| Summary: | 碩士 === 逢甲大學 === 航太與系統工程學系 === 104 === The importance of unmanned aerial vehicle (UAV) has attracted more attention in recent years. In this study, the quadrotor UAV which has high mobility and vertical takeoff and landing (VTOL) ability was adopted to be the study target. Main contents of this study include quadrotor hardware development and assembly, autonomous flight control system design, dynamic simulation and analysis, and real flight tests.
This study will focus on the design and analysis of the position controll for quadrotors by compareing the of difference between the results of real flight and simulation. First, the nonlinear motion equation of quadrotor was derived. Then, a flight simulator was established by using MATLAB / SIMULINK. The controller design is based on Fuzzy controller and PID controller. Both the simulation and real flight experiments were conducted, to compare the performance of different controller for different quadrotor UAVs.
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