Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/54703
Title: Unmanned aerial vehicle formation implementation
Authors: Lee, Na Shen.
Keywords: DRNTU::Engineering::Mechanical engineering
Issue Date: 2012
Abstract: 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.
URI: http://hdl.handle.net/10356/54703
Fulltext Permission: restricted
Fulltext Availability: With Fulltext
Appears in Collections:MAE Theses

Files in This Item:
File Description SizeFormat 
NaShenLee12.pdf
  Restricted Access
Main report1.18 MBAdobe PDFView/Open

Page view(s) 1

222
checked on Oct 19, 2020

Download(s) 1

8
checked on Oct 19, 2020

Google ScholarTM

Check

Items in DR-NTU are protected by copyright, with all rights reserved, unless otherwise indicated.