| dc.contributor.author | Setyamartana, Parman | |
| dc.date.accessioned | 2009-11-06T08:24:40Z | |
| dc.date.available | 2009-11-06T08:24:40Z | |
| dc.date.issued | 2009-10-11 | |
| dc.identifier.citation | p.7F 1 - 7F 7 | en_US |
| dc.identifier.isbn | 978-967-5415-07-4 | |
| dc.identifier.uri | http://dspace.unimap.edu.my/123456789/7209 | |
| dc.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. | en_US |
| dc.description.abstract | 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. | en_US |
| dc.language.iso | en | en_US |
| dc.publisher | Universiti Malaysia Perlis | en_US |
| dc.relation.ispartofseries | Proceedings of International Conference on Applications and Design in Mechanical Engineering 2009 (iCADME 2009) | en_US |
| dc.subject | Artificial satellites | en_US |
| dc.subject | Artificial satellites -- Design and construction | en_US |
| dc.subject | Artificial satellites -- Materials | en_US |
| dc.subject | Lightweight materials | en_US |
| dc.subject | Artificial satellites -- Dynamics | en_US |
| dc.title | Finite element software development for dynamic analysis and simulation of a Flexible Satellite Orbiting in space | en_US |
| dc.type | Working Paper | en_US |
