| dc.contributor.author | Teoh, Vil Cherd | |
| dc.contributor.author | Sazali, Yaacob, Prof. Dr. | |
| dc.contributor.author | Shahriman, Abu Bakar, Dr. | |
| dc.contributor.author | Rakhmad Arief, Siregar, Dr. | |
| dc.date.accessioned | 2013-12-23T07:28:44Z | |
| dc.date.available | 2013-12-23T07:28:44Z | |
| dc.date.issued | 2012-06-18 | |
| dc.identifier.citation | p. 333 - 341 | en_US |
| dc.identifier.isbn | 978-967-5760-11-2 | |
| dc.identifier.uri | http://dspace.unimap.edu.my/123456789/30782 | |
| dc.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. | en_US |
| dc.description.abstract | 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. | en_US |
| dc.language.iso | en | en_US |
| dc.publisher | Universiti Malaysia Perlis (UniMAP) | en_US |
| dc.relation.ispartofseries | Proceedings of the The 2nd International Malaysia-Ireland Joint Symposium on Engineering, Science and Business 2012 (IMiEJS2012); | |
| dc.subject | Flexible | en_US |
| dc.subject | Attitude control | en_US |
| dc.subject | Satellite | en_US |
| dc.title | Dynamic model and simulation on attitude menoeuvring of flexible satellite | en_US |
| dc.type | Working Paper | en_US |
| dc.contributor.url | vaticano87@hotmail.com | en_US |
| dc.contributor.url | s.yaacob@unimap.edu.my | en_US |
| dc.contributor.url | shahriman@unimap.edu.my | en_US |
| dc.contributor.url | rakhmad@unimap.edu.my | en_US |
