dc.contributor.author | Muhyi, Yaakop | |
dc.contributor.author | Sazali, Yaacob | |
dc.contributor.author | Abdul Rahman, Mohd Saad | |
dc.contributor.author | Harihran, M. | |
dc.contributor.author | Nagarajan, R. | |
dc.date.accessioned | 2009-11-17T08:57:10Z | |
dc.date.available | 2009-11-17T08:57:10Z | |
dc.date.issued | 2009-10-11 | |
dc.identifier.citation | p.3A7 1 - 3A7 5 | en_US |
dc.identifier.uri | http://dspace.unimap.edu.my/123456789/7319 | |
dc.description | Organized 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.abstract | This 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.sponsorship | Technical sponsored by IEEE Malaysia Section | en_US |
dc.language.iso | en | en_US |
dc.publisher | Universiti Malaysia Perlis | en_US |
dc.relation.ispartofseries | Proceedings of the International Conference on Man-Machine Systems (ICoMMS 2009) | en_US |
dc.subject | Artificial satellites -- Attitude control systems | en_US |
dc.subject | Artificial satellites | en_US |
dc.subject | RCM3400 microcontroller | en_US |
dc.subject | Attitude control system (ACS) | en_US |
dc.subject | Kalman filtering | en_US |
dc.title | Development of Attitude Control System on RCM3400 microcontroller for Nano-satellite applications | en_US |
dc.type | Working Paper | en_US |