Trajectory-tracking control design and modeling for quadrotor aerial vehicles

A. Margun, D. Bazylev, K. Zimenko, A. Kremlev
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引用次数: 1

Abstract

A control algorithm for finite-time tracking of quadrotor is introduced. The algorithm is based on use of feedback linearization method and finite-time output control presented in [17]. In comparison with commonly used in practice control methods like PD-controller the proposed method allows to estimate the first derivatives of the generalized coordinates, that enable to reduce the number of necessary sensors and thereby reduce the cost of the quadrotor. Moreover, the method is robust with respect to external disturbances and discretization that is useful for quadrotor control due to operating in open areas and digitality of sensors and controller. The performance and effectiveness of the method is demonstrated by simulation results of the system with external perturbations and signal discretization.
四旋翼飞行器轨迹跟踪控制设计与建模
介绍了一种四旋翼飞行器有限时间跟踪控制算法。该算法基于[17]中提出的反馈线性化方法和有限时间输出控制。与实践中常用的控制方法如pd -控制器相比,提出的方法允许估计广义坐标的一阶导数,从而能够减少必要的传感器数量,从而降低四旋翼的成本。此外,该方法对外界干扰和离散化具有鲁棒性,由于在开放区域运行以及传感器和控制器的数字化,对四旋翼控制有用。通过外部扰动和信号离散的仿真结果验证了该方法的性能和有效性。
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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