Cascaded Model-Free Control for trajectory tracking of quadrotors

Maria Bekcheva, C. Join, H. Mounier
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引用次数: 10

Abstract

In the subject of quadrotor controller design, usually modelling and identification are tedious and time-consuming tasks. In this study, we propose a controller design that avoids the quadrotor's system identification procedures while staying robust with respect to endogenous and exogenous disturbances. To reach our goal, based on the cascaded structure of a quadrotor, we divide the system into positional and attitude subsystems each controlled by an independent model-free controller. We validate our control approach in two realistic scenarios : in presence of unknown measurement noise and unknown time-varying wind disturbances. We provide simulations on a realistic nonlinear quadrotor model following an aggressive position-yaw trajectory.
四旋翼机轨迹跟踪的级联无模型控制
在四旋翼控制器设计中,建模和辨识是一项繁琐而耗时的工作。在本研究中,我们提出了一种控制器设计,避免了四旋翼的系统识别过程,同时保持了对内源性和外源性干扰的鲁棒性。为了达到我们的目标,基于四旋翼的级联结构,我们将系统分为位置和姿态子系统,每个子系统由独立的无模型控制器控制。我们在两个现实的场景中验证了我们的控制方法:存在未知的测量噪声和未知的时变风干扰。我们提供了一个现实的非线性四旋翼模型在一个侵略性的位置偏航轨迹。
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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