Fault-Observer-Based Fault-Tolerant Fuzzy Terminal Sliding Mode Control of a Quadrotor Encountered the Deviation of Rotor Thrust

Mohammad Bagher Sajjadi, Nima Safaei, Moosa Ayati
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引用次数: 0

Abstract

Due to the high nonlinearity of the quadrotor dynamics and the generated structural faults, a Fault-Observer-Based Fault-Tolerant Fuzzy Terminal Sliding Mode Controller (FT2SMC) is utilized. This strategic utilization remains effective even when the system encounters input saturation. A fault observer estimates the fault vector since it is applied to the governing equations of motion as external disturbances. Additionally, a Fuzzy Inference System (FIS) has been employed to estimate the discontinuous term of the terminal sliding mode control and to alleviate the chattering phenomenon. The finite-time convergence of the tracking errors of the attitude and the altitude toward the origin has been guaranteed, and the entire closed-loop stability of the faulty quadrotor has been proved using Lyapunov theory, ensuring that it continues following the desired trajectory even in the presence of faults. The simulation results indicate the prodigious effectiveness of the controller, which navigates the quadrotor to a desired altitude. Also, the superiority of this control algorithm is demonstrated by comparing the results of the control inputs with those obtained with a regular terminal sliding mode controller.

基于故障观测器的四旋翼飞行器推力偏差容错模糊终端滑模控制
针对四旋翼系统的高非线性特性和产生的结构故障,采用了基于故障观测器的容错模糊终端滑模控制器(FT2SMC)。即使系统遇到输入饱和,这种策略利用仍然有效。故障观测器估计故障向量,因为它作为外部干扰应用于运动控制方程。此外,采用模糊推理系统(FIS)对末端滑模控制的不连续项进行估计,减轻了抖振现象。保证了姿态和高度跟踪误差向原点的有限时间收敛性,并利用李亚普诺夫理论证明了故障四旋翼飞行器的整个闭环稳定性,保证了故障四旋翼飞行器在存在故障的情况下继续沿期望轨迹飞行。仿真结果表明,该控制器能够有效地将四旋翼飞行器导航到理想的高度。通过与常规终端滑模控制器控制结果的比较,验证了该控制算法的优越性。
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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