Control of co-axial UAV
Over the period of 1 year, an unmanned coaxial helicopter would be designed and tested. The aim of the project is to achieve an unmanned hover. In process, a suitable coaxial helicopter which could carry the electronics payload, which are being used to control the helicopter for an unmanned fligh...
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Other Authors: | |
Format: | Final Year Project (FYP) |
Language: | English |
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2010
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Online Access: | http://hdl.handle.net/10356/40190 |
_version_ | 1826112166832373760 |
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author | Ong, Yi Yang. |
author2 | Wang Jianliang |
author_facet | Wang Jianliang Ong, Yi Yang. |
author_sort | Ong, Yi Yang. |
collection | NTU |
description | Over the period of 1 year, an unmanned coaxial helicopter would be designed and
tested. The aim of the project is to achieve an unmanned hover. In process, a suitable
coaxial helicopter which could carry the electronics payload, which are being used to
control the helicopter for an unmanned flight is to be sourced. Tests are done to
check that the electronics and the helicopter can be integrated together to achieve the
aim of the project.
In this report, research, testing and results of the development of an unmanned
coaxial helicopter will be consolidated and explained. Issues encountered during
each phase of the development progress are noted down so as to prevent similar
mistakes from happening in the future in the development of the project. |
first_indexed | 2024-10-01T03:02:31Z |
format | Final Year Project (FYP) |
id | ntu-10356/40190 |
institution | Nanyang Technological University |
language | English |
last_indexed | 2024-10-01T03:02:31Z |
publishDate | 2010 |
record_format | dspace |
spelling | ntu-10356/401902023-07-07T17:08:25Z Control of co-axial UAV Ong, Yi Yang. Wang Jianliang School of Electrical and Electronic Engineering DRNTU::Engineering::Electrical and electronic engineering::Electric power Over the period of 1 year, an unmanned coaxial helicopter would be designed and tested. The aim of the project is to achieve an unmanned hover. In process, a suitable coaxial helicopter which could carry the electronics payload, which are being used to control the helicopter for an unmanned flight is to be sourced. Tests are done to check that the electronics and the helicopter can be integrated together to achieve the aim of the project. In this report, research, testing and results of the development of an unmanned coaxial helicopter will be consolidated and explained. Issues encountered during each phase of the development progress are noted down so as to prevent similar mistakes from happening in the future in the development of the project. Bachelor of Engineering 2010-06-11T04:48:44Z 2010-06-11T04:48:44Z 2010 2010 Final Year Project (FYP) http://hdl.handle.net/10356/40190 en Nanyang Technological University 42 p. application/pdf |
spellingShingle | DRNTU::Engineering::Electrical and electronic engineering::Electric power Ong, Yi Yang. Control of co-axial UAV |
title | Control of co-axial UAV |
title_full | Control of co-axial UAV |
title_fullStr | Control of co-axial UAV |
title_full_unstemmed | Control of co-axial UAV |
title_short | Control of co-axial UAV |
title_sort | control of co axial uav |
topic | DRNTU::Engineering::Electrical and electronic engineering::Electric power |
url | http://hdl.handle.net/10356/40190 |
work_keys_str_mv | AT ongyiyang controlofcoaxialuav |