Integral backstepping controller for quadrotor path tracking

Wesam M. Jasim, Dongbing Gu
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引用次数: 27

Abstract

An integral backstepping control algorithm is presented for the path tracking problem of a quadrotor in this work. The dynamical model of a quadrotor is represented based on unit quaternion representation and includes some modelled aerodynamical effects as a nonlinear part. The integral backstepping controller is designed for translational part to track the desired trajectory. Stability analysis is achieved via a suitable Lyapunov function. The external disturbance and model parameters uncertainty are considered in the simulation tests to justify the proposed controller stability. Simulation results are compared with a standard backstepping controller results.
四旋翼飞行器路径跟踪的积分反步控制器
针对四旋翼飞行器的路径跟踪问题,提出了一种积分反步控制算法。四旋翼飞行器的动力学模型基于单位四元数表示,并将一些模拟的气动效应作为非线性部分。针对平移部分设计了积分反步控制器,以实现对目标轨迹的跟踪。稳定性分析是通过一个合适的李雅普诺夫函数实现的。在仿真试验中考虑了外部干扰和模型参数的不确定性,验证了所提控制器的稳定性。仿真结果与标准反步控制器的结果进行了比较。
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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