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dc.contributor.authorSiti Maryam, Sharun
dc.contributor.authorMohd. Yusof, Mashor, Prof. Dr.
dc.contributor.authorWan Nur Hadani
dc.contributor.authorM.N., Norhayati
dc.contributor.authorSazali, Yaacob, Prof. Dr.
dc.contributor.authorMuhyi, Yaakob
dc.contributor.authorSoh, Warren
dc.date.accessioned2010-11-19T13:15:54Z
dc.date.available2010-11-19T13:15:54Z
dc.date.issued2010-06-02
dc.identifier.citationVol.1(17), p.109-114en_US
dc.identifier.urihttp://dspace.unimap.edu.my/123456789/10245
dc.description1st Regional Conference on Applied and Engineering Mathematics (RCAEM-I) 2010 organized by Universiti Malaysia Perlis (UniMAP) and co-organized by Universiti Sains Malaysia (USM) & Universiti Kebangsaan Malaysia (UKM), 2nd - 3rd June 2010 at Eastern & Oriental Hotel, Penang.en_US
dc.description.abstractIn this paper, a linear mathematical model of the satellite attitude control is derived for the Gravity Gradient (GG) controls method, which represents a passive control design. Natural physical properties of the satellite and its environment were used to derive the mathematical model. After completing the mathematical derivation, simulation results were carried out using MATLAB software. This paper demonstrates that the purely passive GG stabilization is unsatisfactory and the mathematical model of the new system is developed.en_US
dc.language.isoenen_US
dc.publisherUniversiti Malaysia Perlis (UniMAP)en_US
dc.relation.ispartofseriesProceedings of the 1st Regional Conference on Applied and Engineering Mathematics (RCAEM-I) 2010en_US
dc.subjectSatellite attitude controlen_US
dc.subjectGravity Gradient (GG)en_US
dc.subjectPassive control methoden_US
dc.subjectRegional Conference on Applied and Engineering Mathematics (RCAEM)en_US
dc.titleMathematical modeling and simulation for satellite attitude controlen_US
dc.typeWorking Paperen_US
dc.publisher.departmentInstitut Matematik Kejuruteraanen_US
dc.contributor.urlsiti_mrym@ymail.comen_US
dc.contributor.urlhadani@unimap.edu.myen_US


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