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Please use this identifier to cite or link to this item: http://dspace.unimap.edu.my:80/xmlui/handle/123456789/10138
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dc.contributor.authorMuhyi, Yaakop-
dc.contributor.authorSazali, Yaacob, Prof. Dr.-
dc.contributor.authorAbdul Rahman, Mohd Saad-
dc.contributor.authorZaridah, Mat Zain-
dc.contributor.authorPaulraj, Murugesa Pandiyan, Assoc. Prof. Dr.-
dc.contributor.authorMuthusamy, Hariharan-
dc.contributor.authorRamachandran, Nagarajan, Prof. Dr.-
dc.contributor.authorSoh, Warren Kay-
dc.contributor.authorAhmad Sabirin, Arshad-
dc.date.accessioned2010-11-01T02:20:50Z-
dc.date.available2010-11-01T02:20:50Z-
dc.date.issued2009-12-
dc.identifier.citationp.6-7en_US
dc.identifier.issn1823-9633-
dc.identifier.urihttp://dspace.unimap.edu.my/123456789/10138-
dc.description.abstractA satellite maneuvers through orbit with the use of an attitude control system (ACS) to stay on course and always pointing towards earth reference. This maximizes the solar cell-sun and camera-earth coverage, a process made possible with hardware and software embedded in the satellite that continuously control and adjust for optimun performance.en_US
dc.language.isoenen_US
dc.publisherUniversiti Malaysia Perlis (UniMAP)en_US
dc.relation.ispartofseriesExploreen_US
dc.relation.ispartofseriesDecember 2009en_US
dc.subjectExplore -- Penerbitan universitien_US
dc.subjectUniMAP -- Publicationsen_US
dc.subjectUniMAP -- Research and developmenten_US
dc.subjectAttitude control system (ACS)en_US
dc.subjectSimulationen_US
dc.titleNano-satellite Attitude Control Systemen_US
dc.typeArticleen_US
dc.publisher.departmentPejabat Timbalan Naib Canselor (Penyelidikan dan Inovasi)en_US
dc.contributor.urls.yaacob@unimap.edu.myen_US
Appears in Collections:Publications
Sazali Yaacob, Prof. Dr.
Ramachandran, Nagarajan, Prof. Dr.
Hariharan Muthusamy, Dr.
Paulraj Murugesa Pandiyan, Assoc. Prof. Dr.

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