| dc.contributor.author | Siti Maryam, Sharun | |
| dc.contributor.author | Mohd Yusoff, Mashor, Dr. | |
| dc.contributor.author | Sazali, Yaacob, Prof. Dr. | |
| dc.contributor.author | Zul Azfar, Ahmam | |
| dc.contributor.author | N. Hamzah | |
| dc.date.accessioned | 2013-12-10T04:24:26Z | |
| dc.date.available | 2013-12-10T04:24:26Z | |
| dc.date.issued | 2012-05-18 | |
| dc.identifier.citation | p. 225-234 | en_US |
| dc.identifier.isbn | 978-967-5760-11-2 | |
| dc.identifier.uri | http://dspace.unimap.edu.my/123456789/30298 | |
| dc.description | The 2nd
International Malaysia-Ireland Joint
Symposium on Engineering, Science and Business 2012 (IMiEJS2012) jointly organized by Universiti Malaysia Perlis and Athlone Institute of Technology in collaboration with The Ministry of Higher Education (MOHE) Malaysia, Education Malaysia and Malaysia Postgraduates Student Association Ireland (MyPSI), 18th - 19th June 2012 at Putra World Trade Center (PWTC), Kuala Lumpur, Malaysia. | en_US |
| dc.description.abstract | The current study proposes a novel approach for satellite attitude control simulator
design where the simulator consists of both software and hardware. A software simulator will
represent the satellite dynamic model, incorporating all the operating conditions of the satellite in
orbit, together with all the necessary GUIs. The actuator, ADS and the attitude controller will be
implemented on the actual controller boards that will at the end be placed on the Innovative Satellite
(InnoSAT). The hardware simulator will be interfaced to control the satellite software simulator.
The hardware simulator will include all the necessary interfaces and communication channels to
other parts of InnoSAT. The controller that will be used is the Adaptive Neuro_Controller (ANC)
which is based on Hybrid Multi Layered Perceptron (HMLP) network. A microcontroller unit
(MCU) Rabbit Core Module RCM4100 will be used as a hardware simulator for implementation of
attitude control algorithm. Meanwhile, MATLAB programming in a standard PC will be used as
software simulator for simulating satellite dynamics. The satellite attitude control simulator gives a
satisfactory performance in the real time environment | en_US |
| dc.language.iso | en | en_US |
| dc.publisher | Universiti Malaysia Perlis (UniMAP) | en_US |
| dc.relation.ispartofseries | Proceedings of the The 2nd International Malaysia-Ireland Joint Symposium on Engineering, Science and Business 2012 (IMiEJS2012); | |
| dc.subject | Satellite attitude control simulator | en_US |
| dc.subject | Innovative satellite | en_US |
| dc.subject | Adaptive Neuro_Controller | en_US |
| dc.subject | Hybrid multi layered perceptron network | en_US |
| dc.subject | Rabbit core module | en_US |
| dc.title | Development of attitude control simulator for InnoSAT satellite system | en_US |
| dc.type | Working Paper | en_US |
| dc.contributor.url | siti_mrym@ymail.com | en_US |
| dc.contributor.url | yusoff@unimap.edu.my | en_US |
| dc.contributor.url | s.yaacob@unimap.edu.my | en_US |
| dc.contributor.url | zulazfar.automav@gmail.com | en_US |
| dc.contributor.url | hizam@atsb.my | en_US |
