Quadrotor tuning for attitude control based on PID controller using fictitious reference iterative tuning (FRIT)
作者： Arthit Julkananusar , Itthisek Nilkhamhang , Rangsarit Vanijjirattikhan , Atsushi Takahashi
DOI: 10.1109/ICTEMSYS.2015.7110817
关键词:
摘要: This paper proposes a method for quadrotor tuning focusing on attitude control (roll, pitch and yaw channel). The structure is based upon PID which widely used in many flight controller boards. However, it not easy to tune parameters of that satisfies the desired transient response, especially using manual tuning. Thus, this by fictitious reference iterative (FRIT) gains control. proposed FRIT so response each channel matches with model only one-shot first experimental input-output data from channel. Simulation results are provided show effectiveness method.
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