Genetically Tuned Linear Quadratic Regulator for Trajectory Tracking of a Quadrotor

A. T. Karaşahin
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Abstract

In this paper, a linear quadratic regulator (LQR) controller operating according to the genetically tuned inner-outer loop structure is proposed for trajectory tracking of a quadrotor. Setting the parameters of a linear controller operating according to the inner-outer loop structure is a matter that requires profound expertise. Optimization algorithms are used to cope with the solution of this problem. First, the dynamic equations of motion of the quadrotor are obtained and modelled in state-space form. The LQR controller, which will operate according to the inner-outer loop structure in the MATLAB/Simulink environment, has been developed separately for 6 degrees of freedom (DOF) of the quadrotor. Since adjusting these parameters will take a long time, a genetic algorithm has been used at this point. The LQR controller with optimized coefficients and a proposed LQR controller-based study in the literature are evaluated according to their success in following the reference trajectory and their responses to specific control inputs. According to the results obtained, it was observed that the genetically adjusted LQR controller produced more successful outcomes.
用于四旋翼飞行器轨迹跟踪的基因调谐线性二次调节器
本文针对四旋翼飞行器的轨迹跟踪,提出了一种根据基因调谐内-外环结构运行的线性二次调节器(LQR)控制器。设置根据内-外环结构运行的线性控制器的参数是一个需要深厚专业知识的问题。本文采用优化算法来解决这一问题。首先,获得四旋翼飞行器的动态运动方程,并以状态空间形式建模。在 MATLAB/Simulink 环境中,根据内-外环结构运行的 LQR 控制器已针对四旋翼飞行器的 6 个自由度 (DOF) 单独开发。由于调整这些参数需要很长时间,因此此时采用了遗传算法。根据其跟踪参考轨迹的成功率以及对特定控制输入的响应,对具有优化系数的 LQR 控制器和文献中提出的基于 LQR 控制器的研究进行了评估。根据所得结果,经基因调整的 LQR 控制器产生了更成功的结果。
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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