A new intelligent controller based on integral sliding mode control and extended state observer for nonlinear MIMO drone quadrotor

Moussa Abdillah , El Mehdi Mellouli , Touria Haidi
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引用次数: 0

Abstract

Unmanned aerial vehicles (UAVs) control faces major challenges such as dynamic complexity, unknown external disturbances, parametric uncertainties, time-varying states and delays. The literature proposes different techniques to address these challenges, but little attention has been paid to the design of a hybrid controller combining the advantages of these techniques to improve system performance. This research therefore aims to investigate the design of such a hybrid controller. In this paper, we present a novel intelligent controller based on Integral Sliding Mode Control (ISMC) and Extended State Observer (ESO) for a nonlinear Multiple Input Multiple Output (MIMO) drone quadrotor. First, the kinematic and dynamic models of our quadrotor drone are presented. Second, the ESO is used to estimate external disturbances and model uncertainties. Third, to overcome the problem of the reaching phase and the steady-state error, a new nonlinear ISMC is designed. The additive term of the ISMC structure has also overcome the problem of external disturbances and modelling errors, as well as observational errors. Fourth, an Adaptive Neural Network (ANN) switching control law is developed to surmount the chattering phenomenon. In addition, the stability of the control system is verified using Lyapunov stability theory. Finally, the effectiveness and superiority of the proposed control method are proved by simulation results. The results show that the proposed approach can handle external disturbances and eliminate chatter, leading to smooth control laws and lower power consumption, which is excellent from an energy efficiency perspective.

基于积分滑模控制和扩展状态观测器的非线性 MIMO 无人机四旋翼新型智能控制器
无人飞行器(UAVs)控制面临着动态复杂性、未知外部干扰、参数不确定性、时变状态和延迟等重大挑战。文献中提出了不同的技术来应对这些挑战,但很少有人关注如何设计一种混合控制器,结合这些技术的优势来提高系统性能。因此,本研究旨在研究这种混合控制器的设计。在本文中,我们针对非线性多输入多输出(MIMO)无人机四旋翼提出了一种基于积分滑动模式控制(ISMC)和扩展状态观测器(ESO)的新型智能控制器。首先,介绍了四旋翼无人机的运动学和动力学模型。其次,使用 ESO 估算外部干扰和模型不确定性。第三,为了克服到达阶段和稳态误差问题,设计了一种新的非线性 ISMC。ISMC 结构的加法项也克服了外部干扰和模型误差以及观测误差的问题。第四,开发了自适应神经网络(ANN)开关控制法,以克服颤振现象。此外,还利用 Lyapunov 稳定性理论验证了控制系统的稳定性。最后,通过仿真结果证明了所提控制方法的有效性和优越性。结果表明,所提出的方法可以处理外部干扰并消除颤振,从而获得平滑的控制规律和更低的功耗,从能源效率的角度来看是非常好的。
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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