Adaptive Sliding Mode Control for the Quadrotor with unknown Disturbance and Uncertain Parameters

Long H. Chu, NamHoai Nguyen
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Abstract

With the convenience of maneuvering and taking off easily, quadrotors are becoming more and more popular in military as well as civilian applications recently. The quadrotor is an under-actuated system. Moreover, in the presence of the external disturbance and uncertainties, it’s even more difficult to control. Therefore, the study of flight control algorithms for the quadrotor is absolutely necessary and that is also the main purpose of this study. First, the trajectory tracking problem without disturbance and uncertainties is solved by a backstepping controller (BSC). Then, an adaptive backstepping sliding mode controller (ABSMC) is investigated to solve the influence of external disturbance. Next, a controller was developed from the ABSMC controller to ensure that the tracking errors converge to zero while the coefficients of air resistance are unknown. In addition, all control algorithms are analyzed for stability. Finally, several simulations are performed to verify as well as compare with the studied control algorithms.
未知扰动和参数不确定的四旋翼自适应滑模控制
四旋翼飞行器具有机动方便、起飞方便等特点,近年来在军用和民用领域得到越来越广泛的应用。四旋翼是一个欠驱动系统。而且,在存在外部干扰和不确定性的情况下,控制难度更大。因此,对四旋翼飞行器的飞行控制算法进行研究是十分必要的,也是本文研究的主要目的。首先,利用反步控制器(BSC)解决无干扰和不确定性的轨迹跟踪问题。然后,研究了一种自适应反步滑模控制器(ABSMC)来解决外部干扰的影响。其次,在ABSMC控制器的基础上开发了一种控制器,以保证在空气阻力系数未知的情况下,跟踪误差收敛于零。此外,对所有控制算法进行了稳定性分析。最后,通过仿真对所研究的控制算法进行了验证和比较。
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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