Sigmoid Super-Twisting Extended State Observer and Sliding Mode Controller for Quadrotor UAV Attitude System With Unknown Disturbance

Yongfeng Rong, Ran Jiao, Song Kang, Wusheng Chou
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引用次数: 6

Abstract

The super-twisting algorithm has been verified its effectiveness in attitude control for quadrotor with unknown disturbance. However, the discontinuous signum function in super-twisting formulation causes the unwanted chattering problem and thus affects the attitude control performance. In this paper, we replace the signum function with sigmoid function and propose the sigmoid super-twisting extended state observer (SSTESO) and sliding mode controller (SSTSMC). Besides, a rigorous convergence analysis of proposed nonlinear error system based on the Lyapunov stability theory is performed, and the parameter selection rule is given. Numerical simulations are implemented in presence of manually designed disturbance in order to verify the advantage of the proposed algorithm compared with original super-twisting algorithm. Results show that the introduction of sigmoid function can not only reduce the chattering effect, but also maintain the advantage of supertwisting algorithm.
具有未知扰动的四旋翼无人机姿态系统的s型超扭转扩展状态观测器与滑模控制器
超扭转算法在具有未知扰动的四旋翼飞行器姿态控制中的有效性得到了验证。然而,超扭系统中不连续的sgum函数会引起系统的抖振问题,从而影响系统的姿态控制性能。本文用sigmoid函数代替sgum函数,提出了sigmoid超扭转扩展状态观测器(SSTESO)和滑模控制器(SSTSMC)。此外,基于Lyapunov稳定性理论对所提出的非线性误差系统进行了严格的收敛性分析,并给出了参数选择规则。在人为设计扰动存在的情况下进行了数值仿真,验证了该算法与原有超扭转算法相比的优越性。结果表明,引入s型函数不仅可以减小抖振效应,而且可以保持超扭转算法的优势。
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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