| dc.contributor.author | Muhyi, Yaakop | |
| dc.contributor.author | Sazali, Yaacob, Prof. Dr. | |
| dc.contributor.author | Abdul Rahman, Mohd Saad | |
| dc.contributor.author | Zaridah, Mat Zain | |
| dc.contributor.author | Paulraj, Murugesa Pandiyan, Assoc. Prof. Dr. | |
| dc.contributor.author | Muthusamy, Hariharan | |
| dc.contributor.author | Ramachandran, Nagarajan, Prof. Dr. | |
| dc.contributor.author | Soh, Warren Kay | |
| dc.contributor.author | Ahmad Sabirin, Arshad | |
| dc.date.accessioned | 2010-11-01T02:20:50Z | |
| dc.date.available | 2010-11-01T02:20:50Z | |
| dc.date.issued | 2009-12 | |
| dc.identifier.citation | p.6-7 | en_US |
| dc.identifier.issn | 1823-9633 | |
| dc.identifier.uri | http://dspace.unimap.edu.my/123456789/10138 | |
| dc.description.abstract | A 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.iso | en | en_US |
| dc.publisher | Universiti Malaysia Perlis (UniMAP) | en_US |
| dc.relation.ispartofseries | Explore | en_US |
| dc.relation.ispartofseries | December 2009 | en_US |
| dc.subject | Explore -- Penerbitan universiti | en_US |
| dc.subject | UniMAP -- Publications | en_US |
| dc.subject | UniMAP -- Research and development | en_US |
| dc.subject | Attitude control system (ACS) | en_US |
| dc.subject | Simulation | en_US |
| dc.title | Nano-satellite Attitude Control System | en_US |
| dc.type | Article | en_US |
| dc.publisher.department | Pejabat Timbalan Naib Canselor (Penyelidikan dan Inovasi) | en_US |
| dc.contributor.url | s.yaacob@unimap.edu.my | en_US |
