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Waypoint navigation of quad-rotor MAV

Quad-rotor Micro Aerial Vehicle (MAV) is a multi-rotor MAV with 4 propellers which propel the MAV up to the air and move around. It has high maneuverability to move around, such as roll, pitch and yaw movements. However, line of sight and radio control effective range are the major limitation for t...

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Main Authors: Goh, Ming Qian, Pebrianti, Dwi, Yee, Woon Chun, Yoon, Hooi Hao, Bayuaji, Luhur
Format: Conference or Workshop Item
Language:English
Published: IEEE 2017
Subjects:
TK Electrical engineering. Electronics Nuclear engineering
Online Access:http://umpir.ump.edu.my/id/eprint/21916/7/Waypoint%20Navigation%20of%20Quad-rotor%20MAV1.pdf
http://umpir.ump.edu.my/id/eprint/21916/
https://doi.org/10.1109/ICSEngT.2017.8123417
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spelling my.ump.umpir.219162018-08-30T08:13:18Z http://umpir.ump.edu.my/id/eprint/21916/ Waypoint navigation of quad-rotor MAV Goh, Ming Qian Pebrianti, Dwi Yee, Woon Chun Yoon, Hooi Hao Bayuaji, Luhur TK Electrical engineering. Electronics Nuclear engineering Quad-rotor Micro Aerial Vehicle (MAV) is a multi-rotor MAV with 4 propellers which propel the MAV up to the air and move around. It has high maneuverability to move around, such as roll, pitch and yaw movements. However, line of sight and radio control effective range are the major limitation for the MAVs which significantly shorten the travel distance. Therefore, we proposed a waypoint navigation quad-rotor MAV based on PID controller in this paper. User can set mission with multiple waypoint and the PID controller to control MAV autonomously moving along the waypoint to the desired position without remotely controlled by radio control and guidance of pilot. The results show PID controller is capable to control MAV to move to the desired position with high accuracy. As the conclusion, the result of real flight experiment shows that the %OS of designed PID controller for x is 13% while y is 11.89% and z is 2.34%. Meanwhile, steadystate error for all axis are 0%. This shows that the performance of PID controller is satisfied. Hence, the quadrotor MAV could move to the desired location via waypoint navigation without guidance of pilot. IEEE 2017-10-02 Conference or Workshop Item PeerReviewed pdf en http://umpir.ump.edu.my/id/eprint/21916/7/Waypoint%20Navigation%20of%20Quad-rotor%20MAV1.pdf Goh, Ming Qian and Pebrianti, Dwi and Yee, Woon Chun and Yoon, Hooi Hao and Bayuaji, Luhur (2017) Waypoint navigation of quad-rotor MAV. In: 7th IEEE International Conference on System Engineering and Technology (ICSET 2017), 2-3 October 2017 , Shah Alam, Malaysia. pp. 38-42.. ISBN 978-1-5386-0383-3 https://doi.org/10.1109/ICSEngT.2017.8123417
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 TK Electrical engineering. Electronics Nuclear engineering
spellingShingle TK Electrical engineering. Electronics Nuclear engineering
Goh, Ming Qian
Pebrianti, Dwi
Yee, Woon Chun
Yoon, Hooi Hao
Bayuaji, Luhur
Waypoint navigation of quad-rotor MAV
description Quad-rotor Micro Aerial Vehicle (MAV) is a multi-rotor MAV with 4 propellers which propel the MAV up to the air and move around. It has high maneuverability to move around, such as roll, pitch and yaw movements. However, line of sight and radio control effective range are the major limitation for the MAVs which significantly shorten the travel distance. Therefore, we proposed a waypoint navigation quad-rotor MAV based on PID controller in this paper. User can set mission with multiple waypoint and the PID controller to control MAV autonomously moving along the waypoint to the desired position without remotely controlled by radio control and guidance of pilot. The results show PID controller is capable to control MAV to move to the desired position with high accuracy. As the conclusion, the result of real flight experiment shows that the %OS of designed PID controller for x is 13% while y is 11.89% and z is 2.34%. Meanwhile, steadystate error for all axis are 0%. This shows that the performance of PID controller is satisfied. Hence, the quadrotor MAV could move to the desired location via waypoint navigation without guidance of pilot.
format Conference or Workshop Item
author Goh, Ming Qian
Pebrianti, Dwi
Yee, Woon Chun
Yoon, Hooi Hao
Bayuaji, Luhur
author_facet Goh, Ming Qian
Pebrianti, Dwi
Yee, Woon Chun
Yoon, Hooi Hao
Bayuaji, Luhur
author_sort Goh, Ming Qian
title Waypoint navigation of quad-rotor MAV
title_short Waypoint navigation of quad-rotor MAV
title_full Waypoint navigation of quad-rotor MAV
title_fullStr Waypoint navigation of quad-rotor MAV
title_full_unstemmed Waypoint navigation of quad-rotor MAV
title_sort waypoint navigation of quad-rotor mav
publisher IEEE
publishDate 2017
url http://umpir.ump.edu.my/id/eprint/21916/7/Waypoint%20Navigation%20of%20Quad-rotor%20MAV1.pdf
http://umpir.ump.edu.my/id/eprint/21916/
https://doi.org/10.1109/ICSEngT.2017.8123417
_version_ 1643669247808765952
score 13.211869

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