Modeling and Control of a Quad-rotor Unmanned Aerial Vehicle at Hovering Position

dc.contributor.advisorLebsework Negash (PhD)
dc.contributor.authorTesfaye, Ruth
dc.date.accessioned2018-07-09T11:44:53Z
dc.date.accessioned2023-11-04T15:14:36Z
dc.date.available2018-07-09T11:44:53Z
dc.date.available2023-11-04T15:14:36Z
dc.date.issued2012-12
dc.description.abstractThis thesis titled Modeling and Control of a Quad-rotor Unmanned Aerial vehicle at hovering Position by Ruth Tesfaye presents the study of modeling and control of quad-rotor Unmanned Aerial vehicle (UAV) characteristics that could be used for any of its application. Quad-rotor UAVs consist of two pairs of counter rotating rotors placed at the end of a cross configuration; symmetrical body about the center of gravity that coincides with the origin of the body frame of reference. The Newton-Euler formulation has been used to derive the defining equations of motion of the system at hovering position i.e. the six degree-of-freedom. Based on the verified model, control strategies were developed using linear PID controller and an LQR controller. The PID controller was adopted as a reference control law from the work of A.ouladi [1]. A numerical simulation was then conducted using MATLABĀ® SimulinkĀ®. First, the derived model was simulated to verify the behavior of the quad-rotor for model verification, and then a second simulation was conducted to determine the effectiveness of the developed control law. The results and the interpretations of this study are then presented and discussed on their respective areas.en_US
dc.identifier.urihttp://etd.aau.edu.et/handle/123456789/7351
dc.language.isoenen_US
dc.publisherAddis Ababa Universityen_US
dc.subjectQuad-Rotoren_US
dc.subjectPID Controlleren_US
dc.subjectLQR Controlleren_US
dc.subjectHovering Positionen_US
dc.subjectEquilibrium Pointen_US
dc.titleModeling and Control of a Quad-rotor Unmanned Aerial Vehicle at Hovering Positionen_US
dc.typeThesisen_US

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