Trajectory tracking control of quadrotor based on global stability

Ming-dong Hou, Tian Jie
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引用次数: 2

Abstract

According to the characteristics of the quadrotor' mathematical model and the trajectory tracking control problem, a trajectory tracking control of global stability strategy is proposed in this paper. Based on its features, the model is divided into two parts: an underactuated subsystem and a fully actuated subsystem; sliding mode control method is applied to the design of the controller of the fully actuated subsystem. Based on the global asymptotic stability theorem of dynamic system, the inner loop of an underactuated subsystem is rearranged into a stable global Lipschitz closed-loop system. The outer loop is designed through sliding mode control method, and therefore enables a strictly stable double loop sliding-mode track control for the underactuated subsystem. Simulation results show that the proposed method simplifies the design process of controller and enables the quadrotor to track a trajectory rapidly.
基于全局稳定性的四旋翼飞行器轨迹跟踪控制
针对四旋翼飞行器数学模型的特点和轨迹跟踪控制问题,提出了一种具有全局稳定性的轨迹跟踪控制策略。根据其特点,将模型分为欠驱动子系统和完全驱动子系统两部分;采用滑模控制方法设计了全驱动子系统的控制器。基于动力系统的全局渐近稳定性定理,将欠驱动子系统的内环重组为全局稳定的Lipschitz闭环系统。外环采用滑模控制方法设计,使欠驱动子系统能实现严格稳定的双环滑模轨迹控制。仿真结果表明,该方法简化了控制器的设计过程,使四旋翼飞行器能够快速跟踪轨迹。
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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