http://hdl.handle.net/10356/71489
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