Stabilization and trajectory tracking control for underactuated quadrotor helicopter subject to wind-gust disturbance

The control of quadrotor helicopter has been a great challenge for control engineers and researchers since quadrotor is an underactuated and a highly unstable nonlinear system. In this paper, the dynamic model of quadrotor has been derived and a so-called robust optimal backstepping control (ROBC) i...

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Main Authors: Mohd. Basri, Mohd. Ariffanan, Husain, Abdul Rashid, Danapalasingam, Kumeresan A.
Format: Article
Language:English
Published: Springer India 2015
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Online Access:http://eprints.utm.my/id/eprint/56064/1/MohdAriffananMohdBasri2015_StabilizationandTrajectoryTrackingControlforUnderacturedQuadrotor.pdf
http://eprints.utm.my/id/eprint/56064/
http://dx.doi.org/10.1007/s12046-015-0384-4
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spelling my.utm.560642016-11-15T07:20:22Z http://eprints.utm.my/id/eprint/56064/ Stabilization and trajectory tracking control for underactuated quadrotor helicopter subject to wind-gust disturbance Mohd. Basri, Mohd. Ariffanan Husain, Abdul Rashid Danapalasingam, Kumeresan A. TK Electrical engineering. Electronics Nuclear engineering The control of quadrotor helicopter has been a great challenge for control engineers and researchers since quadrotor is an underactuated and a highly unstable nonlinear system. In this paper, the dynamic model of quadrotor has been derived and a so-called robust optimal backstepping control (ROBC) is designed to address its stabilization and trajectory tracking problem in the existence of external disturbances. The robust controller is achieved by incorporating a prior designed optimal backstepping control (OBC) with a switching function. The control law design utilizes the switching function in order to attenuate the effects caused by external disturbances. In order to eliminate the chattering phenomenon, the sign function is replaced by the saturation function. A new heuristic algorithm namely Gravitational Search Algorithm (GSA) has been employed in designing the OBC. The proposed method is evaluated on a quadrotor simulation environment to demonstrate the effectiveness and merits of the theoretical development. Simulation results show that the proposed ROBC scheme can achieve favorable control performances compared to the OBC for autonomous quadrotor helicopter in the presence of external disturbances. Springer India 2015-08-01 Article PeerReviewed application/pdf en http://eprints.utm.my/id/eprint/56064/1/MohdAriffananMohdBasri2015_StabilizationandTrajectoryTrackingControlforUnderacturedQuadrotor.pdf Mohd. Basri, Mohd. Ariffanan and Husain, Abdul Rashid and Danapalasingam, Kumeresan A. (2015) Stabilization and trajectory tracking control for underactuated quadrotor helicopter subject to wind-gust disturbance. Sadhana - Academy Proceedings in Engineering Sciences, 40 (5). pp. 1531-1553. ISSN 0256-2499 http://dx.doi.org/10.1007/s12046-015-0384-4 DOI:10.1007/s12046-015-0384-4
institution Universiti Teknologi Malaysia
building UTM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknologi Malaysia
content_source UTM Institutional Repository
url_provider http://eprints.utm.my/
language English
topic TK Electrical engineering. Electronics Nuclear engineering
spellingShingle TK Electrical engineering. Electronics Nuclear engineering
Mohd. Basri, Mohd. Ariffanan
Husain, Abdul Rashid
Danapalasingam, Kumeresan A.
Stabilization and trajectory tracking control for underactuated quadrotor helicopter subject to wind-gust disturbance
description The control of quadrotor helicopter has been a great challenge for control engineers and researchers since quadrotor is an underactuated and a highly unstable nonlinear system. In this paper, the dynamic model of quadrotor has been derived and a so-called robust optimal backstepping control (ROBC) is designed to address its stabilization and trajectory tracking problem in the existence of external disturbances. The robust controller is achieved by incorporating a prior designed optimal backstepping control (OBC) with a switching function. The control law design utilizes the switching function in order to attenuate the effects caused by external disturbances. In order to eliminate the chattering phenomenon, the sign function is replaced by the saturation function. A new heuristic algorithm namely Gravitational Search Algorithm (GSA) has been employed in designing the OBC. The proposed method is evaluated on a quadrotor simulation environment to demonstrate the effectiveness and merits of the theoretical development. Simulation results show that the proposed ROBC scheme can achieve favorable control performances compared to the OBC for autonomous quadrotor helicopter in the presence of external disturbances.
format Article
author Mohd. Basri, Mohd. Ariffanan
Husain, Abdul Rashid
Danapalasingam, Kumeresan A.
author_facet Mohd. Basri, Mohd. Ariffanan
Husain, Abdul Rashid
Danapalasingam, Kumeresan A.
author_sort Mohd. Basri, Mohd. Ariffanan
title Stabilization and trajectory tracking control for underactuated quadrotor helicopter subject to wind-gust disturbance
title_short Stabilization and trajectory tracking control for underactuated quadrotor helicopter subject to wind-gust disturbance
title_full Stabilization and trajectory tracking control for underactuated quadrotor helicopter subject to wind-gust disturbance
title_fullStr Stabilization and trajectory tracking control for underactuated quadrotor helicopter subject to wind-gust disturbance
title_full_unstemmed Stabilization and trajectory tracking control for underactuated quadrotor helicopter subject to wind-gust disturbance
title_sort stabilization and trajectory tracking control for underactuated quadrotor helicopter subject to wind-gust disturbance
publisher Springer India
publishDate 2015
url http://eprints.utm.my/id/eprint/56064/1/MohdAriffananMohdBasri2015_StabilizationandTrajectoryTrackingControlforUnderacturedQuadrotor.pdf
http://eprints.utm.my/id/eprint/56064/
http://dx.doi.org/10.1007/s12046-015-0384-4
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score 13.160551