Quadrotor stability using PID

The quad rotor is an aerial vehicle whose motion is based on the speed of four motors. Due to its ease of maintenance, high maneuverability, vertical takeoff and landing capabilities (VTOL), etc., it is being increasingly used. The constraint with the quad rotor is the high degree of control requ...

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Main Author:	Awang Besar, Julkifli
Format:	Thesis
Language:	English English English
Published:	2013
Subjects:	TJ Mechanical engineering and machinery
Online Access:	http://eprints.uthm.edu.my/1928/1/24p%20JULKIFLI%20AWANG%20BESAR.pdf http://eprints.uthm.edu.my/1928/2/JULKIFLI%20AWANG%20BESAR%20COPYRIGHT%20DECLARATION.pdf http://eprints.uthm.edu.my/1928/3/JULKIFLI%20AWANG%20BESAR%20WATERMARK.pdf
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id	my-uthm-ep.1928
record_format	uketd_dc
spelling	my-uthm-ep.19282021-10-14T05:40:18Z Quadrotor stability using PID 2013-01 Awang Besar, Julkifli TJ Mechanical engineering and machinery TJ212-225 Control engineering systems. Automatic machinery (General) The quad rotor is an aerial vehicle whose motion is based on the speed of four motors. Due to its ease of maintenance, high maneuverability, vertical takeoff and landing capabilities (VTOL), etc., it is being increasingly used. The constraint with the quad rotor is the high degree of control required for maintaining the stability of the system. It is an inherently unstable system. There are six degrees of freedom – translational and rotational parameters. These are being controlled by 4 actuating signals. The x and y axis translational motion are coupled with the roll and pitch. Thus we need to constantly monitor the state of the system, and give appropriate control signals to the motors. The variation in speeds of the motors based on these signals will help stabilize the system. The unbalanced problem is one of the major problems for quad-rotor. The quad-rotor balance stability will disturb in case the disturbance exist such direct on it like a high wind speed or during outdoor flight. In this project will implement the PID controller for improving the quad-rotor selfbalancing system. The aim of this development is to give a contribution in field of UAV and control system. 2013-01 Thesis http://eprints.uthm.edu.my/1928/ http://eprints.uthm.edu.my/1928/1/24p%20JULKIFLI%20AWANG%20BESAR.pdf text en public http://eprints.uthm.edu.my/1928/2/JULKIFLI%20AWANG%20BESAR%20COPYRIGHT%20DECLARATION.pdf text en staffonly http://eprints.uthm.edu.my/1928/3/JULKIFLI%20AWANG%20BESAR%20WATERMARK.pdf text en validuser mphil masters Universiti Tun Hussein Malaysia Fakulti Kejuruteraan Elektrik dan Elektronik
institution	Universiti Tun Hussein Onn Malaysia
collection	UTHM Institutional Repository
language	English English English
topic	TJ Mechanical engineering and machinery TJ Mechanical engineering and machinery
spellingShingle	TJ Mechanical engineering and machinery TJ Mechanical engineering and machinery Awang Besar, Julkifli Quadrotor stability using PID
description	The quad rotor is an aerial vehicle whose motion is based on the speed of four motors. Due to its ease of maintenance, high maneuverability, vertical takeoff and landing capabilities (VTOL), etc., it is being increasingly used. The constraint with the quad rotor is the high degree of control required for maintaining the stability of the system. It is an inherently unstable system. There are six degrees of freedom – translational and rotational parameters. These are being controlled by 4 actuating signals. The x and y axis translational motion are coupled with the roll and pitch. Thus we need to constantly monitor the state of the system, and give appropriate control signals to the motors. The variation in speeds of the motors based on these signals will help stabilize the system. The unbalanced problem is one of the major problems for quad-rotor. The quad-rotor balance stability will disturb in case the disturbance exist such direct on it like a high wind speed or during outdoor flight. In this project will implement the PID controller for improving the quad-rotor selfbalancing system. The aim of this development is to give a contribution in field of UAV and control system.
format	Thesis
qualification_name	Master of Philosophy (M.Phil.)
qualification_level	Master's degree
author	Awang Besar, Julkifli
author_facet	Awang Besar, Julkifli
author_sort	Awang Besar, Julkifli
title	Quadrotor stability using PID
title_short	Quadrotor stability using PID
title_full	Quadrotor stability using PID
title_fullStr	Quadrotor stability using PID
title_full_unstemmed	Quadrotor stability using PID
title_sort	quadrotor stability using pid
granting_institution	Universiti Tun Hussein Malaysia
granting_department	Fakulti Kejuruteraan Elektrik dan Elektronik
publishDate	2013
url	http://eprints.uthm.edu.my/1928/1/24p%20JULKIFLI%20AWANG%20BESAR.pdf http://eprints.uthm.edu.my/1928/2/JULKIFLI%20AWANG%20BESAR%20COPYRIGHT%20DECLARATION.pdf http://eprints.uthm.edu.my/1928/3/JULKIFLI%20AWANG%20BESAR%20WATERMARK.pdf
_version_	1747830883614720000

Quadrotor stability using PID

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