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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Bibliographic Details
Main Author: Lee, Na Shen.
Other Authors: School of Mechanical and Aerospace Engineering
Format: Thesis
Language:English
Published: 2013
Subjects:
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.
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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