Leader-follower of quadrotor micro aerial vehicle

A Micro Aerial Vehicle (MAV) is known as a drone or in a bigger size is called Unmanned Aerial Vehicle (UAV). Quadrotors are leading edge of a huge development in military and civilian such as disaster search and rescue, surveillance, aerial mapping and others. However, those applications limits by...

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Main Authors: Pebrianti, Dwi, Chun, Yee Woon, Hao, Yong Hooi, Qian, Goh Ming, Mahfuzah, Mustafa, Rosdiyana, Samad, Bayuaji, Luhur
Format: Article
Language:English
Published: UTeM 2018
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Online Access:http://umpir.ump.edu.my/id/eprint/21014/1/Leader%20follower%20of%20quadrotor%20micro%20aerial%20vehicle.pdf
http://umpir.ump.edu.my/id/eprint/21014/
http://journal.utem.edu.my/index.php/jtec/article/view/3323/2392
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spelling my.ump.umpir.210142018-08-20T05:34:58Z http://umpir.ump.edu.my/id/eprint/21014/ Leader-follower of quadrotor micro aerial vehicle Pebrianti, Dwi Chun, Yee Woon Hao, Yong Hooi Qian, Goh Ming Mahfuzah, Mustafa Rosdiyana, Samad Bayuaji, Luhur QA76 Computer software TK Electrical engineering. Electronics Nuclear engineering A Micro Aerial Vehicle (MAV) is known as a drone or in a bigger size is called Unmanned Aerial Vehicle (UAV). Quadrotors are leading edge of a huge development in military and civilian such as disaster search and rescue, surveillance, aerial mapping and others. However, those applications limits by the payload delivered and long execution time. Hence, this study focuses on Leader-Follower approach of Quadrotor MAV. The study covers the development of quadrotor platform, modelling, controller design and leader-follower implementation. As the preliminary study, an Android phone is used as a leader which is used to provide the desired position and orientation to the follower quadrotor. The follower will be an autonomous quadrotor. Proportional Integral Derivative (PID) controller for the position and attitude control are first designed and tested via simulation. Then, a real flight implementation is conducted. The result shows that the follower can follow the leader on a circular path and straight line path. The settling time for X, Y and Z position of the follower is 10.22, 10.90 and 19.45 seconds, respectively. Additionally, the overshoot percentage for X, Y and Z position are 7%, 0% and 0%, respectively. UTeM 2018 Article PeerReviewed pdf en cc_by http://umpir.ump.edu.my/id/eprint/21014/1/Leader%20follower%20of%20quadrotor%20micro%20aerial%20vehicle.pdf Pebrianti, Dwi and Chun, Yee Woon and Hao, Yong Hooi and Qian, Goh Ming and Mahfuzah, Mustafa and Rosdiyana, Samad and Bayuaji, Luhur (2018) Leader-follower of quadrotor micro aerial vehicle. Journal of Telecommunication, Electronic and Computer Engineering, 10 (1-2). pp. 67-73. ISSN 2180-1843 (Print); 2289-8131 (Online) http://journal.utem.edu.my/index.php/jtec/article/view/3323/2392
institution Universiti Malaysia Pahang
building UMP Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Malaysia Pahang
content_source UMP Institutional Repository
url_provider http://umpir.ump.edu.my/
language English
topic QA76 Computer software
TK Electrical engineering. Electronics Nuclear engineering
spellingShingle QA76 Computer software
TK Electrical engineering. Electronics Nuclear engineering
Pebrianti, Dwi
Chun, Yee Woon
Hao, Yong Hooi
Qian, Goh Ming
Mahfuzah, Mustafa
Rosdiyana, Samad
Bayuaji, Luhur
Leader-follower of quadrotor micro aerial vehicle
description A Micro Aerial Vehicle (MAV) is known as a drone or in a bigger size is called Unmanned Aerial Vehicle (UAV). Quadrotors are leading edge of a huge development in military and civilian such as disaster search and rescue, surveillance, aerial mapping and others. However, those applications limits by the payload delivered and long execution time. Hence, this study focuses on Leader-Follower approach of Quadrotor MAV. The study covers the development of quadrotor platform, modelling, controller design and leader-follower implementation. As the preliminary study, an Android phone is used as a leader which is used to provide the desired position and orientation to the follower quadrotor. The follower will be an autonomous quadrotor. Proportional Integral Derivative (PID) controller for the position and attitude control are first designed and tested via simulation. Then, a real flight implementation is conducted. The result shows that the follower can follow the leader on a circular path and straight line path. The settling time for X, Y and Z position of the follower is 10.22, 10.90 and 19.45 seconds, respectively. Additionally, the overshoot percentage for X, Y and Z position are 7%, 0% and 0%, respectively.
format Article
author Pebrianti, Dwi
Chun, Yee Woon
Hao, Yong Hooi
Qian, Goh Ming
Mahfuzah, Mustafa
Rosdiyana, Samad
Bayuaji, Luhur
author_facet Pebrianti, Dwi
Chun, Yee Woon
Hao, Yong Hooi
Qian, Goh Ming
Mahfuzah, Mustafa
Rosdiyana, Samad
Bayuaji, Luhur
author_sort Pebrianti, Dwi
title Leader-follower of quadrotor micro aerial vehicle
title_short Leader-follower of quadrotor micro aerial vehicle
title_full Leader-follower of quadrotor micro aerial vehicle
title_fullStr Leader-follower of quadrotor micro aerial vehicle
title_full_unstemmed Leader-follower of quadrotor micro aerial vehicle
title_sort leader-follower of quadrotor micro aerial vehicle
publisher UTeM
publishDate 2018
url http://umpir.ump.edu.my/id/eprint/21014/1/Leader%20follower%20of%20quadrotor%20micro%20aerial%20vehicle.pdf
http://umpir.ump.edu.my/id/eprint/21014/
http://journal.utem.edu.my/index.php/jtec/article/view/3323/2392
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score 13.160551