Investigating Quadcopter Control Methods Using Computer Simulation

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dc.contributor.advisorSandor, Hajdu
dc.contributor.authorMana, Muhammad
dc.contributor.departmentDE--Műszaki Kar
dc.date.accessioned2025-12-12T16:30:15Z
dc.date.available2025-12-12T16:30:15Z
dc.date.created2025-12-01
dc.description.abstractIn this thesis, I am working on implementing the P, PI, PD and PID controller to a non-linear quadcopter. Thereafter I will analyse and compare their performances using MATLAB/Simulink. The initial stage of my thesis was to assign material property of the quadcopter in Onshape, thereafter I derived the equations of motion and the aerodynamic forces acting on the quadcopter. The working principle of the controllers is analysed by implementing them on a brushless DC motor, thereafter a cascaded architecture is designed for the controllers. The model has three control loops: position, angular rate and motor speed. The simulation has two scenarios where the first is a quadcopter without a payload and the other a quadcopter with a payload. Both scenarios are simulated in the same environments. At the end I analyse and compare the results.
dc.description.courseMechatronikai mérnöki
dc.description.degreeBSc/BA
dc.format.extent63
dc.identifier.urihttps://hdl.handle.net/2437/399849
dc.language.isoen
dc.rights.infoHozzáférhető a 2022 decemberi felsőoktatási törvénymódosítás értelmében.
dc.subjectQuadcopter
dc.subjectControl
dc.subject.dspaceInformatika
dc.titleInvestigating Quadcopter Control Methods Using Computer Simulation
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