Optimisation of helium-assisted drone : control and flight analysis

Recent developments in technology has led to an increased interest in drones and their applications, as well as widespread usage. While certain industries have managed to exploit the usage of drones to a large degree, applications in other areas such as Human Aid and Disaster Relief has immense pote...

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Main Author: See, Kelwin Chun Gan
Other Authors: Lam Yee Cheong
Format: Final Year Project
Language:English
Published: Nanyang Technological University 2020
Subjects:
Online Access:https://hdl.handle.net/10356/140931
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-1409312023-03-04T18:41:19Z Optimisation of helium-assisted drone : control and flight analysis See, Kelwin Chun Gan Lam Yee Cheong School of Mechanical and Aerospace Engineering myclam@ntu.edu.sg Engineering::Mechanical engineering Recent developments in technology has led to an increased interest in drones and their applications, as well as widespread usage. While certain industries have managed to exploit the usage of drones to a large degree, applications in other areas such as Human Aid and Disaster Relief has immense potential for drone applications. The challenge of using drones in such areas are its low endurance and payload. Endurance is critical especially for drones that are required for surveillance and delivery, and even more important for those operating in disaster relief. Therefore, the project seeks to increase endurance by incorporating helium into the drone to provide static lift. This will be done by modifying and redesigning existing drone structures to incorporate balloons inflated with helium. As such, the effects of incorporating such structures on the drone will be investigated. An experiment on the effects of having a pair toroidal shape balloon around the rotor on the thrust will be conducted, with simulation done to find possible ways to optimise such effects. In the process of experimentation and simulation, a prototype will be built for a flight test and suggestions to be made for further works will be discussed. Bachelor of Engineering (Mechanical Engineering) 2020-06-03T02:41:21Z 2020-06-03T02:41:21Z 2020 Final Year Project (FYP) https://hdl.handle.net/10356/140931 en B211 application/pdf Nanyang Technological University
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic Engineering::Mechanical engineering
spellingShingle Engineering::Mechanical engineering
See, Kelwin Chun Gan
Optimisation of helium-assisted drone : control and flight analysis
description Recent developments in technology has led to an increased interest in drones and their applications, as well as widespread usage. While certain industries have managed to exploit the usage of drones to a large degree, applications in other areas such as Human Aid and Disaster Relief has immense potential for drone applications. The challenge of using drones in such areas are its low endurance and payload. Endurance is critical especially for drones that are required for surveillance and delivery, and even more important for those operating in disaster relief. Therefore, the project seeks to increase endurance by incorporating helium into the drone to provide static lift. This will be done by modifying and redesigning existing drone structures to incorporate balloons inflated with helium. As such, the effects of incorporating such structures on the drone will be investigated. An experiment on the effects of having a pair toroidal shape balloon around the rotor on the thrust will be conducted, with simulation done to find possible ways to optimise such effects. In the process of experimentation and simulation, a prototype will be built for a flight test and suggestions to be made for further works will be discussed.
author2 Lam Yee Cheong
author_facet Lam Yee Cheong
See, Kelwin Chun Gan
format Final Year Project
author See, Kelwin Chun Gan
author_sort See, Kelwin Chun Gan
title Optimisation of helium-assisted drone : control and flight analysis
title_short Optimisation of helium-assisted drone : control and flight analysis
title_full Optimisation of helium-assisted drone : control and flight analysis
title_fullStr Optimisation of helium-assisted drone : control and flight analysis
title_full_unstemmed Optimisation of helium-assisted drone : control and flight analysis
title_sort optimisation of helium-assisted drone : control and flight analysis
publisher Nanyang Technological University
publishDate 2020
url https://hdl.handle.net/10356/140931
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