Finite element software development for dynamic analysis and simulation of a Flexible Satellite Orbiting in space
Organized by School of Mechatronic Engineering (UniMAP) & co-organized by The Institution of Engineering Malaysia (IEM), 11th - 13th October 2009 at Batu Feringhi, Penang, Malaysia.
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Language: | English |
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Universiti Malaysia Perlis
2009
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Online Access: | http://dspace.unimap.edu.my/xmlui/handle/123456789/7209 |
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my.unimap-72092009-11-17T06:18:08Z Finite element software development for dynamic analysis and simulation of a Flexible Satellite Orbiting in space Setyamartana, Parman Artificial satellites Artificial satellites -- Design and construction Artificial satellites -- Materials Lightweight materials Artificial satellites -- Dynamics Organized by School of Mechatronic Engineering (UniMAP) & co-organized by The Institution of Engineering Malaysia (IEM), 11th - 13th October 2009 at Batu Feringhi, Penang, Malaysia. A computer code to simulate dynamics of flexible satellites orbiting the earth is developed. As the particular model, the satellite consisting of a rigid main body and two symmetrical flexible solar panels is observed. The motion of the solar panels is discretized by using finite element method. For this purpose the solar panels are supposed as a number of rectangular plate elements. The natural frequencies are then studied in order to determine the important modes during its operation. 2009-11-06T08:24:40Z 2009-11-06T08:24:40Z 2009-10-11 Working Paper p.7F 1 - 7F 7 978-967-5415-07-4 http://hdl.handle.net/123456789/7209 en Proceedings of International Conference on Applications and Design in Mechanical Engineering 2009 (iCADME 2009) Universiti Malaysia Perlis |
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Artificial satellites Artificial satellites -- Design and construction Artificial satellites -- Materials Lightweight materials Artificial satellites -- Dynamics |
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Artificial satellites Artificial satellites -- Design and construction Artificial satellites -- Materials Lightweight materials Artificial satellites -- Dynamics Setyamartana, Parman Finite element software development for dynamic analysis and simulation of a Flexible Satellite Orbiting in space |
description |
Organized by School of Mechatronic Engineering (UniMAP) & co-organized by The Institution of Engineering Malaysia (IEM), 11th - 13th October 2009 at Batu Feringhi, Penang, Malaysia. |
format |
Working Paper |
author |
Setyamartana, Parman |
author_facet |
Setyamartana, Parman |
author_sort |
Setyamartana, Parman |
title |
Finite element software development for dynamic analysis and simulation of a Flexible Satellite Orbiting in space |
title_short |
Finite element software development for dynamic analysis and simulation of a Flexible Satellite Orbiting in space |
title_full |
Finite element software development for dynamic analysis and simulation of a Flexible Satellite Orbiting in space |
title_fullStr |
Finite element software development for dynamic analysis and simulation of a Flexible Satellite Orbiting in space |
title_full_unstemmed |
Finite element software development for dynamic analysis and simulation of a Flexible Satellite Orbiting in space |
title_sort |
finite element software development for dynamic analysis and simulation of a flexible satellite orbiting in space |
publisher |
Universiti Malaysia Perlis |
publishDate |
2009 |
url |
http://dspace.unimap.edu.my/xmlui/handle/123456789/7209 |
_version_ |
1643788759254171648 |
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13.18916 |