Please use this identifier to cite or link to this item: https://scholarhub.balamand.edu.lb/handle/uob/829
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dc.contributor.authorKhaldi, Mohamaden_US
dc.contributor.authorAbiad, Hassan Elen_US
dc.date.accessioned2020-12-23T08:37:49Z-
dc.date.available2020-12-23T08:37:49Z-
dc.date.issued2009-
dc.identifier.urihttps://scholarhub.balamand.edu.lb/handle/uob/829-
dc.description.abstractScaled-model helicopters are highly nonlinear, coupled, and unstable machines. They have fast response and controlling them is very complicated and need high degree of precision. In this paper, a detailed nonlinear model is derived. An optimal controller that is based upon state estimation is designed and implemented for each of the control inputs using a linearized model around an unaccelerated hovering motion. The optimal linear controller was then applied to the nonlinear model. In addition, input/output measurements of the nonlinear model were used to train the Multi-Layer Neural Networks (MLNNs) of the Nonlinear AutoRegressive with Moving Average (NARMA-L2) controller. Then, NARMA-L2 was applied to the nonlinear model and the results were compared with both the classical, namely PI-D, and the optimal control.en_US
dc.format.extent6 p.en_US
dc.language.isoengen_US
dc.titleState estimation based optimal control and NARMA-L2 controllers of a scaled-model helicopteren_US
dc.typeConference Paperen_US
dc.relation.conferenceIFAC International Conference on Intelligent Control Systems and Signal Processing (ICONS 2009) (2nd : 21-23 Sept 2009 : Istanbul,Turkey)en_US
dc.contributor.affiliationDepartment of Electrical Engineeringen_US
dc.description.startpage55en_US
dc.description.endpage60en_US
dc.date.catalogued2018-03-06-
dc.description.statusPublisheden_US
dc.identifier.OlibID178389-
dc.relation.ispartoftext2nd IFAC International Conference on Intelligent Control Systems and Signal Processing (ICONS 2009)en_US
dc.provenance.recordsourceOliben_US
crisitem.author.parentorgFaculty of Engineering-
Appears in Collections:Department of Electrical Engineering
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