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Dynamic model and simulation on attitude menoeuvring of flexible satellite

The 2nd International Malaysia-Ireland Joint Symposium on Engineering, Science and Business 2012 (IMiEJS2012) jointly organized by Universiti Malaysia Perlis and Athlone Institute of Technology in collaboration with The Ministry of Higher Education (MOHE) Malaysia, Education Malaysia and Malay...

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Main Authors: Teoh, Vil Cherd, Sazali, Yaacob, Prof. Dr., Shahriman, Abu Bakar, Dr., Rakhmad Arief, Siregar, Dr.
Other Authors: vaticano87@hotmail.com
Format: Working Paper
Language:English
Published: Universiti Malaysia Perlis (UniMAP) 2013
Subjects:
Flexible
Attitude control
Satellite
Online Access:http://dspace.unimap.edu.my/xmlui/handle/123456789/30782
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spelling my.unimap-307822013-12-23T07:28:44Z Dynamic model and simulation on attitude menoeuvring of flexible satellite Teoh, Vil Cherd Sazali, Yaacob, Prof. Dr. Shahriman, Abu Bakar, Dr. Rakhmad Arief, Siregar, Dr. vaticano87@hotmail.com s.yaacob@unimap.edu.my shahriman@unimap.edu.my rakhmad@unimap.edu.my Flexible Attitude control Satellite The 2nd International Malaysia-Ireland Joint Symposium on Engineering, Science and Business 2012 (IMiEJS2012) jointly organized by Universiti Malaysia Perlis and Athlone Institute of Technology in collaboration with The Ministry of Higher Education (MOHE) Malaysia, Education Malaysia and Malaysia Postgraduates Student Association Ireland (MyPSI), 18th - 19th June 2012 at Putra World Trade Center (PWTC), Kuala Lumpur, Malaysia. Flexibility has gained much interest in satellite design in recent years due to its capability to accommodate much for functionality with minimum trade-off. A flexible satellite is satellite that consists of many movable components that is much more sceptical towards external and internal interferences. In this paper, the flexible model of the hexagonal bodied satellite with 3 appendages is derived. Natural physical properties of the satellite were used to derive the mathematical model based on the principle axis of the moment of inertia of the satellite. Verification on the mathematical model is done using MATLAB software to simulate the dynamic behaviour of the satellite. This paper only demonstrates the passive control method. 2013-12-23T07:28:44Z 2013-12-23T07:28:44Z 2012-06-18 Working Paper p. 333 - 341 978-967-5760-11-2 http://hdl.handle.net/123456789/30782 en Proceedings of the The 2nd International Malaysia-Ireland Joint Symposium on Engineering, Science and Business 2012 (IMiEJS2012); Universiti Malaysia Perlis (UniMAP)
institution Universiti Malaysia Perlis
building UniMAP Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Malaysia Perlis
content_source UniMAP Library Digital Repository
url_provider http://dspace.unimap.edu.my/
language English
topic Flexible
Attitude control
Satellite
spellingShingle Flexible
Attitude control
Satellite
Teoh, Vil Cherd
Sazali, Yaacob, Prof. Dr.
Shahriman, Abu Bakar, Dr.
Rakhmad Arief, Siregar, Dr.
Dynamic model and simulation on attitude menoeuvring of flexible satellite
description The 2nd International Malaysia-Ireland Joint Symposium on Engineering, Science and Business 2012 (IMiEJS2012) jointly organized by Universiti Malaysia Perlis and Athlone Institute of Technology in collaboration with The Ministry of Higher Education (MOHE) Malaysia, Education Malaysia and Malaysia Postgraduates Student Association Ireland (MyPSI), 18th - 19th June 2012 at Putra World Trade Center (PWTC), Kuala Lumpur, Malaysia.
author2 vaticano87@hotmail.com
author_facet vaticano87@hotmail.com
Teoh, Vil Cherd
Sazali, Yaacob, Prof. Dr.
Shahriman, Abu Bakar, Dr.
Rakhmad Arief, Siregar, Dr.
format Working Paper
author Teoh, Vil Cherd
Sazali, Yaacob, Prof. Dr.
Shahriman, Abu Bakar, Dr.
Rakhmad Arief, Siregar, Dr.
author_sort Teoh, Vil Cherd
title Dynamic model and simulation on attitude menoeuvring of flexible satellite
title_short Dynamic model and simulation on attitude menoeuvring of flexible satellite
title_full Dynamic model and simulation on attitude menoeuvring of flexible satellite
title_fullStr Dynamic model and simulation on attitude menoeuvring of flexible satellite
title_full_unstemmed Dynamic model and simulation on attitude menoeuvring of flexible satellite
title_sort dynamic model and simulation on attitude menoeuvring of flexible satellite
publisher Universiti Malaysia Perlis (UniMAP)
publishDate 2013
url http://dspace.unimap.edu.my/xmlui/handle/123456789/30782
_version_ 1643795597976666112
score 13.209306

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