Please use this identifier to cite or link to this item:
http://dspace.unimap.edu.my:80/xmlui/handle/123456789/30759
Full metadata record
DC Field | Value | Language |
---|---|---|
dc.contributor.author | Fatimatul Anis, Bakri | - |
dc.contributor.author | Mohd Yusoff, Mashor, Prof. Madya Dr. | - |
dc.contributor.author | Siti Maryam, Sharun | - |
dc.date.accessioned | 2013-12-23T03:45:20Z | - |
dc.date.available | 2013-12-23T03:45:20Z | - |
dc.date.issued | 2012-06-18 | - |
dc.identifier.citation | p. 800 - 808 | en_US |
dc.identifier.isbn | 978-967-5760-11-2 | - |
dc.identifier.uri | http://dspace.unimap.edu.my/123456789/30759 | - |
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 | This paper evaluates the performance of Adaptive Fuzzy Logic Control (AFLC) in the process of controlling the attitude of an Innovative Satellite (InnoSAT) system. Y-Thompson spin control is adapted to the satellite system as the reference input throughout the simulation. The basic control structure is presented. The selection of the controller parameter, which proved the attitude stabilization of the satellite, has been analyzed. The adaptive fuzzy control compensates for the plant uncertainties and to increase the robustness of the controller. In the proposed controller structure, an adaptive fuzzy control scheme is used to achieve the parameter tuning and the system stability. The adjustment mechanism applied the technique similar to PID controller to minimize the error and brings it to zero. The principles for tuning UOD of the input and output are proposed in this paper. Simulation results demonstrate that the controller able to accomplished precise attitude control based on the proposed method. The results show an AFLC can cope with the varying operating condition. | 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 | Adaptive fuzzy logic controller | en_US |
dc.subject | Attitude control | en_US |
dc.subject | Innovative satellite | en_US |
dc.subject | Membership function | en_US |
dc.title | Adaptive fuzzy logic controller for innovative satellite | en_US |
dc.type | Working Paper | en_US |
dc.contributor.url | fatimatulanis@yahoo.com.my | en_US |
dc.contributor.url | yusoff@unimap.edu.my | en_US |
dc.contributor.url | siti_mrym@ymail.com | en_US |
Appears in Collections: | Conference Papers |
Files in This Item:
File | Description | Size | Format | |
---|---|---|---|---|
pg 800 - 808.pdf | Access is limited to UniMAP community | 272.25 kB | Adobe PDF | View/Open |
Items in UniMAP Library Digital Repository are protected by copyright, with all rights reserved, unless otherwise indicated.