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dc.contributor.advisorGo, Tiauw Hiong
dc.contributor.authorMangsatabam, Rakhayai
dc.date.accessioned2019-04-12T18:55:19Z
dc.date.available2019-04-12T18:55:19Z
dc.date.created2018-12
dc.date.issued2018-12
dc.date.submittedDecember 2018
dc.identifier.urihttp://hdl.handle.net/11141/2783
dc.descriptionThesis (M.S.) - Florida Institute of Technology, 2018en_US
dc.description.abstractThis thesis focuses on the control development for autonomous landing of a quadcopter on a moving platform. The object tracking and path following is performed through on-board vision-based systems. The goal of the thesis is to develop a controller for autonomous landing of a quadcopter and test its fidelity with simulations and experiments. The thesis is carried out in two sections, simulation and experiment. The simulation was carried out based on the system modeled and a PD (Proportional Derivative) controller was used to simulate the quadcopter landing. The simulation was split into three parts, with each part attempting to become closer to the experiment in terms of how the current states and desired states are observed and computed by the onboard flight controller. The simulation involves targeting the marker, following the marker and finally landing on the marker, while ensuring the marker is directly below the quadcopter to ensure the quadcopter lands on the marker, while the marker is moving. However, the experiments were carried out on a stationary marker. The experiments performed were able to validate the simulation results.en_US
dc.format.mimetypeapplication/pdf
dc.language.isoen_USen_US
dc.rightsCC BY 4.0en_US
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/legalcodeen_US
dc.titleControl Development for Autonomous Landing of Quadcopter on Moving Platformen_US
dc.typeThesisen_US
dc.date.updated2019-03-05T19:54:24Z
thesis.degree.nameMaster of Science in Aerospace Engineering Flight Mechanics and Controlsen_US
thesis.degree.levelMastersen_US
thesis.degree.disciplineAerospace Engineeringen_US
thesis.degree.departmentAerospace, Physics and Space Sciencesen_US
thesis.degree.grantorFlorida Institute of Technologyen_US
dc.type.materialtext


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