1. UniMAP Library Digital Repository
  2. The Library
  3. Conference Papers
Please use this identifier to cite or link to this item: http://dspace.unimap.edu.my:80/xmlui/handle/123456789/30782
Full metadata record
DC FieldValueLanguage
dc.contributor.authorTeoh, Vil Cherd-
dc.contributor.authorSazali, Yaacob, Prof. Dr.-
dc.contributor.authorShahriman, Abu Bakar, Dr.-
dc.contributor.authorRakhmad Arief, Siregar, Dr.-
dc.date.accessioned2013-12-23T07:28:44Z-
dc.date.available2013-12-23T07:28:44Z-
dc.date.issued2012-06-18-
dc.identifier.citationp. 333 - 341en_US
dc.identifier.isbn978-967-5760-11-2-
dc.identifier.urihttp://dspace.unimap.edu.my/123456789/30782-
dc.descriptionThe 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.abstractFlexibility 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.isoenen_US
dc.publisherUniversiti Malaysia Perlis (UniMAP)en_US
dc.relation.ispartofseriesProceedings of the The 2nd International Malaysia-Ireland Joint Symposium on Engineering, Science and Business 2012 (IMiEJS2012);-
dc.subjectFlexibleen_US
dc.subjectAttitude controlen_US
dc.subjectSatelliteen_US
dc.titleDynamic model and simulation on attitude menoeuvring of flexible satelliteen_US
dc.typeWorking Paperen_US
dc.contributor.urlvaticano87@hotmail.comen_US
dc.contributor.urls.yaacob@unimap.edu.myen_US
dc.contributor.urlshahriman@unimap.edu.myen_US
dc.contributor.urlrakhmad@unimap.edu.myen_US
Appears in Collections:Conference Papers
Rakhmad Arief Siregar, Dr.
Sazali Yaacob, Prof. Dr.
Shahriman Abu Bakar, Assoc. Prof. Ir. Ts. Dr.

Files in This Item:
File Description SizeFormat 
pg 333 - 341.pdfAccess is limited to UniMAP community417.59 kBAdobe PDFView/Open
Show simple item record


Items in UniMAP Library Digital Repository are protected by copyright, with all rights reserved, unless otherwise indicated.