Unmanned aerial vehicle formation implementation
Unmanned Aerial Vehicle (UAV) has been a great area of research and the topic of UAV formation is of interest recently. This research focuses on implementing UAV formation on a flying quadrotor platform. The benefits of achieving UAV formation include the capability to provide wider coverag...
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Format: | Thesis |
Language: | English |
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2013
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Online Access: | http://hdl.handle.net/10356/54703 |
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author | Lee, Na Shen. |
author2 | School of Mechanical and Aerospace Engineering |
author_facet | School of Mechanical and Aerospace Engineering Lee, Na Shen. |
author_sort | Lee, Na Shen. |
collection | NTU |
description | Unmanned Aerial Vehicle (UAV) has been a great area of research and the topic of UAV
formation is of interest recently. This research focuses on implementing UAV formation on a
flying quadrotor platform. The benefits of achieving UAV formation include the capability to
provide wider coverage in surveillance and the ability to enhance mission efficiency.
Based on Ascending Technology Pelican quadrotor system, the model of the aircraft was
derived from moment of inertia measurement and parameter estimation. Controllers
(Compensator and PIDcontroller) were designed for simulations and ultimately, PID
controller was implemented on actual flight test.
To simplify the implementation and stay focused on the original objective, the system was
implemented on an unmanned aerial and ground vehicle system (UAV-UGV), with the UGV
as the leader.
There is good matching in the comparison between flight data and simulation results. This
validates the parameters estimation results and proves the performance of the formation
flight controller. |
first_indexed | 2024-10-01T02:41:06Z |
format | Thesis |
id | ntu-10356/54703 |
institution | Nanyang Technological University |
language | English |
last_indexed | 2024-10-01T02:41:06Z |
publishDate | 2013 |
record_format | dspace |
spelling | ntu-10356/547032023-03-11T17:13:22Z Unmanned aerial vehicle formation implementation Lee, Na Shen. School of Mechanical and Aerospace Engineering DRNTU::Engineering::Mechanical engineering Unmanned Aerial Vehicle (UAV) has been a great area of research and the topic of UAV formation is of interest recently. This research focuses on implementing UAV formation on a flying quadrotor platform. The benefits of achieving UAV formation include the capability to provide wider coverage in surveillance and the ability to enhance mission efficiency. Based on Ascending Technology Pelican quadrotor system, the model of the aircraft was derived from moment of inertia measurement and parameter estimation. Controllers (Compensator and PIDcontroller) were designed for simulations and ultimately, PID controller was implemented on actual flight test. To simplify the implementation and stay focused on the original objective, the system was implemented on an unmanned aerial and ground vehicle system (UAV-UGV), with the UGV as the leader. There is good matching in the comparison between flight data and simulation results. This validates the parameters estimation results and proves the performance of the formation flight controller. Master of Engineering (MAE) 2013-07-24T03:31:23Z 2013-07-24T03:31:23Z 2012 2012 Thesis http://hdl.handle.net/10356/54703 en 66 p. application/pdf |
spellingShingle | DRNTU::Engineering::Mechanical engineering Lee, Na Shen. Unmanned aerial vehicle formation implementation |
title | Unmanned aerial vehicle formation implementation |
title_full | Unmanned aerial vehicle formation implementation |
title_fullStr | Unmanned aerial vehicle formation implementation |
title_full_unstemmed | Unmanned aerial vehicle formation implementation |
title_short | Unmanned aerial vehicle formation implementation |
title_sort | unmanned aerial vehicle formation implementation |
topic | DRNTU::Engineering::Mechanical engineering |
url | http://hdl.handle.net/10356/54703 |
work_keys_str_mv | AT leenashen unmannedaerialvehicleformationimplementation |