Please use this identifier to cite or link to this item: https://scholarhub.balamand.edu.lb/handle/uob/3412
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dc.contributor.advisorHaddad, Nicolas K.en_US
dc.contributor.authorSiblini, Carmenen_US
dc.contributor.authorIsmail, Kassemen_US
dc.date.accessioned2020-12-23T14:35:54Z-
dc.date.available2020-12-23T14:35:54Z-
dc.date.issued2016-
dc.identifier.urihttps://scholarhub.balamand.edu.lb/handle/uob/3412-
dc.descriptionIncludes bibliographical references (p. 46-47).en_US
dc.descriptionSupervised by Dr. Nicolas Haddad.en_US
dc.description.abstractThe project consists of analyzing, controlling and linearizing a derived mathematical model of a scaled model helicopter. This mathematical model will be derived based on accurate studies, where each component will be modeled apart. The linearization will be done by taking some assumptions during hovering state and previous studies on scaled model helicopter will be taken into consideration. Analog circuits will be designed, summed and simulated together on Multisim to form the linearized system. After linearization, controllability observability and stability tests should be done to demonstrate the importance of control. The system will be translated from multiple input multiple output into single input single output system. Each input will be controlled apart using PID controller design and modern control as state feedback control and identity observer. Meanwhile, Matlab will be used to tune the PID controller. Moreover, the implementation of the classical and modern control system for the linearized MIMO transfer functions will be done on LabVIEW software. In addition, the linearized model and the controller design was downloaded and simulated on MyRIO hardware.en_US
dc.description.statementofresponsibilityby Carmen Siblini, Kassem Ismailen_US
dc.format.extentviii, 53 p. :ill. ;30 cmen_US
dc.language.isoengen_US
dc.rightsThis object is protected by copyright, and is made available here for research and educational purposes. Permission to reuse, publish, or reproduce the object beyond the personal and educational use exceptions must be obtained from the copyright holderen_US
dc.subject.lcshHelicopters--Mathematical modelsen_US
dc.subject.lcshHelicopters--Control systemsen_US
dc.titleControl design and implementation of a scaled model helicopter using LabVIEW / MyRIO and Matlab / Simulinken_US
dc.typeProjecten_US
dc.contributor.departmentDepartment of Electrical Engineeringen_US
dc.contributor.facultyFaculty of Engineeringen_US
dc.contributor.institutionUniversity of Balamanden_US
dc.date.catalogued2017-01-13-
dc.description.degreeMS in Electrical Engineeringen_US
dc.description.statusPublisheden_US
dc.identifier.ezproxyURLhttp://ezsecureaccess.balamand.edu.lb/login?url=http://olib.balamand.edu.lb/projects_and_theses/GP-EE-201.pdfen_US
dc.identifier.OlibID170197-
dc.provenance.recordsourceOliben_US
Appears in Collections:UOB Theses and Projects
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