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Comparison on the rigid and flexible model of attitude maneuvering of a simple multi-body satellite

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Main Authors: Teoh, Vil Cherd, Shahriman, Abu Bakar, Norhizam, Hamzah, Sazali, Yaacob, Ruslizam, Daud, Rakhmad Arief, Siregar
Other Authors: vaticano87@hotmail.com
Format: Article
Language:English
Published: Institute of Engineering Mathematics, Universiti Malaysia Perlis 2015
Subjects:
Satellite
Flexible
Rigid
Model
Comparison
Online Access:http://dspace.unimap.edu.my:80/xmlui/handle/123456789/40663
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spelling my.unimap-406632018-07-24T01:52:21Z Comparison on the rigid and flexible model of attitude maneuvering of a simple multi-body satellite Teoh, Vil Cherd Shahriman, Abu Bakar Norhizam, Hamzah Sazali, Yaacob Ruslizam, Daud Rakhmad Arief, Siregar vaticano87@hotmail.com Satellite Flexible Rigid Model Comparison Link to publisher's homepage at http://amci.unimap.edu.my Rigid body assumption of a satellite model has been a common practice in spacecraft attitude manoeuvring. However, with the increasing demand for greater functionality of space activities, requires bigger and wider solar panels to cater the power needs. In this paper, simple rigid and flexible multi-body satellite model is derived using basic Newton’s second law and Assumed Mode Method. The response from both model are then simulated using MATLAB software while comparison is done to illustrate the significance of the flexible behaviour that inherited in the satellite system. With the negligence of flexible interference in the rigid model, it is likely to execute an exact attitude motion while the flexible model would yield a harmonic motion that is due to the vibratory motion of the solar panels. 2015-12-30T04:32:10Z 2015-12-30T04:32:10Z 2014 Article Applied Mathematics and Computational Intelligence (AMCI), vol.3 (1), 2014, pages 229-240 2289-1323 (online) 2289-1315 (print) http://amci.unimap.edu.my http://dspace.unimap.edu.my:80/xmlui/handle/123456789/40663 en Institute of Engineering Mathematics, Universiti Malaysia Perlis
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 Satellite
Flexible
Rigid
Model
Comparison
spellingShingle Satellite
Flexible
Rigid
Model
Comparison
Teoh, Vil Cherd
Shahriman, Abu Bakar
Norhizam, Hamzah
Sazali, Yaacob
Ruslizam, Daud
Rakhmad Arief, Siregar
Comparison on the rigid and flexible model of attitude maneuvering of a simple multi-body satellite
description Link to publisher's homepage at http://amci.unimap.edu.my
author2 vaticano87@hotmail.com
author_facet vaticano87@hotmail.com
Teoh, Vil Cherd
Shahriman, Abu Bakar
Norhizam, Hamzah
Sazali, Yaacob
Ruslizam, Daud
Rakhmad Arief, Siregar
format Article
author Teoh, Vil Cherd
Shahriman, Abu Bakar
Norhizam, Hamzah
Sazali, Yaacob
Ruslizam, Daud
Rakhmad Arief, Siregar
author_sort Teoh, Vil Cherd
title Comparison on the rigid and flexible model of attitude maneuvering of a simple multi-body satellite
title_short Comparison on the rigid and flexible model of attitude maneuvering of a simple multi-body satellite
title_full Comparison on the rigid and flexible model of attitude maneuvering of a simple multi-body satellite
title_fullStr Comparison on the rigid and flexible model of attitude maneuvering of a simple multi-body satellite
title_full_unstemmed Comparison on the rigid and flexible model of attitude maneuvering of a simple multi-body satellite
title_sort comparison on the rigid and flexible model of attitude maneuvering of a simple multi-body satellite
publisher Institute of Engineering Mathematics, Universiti Malaysia Perlis
publishDate 2015
url http://dspace.unimap.edu.my:80/xmlui/handle/123456789/40663
_version_ 1643804041929555968
score 13.222552

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