Optimal Tuning Based Linear Active Disturbance Rejection Control Applied to a Quadcopter

S. A. Suhail, M. A. Bazaz, Shoeb Hussain
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Abstract

This paper proposes a novel control approach called the Active Disturbance Rejection Control (ADRC) for the altitude and attitude control of an unmanned quadcopter with disturbances. The quadcopter is an underactuated system subject to parametric perturbations, non-linearity, unmodeled dynamics, strong coupling, and external disturbances. Linear Quadratic Regulator (LQR), an optimal control method, is used for the tuning of ADRC. The proposed control scheme is verified in simulation studies with the presence of sensor noise and external disturbances. The simulation results show that the proposed algorithm can significantly reduce the chattering phenomenon, owing to the estimation capability of the Extended State Observer (ESO). The proposed method also improves the robustness against modeling errors and disturbances and smoothly tracks the reference trajectory compared to PID and sliding mode control (SMC).
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基于最优整定的线性自抗扰控制在四轴飞行器中的应用
针对具有扰动的无人四轴飞行器的高度和姿态控制问题,提出了一种新的自抗扰控制方法。四轴飞行器是一个欠驱动系统,受参数扰动、非线性、未建模动力学、强耦合和外部干扰的影响。采用线性二次型调节器(LQR)作为最优控制方法对自抗扰控制器进行整定。在存在传感器噪声和外界干扰的情况下,对所提出的控制方案进行了仿真研究。仿真结果表明,由于扩展状态观测器(ESO)的估计能力,该算法可以显著降低抖振现象。与PID和滑模控制(SMC)相比,该方法还提高了对建模误差和干扰的鲁棒性,并能平滑地跟踪参考轨迹。
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