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DC Field | Value | Language |
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dc.contributor.author | Nurul Syazwani Hussain | - |
dc.contributor.author | Hassrizal Hasan Basri | - |
dc.contributor.author | Sazali Yaacob | - |
dc.date.accessioned | 2016-04-28T06:32:45Z | - |
dc.date.available | 2016-04-28T06:32:45Z | - |
dc.date.issued | 2015-06 | - |
dc.identifier.citation | Nurul Syazwani Hussain, Hassrizal Hasan Basri, Sazali Yaacob. 2014. “STATE-DEPENDENT BOUNDARY LAYER METHOD FOR ATTITUDE CONTROL OF SATELLITE” 6: 93–97. | en_US |
dc.identifier.issn | 0127-9696 | - |
dc.identifier.uri | http://ir.unikl.edu.my/jspui/handle/123456789/13018 | - |
dc.description | This article index by Scopus. Sazali Yaacob (UniKL MSI) | en_US |
dc.description.abstract | Sliding mode control is known to be robust against parameter uncertainties and external disturbances. Based on the dynamic equation of motion, a sliding mode controller is designed to solve this problem. However, for the sliding surface to be attractive, a switching function is used in the control law, which caused chattering of the control signal. In order to avoid this, a boundary layer method is considered in the modified controller. So this paper proposes new boundary layer designs that resolve the problem in control accuracy and control signal smoothness in sliding mode control. The propose design improve the system state to almost zero with no chattering in the control signals. | en_US |
dc.publisher | Penerbit Universiti Teknologi Malaysia | en_US |
dc.subject | Sliding mode control | en_US |
dc.subject | mathematical model | en_US |
dc.subject | attitude control | en_US |
dc.subject | state dependant boundary layer | en_US |
dc.title | State-Dependent Boundary Layer Method For Attitude Control Of Satellite | en_US |
dc.type | Article | en_US |
Appears in Collections: | Journal Articles |
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File | Description | Size | Format | |
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Nurul Syazwani Hussain, Hassrizal Hasan Basri - 2014 - STATE-DEPENDENT BOUNDARY LAYER METHOD FOR ATTITUDE CONTROL OF SATELLITE.pdf | 493 kB | Adobe PDF | View/Open |
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