基于 FTESO 自适应神经网络的多干扰下四旋翼无人机安全控制:算法与实验

Xin Cai, Xiaozhou Zhu, Wen Yao
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引用次数: 0

摘要

目的四旋翼飞行器已应用于多个领域。然而,由于四旋翼飞行器受到由外部干扰、执行器故障和参数不确定性组成的多重干扰,因此很难控制无人飞行器(UAV)实现高精度的跟踪性能。本文旨在设计一种安全控制器,利用观测器和神经网络方法提高无人飞行器在多重干扰下的跟踪性能。首先,为了主动估计和补偿系统的合成不确定性,研究了一种有限时间扩展状态观测器,并将干扰转化为系统的扩展状态进行估计。其次,根据估计值设计一种不需要精确动态模型知识的自适应神经网络控制器,其中神经网络的权重可通过自适应法则进行动态调整。研究结果图 "8 "爬升飞行仿真和实际飞行实验表明,本文提出的安全控制策略具有良好的跟踪性能。数值仿真结果和实际飞行实验证明了所提控制策略的有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
FTESO-adaptive neural network based safety control for a quadrotor UAV under multiple disturbances: algorithm and experiments

Purpose

Quadrotors have been applied in various fields. However, because the quadrotor is subject to multiple disturbances, consisting of external disturbances, actuator faults and parameter uncertainties, it is difficult to control the unmanned aerial vehicle (UAV) to achieve high-precision tracking performance. This paper aims to design a safety controller that uses observer and neural network method to improve the tracking performance of UAV under multiple disturbances. The experiments prove that this method is effective.

Design/methodology/approach

First, to actively estimate and compensate the synthetic uncertainties of the system, a finite-time extended state observer is investigated, and the disturbances are transformed into the extended state of the system for estimation. Second, an adaptive neural network controller that does not accurately require the dynamic model knowledge is designed based on the estimated value, where the weights of the neural network can be dynamically adjusted by the adaptive law. Furthermore, the finite-time bounded convergence of the proposed observer and the stability of the system are proved through homogeneous theory and Lyapunov method.

Findings

The figure-“8” climbing flight simulation and real flight experiments illustrate that the proposed safety control strategy has good tracking performance.

Originality/value

This paper proposes the safety control structure of the UAV, which combines the extended state observer with the neural network method. Numerical simulation results and actual flight experiments demonstrate the effectiveness of the proposed control strategy.

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