Modeling and PID Control of a Quadrotor Aerial Robot

This paper elucidates the modeling of a + quadrotor configuration aerial vehicle and the design of its attitude and altitude controllers. The aircraft model consists of four fixed pitch angle propeller, each driven by an electric DC motor. The hovering flight of the quadrotor is governed by the Newt...

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Main Authors: Ismail, Mohd Khairuddin, Anwar, P. P. A. Majeed, Abdul Aziz, Jaafar, Jessnor Arif, Mat Jizat
Format: Article
Language:English
Published: Trans Tech Publications, Switzerland 2014
Subjects:
Online Access:http://umpir.ump.edu.my/id/eprint/5545/
http://umpir.ump.edu.my/id/eprint/5545/
http://umpir.ump.edu.my/id/eprint/5545/
http://umpir.ump.edu.my/id/eprint/5545/1/scan0011.pdf
id ump-5545
recordtype eprints
spelling ump-55452018-05-28T07:46:09Z http://umpir.ump.edu.my/id/eprint/5545/ Modeling and PID Control of a Quadrotor Aerial Robot Ismail, Mohd Khairuddin Anwar, P. P. A. Majeed Abdul Aziz, Jaafar Jessnor Arif, Mat Jizat TS Manufactures This paper elucidates the modeling of a + quadrotor configuration aerial vehicle and the design of its attitude and altitude controllers. The aircraft model consists of four fixed pitch angle propeller, each driven by an electric DC motor. The hovering flight of the quadrotor is governed by the Newton-Euler formulation. The attitude and altitude controls of the aircraft were regulated using heuristically tuned (Proportional-Integral-Derivative) PID controller. It was numerically simulated via Simulink that a PID controller was sufficient to bring the aircraft to the required altitude whereas the attitude of the vehicle is adequately controlled by a PD controller. Trans Tech Publications, Switzerland 2014 Article PeerReviewed application/pdf en http://umpir.ump.edu.my/id/eprint/5545/1/scan0011.pdf Ismail, Mohd Khairuddin and Anwar, P. P. A. Majeed and Abdul Aziz, Jaafar and Jessnor Arif, Mat Jizat (2014) Modeling and PID Control of a Quadrotor Aerial Robot. Advanced Materials Research, 903. pp. 327-331. ISSN 1022-6680 (print), 1662-8985 (online) http://www.scientific.net/AMR.903.327 DOI: 10.4028/www.scientific.net/AMR.903.327
repository_type Digital Repository
institution_category Local University
institution Universiti Malaysia Pahang
building UMP Institutional Repository
collection Online Access
language English
topic TS Manufactures
spellingShingle TS Manufactures
Ismail, Mohd Khairuddin
Anwar, P. P. A. Majeed
Abdul Aziz, Jaafar
Jessnor Arif, Mat Jizat
Modeling and PID Control of a Quadrotor Aerial Robot
description This paper elucidates the modeling of a + quadrotor configuration aerial vehicle and the design of its attitude and altitude controllers. The aircraft model consists of four fixed pitch angle propeller, each driven by an electric DC motor. The hovering flight of the quadrotor is governed by the Newton-Euler formulation. The attitude and altitude controls of the aircraft were regulated using heuristically tuned (Proportional-Integral-Derivative) PID controller. It was numerically simulated via Simulink that a PID controller was sufficient to bring the aircraft to the required altitude whereas the attitude of the vehicle is adequately controlled by a PD controller.
format Article
author Ismail, Mohd Khairuddin
Anwar, P. P. A. Majeed
Abdul Aziz, Jaafar
Jessnor Arif, Mat Jizat
author_facet Ismail, Mohd Khairuddin
Anwar, P. P. A. Majeed
Abdul Aziz, Jaafar
Jessnor Arif, Mat Jizat
author_sort Ismail, Mohd Khairuddin
title Modeling and PID Control of a Quadrotor Aerial Robot
title_short Modeling and PID Control of a Quadrotor Aerial Robot
title_full Modeling and PID Control of a Quadrotor Aerial Robot
title_fullStr Modeling and PID Control of a Quadrotor Aerial Robot
title_full_unstemmed Modeling and PID Control of a Quadrotor Aerial Robot
title_sort modeling and pid control of a quadrotor aerial robot
publisher Trans Tech Publications, Switzerland
publishDate 2014
url http://umpir.ump.edu.my/id/eprint/5545/
http://umpir.ump.edu.my/id/eprint/5545/
http://umpir.ump.edu.my/id/eprint/5545/
http://umpir.ump.edu.my/id/eprint/5545/1/scan0011.pdf
first_indexed 2023-09-18T22:00:52Z
last_indexed 2023-09-18T22:00:52Z
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