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Design of aircraft lateral control laws simulation for teaching and learning

This paper studies the design of a simulator to simulate the general behaviour of an aircraft in its lateral motion. The study will be in two parts: the aircraft lateral natural system and the design of the control laws. In the aircraft lateral natural system, all modes will be discussed including...

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Main Authors: Zuhairi Abdul Rashid,, Budinger, Valérie, Pastor, Philippe, Syed Mohd Fairuz Syed Mohd Dardina,, Norzaima Nordin,
Format: Article
Language:English
Published: Penerbit Universiti Kebangsaan Malaysia 2021
Online Access:http://journalarticle.ukm.my/19073/1/15.pdf
http://journalarticle.ukm.my/19073/
https://www.ukm.my/jkukm/si-41-2021/
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spelling my-ukm.journal.190732022-07-26T04:11:32Z http://journalarticle.ukm.my/19073/ Design of aircraft lateral control laws simulation for teaching and learning Zuhairi Abdul Rashid, Budinger, Valérie Pastor, Philippe Syed Mohd Fairuz Syed Mohd Dardina, Norzaima Nordin, This paper studies the design of a simulator to simulate the general behaviour of an aircraft in its lateral motion. The study will be in two parts: the aircraft lateral natural system and the design of the control laws. In the aircraft lateral natural system, all modes will be discussed including the Pure Roll mode, the Dutch Roll mode, and the Spiral mode. In the design of the control laws, two types of control laws were discussed which are the yaw damper and the poles placement method. The result is a complete simulator for aircraft lateral motion which allows the user to simulate and study the lateral characteristic of an aircraft given the desired input. The simulator resulted from this study is suitable to be used for teaching and learning as the changes in parameters yield instantaneous results that can be displayed. Penerbit Universiti Kebangsaan Malaysia 2021 Article PeerReviewed application/pdf en http://journalarticle.ukm.my/19073/1/15.pdf Zuhairi Abdul Rashid, and Budinger, Valérie and Pastor, Philippe and Syed Mohd Fairuz Syed Mohd Dardina, and Norzaima Nordin, (2021) Design of aircraft lateral control laws simulation for teaching and learning. Jurnal Kejuruteraan, 4 (1(SI)). pp. 117-128. ISSN 0128-0198 https://www.ukm.my/jkukm/si-41-2021/
institution Universiti Kebangsaan Malaysia
building Tun Sri Lanang Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Kebangsaan Malaysia
content_source UKM Journal Article Repository
url_provider http://journalarticle.ukm.my/
language English
description This paper studies the design of a simulator to simulate the general behaviour of an aircraft in its lateral motion. The study will be in two parts: the aircraft lateral natural system and the design of the control laws. In the aircraft lateral natural system, all modes will be discussed including the Pure Roll mode, the Dutch Roll mode, and the Spiral mode. In the design of the control laws, two types of control laws were discussed which are the yaw damper and the poles placement method. The result is a complete simulator for aircraft lateral motion which allows the user to simulate and study the lateral characteristic of an aircraft given the desired input. The simulator resulted from this study is suitable to be used for teaching and learning as the changes in parameters yield instantaneous results that can be displayed.
format Article
author Zuhairi Abdul Rashid,
Budinger, Valérie
Pastor, Philippe
Syed Mohd Fairuz Syed Mohd Dardina,
Norzaima Nordin,
spellingShingle Zuhairi Abdul Rashid,
Budinger, Valérie
Pastor, Philippe
Syed Mohd Fairuz Syed Mohd Dardina,
Norzaima Nordin,
Design of aircraft lateral control laws simulation for teaching and learning
author_facet Zuhairi Abdul Rashid,
Budinger, Valérie
Pastor, Philippe
Syed Mohd Fairuz Syed Mohd Dardina,
Norzaima Nordin,
author_sort Zuhairi Abdul Rashid,
title Design of aircraft lateral control laws simulation for teaching and learning
title_short Design of aircraft lateral control laws simulation for teaching and learning
title_full Design of aircraft lateral control laws simulation for teaching and learning
title_fullStr Design of aircraft lateral control laws simulation for teaching and learning
title_full_unstemmed Design of aircraft lateral control laws simulation for teaching and learning
title_sort design of aircraft lateral control laws simulation for teaching and learning
publisher Penerbit Universiti Kebangsaan Malaysia
publishDate 2021
url http://journalarticle.ukm.my/19073/1/15.pdf
http://journalarticle.ukm.my/19073/
https://www.ukm.my/jkukm/si-41-2021/
_version_ 1739829189530353664
score 13.211869

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