Adaptive PID Controller of a Quadrotor

Bassim Maaloul, S. Elloumi
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Abstract

The main purpose of this paper is to develop an adaptive PID controller of a quadrotor. We first developed a linear PID controller based on Ziegler and Nichols method, then we developed a nonlinear controller based on PID regulators with adaptive gains. These gains are adjusted according to Lyapunov's theory. Both of controllers were tested and compared. The results of the simulations on a model of a quadrotor, equipped with the developed control laws, showed the effectiveness of the adaptive PID controller compared to the conventional PID one. The adaptive PID controller reacts well to different types of input signals and can perfectly follow reference trajectories with negligible output error.
四旋翼飞行器的自适应PID控制器
本文的主要目的是开发一种四旋翼飞行器的自适应PID控制器。首先基于Ziegler - Nichols方法设计了线性PID控制器,然后基于自适应增益的PID调节器设计了非线性控制器。这些增益根据李亚普诺夫的理论进行调整。对两种控制器进行了测试和比较。在四旋翼飞行器模型上进行了仿真,仿真结果表明了自适应PID控制器与传统PID控制器相比的有效性。自适应PID控制器对不同类型的输入信号反应良好,可以很好地跟随参考轨迹,输出误差可以忽略不计。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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