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dc.contributor.authorHani Hazza, Ali Ahmed
dc.contributor.authorMohd Yusoff, Mashor
dc.contributor.authorMohammed Chessab, Mahdi
dc.date.accessioned2020-12-16T08:22:39Z
dc.date.available2020-12-16T08:22:39Z
dc.date.issued2019
dc.identifier.citationJournal of Physics: Conference Series, vol.1372, 2019, 6 pagesen_US
dc.identifier.issn1742-6588 (print)
dc.identifier.issn1742-6596 (online)
dc.identifier.urihttp://dspace.unimap.edu.my:80/xmlui/handle/123456789/69022
dc.descriptionLink to publisher's homepage at https://iopscience.iop.org/en_US
dc.description.abstractThis paper discusses the variation of proportional and derivative gains in a system under the control of PD+I controller that uses fuzzy inference method an effort is made to design the fuzzy proportional-derivative (PD) + I controller for a nonlinear the proposed fuzzy PD + I structure shows superior performance in the Nano-satellite attitude control system. Given that 2-input PD type controllers are commonly used to control Nano satellite attitude systems (Innovative Satellite InnoSAT), This paper analysis the performance of Fuzzy PD+I on satellite system. Fuzzy PD+I controller design can control Nano satellite attitude control system nicely and utilized the Fuzzy PD+I controller which optimize the stability of the Nano Satellite control system. In addition, the scheme is robust to variations in nonlinearities, as well as the steady-state gain of the plant. We illustrate the effectiveness of our scheme In MATLAB / SMULINK simulation environment.en_US
dc.language.isoenen_US
dc.publisherIOP Publishingen_US
dc.relation.ispartofseriesInternational Conference on Biomedical Engineering (ICoBE);
dc.subjectPD+I controlleren_US
dc.subjectFuzzy PD+Ien_US
dc.subjectFuzzy PD+I controlleren_US
dc.titleIntelligent Fuzzy PD+I Controller with Stabilizer for Nano Satellite Attitude Control Systemen_US
dc.typeArticleen_US
dc.identifier.urlhttps://iopscience.iop.org/article/10.1088/1742-6596/1372/1/012022/pdf
dc.contributor.urlHaniHazza@gmail.comen_US


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