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Please use this identifier to cite or link to this item: http://dspace.unimap.edu.my:80/xmlui/handle/123456789/7319
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dc.contributor.authorMuhyi, Yaakop-
dc.contributor.authorSazali, Yaacob-
dc.contributor.authorAbdul Rahman, Mohd Saad-
dc.contributor.authorHarihran, M.-
dc.contributor.authorNagarajan, R.-
dc.date.accessioned2009-11-17T08:57:10Z-
dc.date.available2009-11-17T08:57:10Z-
dc.date.issued2009-10-11-
dc.identifier.citationp.3A7 1 - 3A7 5en_US
dc.identifier.urihttp://dspace.unimap.edu.my/123456789/7319-
dc.descriptionOrganized 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.abstractThis paper describes the development of a nano-satellite attitude control system (ACS) which employ a Kalman filter based controller and a simple adaptive predictive fuzzy logic controller (APFLC) for a 1, 2 and 3 axis orientation using RCM3400 microcontroller. This paper presents the performance comparison of the APFLC and Kalman filter based controller implemented in the hardware. The physical interface module, configuration with several key features, communication protocol and data handling for the micro-controller are also described.en_US
dc.description.sponsorshipTechnical sponsored by IEEE Malaysia Sectionen_US
dc.language.isoenen_US
dc.publisherUniversiti Malaysia Perlisen_US
dc.relation.ispartofseriesProceedings of the International Conference on Man-Machine Systems (ICoMMS 2009)en_US
dc.subjectArtificial satellites -- Attitude control systemsen_US
dc.subjectArtificial satellitesen_US
dc.subjectRCM3400 microcontrolleren_US
dc.subjectAttitude control system (ACS)en_US
dc.subjectKalman filteringen_US
dc.titleDevelopment of Attitude Control System on RCM3400 microcontroller for Nano-satellite applicationsen_US
dc.typeWorking Paperen_US
Appears in Collections:Conference Papers
Sazali Yaacob, Prof. Dr.
Ramachandran, Nagarajan, Prof. Dr.

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